A 5-DOF Model for Aeroengine Spindle Dual-rotor System Analysis
This paper develops a five degrees of freedom(5-DOF) model for aeroengine spindle dual-rotor system dynamic analysis.In this system,the dual rotors are supported on two angular contact ball bearings and two deep groove ball bearings,one of the latter-mentioned bearings works as the inter-shaft beari...
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Veröffentlicht in: | Chinese journal of aeronautics 2011-04, Vol.24 (2), p.224-234 |
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description | This paper develops a five degrees of freedom(5-DOF) model for aeroengine spindle dual-rotor system dynamic analysis.In this system,the dual rotors are supported on two angular contact ball bearings and two deep groove ball bearings,one of the latter-mentioned bearings works as the inter-shaft bearing.Driven by respective motors,the dual rotors have different co-rotating speeds.The proposed model mathematically formulates the nonlinear displacements,elastic deflections and contact forces of bearings with consideration of 5-DOF and coupling of dual rotors.The nonlinear equations of motions of dual rotors with 5-DOF are solved using Runge-Kutta-Fehlberg algorithm.In order to investigate the effect of the introduced 5-DOF and nonlinear dy-namic bearing model,we compare the proposed model with two models:the 3-DOF model of this system only considering three translational degrees of freedom(Gupta,1993,rotational freedom is neglected);the 5-DOF model where the deep groove ball bearings are simplified as linear elastic spring(Guskov,2007).The simulation results verify Gupta's prediction(1993) and show that the rotational freedom of rotors and nonlinear dynamic model of bearings have great effect on the system dynamic simula-tion.The quantitative results are given as well. |
doi_str_mv | 10.1016/S1000-9361(11)60027-7 |
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DENG, Sier ; TENG, Hongfei</creator><creatorcontrib>HU, Qinghua ; DENG, Sier ; TENG, Hongfei</creatorcontrib><description>This paper develops a five degrees of freedom(5-DOF) model for aeroengine spindle dual-rotor system dynamic analysis.In this system,the dual rotors are supported on two angular contact ball bearings and two deep groove ball bearings,one of the latter-mentioned bearings works as the inter-shaft bearing.Driven by respective motors,the dual rotors have different co-rotating speeds.The proposed model mathematically formulates the nonlinear displacements,elastic deflections and contact forces of bearings with consideration of 5-DOF and coupling of dual rotors.The nonlinear equations of motions of dual rotors with 5-DOF are solved using Runge-Kutta-Fehlberg algorithm.In order to investigate the effect of the introduced 5-DOF and nonlinear dy-namic bearing model,we compare the proposed model with two models:the 3-DOF model of this system only considering three translational degrees of freedom(Gupta,1993,rotational freedom is neglected);the 5-DOF model where the deep groove ball bearings are simplified as linear elastic spring(Guskov,2007).The simulation results verify Gupta's prediction(1993) and show that the rotational freedom of rotors and nonlinear dynamic model of bearings have great effect on the system dynamic simula-tion.The quantitative results are given as well.