废气涡轮增压器涡轮叶片失谐和高频振动
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- 英文论文题名：Mistuningand High Frequency Vibration of Turbine Wheel Blades
- 论文作者：圣小珍
- 英文论文作者：Sheng Xiaozhen China Chang'an Hunan Tyen Machinery Company Co Ltd.
- 年：2013
- 作者机构：中国长安湖南天雁机械有限责任公司;
- 论文关键词：叶片振动 ; 叶片失谐 ; 叶片高周疲劳
- 英文论文关键词：Blade vibration ; Mistuning ; Bladed wheel HCF
- 会议召开时间：2013-11-26
- 会议录名称：2013中国汽车工程学会年会论文集
- 英文会议录名称：Proceedings of 2013 SAE-China Congress
- 语种：中文
- 分类号：U464.135.2
- 学会代码：QCGC
- 会议名称：2013中国汽车工程学会年会
- 会议地点：中国北京
- 主办单位：中国汽车工程学会
- 学会名称：中国汽车工程学会
- 页数：6
- 文件大小：442k
- 原文格式：O
- 会议级别：全国
摘要
由于涡轮增压能大大提高发动机的动力性、经济性和洁净性,现已成为内燃机节能减排的关键技术之一,正在被大力推广应用。另一方面,增压器的高速、高温和高振动的工作状态和环境,不但使增压器成为发动机和车辆噪声的重要来源,而且严重威胁其可靠性。如何在提高增压器性能的同时又使其噪声小和可靠性高,是一个很复杂的课题。本文对增压器涡轮叶片失谐、高频振动和疲劳问题的研究现状进行介绍。
Turbochargers are being widely applied on IC engines due to their ability to increase engine power,reduce fuel consumption and improve emission.However,the very high speed,gas temperature and vibration,not only make the turbocharger one of the main noise sources,but also impose serious threats to its reliability.How to design and produce turbochargers of high performance, low noise and long life is a complicated topic.This article gives a review on research into turbine wheel blade mistuning,high frequency vibration and high cycle fatigue.
Turbochargers are being widely applied on IC engines due to their ability to increase engine power,reduce fuel consumption and improve emission.However,the very high speed,gas temperature and vibration,not only make the turbocharger one of the main noise sources,but also impose serious threats to its reliability.How to design and produce turbochargers of high performance, low noise and long life is a complicated topic.This article gives a review on research into turbine wheel blade mistuning,high frequency vibration and high cycle fatigue.
引文
[1]关于加强内燃机工业节能减排的意见.国办发[2013]12号.
[2]Tian L,Wang W J,Peng Z J.Dynamic behaviours of a full floating ring bearing supported turbocharger rotor with engine excitation[J].Journal of Sound and Vibration, 2011,330:4851 -4875.
[3]王增全.车用涡轮增压器结构可靠性[M].第1版.北京:科学出版社,2013.
[4]Thomas D L,Dynamics of rotationally periodic structures [J].International Journal of Numerical Methods in Engineering,1979,14:81-102.
[5]Ince A,Glinka G.A modification of Morrow and Smith - Watson - Topper mean stress correction models[J]. Fatigue & Fracture of Engineering Materials & Structures, 2011,34:854-867.
[6]Ewins D J.The effect of detuning upon the forced vibration of bladed disks[J].Journal of Sound and Vibration, 1969,9:65 -79.
[7]Bladh R.Castanier M P,Pierre C.Component -mode-based reduced order modelling techniques for mistuned bladed disks—Part I:theoretical models[J].ASME Journal of Engineering for Gas Turbine and Power,2001, 123:89-99.
[8]Bladh R,Castanier M P,Pierre C.Component - mode- based reduced order modelling techniques for mistuned bladed disks—Part II:Application[J].ASME Journal of Engineering for Gas Turbine and Power,2001,123: 100 -108.
[9]Bladh R,Pierre C,Castanier MP,et al.Dynamic response predictions for a mistuned industrial turbomachinery rotor using reduced - order modelling[J]. ??ASME Journal of Engineering for Gas Turbine and Power,2002,124:311-324.
