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		<title>Assessment of Cable Protection Systems a Cables for Fixed Offshore Wind</title>
		<link>https://pdl-group.com/assessment-of-cable-protection-systems-a-cables-for-fixed-offshore-wind/</link>
					<comments>https://pdl-group.com/assessment-of-cable-protection-systems-a-cables-for-fixed-offshore-wind/#respond</comments>
		
		<dc:creator><![CDATA[marc]]></dc:creator>
		<pubDate>Thu, 16 Feb 2023 11:56:56 +0000</pubDate>
				<category><![CDATA[OFFSHORE WIND]]></category>
		<category><![CDATA[RENEWABLE ENERGY]]></category>
		<category><![CDATA[COMPUTATIONAL FLUID DYNAMICS]]></category>
		<guid isPermaLink="false">https://pdl-group.com/?p=4843</guid>

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<p>The post <a href="https://pdl-group.com/assessment-of-cable-protection-systems-a-cables-for-fixed-offshore-wind/">Assessment of Cable Protection Systems a Cables for Fixed Offshore Wind</a> appeared first on <a href="https://pdl-group.com">PDL Group</a>.</p>
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<section class="av_textblock_section "  itemscope="itemscope" itemtype="https://schema.org/BlogPosting" itemprop="blogPost" ><div class='avia_textblock  '   itemprop="text" ><h1>Assessment of Cable Protection Systems and Cables for Fixed Offshore Wind</h1>
</div></section><br />
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<section class="av_textblock_section "  itemscope="itemscope" itemtype="https://schema.org/BlogPosting" itemprop="blogPost" ><div class='avia_textblock  '   itemprop="text" ><h4>SUMMARY</h4>
<p>Global assessment of Cable Protection Systems (CPSs) and Cables used in fixed offshore wind, subject to hydrodynamic loading.</p>
<h4>SITUATION</h4>
<p>The UK has the largest installed capacity of offshore wind in the world, with around 10GW in operation at the time of writing. In fixed offshore wind, inter-array power cables are used to transfer power from each of the turbines, in series, back to the shore. These cables are buried for the most part but are exposed at the entry to the monopile and protected by a Cable Protection System (CPS) in this region. The power cable sits inside the CPS, which consists of bend stiffener and bend restrictor elements, and there is a small clearance between the two. Due to the often-shallow water depths that fixed wind turbines are installed in, the area is often subject to harsh loading from both current and waves.</p>
<p>PDL has been trusted by Installers, Manufactures and Site Owners to assess the integrity of the cable and CPS in these regions, and calculate the cable’s design life.</p>
<h4>CHALLENGE</h4>
<p>The section between the monopile entry and cable burial is the most critical, from a structural integrity point of view, largely due to excessive movement and potentially leading to fatigue of cable or CPS components.</p>
<p>The environmental loading in the region of the CPS is complex and needs to account for the speed up of wave and current as the water passes around the monopile (potential flow theory) and oscillatory flow conditions.</p>
<p>Oscillatory flow conditions occur in shallow water, when the flow conditions are wave dominated. Due to this, additional considerations are required such as inclusion of the Keulegan-Carpenter (KC) number. The KC number is important to ensure accurate calculation of wave forces around the monopile. The KC number is a unitless value which modifies the force coefficients of an object subject to oscillatory fluid flow, amplifying the inertia and/or drag coefficients.</p>
<h4>SOLUTION</h4>
<p>Given the complex nature of the environmental loading, and the current limitations of OrcaFlex, an external function was required to calculate the relative current and wave velocity at various locations along the exposed length, taking into account of potential flow theory around the monopile and calculation of the KC number. This function, in the form of a python script, was integrated into PDL’s pre-processing scripts and cross-verified through hand calculations for a number of cases.</p>
<p>Once the appropriate force coefficients had been calculated, the simulation was solved for the appropriate number of site locations and CPS/cable configurations.</p>
<p>Ultimate Limit State (ULS) and Fatigue Limit State (FLS) assessments of both the cable armour wires and CPS components for both start of life and end of life scenarios can be considered. The assessments of the power cable take into account the non-linear ‘stick-slip’ behaviour of the cable and bend restrictors, with an external PDL tool calculating an accurate design life for the armour wires based on the calculated non-linear curves (see Case Study X for more details).</p>
<p>PDL has also undertaken studies where the CPS has prematurely failed, leading to increased loading on the cable and reduced life. Often remedial measures are introduced to stabilise the structure in the long term which can be easily optimised using OrcaFlex.</p>
<h4>BENEFITS</h4>
<ul>
<li> Accurate estimate of expected movement and loading on CPS, allowing for:
<ul>
<li>Modification to cable geometry, CPS arrangements and bend stiffeners prior to manufacture</li>
<li>Optimisation of scour protection arrangement</li>
<li>Understanding of site and installation tolerances (latch height).</li>
</ul>
</li>
<li>Decreased risk by accurately assessing the expected life of the<br />
components and updating the cable and CPS designs where appropriate, prior to manufacture</li>
<li>For sites which have failed components, identify timescale for remedial work and optimise solution</li>
<li>Assessment of hanging catenary inside the monopile to cross check hang-off loads and internal cable movements</li>
<li>No or minimal physical testing</li>
<li>Can be coupled with installation analysis.</li>
</ul>
</div></section><br />
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<section class="av_textblock_section "  itemscope="itemscope" itemtype="https://schema.org/BlogPosting" itemprop="blogPost" ><div class='avia_textblock  '   itemprop="text" ><h4>SECTOR</h4>
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<section class="av_textblock_section "  itemscope="itemscope" itemtype="https://schema.org/BlogPosting" itemprop="blogPost" ><div class='avia_textblock  '   itemprop="text" ><h4>NICHE CAPABILITIES</h4>
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<section class="av_textblock_section "  itemscope="itemscope" itemtype="https://schema.org/BlogPosting" itemprop="blogPost" ><div class='avia_textblock  '   itemprop="text" ><p>OrcaFlex</p>
<p>Flow Amplification</p>
<p>Non-linear Cable Behaviour</p>
</div></section><br />
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<section class="av_textblock_section "  itemscope="itemscope" itemtype="https://schema.org/BlogPosting" itemprop="blogPost" ><div class='avia_textblock  '   itemprop="text" ><p>Ultimate Limit State (ULS)</p>
<p>Fatigue Limit State (FLS)</p>
</div></section><br />
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<p>Manufacturers specifications</p>
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<section class="av_textblock_section "  itemscope="itemscope" itemtype="https://schema.org/BlogPosting" itemprop="blogPost" ><div class='avia_textblock  '   itemprop="text" ><p>OrcaFlex</p>
<p>Python</p>
</div></section></p></div>

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<p>The post <a href="https://pdl-group.com/assessment-of-cable-protection-systems-a-cables-for-fixed-offshore-wind/">Assessment of Cable Protection Systems a Cables for Fixed Offshore Wind</a> appeared first on <a href="https://pdl-group.com">PDL Group</a>.</p>
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		<title>Floating Wind Mooring Chain Inclinometer Cable Structural Integrity</title>
		<link>https://pdl-group.com/floating-wind-mooring-chain-inclinometer-cable-structural-integrity/</link>
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		<dc:creator><![CDATA[marc]]></dc:creator>
		<pubDate>Thu, 16 Feb 2023 11:56:40 +0000</pubDate>
				<category><![CDATA[OFFSHORE WIND]]></category>
		<category><![CDATA[RENEWABLE ENERGY]]></category>
		<category><![CDATA[COMPUTATIONAL FLUID DYNAMICS]]></category>
		<guid isPermaLink="false">https://pdl-group.com/?p=4855</guid>

