基于交互正交试验的空间用谐波减速器传动性能影响因素研究

Abstract

Abstract: In view of the multiple factors and their interactive influences affecting the transmission performance of harmonic drives used in spacecraft, thermal-vacuum tests are performed using harmonic drive of type XB1-60-150. Based on the interactive orthogonal design method, the effects of rotational speed, surrounding temperature, output load torque, and lubrication type on the transmission efficiency of the harmonic drive are investigated. Range analysis and variance analysis are applied to analyze the sensitivity of these factors and their coupling influences. The results achieved by both range analysis and variance analysis are close. When confidence p=99%, the study indicaties that rotational speed and surrounding temperature have notable effect on the transmission performance of harmonic drive, and so do the interactive influences of output load torque and lubrication type. The best application conditions are obtained by interactive analysis under which the transmission performance of harmonic drive can achieve the most satisfactory effect.

Key words: harmonic drive, interactive orthogonal experiment, range analysis, variance analysis, transmission perfor-mance

CLC Number:

V519
TH117.3

LI Bo. Research of Factors Affecting Transmission Performance of Harmonic Drive in Spacecraft Based on Interactive Orthogonal Experiment[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2012, 33(2): 375.

References

[1] Wan-Roberts D. New frontiers for space tribology. Tribology International, 1990, 23(2): 149-155.

[2] Shen Y W, Ye Q T. Theory and design of harmonic drive. Beijing: China Machine Press, 1985. (in Chinese) 沈允文, 叶庆泰. 谐波齿轮传动的理论和设计. 北京:机械工业出版社,1985.

[3] Ueura K, Slatter R. Development of harmonic drive gear for space applications. Toulouse: European space mechanisms and tribology symposium, 1999: 259-264.

[4] Fusaro R L. Space Mechanisms Technology Workshop. NASA CP-210971, 2000.

[5] Fusaro R L. Preventing spacecraft failures due to tribolo- gical problems . NASA TM-210806, 2001.

[6] Heimerdinger H, Schmid M. Life test experience on a harmonic drive based actuator. ESA-SP-374, 1995.

[7] Schafer I, Bourlier P, Hantschack F, et al. Space lubrication and performance of harmonic drive gear. Lucerne: Proceedings of the 11the ESMATS Symposium, 2005: 591.

[8] Xue Q J, Yu D Y. Investigation of the lubrication failure mechanisms of several thin solid films. Proceedings of Ⅲ International Symposium on Tribo-Fatigue. 2000: 36-43.

[9] Zhou H, Sun J, Wen Q P, et al. Lubrication and performance of harmonic drive used in spacecraft. Journal of Astronautics, 2009, 30(1): 378-381. (in Chinese) 周晖, 孙京, 温庆平, 等. 谐波减速器空间润滑及性能研究. 宇航学报, 2009, 30(1):378-381.

[10] Zhou H, Wen Q P, Zhang W W. Harmonic drive used in spacecraft. Vacuum and Cryogenics, 2004, 10(4):187-192. (in Chinese) 周晖, 温庆平, 张伟文. 谐波减速器在空间飞行器中的应用. 真空与低温, 2004, 10(4):187-192.

[11] Yu D Y, Weng L J, Ouyang J L. Recent progress of the space mechanism lubrication. Tribology, 1996, 16(1):89-96. (in Chinese) 于德洋, 翁立军, 欧阳锦林. 空间机械润滑研究的发展现状. 摩擦学学报, 1996, 16(1):89-96.

[12] Feng D P, Weng L J, Liu W M. Progress of tribology of perfluoropolyether oil. Tribology, 2005, 25(6):597-602. (in Chinese) 冯大鹏, 翁立军, 刘维民. 全氟聚醚润滑油的摩擦学研究进展. 摩擦学学报, 2005, 25(6):597-602.

[13] Weng L J, Wang X P, Li L X, et al. The failure mechanism of the solid lubrication of a harmonic drive reducer. Tribology, 1997, 17(2):178-181. (in Chinese) 翁立军, 汪晓萍, 李陇旭, 等. 谐波齿轮传动减速器的固体润滑失效机理. 摩擦学学报, 1997, 17(2):178-181.

[14] Li Y Y, Hu C R. Experiment design and data processing.Beijing: Chemical Industry Press, 2005. (in Chinese) 李云雁, 胡传荣.试验设计与数据处理.北京:化学工业出版社, 2005.

[15] Zhuang C Q, He C X. Application mathematical statistic foundation. Guangzhou: South China University of Technology Press, 2006. (in Chinese) 庄楚强,何春雄.应用数理统计基础.广州:华南理工大学出版社,2006.

Research of Factors Affecting Transmission Performance of Harmonic Drive in Spacecraft Based on Interactive Orthogonal Experiment

PDF (PC)

Knowledge

Abstract

Cite this article

share this article

References

Related Articles 3

Recommended Articles

Metrics

Comments

[1]	ZHANG Shuai, ZHANG Qiangbo, ZHANG Xiamei. Identification of foreign object impact on aero-engine fan blades with variance analysis [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2021, 42(5): 524196-524196.
[2]	CHENG Chao, WU Baohai, ZHENG Hai, GAO Limin. Effect of blade machining errors on compressor performance [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2020, 41(2): 623237-623237.
[3]	Li Haitao;Fang Jiancheng;. Study on System Vibration Suppression Method Based on ESO Used in Gimbal Servo System of DGMSCMG [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2010, 31(6): 1213-1219.