航空发动机成附件振动环境试验剖面确定方法研究

推进技术 ›› 2013, Vol. 34 ›› Issue (8): 1101-1107.

航空发动机成附件振动环境试验剖面确定方法研究

王桂华^1,2,刘海年²,张大义¹,洪杰¹

北京航空航天大学能源与动力工程学院,北京 100191;中国航空工业集团公司沈阳发动机设计所,辽宁沈阳 110015;北京航空航天大学能源与动力工程学院,北京 100191;北京航空航天大学能源与动力工程学院,北京 100191

发布日期:2021-08-15
作者简介:王桂华(1965—),女,研究员,研究领域为航空发动机可靠性。E-mail:wangguih@sina.com

Study on Formulating Method for Vibration Environment Test Profiles of Aero-Engine Accessories

School of Energy and Power Engineering,Beijing University of Aeronautics and Astronautics, Beijing 100191,China;Shenyang Engine Design and Research Institute, Aviation Industry Corporation of China,Shenyang 110015,China;School of Energy and Power Engineering,Beijing University of Aeronautics and Astronautics, Beijing 100191,China;School of Energy and Power Engineering,Beijing University of Aeronautics and Astronautics, Beijing 100191,China

Published:2021-08-15

摘要/Abstract

摘要： 针对航空发动机成附件振动环境试验需求,论述了发动机成附件的可靠性试验、功能性试验、耐久性试验以及强化试验的功用与实施流程,明确了各振动环境试验剖面制订中的基本要求。阐述了四类振动环境试验剖面的详细确定步骤、分析方法以及应遵循的基本原则,发展和完善了基于环境测试数据(功率谱密度样本)的振动环境试验剖面确定方法。通过工程实例分析,使读者对试验剖面确定流程形成直观认识,对位于风扇机匣位置的成附件而言,试验剖面的各频段分别用以反映低压转子不平衡激励、高压转子不平衡激励、风扇气动激励以及随机噪声的振动能量。 

关键词: 航空发动机;振动环境试验;功率谱密度;试验剖面 

Abstract: The function and implementing process of four sorts of vibration environment tests were discussed according to the development need of aero engine accessories, including reliability test, function test, endurance test and reliability enhancement test . Thus the characteristics of each test profile and basic requirements of test profile formulation were identified. The detailed formulating steps, analytical method and basic principles were expounded. As a result the formulating method for vibration environment test profiles from power density data was developed. Finally, the formulating process was cleared through an engineering case. The power spectral density value of each frequency range in the test profiles represents the vibration energy caused by the unbalance of lower pressure spool, the unbalance of high pressure spool, the aerodynamic force of fan and random noise, respectively. 

Key words: Aero engine; Vibration environment test; Power spectral density; Test profile

王桂华,刘海年,张大义,洪杰. 航空发动机成附件振动环境试验剖面确定方法研究[J]. 推进技术, 2013, 34(8): 1101-1107.

WANG Gui-hua^1,2, LIU Hai-nian², ZHANG Da-yi¹, HONG Jie¹. Study on Formulating Method for Vibration Environment Test Profiles of Aero-Engine Accessories[J]. Journal of Propulsion Technology, 2013, 34(8): 1101-1107.

参考文献

[1] GJB241-87.航空涡轮喷气和涡轮风扇发动机通用规范[S].1987.
[2] MIL-E-5007D:Engines, Aircraft, Turbojet and Turbofan, General Specification for Military Specification[S].1973.
[3] GJB150.16-86军用设备环境试验方法振动试验[S].1986.
[4] HB5830.5-1984机载设备环境条件及试验方法[S].1984.
[5] 莫昌瑜,袁宏杰.舰载设备可靠性振动试验剖面设计方法研究[J].船舶力学, 2012,6(4):442-448.
[6] 袁宏杰,罗敏,姜同敏.随机振动环境测量数据归纳方法研究[J].航空学报, 2007,8(1):115-117.
[7] 罗敏,姜同敏,袁宏杰.一种可靠性试验实测振动数据的处理方法[J].北京航空航天大学学报, 2007,3(10):1237-1240.
[8] GJB899A-2009.可靠性鉴定和验收试验[S].2009.
[9] GJB150.16A-2009.军用装备实验室环境试验方法, 第16部分:振动试验[S].2009.
[10] 徐明,马升.关于振动耐久试验量值和持续时间方法的讨论[J].航空标准化与质量, 2003,(5):36-41.
[11] 程德斌.可靠性试验评价技术发展及其应用[J].环境适应性和可靠性,2010(10):21-26.
[12] 龚庆祥.型号可靠性工程手册[M].北京:国防工业出版社, 2007.
[13] GJB/Z 126-99.振动、冲击环境测量数据归纳方法[S].1999.
[14] MIL-STD-810G.Environmental Engineering Considerations and Laboratory Tests[S].2008.
[15] 蒋培,陈循,张春华,等.可靠性强化试验技术综述[J].强度与环境, 2003,0(1):58-64.
[16] 姜同敏.可靠性强化试验[J].环境技术,2000,(1):3-6.
[17] 周源泉,朱新伟.论加速可靠性增长试验(I)新方向的提出[J].推进技术, 2000,21(6):6-9.(ZHOU Yuan-quan, ZHU Xin-wei.Research on Accelerated Reliability Growth Test(I) Presentment of a New Direction[J].Journal of Propulsion Technology, 2000,21(6):6-9.)
[18] 周源泉,安维廉,朱新伟.论加速可靠性增长试验 (Ⅶ)步进应力试验方案的统计分析[J].推进技术,2003,24(5):393-396.(ZHOU Yuan-quan,AN Wei-lian, ZHU Xin-wei.Research on Accelerated Reliability Growth Test(Ⅶ) Tatistical Analysis of Step Stress Test Schemes[J].Journal of Propulsion Technology, 2003,24(5):393-396.)
[19] 陈循, 朱文献, 陶俊勇.可靠性强化试验应力剖面的研究[J].电子产品可靠性与环境试验, 2003(1):46-50.