					<description><![CDATA[<p>The post <a href="https://pdl-group.com/floating-wind-mooring-chain-inclinometer-cable-structural-integrity/">Floating Wind Mooring Chain Inclinometer Cable Structural Integrity</a> appeared first on <a href="https://pdl-group.com">PDL Group</a>.</p>
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<section class="av_textblock_section "  itemscope="itemscope" itemtype="https://schema.org/BlogPosting" itemprop="blogPost" ><div class='avia_textblock  '   itemprop="text" ><h1>Floating Wind Mooring Chain Inclinometer Cable Structural Integrity</h1>
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<section class="av_textblock_section "  itemscope="itemscope" itemtype="https://schema.org/BlogPosting" itemprop="blogPost" ><div class='avia_textblock  '   itemprop="text" ><h4>SUMMARY</h4>
<p>Global assessment of inclinometer power cable subject to dynamic mooring movement and hydrodynamic loading.</p>
<h4>SITUATION</h4>
<p>In southern Europe there is now a growing interest in floating wind, particularly for water depths in the region of 50m to 1000m. France’s first floating wind pilot project ‘Provence Grand Large’ will employ three nominally 8MW turbines each supported by a tri-pod semi-submersible platform in up to 100m water depth. The wind farm is located 17 km off Port Saint Louis du Rhone off Frances’ southern coast.</p>
<p>Each corner of the semisubmersible platform is constrained by a pair of mooring chains fixed to the seabed. The chain connectors can rotate about two axes at their upper ends and are fitted with inclinometers so that the rotation angle(s) can be measured. The inclinometer sensor cables have a complex routing and must be able to cope with the maximum in-plane and out-of-plane angles the chain connectors may take up, relative to the platform, in the full range of environmental conditions and maintenance/transport configurations.</p>
<p>PDL was contracted by the inclinometer cable supplier to undertake structural integrity assessments for the key cable components under ultimate limit state (ULS) and fatigue limit state (FLS) conditions.</p>
<h4>CHALLENGE</h4>
<p>Due to the angles the mooring chains take up during operation and transit, the proposed cable must be suitability mounted to be compliant, without becoming taut, exceeding it minimum bend radius or failing due to fatigue.</p>
<p>Contact between the cable sheath and the surrounding structure also needed to be accurately predicted as exposed bolt threads and pinch points could damage the cable.</p>
<h4>SOLUTION</h4>
<p>To develop a dynamic model of the sensor cable and chain connectors, global dynamic analysis software OrcaFlex was used.</p>
<p>PDL used an internal toolset to estimate the non-linear ‘stick-slip’ bending behaviour of the helically wound armour wires. As the behaviour is hysteretic, accurately capturing the stiffness of the cable in both the rigid ‘stick’ and more flexible ‘slip’ regions was critical to realistically predicting the movement of the cable due to the chain block movements.</p>
<p>The tool also calculates the fatigue life of the cable, taking into account the similar non-linear stress transfer functions.</p>
<p>Through python posting scripts, a series of goal seek simulations where run, taking into account such parameters as operating angles, marine growth, cable end angle and length to find an optimised cable route. The desired route was one that best suited the limitations of the cable within the 3D space governed by the two articulations and provided a suitable fatigue life.</p>
<p>Bend stiffeners at the end locations where also specified to reduce the loading into the sensor equipment – these had to be bespoke to each clamp.</p>
<h4>BENEFITS</h4>
<ul>
<li>Reduce risk: Accurately predict fatigue life of cable to ensure no loss of function due to cable failure while operational.</li>
<li>Reduce cost: Working with the cable supplier to optimise the grade and thickness of armour wires used, cable routing and lengths between clamps and clamp bend stiffeners.</li>
<li>Liaise with the FLOAT manufacturer, inclinometer equipment provider to ensure the final cable routing design worked for each party.</li>
</ul>
</div></section><br />
<div   data-size='no scaling'  data-lightbox_size='large'  data-animation='slide'  data-conditional_play=''  data-ids='4857,4858,4856'  data-video_counter='0'  data-autoplay='false'  data-bg_slider='false'  data-slide_height=''  data-handle='av_slideshow'  data-interval='5'  data-class=' avia-builder-el-11  el_after_av_textblock  avia-builder-el-last  '  data-el_id=''  data-css_id=''  data-scroll_down=''  data-control_layout='av-control-default'  data-custom_markup=''  data-perma_caption=''  data-autoplay_stopper=''  data-image_attachment=''  data-min_height='0px'  class='avia-slideshow avia-slideshow-2  av-control-default av-default-height-applied avia-slideshow-no scaling av_slideshow  avia-builder-el-11  el_after_av_textblock  avia-builder-el-last   avia-slide-slider '  itemprop="image" itemscope="itemscope" itemtype="https://schema.org/ImageObject" ><ul class='avia-slideshow-inner ' style='padding-bottom: 68.703108252947%;' ><li  class=' slide-1 ' ><div data-rel='slideshow-2' class='avia-slide-wrap '   ><div class="avia-caption av-slideshow-caption"><div class="avia-inner-caption"><h2  class='avia-caption-title  '  itemprop="name" >Figure -1: PGL Floating Wind Project - artist’s impression</h2></div></div><img src='https://pdl-group.com/wp-content/uploads/2023/01/1-Floating-Wind-Mooring-Chain-Inclinometer-Cable-Structural-Integrity-fig1.png' width='933' height='641' title='1 - Floating Wind Mooring Chain Inclinometer Cable Structural Integrity - fig1' alt=''  itemprop="thumbnailUrl"   /></div></li><li  class=' slide-2 ' ><div data-rel='slideshow-2' class='avia-slide-wrap '   ><div class="avia-caption av-slideshow-caption"><div class="avia-inner-caption"><h2  class='avia-caption-title  '  itemprop="name" >Figure -2: Chain Connector Gimbal</h2></div></div><img src='https://pdl-group.com/wp-content/uploads/2023/01/1-Floating-Wind-Mooring-Chain-Inclinometer-Cable-Structural-Integrity-fig2.png' width='521' height='867' title='1 - Floating Wind Mooring Chain Inclinometer Cable Structural Integrity - fig2' alt=''  itemprop="thumbnailUrl"   /></div></li><li  class=' slide-3 ' ><div data-rel='slideshow-2' class='avia-slide-wrap '   ><div class="avia-caption av-slideshow-caption"><div class="avia-inner-caption"><h2  class='avia-caption-title  '  itemprop="name" >Figure -3: OrcaFlex Model (with and without marine growth)</h2></div></div><img src='https://pdl-group.com/wp-content/uploads/2023/01/1-Floating-Wind-Mooring-Chain-Inclinometer-Cable-Structural-Integrity-fig3.png' width='1052' height='471' title='1 - Floating Wind Mooring Chain Inclinometer Cable Structural Integrity - fig3' alt=''  itemprop="thumbnailUrl"   /></div></li></ul><div class='avia-slideshow-arrows avia-slideshow-controls'><a href='#prev' class='prev-slide' aria-hidden='true' data-av_icon='' data-av_iconfont='entypo-fontello'>Previous</a><a href='#next' class='next-slide' aria-hidden='true' data-av_icon='' data-av_iconfont='entypo-fontello'>Next</a></div><div class='avia-slideshow-dots avia-slideshow-controls'><a href='#1' class='goto-slide active' >1</a><a href='#2' class='goto-slide ' >2</a><a href='#3' class='goto-slide ' >3</a></div></div></p></div><div class="flex_column av_one_fourth  flex_column_div av-zero-column-padding   avia-builder-el-12  el_after_av_three_fourth  avia-builder-el-last  " style='margin-top:0; margin-bottom:30px; border-radius:0px; '><p><div  style=' margin-top:0; margin-bottom:15px;'  class='hr hr-custom hr-center hr-icon-no   avia-builder-el-13  el_before_av_textblock  avia-builder-el-first '><span class='hr-inner   inner-border-av-border-fat' style=' width:100%; border-color:#211f1e;' ><span class='hr-inner-style'></span></span></div><br />
<section class="av_textblock_section "  itemscope="itemscope" itemtype="https://schema.org/BlogPosting" itemprop="blogPost" ><div class='avia_textblock  '   itemprop="text" ><h4>SECTOR</h4>
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</div></section><br />
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<section class="av_textblock_section "  itemscope="itemscope" itemtype="https://schema.org/BlogPosting" itemprop="blogPost" ><div class='avia_textblock  '   itemprop="text" ><h4>NICHE CAPABILITIES</h4>
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<section class="av_textblock_section "  itemscope="itemscope" itemtype="https://schema.org/BlogPosting" itemprop="blogPost" ><div class='avia_textblock  '   itemprop="text" ><p>OrcaFlex</p>
<p>Non-linear Cable Behaviour</p>
</div></section><br />
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<section class="av_textblock_section "  itemscope="itemscope" itemtype="https://schema.org/BlogPosting" itemprop="blogPost" ><div class='avia_textblock  '   itemprop="text" ><p>Ultimate Limit State (ULS)</p>
<p>Fatigue Limit State (FLS)</p>
</div></section><br />
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<section class="av_textblock_section "  itemscope="itemscope" itemtype="https://schema.org/BlogPosting" itemprop="blogPost" ><div class='avia_textblock  '   itemprop="text" ><p>OrcaFlex</p>
<p>Python</p>
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<p>The post <a href="https://pdl-group.com/floating-wind-mooring-chain-inclinometer-cable-structural-integrity/">Floating Wind Mooring Chain Inclinometer Cable Structural Integrity</a> appeared first on <a href="https://pdl-group.com">PDL Group</a>.</p>
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		<title>Thermal Assessment of a Dynamic Bend Stiffener Cooling System</title>
		<link>https://pdl-group.com/thermal-assessment-of-a-dynamic-bend-stiffener-cooling-system/</link>
					<comments>https://pdl-group.com/thermal-assessment-of-a-dynamic-bend-stiffener-cooling-system/#respond</comments>
		
		<dc:creator><![CDATA[marc]]></dc:creator>
		<pubDate>Thu, 16 Feb 2023 11:56:16 +0000</pubDate>
				<category><![CDATA[OFFSHORE WIND]]></category>
		<category><![CDATA[RENEWABLE ENERGY]]></category>
		<category><![CDATA[COMPUTATIONAL FLUID DYNAMICS]]></category>
		<guid isPermaLink="false">https://pdl-group.com/?p=4860</guid>

					<description><![CDATA[<p>The post <a href="https://pdl-group.com/thermal-assessment-of-a-dynamic-bend-stiffener-cooling-system/">Thermal Assessment of a Dynamic Bend Stiffener Cooling System</a> appeared first on <a href="https://pdl-group.com">PDL Group</a>.</p>
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<section class="av_textblock_section "  itemscope="itemscope" itemtype="https://schema.org/BlogPosting" itemprop="blogPost" ><div class='avia_textblock  '   itemprop="text" ><h1>Thermal Assessment of a Dynamic Bend Stiffener Cooling<br />
System</h1>
</div></section><br />
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<section class="av_textblock_section "  itemscope="itemscope" itemtype="https://schema.org/BlogPosting" itemprop="blogPost" ><div class='avia_textblock  '   itemprop="text" ><h4>SUMMARY</h4>
<p>We were asked to verify a bend stiffener cooling system by determining a viable working fluid and corresponding minimum required flow rates, as well as calculating the maximum temperatures in both the bend stiffener and power cable.</p>
<p>FEA was used to determine the deformed bend stiffener shapes when subjected to their maximum service angles. CFD was then used to disprove a water-based approach (hence confirming an air-based approach). We were then able to carry out detailed 3D thermal fluid flow simulations to calculate flow rate against temperature pass/fail envelopes and identify hot spot locations in terms of temperature and flow velocity.</p>
<h4>SITUATION</h4>
<p>Our client is a leading provider of subsea cable technology and offshore services connecting the global offshore energy industry. Power cables for oil and gas and offshore wind usually require a cable protection system that protects the cable from over-bending due, predominantly, to environmental loads. The power cable sits inside the cable protection system so that there is a small clearance between the two. Two of the client’s power cable bend stiffeners required a bespoke cooling system design to ensure the temperature of the various power cable components, as well as the bend stiffener, remained within their operational temperature ranges when running.</p>
<p>A fluid-based cooling strategy was proposed by the client, considering both air and seawater, and PDL were contracted to validate the design by conducting a thermal assessment of the power cable/bend stiffener assemblies when subjected to their worst-case tolerance stack-ups and service angles. An accurate prediction was required to prevent overheating of the power cables (and bend stiffeners) within the operating envelope bearing in mind the high cost associated with replacing cables.</p>
<h4>CHALLENGE</h4>
<p>The proposed cooling system design consisted of fluid flow being forced into the base of the bend stiffener via supply channels, carrying heat away from the stiffener and cable via the gap between the two solid assemblies.</p>
<p>Previous thermal assessments had been undertaken by 3rd parties, but these did not account for the deformed shape of the cable and bend stiffener when in their<br />
operational positions. During operation, the maximum service angles for the cables was between 25° and 35°, thus a portion of the power cable pushes up against the bend stiffener, resulting in a non-uniform thermal profile along the length of the bend stiffener. This prompted the need for a 3D analysis to determine:<br />
1. The deformed shape of the bend stiffeners/cables when subjected to their<br />
maximum service angles.<br />
2. The most suitable working fluid (water vs air).<br />
3. The minimum required flow rate of the working fluid to meet the maximum temperature requirements.</p>
<p>FEA was required to determine the deformed shapes, followed by CFD to finalise a working fluid and minimum flow rate.</p>
<h4>SOLUTION</h4>
<p>Using the drawings provided by the client, we first generated 3D models for both the bend stiffeners for the extreme tolerance stack-ups. Finite Element Analysis was then used to generate the cable and bend stiffener geometry in the deformed configurations, this accurately captured the shapes of the 3D gaps.</p>
<p>ANSYS Fluent was then used to set up thermal fluid flow simulations for worst-case ambient conditions (i.e., solar radiation and no wind) to confirm that the maximum tolerance stack-up models were conservative from a maximum temperature perspective. By running a transient water fill analysis, it was concluded that a water-based cooling system was impractical due to the relatively high pumping flow rates required to achieve a good volume fill.</p>
<p>Several steady-state simulations were carried out on the models, using air as the working fluid. Following which, a pass/fail envelope of flow rate against maximum temperature was determined to help the client quantify the required airflow in each case. By parameterising the inlet flow rate in the model, we were able to save time running 10-off repetitive simulations. Contour plots of temperature and velocity were also provided to the client in a technical report to help identify any hot spot regions and to understand the velocities of the airflow.</p>
<h4>BENEFITS</h4>
<ul>
<li>Reduced the need for complex physical testing, iterating air temperature and flow rate.</li>
<li>Allowed for an appropriate cooling system to be specified, understanding the specific flow rate and air temperature required.</li>
<li>Accounted for solar radiation and emissivity.</li>
<li>Determined hot spot locations not easily calculated by hand.</li>
</ul>
</div></section><br />
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<section class="av_textblock_section "  itemscope="itemscope" itemtype="https://schema.org/BlogPosting" itemprop="blogPost" ><div class='avia_textblock  '   itemprop="text" ><h4>SECTOR</h4>
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<p>Fatigue Limit State (FLS)</p>
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<p>ANSYS CFD-Post</p>
<p>Volume of Fluid (Multi-Phase)</p>
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<p>The post <a href="https://pdl-group.com/thermal-assessment-of-a-dynamic-bend-stiffener-cooling-system/">Thermal Assessment of a Dynamic Bend Stiffener Cooling System</a> appeared first on <a href="https://pdl-group.com">PDL Group</a>.</p>
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		<title>FRACTURE MECHANICS FINDS SAFE CYCLES FOR SUBSEA FLANGE</title>
		<link>https://pdl-group.com/fracture-mechanics-finds-safe-cycles-for-subsea-flange/</link>
					<comments>https://pdl-group.com/fracture-mechanics-finds-safe-cycles-for-subsea-flange/#respond</comments>
		
		<dc:creator><![CDATA[marc]]></dc:creator>
		<pubDate>Mon, 28 Nov 2022 08:50:46 +0000</pubDate>
				<category><![CDATA[OIL & GAS]]></category>
		<category><![CDATA[VALVE CAPABILITY]]></category>
		<category><![CDATA[FINITE ELEMENT ANALYSIS]]></category>
		<guid isPermaLink="false">https://pdl-group.com/?p=4748</guid>

