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Optimizing Load Capacity Predictions in Gas Foil Thrust Bearings: A Novel Full-Ramp Model
Gas film thickness significantly influences the performance prediction of Gas Foil Thrust Bearings (GFTB). However, the Classical Model (CM) for GFTBs exhibits inaccuracies in describing gas film thickness. In this paper, we explore the differences in the details of gas film thickness modeling and p...
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Published in: | Lubricants 2024-03, Vol.12 (3), p.76 |
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description | Gas film thickness significantly influences the performance prediction of Gas Foil Thrust Bearings (GFTB). However, the Classical Model (CM) for GFTBs exhibits inaccuracies in describing gas film thickness. In this paper, we explore the differences in the details of gas film thickness modeling and propose a Parallel Segmentation Model (PSM), which fixes the errors of the CM in describing the gas film thickness in the ramp section, and a Full-Ramp Model (FRM), to which a more realistic description of the gas film in the flat section is also added. Comparative analysis, utilizing a publicly available test dataset based on the open-source GFTB structure, establishes that the FRM surpasses the CM and PSM in accurately predicting load capacity. In-depth analysis shows that the location of the minimum gas film thickness for determining the load capacity is located at the innermost circle of the free end of the top foil, whereas the FRM is subjected to the same load with a larger film thickness at this location, which may be due to the unique geometry of the top foil of the FRM. Subsequently, employing the FRM, a parametric study explores load capacity in GFTB, considering variables such as ramp height, top foil thickness, bump foil stiffness, ramp section extent, and top foil area. The results demonstrate that GFTB load capacity exhibits a linear increase with the expansion of the top foil area. Moreover, the load capacity increases with augmented top foil thickness and bump foil stiffness, albeit at a decreasing rate. Additionally, an increase in ramp section extent initially enhances load capacity, reaching a maximum value before declining. Similarly, an increase in ramp height initially augments load capacity, attaining a maximum before subsequent diminution. |
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However, the Classical Model (CM) for GFTBs exhibits inaccuracies in describing gas film thickness. In this paper, we explore the differences in the details of gas film thickness modeling and propose a Parallel Segmentation Model (PSM), which fixes the errors of the CM in describing the gas film thickness in the ramp section, and a Full-Ramp Model (FRM), to which a more realistic description of the gas film in the flat section is also added. Comparative analysis, utilizing a publicly available test dataset based on the open-source GFTB structure, establishes that the FRM surpasses the CM and PSM in accurately predicting load capacity. In-depth analysis shows that the location of the minimum gas film thickness for determining the load capacity is located at the innermost circle of the free end of the top foil, whereas the FRM is subjected to the same load with a larger film thickness at this location, which may be due to the unique geometry of the top foil of the FRM. Subsequently, employing the FRM, a parametric study explores load capacity in GFTB, considering variables such as ramp height, top foil thickness, bump foil stiffness, ramp section extent, and top foil area. The results demonstrate that GFTB load capacity exhibits a linear increase with the expansion of the top foil area. Moreover, the load capacity increases with augmented top foil thickness and bump foil stiffness, albeit at a decreasing rate. Additionally, an increase in ramp section extent initially enhances load capacity, reaching a maximum value before declining. Similarly, an increase in ramp height initially augments load capacity, attaining a maximum before subsequent diminution.</description><identifier>ISSN: 2075-4442</identifier><identifier>EISSN: 2075-4442</identifier><identifier>DOI: 10.3390/lubricants12030076</identifier><language>eng</language><publisher>Basel: MDPI AG</publisher><subject>Engineering research ; Film thickness ; Foils ; full-ramp model ; gas film thickness ; gas foil thrust bearing ; Journal bearings ; load capacity ; Mathematical optimization ; parametric study ; Performance prediction ; Prediction theory ; Stiffness ; Thrust bearings</subject><ispartof>Lubricants, 2024-03, Vol.12 (3), p.76</ispartof><rights>COPYRIGHT 2024 MDPI AG</rights><rights>2024 by the authors. Licensee MDPI, Basel, Switzerland. This article is an open access article distributed under the terms and conditions of the Creative Commons Attribution (CC BY) license (https://creativecommons.org/licenses/by/4.0/). Notwithstanding the ProQuest Terms and Conditions, you may use this content in accordance with the terms of the License.