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

doi:10.1007/s12204-022-2473-y

J Shanghai Jiaotong Univ Sci ›› 2022, Vol. 27 ›› Issue (6): 855-866.doi: 10.1007/s12204-022-2473-y

收稿日期:2021-04-08 出版日期:2022-11-28 发布日期:2022-10-13

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

WANG Kai∗ (汪凯), WANG Xianliang (王宪良), ZHU Jiazan (朱加赞), OU Daisong (欧代松), PAN Daifeng (潘代锋)

(AECC Sichuan Gas Turbine Establishment, Chengdu 610500, China)

Received:2021-04-08 Online:2022-11-28 Published:2022-10-13

摘要/Abstract

Abstract: A mathematical model for system life and reliability of a multiple power takeoffs aeroengine accessory gearbox transmission is presented. The geometry model of gear train is distributed into several subsystems by different transmitted powers. The lives of each component are combined to determine the units, subsystems and entire system lives sequentially according to a strict series probability model. The unit and subsystem interface models are defined to dispose the loads of common components. The algorithm verification is presented and a numerical example is given to illustrate the use of this program. The initial design could not fulfill the life requirement. A design modification shows that the gear train has a more balanced life distribution by strengthening the weak parts, and the overall life of entire system is increased above the design requirement. This program can help the designer to approach an optimal accessory gearbox transmission design efficiently.

Key words: aeroengine, accessory gearbox, power takeoff, gear train, life model, reliability, numerical program

中图分类号:

V 233.1

. [J]. J Shanghai Jiaotong Univ Sci, 2022, 27(6): 855-866.

WANG Kai∗ (汪凯), WANG Xianliang (王宪良), ZHU Jiazan (朱加赞), OU Daisong (欧代松), PAN Daifeng (潘代锋). System Life and Reliability Modeling of a Multiple Power Takeoffs Accessory Gearbox Transmission[J]. J Shanghai Jiaotong Univ Sci, 2022, 27(6): 855-866.

参考文献 22

[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.
[6]	KUZNAR R. GE Aircraft Engines and Fiat Avio high electrical output accessory drive system [C]//34th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit. Cleveland, OH: AIAA, 1998: 3584.
[7]	Rolling bearings: Dynamic load ratings and rating life: ISO 281 [S]. Geneva: ISO, 2007.
[8]	HARRIS T, RUMBARGER J H, BUTTERFIELD C P. Wind turbine design guideline DG03: Yaw and pitch rolling bearing life [R]. Golden: National Renewable Energy Laboratory, 2009.
[9]	SAVAGE M, RADIL K C, LEWICKI D G, et al. Computerized life and reliability modeling for turboprop transmissions [J]. Journal of Propulsion and Power, 1989, 5(5): 610-614.
[10]	ZARETSKY E V. Design of oil-lubricated machine components for life and reliability [C]//Seventh International Symposia on Tribology. Cracow: NASA, 2006: 1-10.
[11]	SAVAGE M, PRASANNA M, COE H. Maximum life spiral bevel reduction design [C]//28th Joint Propulsion Conference and Exhibit. Nashville, TN: AIAA, 1992: 1-15.
[12]	SAVAGE M, RUBADEAUX K L, COE H H, et al. Spur, helical, and spiral bevel transmission life modeling [J]. Journal of Propulsion and Power, 1996, 12(2): 283-288.
[13]	SAVAGE M, PRASANNA M G, RUBADEUX K L. TLIFE: A program for spur, helical and spiral bevel transmission life and reliability modeling [R]. Adelphi: Army Research Laboratory, 1994.
[14]	ZARETSKY E V, LEWICKI D G, SAVAGE M, et al. Determination of turboprop reduction gearbox system fatigue life and reliability [J]. Tribology Transactions, 2007, 50(4): 507-516.
[15]	HU Q C, DUAN F H, WU S S. Research on reliability of closed planetary transmission systems [J]. China Mechanical Engineering, 2007, 18(2): 146-149 (in Chinese).
[16]	XUE X Z, LI Y X, WANG S M. Method of lifetime and reliability of some helicopter’s main reducer [J]. Journal of Aerospace Power, 2011, 26(3): 635-641 (in Chinese).
[17]	LI M, XIE L Y, LI H Y, et al. Life distribution transformation model of planetary gear system [J]. Chinese Journal of Mechanical Engineering, 2018, 31: 24.
[18]	ZHOU Z G, XU F. Dynamic reliability analysis of gear transmission system of wind turbine considering strength degradation and dependent failure [J]. Journal of Mechanical Engineering, 2016, 52: 80-87.
[19]	AN Z W, ZHANG Y, WANG Z L. Reliability Copula model for wind turbine gearbox based on failure correlation [J]. Journal of Shanghai Jiaotong University (Science), 2015, 20(3): 312-316.
[20]	Geometry factors for determining the pitting resistance and bending strength of spur, helical and herringbone gear teeth: ANSI/AGMA 908-B89 [S]. Alexandria: AGMA, 1989.
[21]	Rating the pitting resistance and bending strength of generated straight bevel, zerol bevel and spiral bevel gear teeth: ANSI/AGMA 2003-B97 [S]. Alexandria: AGMA, 1997.
[22]	ZARETSKY E V. Rolling bearing life prediction, theory, and application [R]. Cleveland: Glenn Research Center, 2013.

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

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