					<description><![CDATA[<p><span class="av_font_icon avia_animate_when_visible avia-icon-animate av-icon-style- av-no-color avia-icon-pos-left avia_start_animation avia_start_delayed_animation" style=""><span class="av-icon-char" style="font-size:20px;line-height:20px;" aria-hidden="true" data-av_icon="" data-av_iconfont="entypo-fontello"></span></span>INDEPENDENTLY VERIFIED PRODUCT COMPLIANCE</p>
<p><span class="av_font_icon avia_animate_when_visible avia-icon-animate av-icon-style- av-no-color avia-icon-pos-left avia_start_animation avia_start_delayed_animation" style=""><span class="av-icon-char" style="font-size:20px;line-height:20px;" aria-hidden="true" data-av_icon="" data-av_iconfont="entypo-fontello"></span></span>REDUCED DEVELOPMENT TIME BY 24 WEEKS (50% REDUCTION)</p>
<p><span class="av_font_icon avia_animate_when_visible avia-icon-animate av-icon-style- av-no-color avia-icon-pos-left avia_start_animation avia_start_delayed_animation" style=""><span class="av-icon-char" style="font-size:20px;line-height:20px;" aria-hidden="true" data-av_icon="" data-av_iconfont="graph-down"></span></span>PROVIDED CERTAINTY OF THE QUALIFICATION TESTING</p>
<p>The post <a href="https://pdl-group.com/fracture-mechanics-finds-safe-cycles-for-subsea-flange/">FRACTURE MECHANICS FINDS SAFE CYCLES FOR SUBSEA FLANGE</a> appeared first on <a href="https://pdl-group.com">PDL Group</a>.</p>
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<section class="av_textblock_section "  itemscope="itemscope" itemtype="https://schema.org/BlogPosting" itemprop="blogPost" ><div class='avia_textblock  '   itemprop="text" ><h1>FRACTURE MECHANICS FINDS SAFE CYCLES FOR SUBSEA FLANGE</h1>
</div></section><br />
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<section class="av_textblock_section "  itemscope="itemscope" itemtype="https://schema.org/BlogPosting" itemprop="blogPost" ><div class='avia_textblock  '   itemprop="text" ><h4>SUMMARY</h4>
<p>A manufacturer of subsea components contacted us to assess three subsea flange designs, which were designed to operate under High-Pressure, High-Temperature (HPHT) conditions. The flanges were to be installed in two oil fields with extreme requirements, including pressures and temperatures of up to 20ksi and 400°F.</p>
<p>PDL performed Finite Element Analysis (FEA) to produce a capacity chart finding upper bounds on safe loading conditions, design verification in accordance with API 17TR8 and ASME BPVC Sec. VIII Div. 3, and fracture mechanics (FM) assessments to API 579-1 / ASME FFS. A new screening method was internally developed to quickly identify the critical paths for crack growth based on the stresses within each component. FM calculations were completed based on the provided load histogram and we showed that the flanges were suitable for HPHT and met the desired operational cycles.</p>
<p>The analyses were required were complex and involved, and the efficiencies introduced by PDL’s in-house tools allowed both a more thorough assessment whilst reducing timescales.</p>
<h4>SITUATION</h4>
<p>The client had been awarded a contract to provide HPHT flanges for use across two oil fields. Three different sizes were assessed. There is a growing requirement for components to operate at higher pressures and temperature in the subsea industry, with API 17TR8 providing guidance on the procedure for assessing such components. PDL are world leaders in HPHT assessments and have developed several in-house postprocessing and calculation tools to improve the efficiency of obtaining results.</p>
<h4>CHALLENGE</h4>
<p>Our client needed multiple complex assessments to be performed on three different flanges under two different extreme operational conditions. Design validation and fracture mechanics assessments needed to be performed to give the end client confidence in the compliance of the designs.</p>
<p>We have significant experience in the analysis of highly non-linear and dynamic systems and were approached to provide technical support to our client’s team using FEA.</p>
<h4>SOLUTION</h4>
<p>Starting with an analysis plan, we summarised the bounding load cases and also identified all other critical parameters, such as the data source for the gasholder geometry, material properties, the assessment code, software of choice and post-processing requirements. The model assemblies all contained a flange, mating block, gasket, internal cladding, with modelled studs and nuts. Different material properties were assigned to each part, which had been obtained through the clients own<br />
physical testing.</p>
<p>Half-symmetry FEA models were created, using the ANSYS Parametric Design Language (APDL) graphical user interface for ANSYS Mechanical, to represent the multiple loading scenarios required for the assessment.</p>
<p>A Pressure-Bending-Tension (PBT) capacity chart was produced, considering both structural and serviceability limit criteria.</p>
<p>The flange design was then validated in accordance with API 17TR8 and ASME VIII Div. 3 for design conditions. This considered protection against global plastic collapse, local failure, hydrostatic pressure test and ratcheting.</p>
<p>Linear Elastic Fracture Mechanics (LEFM) assessments were then performed on all components. LEFM examines highly-stressed regions in the model and predicts how a crack would grow if there was an existing flaw in the material. The initial flaw size is based on the examinable limits of non-destructive testing (NDT) or design code recommendations. The results of FEA can be used to evaluate the crack propagation characteristics such as initiation site, direction and growth rate.</p>
<p>For efficiency, we developed a macro using APDL to identify the peak stress locations in each component and perform fracture mechanics assessments on multiple paths from these points.</p>
<p>Our in-house calculation sheets were able to predict the behaviour of theoretical “cracks” originating from these locations, which accounted for the geometry of the model and the direction of crack growth.</p>
<p>The fracture mechanics assessments required the individual threads to be represented, therefore a sub-model was generated with a refined mesh, to accurately capture the stress distribution around the thread root. This stress profile dictated the crack growth rate and direction of propagation.</p>
<p>Through demonstrating that the model replicated current failure modes, sufficient confidence was achieved to use the model as a virtual test bed for a number of corrective actions and ultimately practical interventions that improved the gas holder performance.</p>
<h4>BENEFITS</h4>
<ul>
<li>The capacity assessment identified the bounding load-limits of the flange, considering pressure, bending moment and tension.</li>
<li>The fracture mechanics analysis we performed gave confidence for through-life operation.</li>
<li>Our experience in fracture mechanics allowed a thorough screening of the model, using our in-house calculation sheets to assess multiple potential crack locations without adding to the project timescale.</li>
<li>A similar methodology could be adopted across the three flange designs, significantly reducing timescales for the client and reducing costs.</li>
<li>We had a close partnership with the client to address 3 rd party comments and support the review process.</li>
</ul>
</div></section><br />
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<li>FEA</li>
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<ul>
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<p>The post <a href="https://pdl-group.com/fracture-mechanics-finds-safe-cycles-for-subsea-flange/">FRACTURE MECHANICS FINDS SAFE CYCLES FOR SUBSEA FLANGE</a> appeared first on <a href="https://pdl-group.com">PDL Group</a>.</p>
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		<title>HISC ASSESSMENT TO PREVENT BRITTLE FRACTURE OF VALVE</title>
		<link>https://pdl-group.com/hisc-assessment-to-prevent-brittle-fracture-of-valve/</link>
					<comments>https://pdl-group.com/hisc-assessment-to-prevent-brittle-fracture-of-valve/#respond</comments>
		
		<dc:creator><![CDATA[marc]]></dc:creator>
		<pubDate>Mon, 28 Nov 2022 08:49:53 +0000</pubDate>
				<category><![CDATA[OIL & GAS]]></category>
		<category><![CDATA[VALVE CAPABILITY]]></category>
		<category><![CDATA[FINITE ELEMENT ANALYSIS]]></category>
		<guid isPermaLink="false">https://pdl-group.com/?p=4767</guid>

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		</span>MINIMISED REVENUE LOSSES
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<p>The post <a href="https://pdl-group.com/hisc-assessment-to-prevent-brittle-fracture-of-valve/">HISC ASSESSMENT TO PREVENT BRITTLE FRACTURE OF VALVE</a> appeared first on <a href="https://pdl-group.com">PDL Group</a>.</p>
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<section class="av_textblock_section "  itemscope="itemscope" itemtype="https://schema.org/BlogPosting" itemprop="blogPost" ><div class='avia_textblock  '   itemprop="text" ><h1>HISC ASSESSMENT TO PREVENT BRITTLE FRACTURE OF VALVE</h1>
</div></section><br />
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<section class="av_textblock_section "  itemscope="itemscope" itemtype="https://schema.org/BlogPosting" itemprop="blogPost" ><div class='avia_textblock  '   itemprop="text" ><h4>SUMMARY</h4>
<p>PDL were contracted by a valve manufacturer to assess their Duplex steel, 15 ksi subsea gate valve using Finite Element Analysis (FEA). The material and operational environment of the valve raised concerns of Hydrogen Induced Stress Cracking (HISC), as this would be subjected to cathodic protection when installed subsea. The assessment was carried out in accordance with the Category 2 criteria of DNVGL-RP-F112.</p>
<p>All components except for the body were found to pass the HISC assessment. Failures were identified in the body gasket groove, exhibiting high levels of strain. We discussed with the client potential design modifications to address these areas, and methods to reduce conservatism in the analysis. Quick identification of failures meant that design issues were discovered before manufacturing had begun, reducing costs and wastage for the client. We also recommended that an additional assessment to ASME BPVC Sec. VIII Div. 2 be performed to fully validate the valve, due to very high stress levels in one region.</p>
<h4>SITUATION</h4>
<p>Our client was a valve manufacturer, who had produced a gate valve for use subsea in the oil and gas industry. Duplex stainless steel was used for the valve components as this has advantages with regard to corrosion resistance, ease of manufacture, and strength. However, Duplex stainless steel is susceptible to Hydrogen Induced Stress Cracking (HISC), with design guideline DNV-RP-F112 established for the offshore industry. Our client needed to show compliance to this standard for the end customer to have confidence in their product.</p>
<h4>CHALLENGE</h4>
<p>Subsea metallic components that are exposed or have damaged polymetric coating will experience electrochemical reactions due to cathodic protection. Hydrogen is one of the products, which can penetrate hardened steel and diffuse into the bulk of the material. This can potentially lead to brittle fracture in materials that are normally ductile. High tensile stress is a main contributor to HISC and valves operating in extreme environments are particularly susceptible due to the high pressures and thermal gradients present. Since it is impractical to examine components without bringing them out of service HISC assessments are an important screening procedure prior to installation.</p>
<h4>SOLUTION</h4>
<p>We received a 3D CAD model of the valve from the client and prepared this for the analysis. On inspection of the geometry and loading, it was identified that a half-symmetry model could be used. This reduced solving time, whilst maintaining accuracy. Components of interest were the Valve Body, Bonnet, Pusher and Housing. The flange connection, bolts, and seal ring were included in the model to create an overall representative setup, although these parts were not directly assessed. Non-linear material properties were assigned for the assessed components to comply with the Category 2 criteria of DNVGL-RP-F112.</p>
<p>The analysis considered design loads in the open and closed conditions to identify the worst-case combination. Hydrostatic test conditions were not assessed, as this is assumed to take place topside, prior to the application of cathodic protection.</p>
<p>Convection effects were applied to the external surfaces of the valve which represented heat transfer to the surrounding seawater. The calculated (temperature dependent) coefficients were generated using PDL’s in-house tool and considered the geometry and orientation of the valves faces. The results of the thermal analyses were imported into the structural load cases to determine the stresses and deflections due to thermal gradients.</p>
<p>At locations of high maximum principal strains, paths were considered through the wall thickness. Linearised stresses were taken for each path.</p>
<p>Significant failures against DNVGL-RP-F112 were identified in one component, and as such PDL provided multiple potential design recommendations to address the issue. Within the same component there were locations with a more marginal failure, and for these failures we also suggested modifications that could be made to the analysis to reduce some conservatism.</p>
<p>A pass against the HISC assessment criteria was demonstrated for the Housing component, however, the stresses were found to be beyond the material yield stress through-section in some regions. Further structural assessment, in line with an applicable design code such as ASME BPVC Sec. VIII Div. 2 was recommended.</p>
<h4>BENEFITS</h4>
<ul>
<li>PDL’s investigations showed which components and locations were most at risk of HISC, and whether these regions passed the criteria of DNVGL-RP-F112.</li>
<li>Quick identification of failures meant that design issues were discovered before manufacturing had begun, reducing costs and wastage for the client.</li>
<li>Potential design changes were recommended to the client.</li>
<li>We identified that an additional ASME BPVC Sec. VIII Div. 2 assessment was required for the valve to be acceptable for use.</li>
</ul>
</div></section><br />
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<section class="av_textblock_section "  itemscope="itemscope" itemtype="https://schema.org/BlogPosting" itemprop="blogPost" ><div class='avia_textblock  '   itemprop="text" ><h4>ANALYSIS TOOLSET</h4>
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<ul>
<li>ANSYS Mechanical</li>
<li>ANSYS DesignModeler</li>
<li>In-house calculation tool for definition of convection coefficient</li>
</ul>
</div></section><br />
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<ul>
<li>DNVGL-RP-F112</li>
</ul>
</div></section><br />
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<p style="text-align: center;">We’ve delivered over 1,500 successfully completed projects. If you’re working on a safety critical project or complex engineering challenge and need a technical solution, our engineering experts can help.</p>
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<p>The post <a href="https://pdl-group.com/hisc-assessment-to-prevent-brittle-fracture-of-valve/">HISC ASSESSMENT TO PREVENT BRITTLE FRACTURE OF VALVE</a> appeared first on <a href="https://pdl-group.com">PDL Group</a>.</p>
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		<title>FATIGUE ASSESSMENT FOR DESIGN-LIFE OF SUBSEA GATE VALVE</title>
		<link>https://pdl-group.com/fatigue-assessment-for-design-life-of-subsea-gate-valve/</link>
					<comments>https://pdl-group.com/fatigue-assessment-for-design-life-of-subsea-gate-valve/#respond</comments>
		
