System Life and Reliability Modeling of a Multiple Power Takeoffs Accessory Gearbox Transmission-Reference-Cited by-同舟云学术

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System Life and Reliability Modeling of a Multiple Power Takeoffs Accessory Gearbox Transmission

Published:2022-07-22 Issue:6 Volume:27 Page:855-866
ISSN:1007-1172
Container-title:Journal of Shanghai Jiaotong University (Science)
language:en
Short-container-title:J. Shanghai Jiaotong Univ. (Sci.)

Author:

Wang Kai,Wang Xianliang,Zhu Jiazan,Ou Daisong,Pan Daifeng

Publisher

Springer Science and Business Media LLC

Subject

Multidisciplinary

Link

https://link.springer.com/content/pdf/10.1007/s12204-022-2473-y.pdf

Reference22 articles.

1. Engine, aircraft, turbojet and turbofan, general specification: MIL-E-5007E [S]. Washington: United States Department of Defense, 1983.

2. CHAUDHARI V, MONIZ T, NAIKTARI C, et al. Integrated preliminary design approach for turbomachinery design [C]//ASME 2011 Turbo Expo. Vancouver: ASME, 2012: 171–176.

3. Joint service specification guide: Engines, aircraft, turbine: JSSG-2007A [S]. Washington: United States Department of Defense, 2004.

4. INGISTOV S. Failures of the high energy, high pitch velocity gear boxes [C]//ASME Turbo Expo 2004. Vienna: ASME, 2008: 783–794.

5. DAVIS J D. An appraisal of cost-effectiveness models used in the air force and navy aircraft engine component improvement programs [D]. Monterey: Naval Postgraduate School, 1991.

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