</rights><lds50>peer_reviewed</lds50><oa>free_for_read</oa><woscitedreferencessubscribed>false</woscitedreferencessubscribed><citedby>FETCH-LOGICAL-c424t-53fa09c76e86467d71f43a005611b2e760317ab7db77f374b9cf2e7c386d20363</citedby><cites>FETCH-LOGICAL-c424t-53fa09c76e86467d71f43a005611b2e760317ab7db77f374b9cf2e7c386d20363</cites><orcidid>0009-0009-3953-8215</orcidid></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><linktopdf>$$Uhttps://www.proquest.com/docview/3003332166/fulltextPDF?pq-origsite=primo$$EPDF$$P50$$Gproquest$$Hfree_for_read</linktopdf><linktohtml>$$Uhttps://www.proquest.com/docview/3003332166?pq-origsite=primo$$EHTML$$P50$$Gproquest$$Hfree_for_read</linktohtml><link.rule.ids>314,776,780,25731,27901,27902,36989,44566,74869</link.rule.ids></links><search><creatorcontrib>Ying, Ming</creatorcontrib><creatorcontrib>Liu, Xinghua</creatorcontrib><creatorcontrib>Zhang, Yue</creatorcontrib><creatorcontrib>Zhang, Chongbin</creatorcontrib><title>Optimizing Load Capacity Predictions in Gas Foil Thrust Bearings: A Novel Full-Ramp Model</title><title>Lubricants</title><description>Gas film thickness significantly influences the performance prediction of Gas Foil Thrust Bearings (GFTB). However, the Classical Model (CM) for GFTBs exhibits inaccuracies in describing gas film thickness. In this paper, we explore the differences in the details of gas film thickness modeling and propose a Parallel Segmentation Model (PSM), which fixes the errors of the CM in describing the gas film thickness in the ramp section, and a Full-Ramp Model (FRM), to which a more realistic description of the gas film in the flat section is also added. Comparative analysis, utilizing a publicly available test dataset based on the open-source GFTB structure, establishes that the FRM surpasses the CM and PSM in accurately predicting load capacity. In-depth analysis shows that the location of the minimum gas film thickness for determining the load capacity is located at the innermost circle of the free end of the top foil, whereas the FRM is subjected to the same load with a larger film thickness at this location, which may be due to the unique geometry of the top foil of the FRM. Subsequently, employing the FRM, a parametric study explores load capacity in GFTB, considering variables such as ramp height, top foil thickness, bump foil stiffness, ramp section extent, and top foil area. The results demonstrate that GFTB load capacity exhibits a linear increase with the expansion of the top foil area. Moreover, the load capacity increases with augmented top foil thickness and bump foil stiffness, albeit at a decreasing rate. Additionally, an increase in ramp section extent initially enhances load capacity, reaching a maximum value before declining. Similarly, an increase in ramp height initially augments load capacity, attaining a maximum before subsequent diminution.</description><subject>Engineering research</subject><subject>Film thickness</subject><subject>Foils</subject><subject>full-ramp model</subject><subject>gas film thickness</subject><subject>gas foil thrust bearing</subject><subject>Journal bearings</subject><subject>load capacity</subject><subject>Mathematical optimization</subject><subject>parametric study</subject><subject>Performance prediction</subject><subject>Prediction theory</subject><subject>Stiffness</subject><subject>Thrust bearings</subject><issn>2075-4442</issn><issn>2075-4442</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2024</creationdate><recordtype>article</recordtype><sourceid>PIMPY</sourceid><sourceid>DOA</sourceid><recordid>eNplUU1r3DAQNaWBhjR_ICdBz04ljSzZvW2WbhrYJqGkh5zEWJK3WryWK8mF9NdX6ZZQyMxhhse8N19VdcHoJUBHP45LH73BKSfGKVCq5JvqlFPV1EII_va__F11ntKeFusYtEKdVo93c_YH_9tPO7INaMkaZzQ-P5H76Kw32YcpET-Ra0xkE_xIHn7EJWVy5TAWUvpEVuQ2_HIj2SzjWH_Dw0y-BuvG99XJgGNy5__iWfV98_lh_aXe3l3frFfb2gguct3AgLQzSrpWCqmsYoMApLSRjPXcKUmBKeyV7ZUaQIm-M0OBDbTSlm0lnFU3R10bcK_n6A8Yn3RAr_8CIe40xuzN6DTrKXWSUhCMC-wAGXSKtc6ibRk2WLQ-HLXmGH4uLmW9D0ucyvi63BUAOJPPHS-PVTsson4aQo5oilt38CZMbvAFX6m25aLroCkEfiSYGFKKbngZk1H9_EL9-oXwB_I5jlE</recordid><startdate>20240301</startdate><enddate>20240301</enddate><creator>Ying, Ming</creator><creator>Liu, Xinghua</creator><creator>Zhang, Yue</creator><creator>Zhang, Chongbin</creator><general>MDPI AG</general><scope>AAYXX</scope><scope>CITATION</scope><scope>7SR</scope><scope>7TB</scope><scope>8BQ</scope><scope>8FD</scope><scope>8FE</scope><scope>8FG</scope><scope>ABJCF</scope><scope>ABUWG</scope><scope>AFKRA</scope><scope>AZQEC</scope><scope>BENPR</scope><scope>BGLVJ</scope><scope>CCPQU</scope><scope>DWQXO</scope><scope>FR3</scope><scope>HCIFZ</scope><scope>JG9</scope><scope>L6V</scope><scope>M7S</scope><scope>PIMPY</scope><scope>PQEST</scope><scope>PQQKQ</scope><scope>PQUKI</scope><scope>PTHSS</scope><scope>DOA</scope><orcidid>https://orcid.org/0009-0009-3953-8215</orcidid></search><sort><creationdate>20240301</creationdate><title>Optimizing Load Capacity Predictions in Gas Foil Thrust Bearings: A Novel Full-Ramp Model</title><author>Ying, Ming ; Liu, Xinghua ; Zhang, Yue ; Zhang, Chongbin</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-c424t-53fa09c76e86467d71f43a005611b2e760317ab7db77f374b9cf2e7c386d20363</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>2024</creationdate><topic>Engineering research</topic><topic>Film thickness</topic><topic>Foils</topic><topic>full-ramp model</topic><topic>gas film thickness</topic><topic>gas foil thrust bearing</topic><topic>Journal bearings</topic><topic>load capacity</topic><topic>Mathematical optimization</topic><topic>parametric study</topic><topic>Performance prediction</topic><topic>Prediction theory</topic><topic>Stiffness</topic><topic>Thrust bearings</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Ying, Ming</creatorcontrib><creatorcontrib>Liu, Xinghua</creatorcontrib><creatorcontrib>Zhang, Yue</creatorcontrib><creatorcontrib>Zhang, Chongbin</creatorcontrib><collection>CrossRef</collection><collection>Engineered Materials Abstracts</collection><collection>Mechanical & Transportation Engineering Abstracts</collection><collection>METADEX</collection><collection>Technology Research Database</collection><collection>ProQuest SciTech Collection</collection><collection>ProQuest Technology Collection</collection><collection>Materials Science & Engineering Collection</collection><collection>ProQuest Central (Alumni)</collection><collection>ProQuest Central UK/Ireland</collection><collection>ProQuest Central Essentials</collection><collection>AUTh Library subscriptions: ProQuest Central</collection><collection>Technology Collection</collection><collection>ProQuest One Community College</collection><collection>ProQuest Central</collection><collection>Engineering Research Database</collection><collection>SciTech Premium Collection</collection><collection>Materials Research Database</collection><collection>ProQuest Engineering Collection</collection><collection>ProQuest Engineering Database</collection><collection>Publicly Available Content Database</collection><collection>ProQuest One Academic Eastern Edition (DO NOT USE)</collection><collection>ProQuest One Academic</collection><collection>ProQuest One Academic UKI Edition</collection><collection>Engineering collection</collection><collection>DOAJ Directory of Open Access Journals</collection><jtitle>Lubricants</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Ying, Ming</au><au>Liu, Xinghua</au><au>Zhang, Yue</au><au>Zhang, Chongbin</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>Optimizing Load Capacity Predictions in Gas Foil Thrust Bearings: A Novel Full-Ramp Model</atitle><jtitle>Lubricants</jtitle><date>2024-03-01</date><risdate>2024</risdate><volume>12</volume><issue>3</issue><spage>76</spage><pages>76-</pages><issn>2075-4442</issn><eissn>2075-4442</eissn><abstract>Gas film thickness significantly influences the performance prediction of Gas Foil Thrust Bearings (GFTB). However, the Classical Model (CM) for GFTBs exhibits inaccuracies in describing gas film thickness. In this paper, we explore the differences in the details of gas film thickness modeling and propose a Parallel Segmentation Model (PSM), which fixes the errors of the CM in describing the gas film thickness in the ramp section, and a Full-Ramp Model (FRM), to which a more realistic description of the gas film in the flat section is also added. Comparative analysis, utilizing a publicly available test dataset based on the open-source GFTB structure, establishes that the FRM surpasses the CM and PSM in accurately predicting load capacity. In-depth analysis shows that the location of the minimum gas film thickness for determining the load capacity is located at the innermost circle of the free end of the top foil, whereas the FRM is subjected to the same load with a larger film thickness at this location, which may be due to the unique geometry of the top foil of the FRM. Subsequently, employing the FRM, a parametric study explores load capacity in GFTB, considering variables such as ramp height, top foil thickness, bump foil stiffness, ramp section extent, and top foil area. The results demonstrate that GFTB load capacity exhibits a linear increase with the expansion of the top foil area. Moreover, the load capacity increases with augmented top foil thickness and bump foil stiffness, albeit at a decreasing rate. Additionally, an increase in ramp section extent initially enhances load capacity, reaching a maximum value before declining. Similarly, an increase in ramp height initially augments load capacity, attaining a maximum before subsequent diminution.</abstract><cop>Basel</cop><pub>MDPI AG</pub><doi>10.3390/lubricants12030076</doi><orcidid>https://orcid.org/0009-0009-3953-8215</orcidid><oa>free_for_read</oa></addata></record> |
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subjects | Engineering research Film thickness Foils full-ramp model gas film thickness gas foil thrust bearing Journal bearings load capacity Mathematical optimization parametric study Performance prediction Prediction theory Stiffness Thrust bearings |
title | Optimizing Load Capacity Predictions in Gas Foil Thrust Bearings: A Novel Full-Ramp Model |
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