		<dc:creator><![CDATA[marc]]></dc:creator>
		<pubDate>Mon, 28 Nov 2022 08:48:59 +0000</pubDate>
				<category><![CDATA[OIL & GAS]]></category>
		<category><![CDATA[VALVE CAPABILITY]]></category>
		<category><![CDATA[FINITE ELEMENT ANALYSIS]]></category>
		<guid isPermaLink="false">https://pdl-group.com/?p=4743</guid>

					<description><![CDATA[<p><span class="av_font_icon avia_animate_when_visible avia-icon-animate av-icon-style- av-no-color avia-icon-pos-left avia_start_animation avia_start_delayed_animation" style=""><span class="av-icon-char" style="font-size:20px;line-height:20px;" aria-hidden="true" data-av_icon="" data-av_iconfont="entypo-fontello"></span></span>INDEPENDENTLY VERIFIED PRODUCT COMPLIANCE</p>
<p><span class="av_font_icon avia_animate_when_visible avia-icon-animate av-icon-style- av-no-color avia-icon-pos-left avia_start_animation avia_start_delayed_animation" style=""><span class="av-icon-char" style="font-size:20px;line-height:20px;" aria-hidden="true" data-av_icon="" data-av_iconfont="entypo-fontello"></span></span>REDUCED DEVELOPMENT TIME BY 24 WEEKS (50% REDUCTION)</p>
<p><span class="av_font_icon avia_animate_when_visible avia-icon-animate av-icon-style- av-no-color avia-icon-pos-left avia_start_animation avia_start_delayed_animation" style=""><span class="av-icon-char" style="font-size:20px;line-height:20px;" aria-hidden="true" data-av_icon="" data-av_iconfont="graph-down"></span></span>PROVIDED CERTAINTY OF THE QUALIFICATION TESTING</p>
<p>The post <a href="https://pdl-group.com/fatigue-assessment-for-design-life-of-subsea-gate-valve/">FATIGUE ASSESSMENT FOR DESIGN-LIFE OF SUBSEA GATE VALVE</a> appeared first on <a href="https://pdl-group.com">PDL Group</a>.</p>
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<section class="av_textblock_section "  itemscope="itemscope" itemtype="https://schema.org/BlogPosting" itemprop="blogPost" ><div class='avia_textblock  '   itemprop="text" ><h1>FATIGUE ASSESSMENT FOR DESIGN-LIFE OF SUBSEA GATE VALVE</h1>
</div></section><br />
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<section class="av_textblock_section "  itemscope="itemscope" itemtype="https://schema.org/BlogPosting" itemprop="blogPost" ><div class='avia_textblock  '   itemprop="text" ><h4>SUMMARY</h4>
<p>We were contacted by our client (a valve manufacturer) to assess two High Pressure, High Temperature (HPHT) subsea gate valves with a Rated Working Pressure (RWP) of 20ksi and Rated Working Temperature (RWT) of 150°C, in accordance with API 17TR8. To assess compliance, PDL performed Finite Element Analysis (FEA) to check for protection against excessive yielding, local failure and ratcheting in accordance with the elastic-plastic analysis methodologies in ASME BPVC Sec. VIII Div. 2. A serviceability assessment was also completed looking at fastener utilisation and seal pocket deformation (to assess whether leakage could be expected).</p>
<p>Fatigue calculations were completed using FEA in conjunction with the equivalent stress method outlined in ASME BPVC Sec. VIII Div. 2. This approach is applicable to Low Cycle Fatigue (LCF) since the provided fatigue curves are based on a ‘pseudo stress’ calculated from strain-controlled fatigue testing. Fatigue calculations were completed based on the provided load histogram and issues were highlighted, primarily relating to thermal expansion effects. PDL worked closely with the client to highlight potential conservatism in the input data and define what changes could be made such that the valves were fit for purpose. The quality of the final report was noted to be excellent by the end client (tier 1 contractor).</p>
<h4>SITUATION</h4>
<p>Our client was supplying two designs of HPHT gate valve for use in an onerous and safety critical subsea operating environment. They were under pressure to demonstrate compliance to API 17TR8 to their end client, or risking losing the order.</p>
<h4>CHALLENGE</h4>
<p>Our client had limited time and budget but needed to complete a large number of complex simulations in order to prove compliance with API 17TR8. The imposed operating conditions and provided fatigue histogram were onerous.</p>
<h4>SOLUTION</h4>
<p>Since the two gate valves were of similar design, the worst-case setup could be assessed directly using FEA, with the other valve verified through supporting engineering judgement. This resulted in a significant time and cost saving.</p>
<p>Material properties were supplied by the client, with additional data taken from ASME BPVC Sec. II Part D. With accurate and referenced inputs, the model could be accurately represented.</p>
<p>Loads were applied to the model which included internal pressure, self-weight, and temperature. These were factored to match the ASME assessment criteria. Convection effects were applied to the external surfaces of the valve which represented heat transfer to the surrounding seawater. The calculated (temperature dependent) coefficients were generated using PDL’s in-house tool and considered the geometry and orientation of the valves faces.</p>
<p>The fatigue assessment used a load histogram provided by the client which detailed the operation for a 20-year design life. The histogram detailed the pressure, temperature, and fluid exposure across a 5-year window.</p>
<p>The fatigue assessment used material-specific design curves to calculate the maximum number of acceptable cycles, with a “knock down” penalty applied to account for the subsea environment. The fatigue damage was calculated for the critical regions in the valve body and the fasteners using PDL’s in-house tools. Through close discussions with the client, a maximum operating temperature was found which satisfied the assessment criteria.</p>
<p>Our extensive experience working with complex FEA to the provisions of the ASME design codes meant that all the above could be completed in an efficient and timely manner. We also supported the client in responding to numerous queries from the end client; with all responses found to be satisfactory.</p>
<h4>BENEFITS</h4>
<ul>
<li>PDL were able to save our clients money by assessing the worst-case loading and setup, which verified the two valve designs.</li>
<li>We found the maximum operating conditions that conformed to ASME and API standards and was acceptable to both client and customer.</li>
<li>We had a close partnership with the client to address 3rd party comments and support the review process.</li>
<li>Our experience in fatigue assessments allowed a thorough screening of the model, using our in-house calculation sheets.</li>
<li>Our extensive experience working with complex FEA to the provisions of the ASME design codes, allowed for completion of multiple complex simulations in a timely manner.</li>
</ul>
</div></section><br />
<div   data-size='no scaling'  data-lightbox_size='large'  data-animation='slide'  data-conditional_play=''  data-ids='4746,4744,4745'  data-video_counter='0'  data-autoplay='false'  data-bg_slider='false'  data-slide_height=''  data-handle='av_slideshow'  data-interval='5'  data-class=' avia-builder-el-13  el_after_av_textblock  avia-builder-el-last  '  data-el_id=''  data-css_id=''  data-scroll_down=''  data-control_layout='av-control-default'  data-custom_markup=''  data-perma_caption=''  data-autoplay_stopper=''  data-image_attachment=''  data-min_height='0px'  class='avia-slideshow avia-slideshow-6  av-control-default av-default-height-applied avia-slideshow-no scaling av_slideshow  avia-builder-el-13  el_after_av_textblock  avia-builder-el-last   avia-slide-slider '  itemprop="image" itemscope="itemscope" itemtype="https://schema.org/ImageObject" ><ul class='avia-slideshow-inner ' style='padding-bottom: 139.41908713693%;' ><li  class=' slide-1 ' ><div data-rel='slideshow-6' class='avia-slide-wrap '   ><div class="avia-caption av-slideshow-caption"><div class="avia-inner-caption"><h2  class='avia-caption-title  '  itemprop="name" >Fig 1: Temperature profile through the valve when submerged</h2></div></div><img src='https://pdl-group.com/wp-content/uploads/2022/11/5-OVT-Gate-Valve-Fatigue-1.png' width='241' height='336' title='5 - OVT Gate Valve Fatigue 1' alt=''  itemprop="thumbnailUrl"   /></div></li><li  class=' slide-2 ' ><div data-rel='slideshow-6' class='avia-slide-wrap '   ><div class="avia-caption av-slideshow-caption"><div class="avia-inner-caption"><h2  class='avia-caption-title  '  itemprop="name" >Fig 2: Supporting boundary conditions for the gate valve</h2></div></div><img src='https://pdl-group.com/wp-content/uploads/2022/11/5-OVT-Gate-Valve-Fatigue-2.png' width='467' height='268' title='5 - OVT Gate Valve Fatigue 2' alt=''  itemprop="thumbnailUrl"   /></div></li><li  class=' slide-3 ' ><div data-rel='slideshow-6' class='avia-slide-wrap '   ><div class="avia-caption av-slideshow-caption"><div class="avia-inner-caption"><h2  class='avia-caption-title  '  itemprop="name" >Fig 3: Gate valve mesh</h2></div></div><img src='https://pdl-group.com/wp-content/uploads/2022/11/5-OVT-Gate-Valve-Fatigue-3.png' width='357' height='349' title='5 - OVT Gate Valve Fatigue 3' alt=''  itemprop="thumbnailUrl"   /></div></li></ul><div class='avia-slideshow-arrows avia-slideshow-controls'><a href='#prev' class='prev-slide' aria-hidden='true' data-av_icon='' data-av_iconfont='entypo-fontello'>Previous</a><a href='#next' class='next-slide' aria-hidden='true' data-av_icon='' data-av_iconfont='entypo-fontello'>Next</a></div><div class='avia-slideshow-dots avia-slideshow-controls'><a href='#1' class='goto-slide active' >1</a><a href='#2' class='goto-slide ' >2</a><a href='#3' class='goto-slide ' >3</a></div></div></p></div><div class="flex_column av_one_fourth  flex_column_div av-zero-column-padding   avia-builder-el-14  el_after_av_three_fourth  avia-builder-el-last  " style='margin-top:0; margin-bottom:30px; border-radius:0px; '><p><div  style=' margin-top:0; margin-bottom:15px;'  class='hr hr-custom hr-center hr-icon-no   avia-builder-el-15  el_before_av_textblock  avia-builder-el-first '><span class='hr-inner   inner-border-av-border-fat' style=' width:100%; border-color:#211f1e;' ><span class='hr-inner-style'></span></span></div><br />
<section class="av_textblock_section "  itemscope="itemscope" itemtype="https://schema.org/BlogPosting" itemprop="blogPost" ><div class='avia_textblock  '   itemprop="text" ><h4>SECTOR</h4>
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<section class="av_textblock_section "  itemscope="itemscope" itemtype="https://schema.org/BlogPosting" itemprop="blogPost" ><div class='avia_textblock  '   itemprop="text" ><h4>ANALYSIS TOOLSET</h4>
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<ul>
<li>ANSYS Mechanical</li>
<li>ANSYS Design Modeler</li>
<li>In-house calculation tool for definition of convection coefficient</li>
<li>In-house fatigue calculation tools</li>
</ul>
</div></section><br />
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<section class="av_textblock_section "  itemscope="itemscope" itemtype="https://schema.org/BlogPosting" itemprop="blogPost" ><div class='avia_textblock  '   itemprop="text" ><h4>CODES</h4>
<div  style=' margin-top:0; margin-bottom:0;'  class='hr hr-custom hr-center hr-icon-no   avia-builder-el-24  avia-builder-el-no-sibling '><span class='hr-inner   inner-border-av-border-thin' style=' width:100%; border-color:#211f1e;' ><span class='hr-inner-style'></span></span></div>
<ul>
<li>API 17TR8</li>
<li>ASME BPVC Sec. VIII Div. 2</li>
<li>ASME BPVC Sec. II Part D</li>
</ul>
</div></section></p></div></div></div></div><!-- close content main div --></div></div><div id='av_section_24'  class='avia-section alternate_color avia-section-default avia-no-border-styling avia-bg-style-scroll  avia-builder-el-25  el_after_av_section  avia-builder-el-last   container_wrap fullsize' style='background-color: #ebeaf1; background-image: linear-gradient(45deg,#223d4f,#1d4b79); '  ><div class='container' ><div class='template-page content  av-content-full alpha units'><div class='post-entry post-entry-type-page post-entry-4843'><div class='entry-content-wrapper clearfix'>
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<p style="text-align: center;">We’ve delivered over 1,500 successfully completed projects. If you’re working on a safety critical project or complex engineering challenge and need a technical solution, our engineering experts can help.</p>
</div></section>
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<p>The post <a href="https://pdl-group.com/fatigue-assessment-for-design-life-of-subsea-gate-valve/">FATIGUE ASSESSMENT FOR DESIGN-LIFE OF SUBSEA GATE VALVE</a> appeared first on <a href="https://pdl-group.com">PDL Group</a>.</p>
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		<title>HPHT VALVE FOR EXTREME SUBSEA ENVIRONMENT</title>
		<link>https://pdl-group.com/hpht-valve-for-extreme-subsea-environment/</link>
					<comments>https://pdl-group.com/hpht-valve-for-extreme-subsea-environment/#respond</comments>
		
