随机振动环境下航天器结构强度设计方法综述
|
摘要
随机振动环境是航天器结构强度设计重点考虑的因素之一.目前,在随机振动环境条件下,航天器结构强度设计采取的方法主要为等效的准静态设计方法,其等效原则可分为加速度响应等效、位移响应等效以及应力响应等效.本文重点介绍了3种等效原则的基本原理、处理方法、国内外发展现状及工程应用情况,并在综合分析的基础上推荐使用基于位移和应力峰值响应等效的设计方法.最后针对需进一步开展的研究工作提出了建议.
Random vibration is an important part of spacecraft structure design. Now, the main method used in the structural strength design of spacecrafts is equivalent static design method. Its equivalent princi-ples include equivalent acceleration response, equivalent displacement response and equivalent stress response. Respective theories, methods, domestic and overseas research status, advantages and disadvantages and engineering applications are presented. The design method based on the peak values of displacement and stress response is recommended. And the problems in need of further research are finally suggested.
Random vibration is an important part of spacecraft structure design. Now, the main method used in the structural strength design of spacecrafts is equivalent static design method. Its equivalent princi-ples include equivalent acceleration response, equivalent displacement response and equivalent stress response. Respective theories, methods, domestic and overseas research status, advantages and disadvantages and engineering applications are presented. The design method based on the peak values of displacement and stress response is recommended. And the problems in need of further research are finally suggested.
引文
1朱凤梧,张小达,金枸叔.GJB1027A-2005运载器、上面级和航天器试验要求.国防科学技术工业委员会.2006.23-30
2刘旭华.结构动力可靠性研究:[博士论文].哈尔滨:工程大学固体力学院,2006.1-10
3Anderson A,Bair J,Bell D.MIL-STD-810F-2000Test method standard for environmental engineering consid-erations and laboratory tests.The US Department of Defense.2000.320-324
4杨宝宁.随机振动条件下设计载荷的确定.航天器工程,2006,5:89-96
5Chung Y T,Krebs D J,Peebles J H.Estimation of pay-load random vibration loads for proper structure design.AIAA,2001-1667.1-19
6Miles J W.On structural fatigue under random loading.J.Acoust.Soc.Am.,1957,29:176-176
7Frerbee R C,Jones J H.Comparison of miles relation-ship to the true mean square value of response for a single degree of freedom system.NASA,19910073736.1-18
8Suryanarayan S,Murali M R K.Improved estimation of random vibration loads in launch vehicles.AIAA,1993-1092.1-29
9李兴超.航天器结构随机振动响应等效为准静态载荷的方法研究:[硕士论文].哈尔滨:哈尔滨工程大学固体力学院,2008.1-20
10Jaap W.Random vibrations in spacecraft structures de-sign.USA:Springer,2009.162-163
11伍定一.有效质量法确定合理振型数的探讨.山西建筑,2007,6:34-40
12陈奎孚.半功率点法估计阻尼比的误差分析.机械强度,2002,8:45-50
13Leung K,Foist B L.Prediction of acoustically induced random vibration loads for shuttle payloads.AIAA,1995-1200.1-22
14Chung Y T,Foist B L.Prediction of payload random vi-bration loads.In:13th International Modal Analysis Con-ference,2004.56-78
15邹元杰.基础激励和声激励下的设计载荷估算方法.结构动力学会议,哈尔滨,2009
16Lee H M.Testing for random limit load versus static limit load.NASA,19970028919.1-41
17Wada B K.Historical overview of structural modeling,de-sign loads and testing of spacecraft.AIAA,2000-25766.1-25
18Kang B S,Choi W S,Park G J.Structural optimization under equivalent static loads transformed from dynamic loads based on displacement.AIAA,1999-1259.12-59
19Choi W S,Park G J.Structural optimization using equiv-alent static loads transformed from dynamic loads at all time intervals.Computer Methods in Applied Mechanics and Engineering,2002,191:191-213
20朱学旺,刘青林.多点不相关随机振动载荷的动力学等效模拟.电子产品可靠性与环境试验,2007,5:25-41
21Kang B S,Shyy Y K.Design of flexible bodies in multi-body dynamics systems using equivalent static load method.AIAA,2008-1708.67-86
