航空
压力角
工程类
齿面
木桶(钟表)
航程(航空)
结构工程
轮齿
可靠性(半导体)
汽车工程
机械工程
航空航天工程
功率(物理)
物理
量子力学
作者
Jinxiao Chen,Caichao Zhu,Peitang Wei,Ping Zeng,Bi-Yao Wang,Taimin Chen,Huaiju Liu
出处
期刊:Tribology Transactions
日期:2024-03-03
卷期号:67 (2): 280-293
被引量:7
标识
DOI:10.1080/10402004.2024.2309906
摘要
Scuffing failure in high-speed aviation gears is a critical issue that hinders the improvement of operating performance and reliability in modern aviation equipment. The unclear failure mechanism limits the effective design of anti-scuffing measures. In this study, a scuffing test method was designed for high-speed aviation gears to investigate the effects of tooth profiles and surface treatment on the gear scuffing performance. The results indicate that both the pressure angle and surface treatment significantly affect gear scuffing behavior. Under different geometric treatment states, the range of the Ryder load stages at which gear scuffing initiated was between 5 and 13. The 25° pressure angle gear with barrel finishing treatment exhibited the optimal anti-scuffing performance. Compared to the ground state, barrel finishing increases gear scuffing loading capacity by 30% to 33%. Tooth profile optimization based on pressure angle changes improves gear loading capacity by 56.9%. This work provides an exploration of the anti-scuffing design of high-speed gears.
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