		<dc:creator><![CDATA[marc]]></dc:creator>
		<pubDate>Mon, 28 Nov 2022 08:48:26 +0000</pubDate>
				<category><![CDATA[OIL & GAS]]></category>
		<category><![CDATA[VALVE CAPABILITY]]></category>
		<guid isPermaLink="false">https://pdl-group.com/?p=4731</guid>

					<description><![CDATA[<p><span class="av_font_icon avia_animate_when_visible avia-icon-animate av-icon-style- av-no-color avia-icon-pos-left avia_start_animation avia_start_delayed_animation" style=""><span class="av-icon-char" style="font-size:20px;line-height:20px;" aria-hidden="true" data-av_icon="" data-av_iconfont="entypo-fontello"></span></span>INDEPENDENTLY VERIFIED PRODUCT COMPLIANCE</p>
<p><span class="av_font_icon avia_animate_when_visible avia-icon-animate av-icon-style- av-no-color avia-icon-pos-left avia_start_animation avia_start_delayed_animation" style=""><span class="av-icon-char" style="font-size:20px;line-height:20px;" aria-hidden="true" data-av_icon="" data-av_iconfont="entypo-fontello"></span></span>REDUCED DEVELOPMENT TIME BY 24 WEEKS (50% REDUCTION)</p>
<p><span class="av_font_icon avia_animate_when_visible avia-icon-animate av-icon-style- av-no-color avia-icon-pos-left avia_start_animation avia_start_delayed_animation" style=""><span class="av-icon-char" style="font-size:20px;line-height:20px;" aria-hidden="true" data-av_icon="" data-av_iconfont="graph-down"></span></span>PROVIDED CERTAINTY OF THE QUALIFICATION TESTING</p>
<p>The post <a href="https://pdl-group.com/hpht-valve-for-extreme-subsea-environment/">HPHT VALVE FOR EXTREME SUBSEA ENVIRONMENT</a> appeared first on <a href="https://pdl-group.com">PDL Group</a>.</p>
]]></description>
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<section class="av_textblock_section "  itemscope="itemscope" itemtype="https://schema.org/BlogPosting" itemprop="blogPost" ><div class='avia_textblock  '   itemprop="text" ><h1>HPHT VALVE FOR EXTREME SUBSEA ENVIRONMENT</h1>
</div></section><br />
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<section class="av_textblock_section "  itemscope="itemscope" itemtype="https://schema.org/BlogPosting" itemprop="blogPost" ><div class='avia_textblock  '   itemprop="text" ><h4>SUMMARY</h4>
<p>Our client (a valve manufacturer) contacted us to assess a large subsea High-Pressure, High-Temperature (HPHT) gate valve prior to physical testing. Their end-customer wanted the valve to be installed in two oil fields which had different operational requirements. This included a Rated Working Pressure (RWP) of 20ksi and Rated Working Temperature (RWT) of 400°F. To assess compliance, PDL performed Finite Element Analysis (FEA) to check for excessive yielding, local failure and ratcheting in accordance with the elastic-plastic analysis methodologies in API 17TR8 and ASME BPVC Sec. VIII Div. 3. A serviceability assessment was also completed looking at fastener utilisation and seal pocket deformation (to assess whether leakage could be expected).</p>
<h4>SITUATION</h4>
<p>The client had designed a large HPHT gate valve for use in an extreme subsea environment. They needed to show compliance to API 17TR8 and ASME BPVC Sec. VIII Div.3 which had been requested by their end client, for two different operational conditions. PDL had previously assessed several of the clients other valve designs, and they knew that we could provide an in-depth analysis efficiently, to meet the deadline of submitting their bid.</p>
<h4>CHALLENGE</h4>
<p>Subsea valves are often required to operate in extreme environments and ASME BPVC Sec. VIII Div. 3 has been established to assess HPHT vessels for these applications. The difference in bore fluid and seawater temperature produces large thermal gradients through the valve. When this is combined with high operating pressures, the loading on the valve is onerous. A thorough FEA assessment is required to ensure safe physical testing and give confidence in a valve’s integrity over its design life, since it is impractical to bring components out of service for inspection.</p>
<h4>SOLUTION</h4>
<p>We used ANSYS DesignModeler to prepare a computationally efficient model using the clients existing geometry. A critical part of this process was to ensure that the model response remained accurate, whilst removing features and components which were not relevant to the assessment. The internal cladding was modelled by referring to section drawings received from the client. This region<br />
was assigned unique material properties and provided the best representation of the valve.</p>
<p>During the model setup within ANSYS Mechanical, using the ANSYS Parametric Design Language (APDL) graphical user interface, representative connections and interfaces between all the valve components were defined, ensuring the load paths between components were accurately modelled.</p>
<p>We took the end user’s specification and translated this into a detailed analysis specification. It was critically important that not only the assessment method but also the setup of the model was identical to that used for the actual tests.</p>
<p>PDL showed that the HPHT gate valve passed all API 17TR8 and ASME BPVC Sec. VIII Div. 3 criteria. Additionally, serviceability of certain valve components, including sealing at the top and bottom bonnets and fastener loading was assessed and found to be acceptable.</p>
<h4>BENEFITS</h4>
<ul>
<li>We decreased risk by allowing valves to be “tested” in the virtual world prior to manufacture.</li>
<li>PDL were able to save our clients money by assessing the manual and hydraulic configurations of the gate simultaneously in a conservative case.</li>
<li>We had a close partnership with the client to address 3rd party comments and support the review process.</li>
<li>Our extensive experience working with complex FEA to the provisions of the ASME design codes, allowed for completion of multiple complex simulations in a timely manner.</li>
</ul>
</div></section><br />
<div   data-size='no scaling'  data-lightbox_size='large'  data-animation='slide'  data-conditional_play=''  data-ids='4734,4735,4733'  data-video_counter='0'  data-autoplay='false'  data-bg_slider='false'  data-slide_height=''  data-handle='av_slideshow'  data-interval='5'  data-class=' avia-builder-el-13  el_after_av_textblock  avia-builder-el-last  '  data-el_id=''  data-css_id=''  data-scroll_down=''  data-control_layout='av-control-default'  data-custom_markup=''  data-perma_caption=''  data-autoplay_stopper=''  data-image_attachment=''  data-min_height='0px'  class='avia-slideshow avia-slideshow-7  av-control-default av-default-height-applied avia-slideshow-no scaling av_slideshow  avia-builder-el-13  el_after_av_textblock  avia-builder-el-last   avia-slide-slider '  itemprop="image" itemscope="itemscope" itemtype="https://schema.org/ImageObject" ><ul class='avia-slideshow-inner ' style='padding-bottom: 79.542203147353%;' ><li  class=' slide-1 ' ><div data-rel='slideshow-7' class='avia-slide-wrap '   ><div class="avia-caption av-slideshow-caption"><div class="avia-inner-caption"><h2  class='avia-caption-title  '  itemprop="name" >Fig 1: Sectioned view showing model mesh and gasket</h2></div></div><img src='https://pdl-group.com/wp-content/uploads/2022/11/4-HPHT-Valve-Image-1.png' width='699' height='556' title='4 - HPHT Valve Image 1' alt=''  itemprop="thumbnailUrl"   /></div></li><li  class=' slide-2 ' ><div data-rel='slideshow-7' class='avia-slide-wrap '   ><div class="avia-caption av-slideshow-caption"><div class="avia-inner-caption"><h2  class='avia-caption-title  '  itemprop="name" >Fig 2: Stress distribution under Hydrostatic test pressure</h2></div></div><img src='https://pdl-group.com/wp-content/uploads/2022/11/4-HPHT-Valve-Image-2.png' width='167' height='238' title='4 - HPHT Valve Image 2' alt=''  itemprop="thumbnailUrl"   /></div></li><li  class=' slide-3 ' ><div data-rel='slideshow-7' class='avia-slide-wrap '   ><div class="avia-caption av-slideshow-caption"><div class="avia-inner-caption"><h2  class='avia-caption-title  '  itemprop="name" >Fig 3: Contact status of sealing faces</h2></div></div><img src='https://pdl-group.com/wp-content/uploads/2022/11/4-HPHT-Valve-Image-3.png' width='317' height='203' title='4 - HPHT Valve Image 3' alt=''  itemprop="thumbnailUrl"   /></div></li></ul><div class='avia-slideshow-arrows avia-slideshow-controls'><a href='#prev' class='prev-slide' aria-hidden='true' data-av_icon='' data-av_iconfont='entypo-fontello'>Previous</a><a href='#next' class='next-slide' aria-hidden='true' data-av_icon='' data-av_iconfont='entypo-fontello'>Next</a></div><div class='avia-slideshow-dots avia-slideshow-controls'><a href='#1' class='goto-slide active' >1</a><a href='#2' class='goto-slide ' >2</a><a href='#3' class='goto-slide ' >3</a></div></div></p></div><div class="flex_column av_one_fourth  flex_column_div av-zero-column-padding   avia-builder-el-14  el_after_av_three_fourth  avia-builder-el-last  " style='margin-top:0; margin-bottom:30px; border-radius:0px; '><p><div  style=' margin-top:0; margin-bottom:15px;'  class='hr hr-custom hr-center hr-icon-no   avia-builder-el-15  el_before_av_textblock  avia-builder-el-first '><span class='hr-inner   inner-border-av-border-fat' style=' width:100%; border-color:#211f1e;' ><span class='hr-inner-style'></span></span></div><br />
<section class="av_textblock_section "  itemscope="itemscope" itemtype="https://schema.org/BlogPosting" itemprop="blogPost" ><div class='avia_textblock  '   itemprop="text" ><h4>SECTOR</h4>
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</div></section><br />
<section class="av_textblock_section "  itemscope="itemscope" itemtype="https://schema.org/BlogPosting" itemprop="blogPost" ><div class='avia_textblock  '   itemprop="text" ><p><a href="https://pdl-group.com/sectors/oil-gas/">Oil &amp; Gas</a></p>
</div></section><br />
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<section class="av_textblock_section "  itemscope="itemscope" itemtype="https://schema.org/BlogPosting" itemprop="blogPost" ><div class='avia_textblock  '   itemprop="text" ><h4>ANALYSIS TOOLSET</h4>
<div  style=' margin-top:0; margin-bottom:0;'  class='hr hr-custom hr-center hr-icon-no   avia-builder-el-21  avia-builder-el-no-sibling '><span class='hr-inner   inner-border-av-border-thin' style=' width:100%; border-color:#211f1e;' ><span class='hr-inner-style'></span></span></div>
<ul>
<li>ANSYS Parametric Design Language (ADPL)</li>
<li>ANSYS Design Modeler</li>
<li>In-house ANSYS APDL macros for postprocessing</li>
</ul>
</div></section><br />
<div  style=' margin-top:0; margin-bottom:15px;'  class='hr hr-custom hr-center hr-icon-no   avia-builder-el-22  el_after_av_textblock  el_before_av_textblock '><span class='hr-inner   inner-border-av-border-fat' style=' width:100%; border-color:#211f1e;' ><span class='hr-inner-style'></span></span></div><br />
<section class="av_textblock_section "  itemscope="itemscope" itemtype="https://schema.org/BlogPosting" itemprop="blogPost" ><div class='avia_textblock  '   itemprop="text" ><h4>CODES</h4>
<div  style=' margin-top:0; margin-bottom:0;'  class='hr hr-custom hr-center hr-icon-no   avia-builder-el-24  avia-builder-el-no-sibling '><span class='hr-inner   inner-border-av-border-thin' style=' width:100%; border-color:#211f1e;' ><span class='hr-inner-style'></span></span></div>
<ul>
<li>API 17TR8</li>
<li>ASME BPVC Sec. VIII Div. 3</li>
</ul>
</div></section></p></div></div></div></div><!-- close content main div --></div></div><div id='av_section_28'  class='avia-section alternate_color avia-section-default avia-no-border-styling avia-bg-style-scroll  avia-builder-el-25  el_after_av_section  avia-builder-el-last   container_wrap fullsize' style='background-color: #ebeaf1; background-image: linear-gradient(45deg,#223d4f,#1d4b79); '  ><div class='container' ><div class='template-page content  av-content-full alpha units'><div class='post-entry post-entry-type-page post-entry-4843'><div class='entry-content-wrapper clearfix'>
<section class="av_textblock_section "  itemscope="itemscope" itemtype="https://schema.org/BlogPosting" itemprop="blogPost" ><div class='avia_textblock  '   itemprop="text" ><h2 style="text-align: center;">PDL CAN DELIVER FOR YOU</h2>
<p style="text-align: center;">We’ve delivered over 1,500 successfully completed projects. If you’re working on a safety critical project or complex engineering challenge and need a technical solution, our engineering experts can help.</p>
</div></section>
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<p>The post <a href="https://pdl-group.com/hpht-valve-for-extreme-subsea-environment/">HPHT VALVE FOR EXTREME SUBSEA ENVIRONMENT</a> appeared first on <a href="https://pdl-group.com">PDL Group</a>.</p>
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		<title>TRANSIENT RESPONSE OF SWING VALVE DUE TO FLOW INDUCED PULSATIONS</title>
		<link>https://pdl-group.com/transient-response-of-swing-valve-due-to-flow-induced-pulsations/</link>
					<comments>https://pdl-group.com/transient-response-of-swing-valve-due-to-flow-induced-pulsations/#respond</comments>
		