22Park G J.Nonlinear dynamics response structural opti-mization of a joined-wing using equivalent static loads.AD,2008A487090.1-32
23Nicholas S G.Structural optimization of joined-wing beam model with bendtwist coupling using ESL.AD,200A502107.1-43
24赵礼辉.ESL法在汽车结构优化设计中的应用:[硕士论文],上海:交通大学车辆工程院,2009.1-10
25Lee J J,Jung U J.A preliminary study on the optimal per-form design in the forging process using equivalent static loads.AIAA,2010-9046.1-43
26肖燕武.地震反应谱的局限性及最新发展.水利与建筑工程学报,2010,12:45-54
27Kiureghian A D.A response spectrum method for random vibration analysis of MDF systems.Earthquake Engineer-ing and Structural Dynamics,1981,9:187-194
28刘庆林.传统反应谱CQC法研究与进展:[博士论文].杭州:浙江大学建筑工程学院,2007.11-25
29徐欣国.桥梁抗震性能分析与评价方法初步研究,重庆:重庆交通学院结构工程,2005.1-126
30杨志勇.弹性与弹塑性动力时程分析方法中若干问题探讨:[硕士论文].北京:中国建筑科学研究院结构所,2009.15-30
31林家浩.线性随机结构的平稳随机响应.计算力学学报,2001,18(4):65-73
32戴新进.复合材料结构随机振动的虚拟激励法及在航空航天领域的应用:[博士论文].大连:大连理工大学工程力学,2007
33Hampton R W.MSC NASTRAN stress analysis of com-plete models subjected to random and quasi-static loads.NASA,2000209585.1-19
34Bendat J S,Piersol A G.Random Data:Analysis and Measurement Procedures.New Jersey:Wiley-NY,2000.318-326
35Wirshing P H,Paez T L,Ortiz H.Random Vibrations:Theory and Applications.New Jersey:Wiley-NY,1995.219-231
36Hunt F V.Stress and strain limits on the attainable ve-locity in mechanical vibration.J.Acoust.Soc.Amer.,1960,9(32):1123-1128
37Ungar E E.Maximum stresses in beams and plates vi-brating at resonance.Trans.ASME,J.Engrg Ind.,1962,1(82B):149-155
38Crandall S H.Relation between strain and velocity in res-onant vibration.J.Acoust.Soc.Amer.,1962,12(34):1960-1961
39Harry H,Kern D L,Piersol A G.HDBK-7005dynamic environmental criteria.NASA,2001.1-302
40Segalman D J.An efficient method for calculating RMS von Mises stress in a random vibration environment.SANDIA,1998,4:98-103
41Segalman D.Estimating the probability distribution of von Mises stress for structures undergoing random excita-tion.Journal of Vibration and Acoustics,2000,1(122):84-91
42Reese G M.A tutorial on design analysis for random vi-bration.DE,2000-28753406.1-32
43Quaranta G,Mantegazza P.Randomly excited structures reliability by means of the von Mises stress response.DOD,1994:1-34
44Elishakoff I.Stochasticity and safety factors:part1.ran-dom actual stress and deterministic yield stress.Chaos Solitons&Fractals2005,4:344-356
45de Fuente E.von Mises stresses in random vibration of lin-ear structures.Computers and Structures,2009,7:1253-1262
46廖海涛.噪声载荷作用下航空薄壁壳体的随机振动响应:[硕士论文].沈阳:沈阳航空工业学院,2007.21-30
47李德葆.应变模态分析和曲率模态分析.见:第15届全国振动与噪声控制高技术及应用会议,北京,2001
2刘旭华.结构动力可靠性研究:[博士论文].哈尔滨:工程大学固体力学院,2006.1-10
3Anderson A,Bair J,Bell D.MIL-STD-810F-2000Test method standard for environmental engineering consid-erations and laboratory tests.The US Department of Defense.2000.320-324
4杨宝宁.随机振动条件下设计载荷的确定.航天器工程,2006,5:89-96
5Chung Y T,Krebs D J,Peebles J H.Estimation of pay-load random vibration loads for proper structure design.AIAA,2001-1667.1-19
6Miles J W.On structural fatigue under random loading.J.Acoust.Soc.Am.,1957,29:176-176
7Frerbee R C,Jones J H.Comparison of miles relation-ship to the true mean square value of response for a single degree of freedom system.NASA,19910073736.1-18
8Suryanarayan S,Murali M R K.Improved estimation of random vibration loads in launch vehicles.AIAA,1993-1092.1-29
9李兴超.航天器结构随机振动响应等效为准静态载荷的方法研究:[硕士论文].哈尔滨:哈尔滨工程大学固体力学院,2008.1-20
10Jaap W.Random vibrations in spacecraft structures de-sign.USA:Springer,2009.162-163
11伍定一.有效质量法确定合理振型数的探讨.山西建筑,2007,6:34-40
12陈奎孚.半功率点法估计阻尼比的误差分析.机械强度,2002,8:45-50
13Leung K,Foist B L.Prediction of acoustically induced random vibration loads for shuttle payloads.AIAA,1995-1200.1-22