[10]Feiner D M,Griffin J H.A fundamental model of mistuning for a single family of modes[J].ASME Journal of Turbomachinery,2002,124:597-605.
[11]Feiner D M,Griffin J H.Mistuning identification of bladed disks using a fundamental mistuning model—Part I:Theory[J].ASME Journal of Turbomachinery, 2004,126:150-158.
[12]Feiner D M,Griffin J H.Mistuning identification of bladed disks using a fundamental mistuning model—Part II:Application[J]? ASME Journal of Turbomachinery,2004,126:159-165.
[13]Bendiksen O O.Localisation phenomena in structural dynamics[J].Chaos,Solitons and Fractals,2000, 11:1621-1660.
[14]Ottarsson G,Pierre C.A transfer matrix approach to free vibration localisation in mistuned bladed assemblies [J].Journal of Sound and Vibration,1996,197: 589-618.
[15]Castanier M P,Pierre C.Using Intentional Mistuning in the Design of Turbomachinery Rotors[J].AIAA Journal,2002,40:2077-2086.
[16]Shahruz M S.Elimination of vibration localisation in mistuned periodic structures[J].Journal of Sound and Vibration,2005,281:452-462.
[17]王红建,贺尔铭,赵志彬.频率转向特征对失谐叶盘模态局部化的作用[J].中国机械工程, 2009,20:82-85.
[18]王红建,贺尔铭.叶片失谐对叶盘结构振动特性的影响[J].西北工业大学学报,2009,27: 645-650.
[19]王红建,贺尔铭,赵志斌.叶片随机失谐与叶盘结构共振特性分析[J].西北工业大学学报, 2011,29:189-193.
[20]赵志斌,贺尔铭,王红建.叶盘振动失谐敏感性与频率转向特性内在关系研究[J].机械科学和技术,2010,29:1606-1611.
[21]王帅,王建军,李其汉.一种基于响应信息的整体叶盘结构失谐识别方法[J].航空学报, 2009,30:1863-1870.
[22]王帅,王建军,李其汉.一种基于模态减缩技术的整体叶盘结构失谐识别方法[J].航空动力学报,2009,24:662-669.
[23]王建军,姚建尧,李其汉.刚度随机失谐叶盘结构概率模态特性分析[J].航空动力学报, 2008,23:257-262.
[24]廖海涛,王建军,李其汉.随机失谐叶盘结构失谐特性分析[J].航空动力学报,2010,25:161-168.
[25]Sheng X Z,Clay D C,Allport J.Dynamics of mistuned radial turbine wheels[M].Proceedings of the 8th ??International Conference on Turbochargers and Turbocharging,17-18 May 2006,London,England.
[26]Sheng X Z.Model identification and order response prediction for bladed wheels[J].Journal of Sound and Vibration,2009,323:194-213.
[27]Sheng X Z.A new experimental modal analysis method based on double-exponential windowing and application to lightly damped bladed wheels[J]. Journal of Sound and Vibration,2012,331: 2824-2835.
[28]Sheng X Z.Determination of modal parameters from off-diagonal FRFs using the double-exponential windowing method[J].Accepted by Journal of Sound and Vibration,2013.
[29]Allpot J M,Jupp ML,et al.Turbocharger blade vibration:Measurement and validation through laser tip-timing[M].Proceedings of the 10~(th) International Conference on Turbochargers and Turbocharging,15- 16 May 2012,London,England.
[2]Tian L,Wang W J,Peng Z J.Dynamic behaviours of a full floating ring bearing supported turbocharger rotor with engine excitation[J].Journal of Sound and Vibration, 2011,330:4851 -4875.
[3]王增全.车用涡轮增压器结构可靠性[M].第1版.北京:科学出版社,2013.
[4]Thomas D L,Dynamics of rotationally periodic structures [J].International Journal of Numerical Methods in Engineering,1979,14:81-102.
[5]Ince A,Glinka G.A modification of Morrow and Smith - Watson - Topper mean stress correction models[J]. Fatigue & Fracture of Engineering Materials & Structures, 2011,34:854-867.
[6]Ewins D J.The effect of detuning upon the forced vibration of bladed disks[J].Journal of Sound and Vibration, 1969,9:65 -79.