		<dc:creator><![CDATA[marc]]></dc:creator>
		<pubDate>Mon, 28 Nov 2022 08:47:38 +0000</pubDate>
				<category><![CDATA[OIL & GAS]]></category>
		<category><![CDATA[VALVE CAPABILITY]]></category>
		<category><![CDATA[COMPUTATIONAL FLUID DYNAMICS]]></category>
		<guid isPermaLink="false">https://pdl-group.com/?p=4676</guid>

					<description><![CDATA[<p><span class="av_font_icon avia_animate_when_visible avia-icon-animate av-icon-style- av-no-color avia-icon-pos-left avia_start_animation avia_start_delayed_animation" style=""><span class="av-icon-char" style="font-size:20px;line-height:20px;" aria-hidden="true" data-av_icon="" data-av_iconfont="entypo-fontello"></span></span>INDEPENDENTLY VERIFIED PRODUCT COMPLIANCE</p>
<p><span class="av_font_icon avia_animate_when_visible avia-icon-animate av-icon-style- av-no-color avia-icon-pos-left avia_start_animation avia_start_delayed_animation" style=""><span class="av-icon-char" style="font-size:20px;line-height:20px;" aria-hidden="true" data-av_icon="" data-av_iconfont="entypo-fontello"></span></span>REDUCED DEVELOPMENT TIME BY 24 WEEKS (50% REDUCTION)</p>
<p><span class="av_font_icon avia_animate_when_visible avia-icon-animate av-icon-style- av-no-color avia-icon-pos-left avia_start_animation avia_start_delayed_animation" style=""><span class="av-icon-char" style="font-size:20px;line-height:20px;" aria-hidden="true" data-av_icon="" data-av_iconfont="graph-down"></span></span>PROVIDED CERTAINTY OF THE QUALIFICATION TESTING</p>
<p>The post <a href="https://pdl-group.com/transient-response-of-swing-valve-due-to-flow-induced-pulsations/">TRANSIENT RESPONSE OF SWING VALVE DUE TO FLOW INDUCED PULSATIONS</a> appeared first on <a href="https://pdl-group.com">PDL Group</a>.</p>
]]></description>
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<section class="av_textblock_section "  itemscope="itemscope" itemtype="https://schema.org/BlogPosting" itemprop="blogPost" ><div class='avia_textblock  '   itemprop="text" ><h1>TRANSIENT RESPONSE OF SWING VALVE DUE TO FLOW INDUCED PULSATIONS</h1>
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<div  class='avia-icon-list-container   avia-builder-el-10  el_after_av_hr  el_before_av_hr '><ul class='avia-icon-list avia-icon-list-left av-iconlist-big avia_animate_when_almost_visible '>
<li><div  style='background-color:#ffffff; color:#5a666a; ' class='iconlist_icon  avia-font-graph-down'><span class='iconlist-char ' aria-hidden='true' data-av_icon='' data-av_iconfont='graph-down'></span></div><article class="article-icon-entry av-iconlist-empty"  itemscope="itemscope" itemtype="https://schema.org/BlogPosting" itemprop="blogPost" ><div class='iconlist_content_wrap'><header class="entry-content-header"><h6 class='av_iconlist_title iconlist_title   '  itemprop="headline"  >REDUCED AMOUNT OF PHYSICAL TESTING</h6></header><div class='iconlist_content  '  itemprop="text"  ></div></div><footer class="entry-footer"></footer></article><div class='iconlist-timeline'></div></li>
<li><div  style='background-color:#ffffff; color:#5a666a; ' class='iconlist_icon  avia-font-savings'><span class='iconlist-char ' aria-hidden='true' data-av_icon='' data-av_iconfont='savings'></span></div><article class="article-icon-entry av-iconlist-empty"  itemscope="itemscope" itemtype="https://schema.org/BlogPosting" itemprop="blogPost" ><div class='iconlist_content_wrap'><header class="entry-content-header"><h6 class='av_iconlist_title iconlist_title   '  itemprop="headline"  >SIGNIFICANT COST REDUCTION</h6></header><div class='iconlist_content  '  itemprop="text"  ></div></div><footer class="entry-footer"></footer></article><div class='iconlist-timeline'></div></li>
<li><div  style='background-color:#ffffff; color:#5a666a; ' class='iconlist_icon  avia-font-entypo-fontello'><span class='iconlist-char ' aria-hidden='true' data-av_icon='' data-av_iconfont='entypo-fontello'></span></div><article class="article-icon-entry av-iconlist-empty"  itemscope="itemscope" itemtype="https://schema.org/BlogPosting" itemprop="blogPost" ><div class='iconlist_content_wrap'><header class="entry-content-header"><h6 class='av_iconlist_title iconlist_title   '  itemprop="headline"  >SIGNIFICANTLY REDUCED TIMESCALES</h6></header><div class='iconlist_content  '  itemprop="text"  ></div></div><footer class="entry-footer"></footer></article><div class='iconlist-timeline'></div></li>
<li><div  style='background-color:#ffffff; color:#5a666a; ' class='iconlist_icon  avia-font-entypo-fontello'><span class='iconlist-char ' aria-hidden='true' data-av_icon='' data-av_iconfont='entypo-fontello'></span></div><article class="article-icon-entry av-iconlist-empty"  itemscope="itemscope" itemtype="https://schema.org/BlogPosting" itemprop="blogPost" ><div class='iconlist_content_wrap'><header class="entry-content-header"><h4 class='av_iconlist_title iconlist_title   '  itemprop="headline"  >ACCESS TO A WIDER RANGE OF MEASUREMENTS</h4></header><div class='iconlist_content  '  itemprop="text"  ></div></div><footer class="entry-footer"></footer></article><div class='iconlist-timeline'></div></li>
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<section class="av_textblock_section "  itemscope="itemscope" itemtype="https://schema.org/BlogPosting" itemprop="blogPost" ><div class='avia_textblock  '   itemprop="text" ><h4>SUMMARY</h4>
<p>We were contracted to validate a client’s non-return valve design in order to save costs on physical testing.</p>
<p>An analytical model of the valve was created using Computational Fluid Dynamics (CFD), with the disc angle parameterised to determine the relationship between angle and fluid flow rate. The analytical model was also used to investigate the risk of Fluid Induced Pulsation (FLIP) and fluttering, with output frequencies and amplitudes were quantified. A final assessment of low flow chattering was conducted qualitatively. Our analysis was summarised in a technical report, which includes detailed contour plots of fluid flow patterns and graphical representations of the complex phenomena.</p>
<h4>SITUATION</h4>
<p>Our client is an internationally renowned supplier of high-pressure valves, actuators and controls to the oil and gas industry. During the development of a subsea non-return valve, which would be subject to a range of operating conditions, the client required design validation to progress through a legislative approval process.</p>
<p>An investigation into Fluid Induced Pulsation (FLIP) formulated part of the validation. FLIP often occurs in flexible pipes with a corrugates profile on the inner layer, as this profile can cause a build-up of vortex shedding which leads to flow induced pulsations. FLIP can cause excessive oscillatory motions and forces, in valves, resulting in a potential early onset of failure. Investigations into ‘fluttering’ of the valve disc, low flow chattering and an understanding of disc position as a function of flow rate were also required.</p>
<h4>CHALLENGE</h4>
<p>We were asked to use CFD and supporting hand calculations to validate the valve design by determining the following:<br />
1. Disc opening position as a function of mass flow rate<br />
2. Disc oscillatory flutter due to a constant flow<br />
3. Disc response due to FLIP<br />
4. Susceptibility to low flow chattering (repeated impact of the disc onto the valve seat due to flutter)</p>
<h4>SOLUTION</h4>
<p>After confirming the valve operating conditions by reviewing supplied specifications, we summarised our approach for each investigation in an Analysis Plan document.</p>
<p>Hand calculations were first carried out for a range of discrete disc angles to determine the torque, acting to close the valve, due to disc mass. A CFD model was then created and parameterised by disc angle, saving time (hence cost) on running a separate case for each position. For each case, the mass flow rate was ramped until the torque due to fluid forces balanced with the disc mass torques calculated by hand. Using machine learning methods employed by Design of Experiments and response surfaces generated within ANSYS Workbench, a curve was fitted for the relationship between disc angle and mass flow rate.</p>
<p>Disc oscillatory flutter was considered by specifying a time-dependent transient analysis to capture the oscillatory motion of the disc under steady flow conditions. The disc was initially positioned at the torque balancing angle for each flow rate and was then controlled using CFX Expression Language (CEL) and backwards Euler equations. This involved rigid body mesh deformation to capture movement of the disc. A monitor of disc angle over time was used to illustrate and quantify the extent of transient flutter at both prescribed flow rates in terms of frequency and amplitude.</p>
<p>FLIP was investigated by taking the flutter investigation a step further and applying a sinusoidal pressure profile. The frequency and amplitude of the FLIP was defined and its effects on disc flutter were determined, as well as average forces acting on the disc.</p>
<p>Susceptibility to low flow chattering was qualitative. The response was inferred from the flutter and FLIP responses and the risk of chattering was identified and summarised in a technical report (along with the approaches and results from the other investigations).</p>
<p>Post-processing each of the CFD simulations enabled flow patterns to be plotted and provided access to a wider range of flow variables than in the case of physical testing.</p>
<h4>BENEFITS</h4>
<ul>
<li>Reduced time spent on determining a relationship between angle and flow rate by using a parametric analytical model.</li>
<li>Reduced costs associated with physical testing.</li>
<li>Fluid flow patterns were provided.</li>
<li>CFD analysis enables access to a wider range of variables than by means of physical measurement.</li>
</ul>
</div></section><br />
<div   data-size='no scaling'  data-lightbox_size='large'  data-animation='slide'  data-conditional_play=''  data-ids='4722,4723,4721'  data-video_counter='0'  data-autoplay='false'  data-bg_slider='false'  data-slide_height=''  data-handle='av_slideshow'  data-interval='5'  data-class=' avia-builder-el-13  el_after_av_textblock  avia-builder-el-last  '  data-el_id=''  data-css_id=''  data-scroll_down=''  data-control_layout='av-control-default'  data-custom_markup=''  data-perma_caption=''  data-autoplay_stopper=''  data-image_attachment=''  data-min_height='0px'  class='avia-slideshow avia-slideshow-8  av-control-default av-default-height-applied avia-slideshow-no scaling av_slideshow  avia-builder-el-13  el_after_av_textblock  avia-builder-el-last   avia-slide-slider '  itemprop="image" itemscope="itemscope" itemtype="https://schema.org/ImageObject" ><ul class='avia-slideshow-inner ' style='padding-bottom: 70.319634703196%;' ><li  class=' slide-1 ' ><div data-rel='slideshow-8' class='avia-slide-wrap '   ><div class="avia-caption av-slideshow-caption"><div class="avia-inner-caption"><h2  class='avia-caption-title  '  itemprop="name" >Figure 1: Total pressure contours</h2></div></div><img src='https://pdl-group.com/wp-content/uploads/2022/11/3-Transient-Response-of-Swing-Image-1.png' width='438' height='308' title='3 - Transient Response of Swing Image 1' alt=''  itemprop="thumbnailUrl"   /></div></li><li  class=' slide-2 ' ><div data-rel='slideshow-8' class='avia-slide-wrap '   ><div class="avia-caption av-slideshow-caption"><div class="avia-inner-caption"><h2  class='avia-caption-title  '  itemprop="name" >Figure 2: Velocity contours and vectors</h2></div></div><img src='https://pdl-group.com/wp-content/uploads/2022/11/3-Transient-Response-of-Swing-Image-2.png' width='453' height='307' title='3 - Transient Response of Swing Image 2' alt=''  itemprop="thumbnailUrl"   /></div></li><li  class=' slide-3 ' ><div data-rel='slideshow-8' class='avia-slide-wrap '   ><div class="avia-caption av-slideshow-caption"><div class="avia-inner-caption"><h2  class='avia-caption-title  '  itemprop="name" >Figure 3: Relationship between disc angle and flow rate</h2></div></div><img src='https://pdl-group.com/wp-content/uploads/2022/11/3-Transient-Response-of-Swing-Image-3.png' width='2071' height='1369' title='3 - Transient Response of Swing Image 3' alt=''  itemprop="thumbnailUrl"   /></div></li></ul><div class='avia-slideshow-arrows avia-slideshow-controls'><a href='#prev' class='prev-slide' aria-hidden='true' data-av_icon='' data-av_iconfont='entypo-fontello'>Previous</a><a href='#next' class='next-slide' aria-hidden='true' data-av_icon='' data-av_iconfont='entypo-fontello'>Next</a></div><div class='avia-slideshow-dots avia-slideshow-controls'><a href='#1' class='goto-slide active' >1</a><a href='#2' class='goto-slide ' >2</a><a href='#3' class='goto-slide ' >3</a></div></div></p></div><div class="flex_column av_one_fourth  flex_column_div av-zero-column-padding   avia-builder-el-14  el_after_av_three_fourth  avia-builder-el-last  " style='margin-top:0; margin-bottom:30px; border-radius:0px; '><p><div  style=' margin-top:0; margin-bottom:15px;'  class='hr hr-custom hr-center hr-icon-no   avia-builder-el-15  el_before_av_textblock  avia-builder-el-first '><span class='hr-inner   inner-border-av-border-fat' style=' width:100%; border-color:#211f1e;' ><span class='hr-inner-style'></span></span></div><br />
<section class="av_textblock_section "  itemscope="itemscope" itemtype="https://schema.org/BlogPosting" itemprop="blogPost" ><div class='avia_textblock  '   itemprop="text" ><h4>SECTOR</h4>
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<section class="av_textblock_section "  itemscope="itemscope" itemtype="https://schema.org/BlogPosting" itemprop="blogPost" ><div class='avia_textblock  '   itemprop="text" ><h4>PROJECT ATTRIBUTES</h4>
<p>Computational Fluid Dynamics</p>
<ul>
<li>ANSYS Workbench Parametric</li>
<li>ANSYS DesignXplorer</li>
<li>ANSYS DesignModeler</li>
<li>ANSYS Meshing</li>
<li>ANSYS CFX</li>
<li>ANSYS CFD-Post</li>
</ul>
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<blockquote>
<p>WE WERE APPROACHED DUE TO OUR SIGNIFICANT CFD EXPERIENCE,<br />
GATHERED OVER MULTIPLE PROJECTS, AND FOLLOWING A NUMBER OF<br />
SUCCESSFUL VALVE ASSESSMENTS</p>
</blockquote>
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<p style="text-align: center;">We’ve delivered over 1,500 successfully completed projects. If you’re working on a safety critical project or complex engineering challenge and need a technical solution, our engineering experts can help.</p>
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<p>The post <a href="https://pdl-group.com/transient-response-of-swing-valve-due-to-flow-induced-pulsations/">TRANSIENT RESPONSE OF SWING VALVE DUE TO FLOW INDUCED PULSATIONS</a> appeared first on <a href="https://pdl-group.com">PDL Group</a>.</p>
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		<title>DETERMINATION OF VALVE FLOW COEFFICIENTS USING PARAMETRIC CFD METHODS</title>
		<link>https://pdl-group.com/determination-of-valve-flow-coefficients-using-parametric-cfd-methods/</link>
					<comments>https://pdl-group.com/determination-of-valve-flow-coefficients-using-parametric-cfd-methods/#respond</comments>
		