</description><identifier>ISSN: 1000-9361</identifier><identifier>DOI: 10.1016/S1000-9361(11)60027-7</identifier><language>eng</language><publisher>Elsevier Ltd</publisher><subject>aeroengine ; ball bearing ; Ball bearings ; Bearings ; Computer simulation ; dual-rotor ; Dynamical systems ; five degrees of freedom ; Grooves ; Mathematical models ; Nonlinear dynamics ; Rotors ; 主轴 ; 动态分析模型 ; 双转子系统 ; 深沟球轴承 ; 自由度模型 ; 航空发动机 ; 非线性位移 ; 非线性动态模型</subject><ispartof>Chinese journal of aeronautics, 2011-04, Vol.24 (2), p.224-234</ispartof><rights>2011 Chinese Journal of Aeronautics</rights><lds50>peer_reviewed</lds50><oa>free_for_read</oa><woscitedreferencessubscribed>false</woscitedreferencessubscribed><citedby>FETCH-LOGICAL-c414t-2c0449706a913c02e15df93751a3d3ccbd1b905c317d348d169ed8f5df9863123</citedby><cites>FETCH-LOGICAL-c414t-2c0449706a913c02e15df93751a3d3ccbd1b905c317d348d169ed8f5df9863123</cites></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Uhttp://image.cqvip.com/vip1000/qk/83889X/83889X.jpg</thumbnail><linktohtml>$$Uhttps://dx.doi.org/10.1016/S1000-9361(11)60027-7$$EHTML$$P50$$Gelsevier$$Hfree_for_read</linktohtml><link.rule.ids>315,781,785,3551,27929,27930,46000</link.rule.ids></links><search><creatorcontrib>HU, Qinghua</creatorcontrib><creatorcontrib>DENG, Sier</creatorcontrib><creatorcontrib>TENG, Hongfei</creatorcontrib><title>A 5-DOF Model for Aeroengine Spindle Dual-rotor System Analysis</title><title>Chinese journal of aeronautics</title><addtitle>Chinese Journal of Aeronautics</addtitle><description>This paper develops a five degrees of freedom(5-DOF) model for aeroengine spindle dual-rotor system dynamic analysis.In this system,the dual rotors are supported on two angular contact ball bearings and two deep groove ball bearings,one of the latter-mentioned bearings works as the inter-shaft bearing.Driven by respective motors,the dual rotors have different co-rotating speeds.The proposed model mathematically formulates the nonlinear displacements,elastic deflections and contact forces of bearings with consideration of 5-DOF and coupling of dual rotors.The nonlinear equations of motions of dual rotors with 5-DOF are solved using Runge-Kutta-Fehlberg algorithm.In order to investigate the effect of the introduced 5-DOF and nonlinear dy-namic bearing model,we compare the proposed model with two models:the 3-DOF model of this system only considering three translational degrees of freedom(Gupta,1993,rotational freedom is neglected);the 5-DOF model where the deep groove ball bearings are simplified as linear elastic spring(Guskov,2007).The simulation results verify Gupta's prediction(1993) and show that the rotational freedom of rotors and nonlinear dynamic model of bearings have great effect on the system dynamic simula-tion.The quantitative results are given as well.</description><subject>aeroengine</subject><subject>ball bearing</subject><subject>Ball bearings</subject><subject>Bearings</subject><subject>Computer simulation</subject><subject>dual-rotor</subject><subject>Dynamical systems</subject><subject>five degrees of freedom</subject><subject>Grooves</subject><subject>Mathematical models</subject><subject>Nonlinear dynamics</subject><subject>Rotors</subject><subject>主轴</subject><subject>动态分析模型</subject><subject>双转子系统</subject><subject>深沟球轴承</subject><subject>自由度模型</subject><subject>航空发动机</subject><subject>非线性位移</subject><subject>非线性动态模型</subject><issn>1000-9361</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2011</creationdate><recordtype>article</recordtype><recordid>eNqFkM1OwzAQhHMAifLzCEjhBBwC3jix41MVtRSQinoonK3U3hSj1G7tFKlvT9JWvXJaaXdmVvNF0S2QJyDAnudACEkEZfAA8MgISXnCz6LBaX0RXYbwQwgVHMggGpZxnoxnk_jDaWzi2vm4RO_QLo3FeL42VjcYj7dVk3jXdtf5LrS4iktbNbtgwnV0XldNwJvjvIq-Ji-fo7dkOnt9H5XTRGWQtUmqSJYJTlglgCqSIuS6FpTnUFFNlVpoWAiSKwpc06zQwATqou5FBaOQ0qvo_pC79m6zxdDKlQkKm6ay6LZBFgVhTDDRK_ODUnkXgsdarr1ZVX4ngciekdwzkj0MCSD3jCTvfMODD7savwa9DMqgVaiNR9VK7cy_CXfHz9_OLjfGLk-vKee865_RP11MeM0</recordid><startdate>20110401</startdate><enddate>20110401</enddate><creator>HU, Qinghua</creator><creator>DENG, Sier</creator><creator>TENG, Hongfei</creator><general>Elsevier Ltd</general><scope>2RA</scope><scope>92L</scope><scope>CQIGP</scope><scope>W92</scope><scope>~WA</scope><scope>6I.