[7]Bladh R.Castanier M P,Pierre C.Component -mode-based reduced order modelling techniques for mistuned bladed disks—Part I:theoretical models[J].ASME Journal of Engineering for Gas Turbine and Power,2001, 123:89-99.
[8]Bladh R,Castanier M P,Pierre C.Component - mode- based reduced order modelling techniques for mistuned bladed disks—Part II:Application[J].ASME Journal of Engineering for Gas Turbine and Power,2001,123: 100 -108.
[9]Bladh R,Pierre C,Castanier MP,et al.Dynamic response predictions for a mistuned industrial turbomachinery rotor using reduced - order modelling[J]. ??ASME Journal of Engineering for Gas Turbine and Power,2002,124:311-324.
[10]Feiner D M,Griffin J H.A fundamental model of mistuning for a single family of modes[J].ASME Journal of Turbomachinery,2002,124:597-605.
[11]Feiner D M,Griffin J H.Mistuning identification of bladed disks using a fundamental mistuning model—Part I:Theory[J].ASME Journal of Turbomachinery, 2004,126:150-158.
[12]Feiner D M,Griffin J H.Mistuning identification of bladed disks using a fundamental mistuning model—Part II:Application[J]? ASME Journal of Turbomachinery,2004,126:159-165.
[13]Bendiksen O O.Localisation phenomena in structural dynamics[J].Chaos,Solitons and Fractals,2000, 11:1621-1660.
[14]Ottarsson G,Pierre C.A transfer matrix approach to free vibration localisation in mistuned bladed assemblies [J].Journal of Sound and Vibration,1996,197: 589-618.
[15]Castanier M P,Pierre C.Using Intentional Mistuning in the Design of Turbomachinery Rotors[J].AIAA Journal,2002,40:2077-2086.
[16]Shahruz M S.Elimination of vibration localisation in mistuned periodic structures[J].Journal of Sound and Vibration,2005,281:452-462.
[17]王红建,贺尔铭,赵志彬.频率转向特征对失谐叶盘模态局部化的作用[J].中国机械工程, 2009,20:82-85.
[18]王红建,贺尔铭.叶片失谐对叶盘结构振动特性的影响[J].西北工业大学学报,2009,27: 645-650.
[19]王红建,贺尔铭,赵志斌.叶片随机失谐与叶盘结构共振特性分析[J].西北工业大学学报, 2011,29:189-193.
[20]赵志斌,贺尔铭,王红建.叶盘振动失谐敏感性与频率转向特性内在关系研究[J].机械科学和技术,2010,29:1606-1611.
[21]王帅,王建军,李其汉.一种基于响应信息的整体叶盘结构失谐识别方法[J].航空学报, 2009,30:1863-1870.
[22]王帅,王建军,李其汉.一种基于模态减缩技术的整体叶盘结构失谐识别方法[J].航空动力学报,2009,24:662-669.
[23]王建军,姚建尧,李其汉.刚度随机失谐叶盘结构概率模态特性分析[J].航空动力学报, 2008,23:257-262.
[24]廖海涛,王建军,李其汉.随机失谐叶盘结构失谐特性分析[J].航空动力学报,2010,25:161-168.
[25]Sheng X Z,Clay D C,Allport J.Dynamics of mistuned radial turbine wheels[M].Proceedings of the 8th ??International Conference on Turbochargers and Turbocharging,17-18 May 2006,London,England.
[26]Sheng X Z.Model identification and order response prediction for bladed wheels[J].Journal of Sound and Vibration,2009,323:194-213.
[27]Sheng X Z.A new experimental modal analysis method based on double-exponential windowing and application to lightly damped bladed wheels[J]. Journal of Sound and Vibration,2012,331: 2824-2835.
[28]Sheng X Z.Determination of modal parameters from off-diagonal FRFs using the double-exponential windowing method[J].Accepted by Journal of Sound and Vibration,2013.
[29]Allpot J M,Jupp ML,et al.Turbocharger blade vibration:Measurement and validation through laser tip-timing[M].Proceedings of the 10~(th) International Conference on Turbochargers and Turbocharging,15- 16 May 2012,London,England.