		<dc:creator><![CDATA[marc]]></dc:creator>
		<pubDate>Mon, 28 Nov 2022 08:46:48 +0000</pubDate>
				<category><![CDATA[NUCLEAR]]></category>
		<category><![CDATA[OIL & GAS]]></category>
		<category><![CDATA[VALVE CAPABILITY]]></category>
		<category><![CDATA[COMPUTATIONAL FLUID DYNAMICS]]></category>
		<guid isPermaLink="false">https://pdl-group.com/?p=4704</guid>

					<description><![CDATA[<p><span class="av_font_icon avia_animate_when_visible avia-icon-animate av-icon-style- av-no-color avia-icon-pos-left avia_start_animation avia_start_delayed_animation" style=""><span class="av-icon-char" style="font-size:20px;line-height:20px;" aria-hidden="true" data-av_icon="" data-av_iconfont="entypo-fontello"></span></span>INDEPENDENTLY VERIFIED PRODUCT COMPLIANCE</p>
<p><span class="av_font_icon avia_animate_when_visible avia-icon-animate av-icon-style- av-no-color avia-icon-pos-left avia_start_animation avia_start_delayed_animation" style=""><span class="av-icon-char" style="font-size:20px;line-height:20px;" aria-hidden="true" data-av_icon="" data-av_iconfont="entypo-fontello"></span></span>REDUCED DEVELOPMENT TIME BY 24 WEEKS (50% REDUCTION)</p>
<p><span class="av_font_icon avia_animate_when_visible avia-icon-animate av-icon-style- av-no-color avia-icon-pos-left avia_start_animation avia_start_delayed_animation" style=""><span class="av-icon-char" style="font-size:20px;line-height:20px;" aria-hidden="true" data-av_icon="" data-av_iconfont="graph-down"></span></span>PROVIDED CERTAINTY OF THE QUALIFICATION TESTING</p>
<p>The post <a href="https://pdl-group.com/determination-of-valve-flow-coefficients-using-parametric-cfd-methods/">DETERMINATION OF VALVE FLOW COEFFICIENTS USING PARAMETRIC CFD METHODS</a> appeared first on <a href="https://pdl-group.com">PDL Group</a>.</p>
]]></description>
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<section class="av_textblock_section "  itemscope="itemscope" itemtype="https://schema.org/BlogPosting" itemprop="blogPost" ><div class='avia_textblock  '   itemprop="text" ><h1>DETERMINATION OF VALVE FLOW COEFFICIENTS USING PARAMETRIC CFD METHODS</h1>
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<div  class='avia-icon-list-container   avia-builder-el-10  el_after_av_hr  el_before_av_hr '><ul class='avia-icon-list avia-icon-list-left av-iconlist-big avia_animate_when_almost_visible '>
<li><div  style='background-color:#ffffff; color:#5a666a; ' class='iconlist_icon  avia-font-graph-down'><span class='iconlist-char ' aria-hidden='true' data-av_icon='' data-av_iconfont='graph-down'></span></div><article class="article-icon-entry av-iconlist-empty"  itemscope="itemscope" itemtype="https://schema.org/BlogPosting" itemprop="blogPost" ><div class='iconlist_content_wrap'><header class="entry-content-header"><h4 class='av_iconlist_title iconlist_title   '  itemprop="headline"  >REDUCED AMOUNT OF PHYSICAL TESTING</h4></header><div class='iconlist_content  '  itemprop="text"  ></div></div><footer class="entry-footer"></footer></article><div class='iconlist-timeline'></div></li>
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<section class="av_textblock_section "  itemscope="itemscope" itemtype="https://schema.org/BlogPosting" itemprop="blogPost" ><div class='avia_textblock  '   itemprop="text" ><h4>SUMMARY</h4>
<p>We were asked to calculate the flow coefficient of 20-off phase check valves using Computational Fluid Dynamics (CFD) to save money on physical testing.</p>
<p>A series of valves were generated parametrically in line with a set of drawings to save time modelling each valve individually. CFD analysis was carried out for the full set of valves to calculated pressure drop based on flow rates for use in the subsequent flow coefficient calculations. The calculations followed the procedure<br />
outlined in ISA75.01 and accounted for a range of flow effects that could influence the valve performance. Our analysis was summarised and presented to the client to showcase trends and fluid flow patterns, saving money on physically testing each valve individually and gaining access to a wider range of variables.</p>
<h4>SITUATION</h4>
<p>Our client design, manufacture and distribute a comprehensive range of industrial valves, instrumentation and associated equipment to a wide range of sectors such as Oil &amp; Gas, Nuclear and Food &amp; Beverage. A range of phase check valves were being developed by the client in both “long” and “short” patterns, and the flow coefficient of each was required for technical specification purposes. The valves were designed to protect systems and equipment from reverse flow, utilising a spring-loading mechanism.</p>
<p>Flow coefficient is often used to specify the capacity and flow characteristics of a component by relating flow rate to the resulting pressure differential. The flow metric can be calculated using physical testing methods and/or using CFD, with the latter becoming increasingly more common due to a reduction in time and<br />
enabling access to a wider range of flow measurements.</p>
<h4>CHALLENGE</h4>
<p>We were asked to generate a parametric analytical model which could be used to represent 20-off phase check valves by modifying a series of key internal bore dimensions. A CFD analysis of the model was then required to calculate a table of flow coefficients for the valves in their fully open positions in line with valve sizing equations outlined in ISA75.01.</p>
<h4>SOLUTION</h4>
<p>The nature of the valve geometry and the equations in ISA75.01 prompted the need for a 3D CFD analysis.</p>
<p>Based on the drawings provided by the client, ANSYS DesignModeler was used to carefully parametrise the internal valve bore dimensions and the adjoining pipes, with the latter varying in terms of schedule.</p>
<p>We then used ANSYS Meshing tools to create a detailed mesh, which was also set up parametrically to allow the inflation layer thickness to be modified between valves due to variations in flow speed. Appropriate inflation layer thicknesses to resolve fluid flow boundary layers were calculated when conducting a mesh independence study, where a target Y+ value was achieved.</p>
<p>An appropriate flow rate for each model to use as an input to the analysis was calculated based on the force required to fully open the spring-loaded valve. ANSYS Fluent was the CFD software used to set up and solve steady-state fluid flow simulations for the valves.</p>
<p>By post-processing the CFD analysis and following the steps outlined in ISA75.01, flow coefficients were calculated. The calculations also checked whether the fluid flow was being choked and accounted for pressure recovery, fluid flow regime and adjoining pipe fittings. Flow coefficient vs valve size trends were plotted and CFD contour plots of pressure and velocity were provided to the client to identify any regions of high velocity. Flow patterns were compared between valves to help the client verify design intentions.</p>
<h4>BENEFITS</h4>
<ul>
<li>Reduced time spent on calculating flow coefficient by using a parametric analytical model.</li>
<li>Reduced costs associated with physical testing.</li>
<li>Regions of high velocity and pressure were identified.</li>
</ul>
</div></section><br />
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<section class="av_textblock_section "  itemscope="itemscope" itemtype="https://schema.org/BlogPosting" itemprop="blogPost" ><div class='avia_textblock  '   itemprop="text" ><h4>PROJECT ATTRIBUTES</h4>
<p>Computational Fluid Dynamics</p>
<ul>
<li>ANSYS Workbench Parametric</li>
<li>ANSYS DesignModeler</li>
<li>ANSYS Meshing</li>
<li>ANSYS FLUENT</li>
<li>ANSYS CFD-Post</li>
<li>Microsoft Excel</li>
</ul>
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<blockquote>
<p>WE WERE APPROACHED DUE TO OUR SIGNIFICANT CFD EXPERIENCE, GATHERED OVER MULTIPLE PROJECTS, AND FOLLOWING A NUMBER OF SUCCESSFUL VALVE FLOW COEFFICIENT ASSESSMENTS.</p>
</blockquote>
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<p>The post <a href="https://pdl-group.com/determination-of-valve-flow-coefficients-using-parametric-cfd-methods/">DETERMINATION OF VALVE FLOW COEFFICIENTS USING PARAMETRIC CFD METHODS</a> appeared first on <a href="https://pdl-group.com">PDL Group</a>.</p>
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		<title>VALVE EROSION CFD TO SUPPORT MAINTENANCE SCHEDULING</title>
		<link>https://pdl-group.com/valve-erosion-cfd-to-support-maintenance-scheduling/</link>
					<comments>https://pdl-group.com/valve-erosion-cfd-to-support-maintenance-scheduling/#respond</comments>
		