14Chung Y T,Foist B L.Prediction of payload random vi-bration loads.In:13th International Modal Analysis Con-ference,2004.56-78
15邹元杰.基础激励和声激励下的设计载荷估算方法.结构动力学会议,哈尔滨,2009
16Lee H M.Testing for random limit load versus static limit load.NASA,19970028919.1-41
17Wada B K.Historical overview of structural modeling,de-sign loads and testing of spacecraft.AIAA,2000-25766.1-25
18Kang B S,Choi W S,Park G J.Structural optimization under equivalent static loads transformed from dynamic loads based on displacement.AIAA,1999-1259.12-59
19Choi W S,Park G J.Structural optimization using equiv-alent static loads transformed from dynamic loads at all time intervals.Computer Methods in Applied Mechanics and Engineering,2002,191:191-213
20朱学旺,刘青林.多点不相关随机振动载荷的动力学等效模拟.电子产品可靠性与环境试验,2007,5:25-41
21Kang B S,Shyy Y K.Design of flexible bodies in multi-body dynamics systems using equivalent static load method.AIAA,2008-1708.67-86
22Park G J.Nonlinear dynamics response structural opti-mization of a joined-wing using equivalent static loads.AD,2008A487090.1-32
23Nicholas S G.Structural optimization of joined-wing beam model with bendtwist coupling using ESL.AD,200A502107.1-43
24赵礼辉.ESL法在汽车结构优化设计中的应用:[硕士论文],上海:交通大学车辆工程院,2009.1-10
25Lee J J,Jung U J.A preliminary study on the optimal per-form design in the forging process using equivalent static loads.AIAA,2010-9046.1-43
26肖燕武.地震反应谱的局限性及最新发展.水利与建筑工程学报,2010,12:45-54
27Kiureghian A D.A response spectrum method for random vibration analysis of MDF systems.Earthquake Engineer-ing and Structural Dynamics,1981,9:187-194
28刘庆林.传统反应谱CQC法研究与进展:[博士论文].杭州:浙江大学建筑工程学院,2007.11-25
29徐欣国.桥梁抗震性能分析与评价方法初步研究,重庆:重庆交通学院结构工程,2005.1-126
30杨志勇.弹性与弹塑性动力时程分析方法中若干问题探讨:[硕士论文].北京:中国建筑科学研究院结构所,2009.15-30
31林家浩.线性随机结构的平稳随机响应.计算力学学报,2001,18(4):65-73
32戴新进.复合材料结构随机振动的虚拟激励法及在航空航天领域的应用:[博士论文].大连:大连理工大学工程力学,2007
33Hampton R W.MSC NASTRAN stress analysis of com-plete models subjected to random and quasi-static loads.NASA,2000209585.1-19
34Bendat J S,Piersol A G.Random Data:Analysis and Measurement Procedures.New Jersey:Wiley-NY,2000.318-326
35Wirshing P H,Paez T L,Ortiz H.Random Vibrations:Theory and Applications.New Jersey:Wiley-NY,1995.219-231
36Hunt F V.Stress and strain limits on the attainable ve-locity in mechanical vibration.J.Acoust.Soc.Amer.,1960,9(32):1123-1128
37Ungar E E.Maximum stresses in beams and plates vi-brating at resonance.Trans.ASME,J.Engrg Ind.,1962,1(82B):149-155
38Crandall S H.Relation between strain and velocity in res-onant vibration.J.Acoust.Soc.Amer.,1962,12(34):1960-1961
39Harry H,Kern D L,Piersol A G.HDBK-7005dynamic environmental criteria.NASA,2001.1-302
40Segalman D J.An efficient method for calculating RMS von Mises stress in a random vibration environment.SANDIA,1998,4:98-103
41Segalman D.Estimating the probability distribution of von Mises stress for structures undergoing random excita-tion.Journal of Vibration and Acoustics,2000,1(122):84-91
42Reese G M.A tutorial on design analysis for random vi-bration.DE,2000-28753406.1-32
43Quaranta G,Mantegazza P.Randomly excited structures reliability by means of the von Mises stress response.DOD,1994:1-34
44Elishakoff I.Stochasticity and safety factors:part1.ran-dom actual stress and deterministic yield stress.Chaos Solitons&Fractals2005,4:344-356
45de Fuente E.von Mises stresses in random vibration of lin-ear structures.Computers and Structures,2009,7:1253-1262
46廖海涛.噪声载荷作用下航空薄壁壳体的随机振动响应:[硕士论文].沈阳:沈阳航空工业学院,2007.21-30
47李德葆.应变模态分析和曲率模态分析.见:第15届全国振动与噪声控制高技术及应用会议,北京,2001
版权所有：© 2023 中国地质图书馆 中国地质调查局地学文献中心