</scope><scope>AAFTH</scope><scope>AAYXX</scope><scope>CITATION</scope><scope>7TB</scope><scope>8FD</scope><scope>FR3</scope><scope>H8D</scope><scope>L7M</scope></search><sort><creationdate>20110401</creationdate><title>A 5-DOF Model for Aeroengine Spindle Dual-rotor System Analysis</title><author>HU, Qinghua ; DENG, Sier ; TENG, Hongfei</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-c414t-2c0449706a913c02e15df93751a3d3ccbd1b905c317d348d169ed8f5df9863123</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>2011</creationdate><topic>aeroengine</topic><topic>ball bearing</topic><topic>Ball bearings</topic><topic>Bearings</topic><topic>Computer simulation</topic><topic>dual-rotor</topic><topic>Dynamical systems</topic><topic>five degrees of freedom</topic><topic>Grooves</topic><topic>Mathematical models</topic><topic>Nonlinear dynamics</topic><topic>Rotors</topic><topic>主轴</topic><topic>动态分析模型</topic><topic>双转子系统</topic><topic>深沟球轴承</topic><topic>自由度模型</topic><topic>航空发动机</topic><topic>非线性位移</topic><topic>非线性动态模型</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>HU, Qinghua</creatorcontrib><creatorcontrib>DENG, Sier</creatorcontrib><creatorcontrib>TENG, Hongfei</creatorcontrib><collection>中文科技期刊数据库</collection><collection>中文科技期刊数据库-CALIS站点</collection><collection>中文科技期刊数据库-7.0平台</collection><collection>中文科技期刊数据库-工程技术</collection><collection>中文科技期刊数据库- 镜像站点</collection><collection>ScienceDirect Open Access Titles</collection><collection>Elsevier:ScienceDirect:Open Access</collection><collection>CrossRef</collection><collection>Mechanical & Transportation Engineering Abstracts</collection><collection>Technology Research Database</collection><collection>Engineering Research Database</collection><collection>Aerospace Database</collection><collection>Advanced Technologies Database with Aerospace</collection><jtitle>Chinese journal of aeronautics</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>HU, Qinghua</au><au>DENG, Sier</au><au>TENG, Hongfei</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>A 5-DOF Model for Aeroengine Spindle Dual-rotor System Analysis</atitle><jtitle>Chinese journal of aeronautics</jtitle><addtitle>Chinese Journal of Aeronautics</addtitle><date>2011-04-01</date><risdate>2011</risdate><volume>24</volume><issue>2</issue><spage>224</spage><epage>234</epage><pages>224-234</pages><issn>1000-9361</issn><abstract>This paper develops a five degrees of freedom(5-DOF) model for aeroengine spindle dual-rotor system dynamic analysis.In this system,the dual rotors are supported on two angular contact ball bearings and two deep groove ball bearings,one of the latter-mentioned bearings works as the inter-shaft bearing.Driven by respective motors,the dual rotors have different co-rotating speeds.The proposed model mathematically formulates the nonlinear displacements,elastic deflections and contact forces of bearings with consideration of 5-DOF and coupling of dual rotors.The nonlinear equations of motions of dual rotors with 5-DOF are solved using Runge-Kutta-Fehlberg algorithm.In order to investigate the effect of the introduced 5-DOF and nonlinear dy-namic bearing model,we compare the proposed model with two models:the 3-DOF model of this system only considering three translational degrees of freedom(Gupta,1993,rotational freedom is neglected);the 5-DOF model where the deep groove ball bearings are simplified as linear elastic spring(Guskov,2007).The simulation results verify Gupta's prediction(1993) and show that the rotational freedom of rotors and nonlinear dynamic model of bearings have great effect on the system dynamic simula-tion.The quantitative results are given as well.</abstract><pub>Elsevier Ltd</pub><doi>10.1016/S1000-9361(11)60027-7</doi><tpages>11</tpages><oa>free_for_read</oa></addata></record> |
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subjects | aeroengine ball bearing Ball bearings Bearings Computer simulation dual-rotor Dynamical systems five degrees of freedom Grooves Mathematical models Nonlinear dynamics Rotors 主轴 动态分析模型 双转子系统 深沟球轴承 自由度模型 航空发动机 非线性位移 非线性动态模型 |
title | A 5-DOF Model for Aeroengine Spindle Dual-rotor System Analysis |
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