		<dc:creator><![CDATA[marc]]></dc:creator>
		<pubDate>Mon, 28 Nov 2022 08:46:05 +0000</pubDate>
				<category><![CDATA[OIL & GAS]]></category>
		<category><![CDATA[VALVE CAPABILITY]]></category>
		<category><![CDATA[COMPUTATIONAL FLUID DYNAMICS]]></category>
		<guid isPermaLink="false">https://pdl-group.com/?p=4696</guid>

					<description><![CDATA[<p><span class="av_font_icon avia_animate_when_visible avia-icon-animate av-icon-style- av-no-color avia-icon-pos-left avia_start_animation avia_start_delayed_animation" style=""><span class="av-icon-char" style="font-size:20px;line-height:20px;" aria-hidden="true" data-av_icon="" data-av_iconfont="entypo-fontello"></span></span>INDEPENDENTLY VERIFIED PRODUCT COMPLIANCE</p>
<p><span class="av_font_icon avia_animate_when_visible avia-icon-animate av-icon-style- av-no-color avia-icon-pos-left avia_start_animation avia_start_delayed_animation" style=""><span class="av-icon-char" style="font-size:20px;line-height:20px;" aria-hidden="true" data-av_icon="" data-av_iconfont="entypo-fontello"></span></span>REDUCED DEVELOPMENT TIME BY 24 WEEKS (50% REDUCTION)</p>
<p><span class="av_font_icon avia_animate_when_visible avia-icon-animate av-icon-style- av-no-color avia-icon-pos-left avia_start_animation avia_start_delayed_animation" style=""><span class="av-icon-char" style="font-size:20px;line-height:20px;" aria-hidden="true" data-av_icon="" data-av_iconfont="graph-down"></span></span>PROVIDED CERTAINTY OF THE QUALIFICATION TESTING</p>
<p>The post <a href="https://pdl-group.com/valve-erosion-cfd-to-support-maintenance-scheduling/">VALVE EROSION CFD TO SUPPORT MAINTENANCE SCHEDULING</a> appeared first on <a href="https://pdl-group.com">PDL Group</a>.</p>
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<section class="av_textblock_section "  itemscope="itemscope" itemtype="https://schema.org/BlogPosting" itemprop="blogPost" ><div class='avia_textblock  '   itemprop="text" ><h1>Valve Erosion CFD to Support Maintenance Scheduling</h1>
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<li><div  style='background-color:#ffffff; color:#5a666a; ' class='iconlist_icon  avia-font-entypo-fontello'><span class='iconlist-char ' aria-hidden='true' data-av_icon='' data-av_iconfont='entypo-fontello'></span></div><article class="article-icon-entry av-iconlist-empty"  itemscope="itemscope" itemtype="https://schema.org/BlogPosting" itemprop="blogPost" ><div class='iconlist_content_wrap'><header class="entry-content-header"><h4 class='av_iconlist_title iconlist_title   '  itemprop="headline"  >REDUCED RISK TO ENVIRONMENT</h4></header><div class='iconlist_content  '  itemprop="text"  ></div></div><footer class="entry-footer"></footer></article><div class='iconlist-timeline'></div></li>
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<li><div  style='background-color:#ffffff; color:#5a666a; ' class='iconlist_icon  avia-font-entypo-fontello'><span class='iconlist-char ' aria-hidden='true' data-av_icon='' data-av_iconfont='entypo-fontello'></span></div><article class="article-icon-entry av-iconlist-empty"  itemscope="itemscope" itemtype="https://schema.org/BlogPosting" itemprop="blogPost" ><div class='iconlist_content_wrap'><header class="entry-content-header"><h4 class='av_iconlist_title iconlist_title   '  itemprop="headline"  >USUAL METHODS COULDN’T PREDICT EROSION RATE</h4></header><div class='iconlist_content  '  itemprop="text"  ></div></div><footer class="entry-footer"></footer></article><div class='iconlist-timeline'></div></li>
<li><div  style='background-color:#ffffff; color:#5a666a; ' class='iconlist_icon  avia-font-entypo-fontello'><span class='iconlist-char ' aria-hidden='true' data-av_icon='' data-av_iconfont='entypo-fontello'></span></div><article class="article-icon-entry av-iconlist-empty"  itemscope="itemscope" itemtype="https://schema.org/BlogPosting" itemprop="blogPost" ><div class='iconlist_content_wrap'><header class="entry-content-header"><h4 class='av_iconlist_title iconlist_title   '  itemprop="headline"  >DETAILED INSIGHT INTO VALVE EROSION RESISTANCE</h4></header><div class='iconlist_content  '  itemprop="text"  ></div></div><footer class="entry-footer"></footer></article><div class='iconlist-timeline'></div></li>
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<section class="av_textblock_section "  itemscope="itemscope" itemtype="https://schema.org/BlogPosting" itemprop="blogPost" ><div class='avia_textblock  '   itemprop="text" ><h4>SUMMARY</h4>
<p>We were asked to calculate the longevity and the risk of a pressure boundary failure for a set of plug valves containing varying amounts of sand in the working fluids.</p>
<p>Computational Fluid Dynamics (CFD) analysis was used to calculate the erosion rates at 6-month intervals, over a 3-year period, using 3D multi-phase particle tracking simulations with the DNV erosion model activated. The geometry was repeatedly updated to include material losses due to erosion for each 6-month interval to capture a changing flow field hence pressure envelope. Our analysis helped the client determine whether changes to maintenance scheduling were required in order to reduce costs and potential environmental impact as a result of valve failure.</p>
<h4>SITUATION</h4>
<p>Our client offers valve engineering expertise globally and operates as a valve management and aftermarket support company. Several plug valves belonging to the client were operating in a producing conventional gas field with varying sand content flowing through them. Erosion was found through practical investigation of a similar set of valves, which raised a question of the longevity of the operating valves. Ultrasound equipment was used to monitor the pipework but could not be used on the valve geometry. Therefore, a prediction of time and severity of valve wear was required to determine maintenance scheduling in order to avoid a complete loss of pressure containment. An accurate prediction was required due to the potential environmental impact complete valve failure could cause, but also due to the high cost associated with replacing the valves.</p>
<h4>CHALLENGE</h4>
<p>We were asked to carry out an Erosion CFD analysis representing 3-year period of operation for each valve to accurately predict:<br />
1) How long the valve trims would last<br />
2) How long the pressure containment would last<br />
This required a set of very detailed CFD models, with erosion, hence loss of material, calculated at regular intervals to capture the change in pressure envelope over time.</p>
<h4>SOLUTION</h4>
<p>The complex valve geometry and fluid/sand interactions prompted the need for<br />
3D multi-phase CFD, with an appropriate erosion model activated.</p>
<p>An analysis plan was first created which summarised our approach including assumptions, flow conditions, inputs and expected outputs. We then used ANSYS SpaceClaim to carry out a significant level of geometry clean-up and fluid flow extraction on the undeformed valve geometries to allow detailed meshes to be created, appropriate for CFD solving.</p>
<p>ANSYS Fluent was then used to set up and solve Eulerian-Lagrangian multi-phase CFD simulations to calculate sand particle tracks in the fluid continuums. The DNV erosion model was activated to calculate erosion rates based on empirical data taken from recognised DNV standards to account for the various valve materials and sand particle restitution coefficients.</p>
<p>Using the post-processed erosion rates, material loss was calculated and plotted on the internal walls for the first 6-month period. We then began the iterative procedure of modifying the valve geometry to include the damage to capture the changing flow field, hence changing pressure envelope, which impacted the amount of erosion and material loss over the subsequent interval. The simulation procedure was repeated up to the 3-year period to determine overall damage to the internal valve geometry, which was quantified as wall loss and changes to the inlet mass flow rate over time. Contour plots of wall deformation were used to visualise regions of relatively high erosion. The full analysis approach, including the results and interpretations, was summarised in a technical report which was issued to the client to help inform the decision of changing the maintenance schedule.</p>
<h4>BENEFITS</h4>
<ul>
<li>Reduced risk: environmental impact as a result of valve failure was<br />
eliminated.</li>
<li>Reduced downtime associated with inspecting the valves.</li>
<li>Reduced costs associated with prematurely replacing the valves.</li>
<li>Valve erosion resistance was quantified and visualised through the use of<br />
CFD, identifying erosion hotspots and overall bottleneck components.</li>
</ul>
</div></section><br />
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<section class="av_textblock_section "  itemscope="itemscope" itemtype="https://schema.org/BlogPosting" itemprop="blogPost" ><div class='avia_textblock  '   itemprop="text" ><h4>PROJECT ATTRIBUTES</h4>
<p>Computational Fluid Dynamics</p>
<ul>
<li>ANSYS SpaceClaim</li>
<li>ANSYS Fluent Meshing</li>
<li>ANSYS FLUENT</li>
<li>ANSYS CFD-Post</li>
<li>Discrete Phase Model (Multi-Phase)</li>
<li>DNV Erosion Model</li>
</ul>
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<blockquote>
<p>WE WERE APPROACHED DUE TO OUR SIGNIFICANT CFD EXPERIENCE,<br />
GATHERED OVER MULTIPLE PROJECTS, AND FOLLOWING A NUMBER OF<br />
SUCCESSFUL EROSION ASSESSMENTS.</p>
</blockquote>
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<p>The post <a href="https://pdl-group.com/valve-erosion-cfd-to-support-maintenance-scheduling/">VALVE EROSION CFD TO SUPPORT MAINTENANCE SCHEDULING</a> appeared first on <a href="https://pdl-group.com">PDL Group</a>.</p>
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