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第 45 卷 第 4 期 摩擦学学报(中英文) Vol 45 No 4
2025 年 4 月 Tribology Apr, 2025
DOI: 10.16078/j.tribology.2024020 CSTR: 32261.14.j.tribology.2024020
文武翊, 林勤杰, 王中荣, 朱才朝, 刘怀举. 高速航空锥齿轮线速度对喷油润滑流场与温度场影响研究[J]. 摩擦学学报(中英文),
2025, 45(4): 525−536. WEN Wuyi, LIN Qinjie, WANG Zhongrong, ZHU Caichao, LIU Huaiju. Influence of the Impact of
Velocity on Oil Injection Lubrication Flow Field and Temperature Field in High-Speed Aeronautical Bevel Gears[J]. Tribology,
2025, 45(4): 525−536.
高速航空锥齿轮线速度对喷油润滑流场与
温度场影响研究
1
1
2
1
文武翊 , 林勤杰 , 王中荣 , 朱才朝 , 刘怀举 1*
(1. 重庆大学 高端装备机械传动全国重点实验室,重庆 400044;
2. 中国航发四川燃气涡轮研究院,四川 成都 610500)
摘 要: 喷油润滑的航空弧齿锥齿轮由于高线速度常导致射流破碎和乏断油现象,并产生异常温升和变形,严重影
响齿轮传动的寿命和服役性能. 针对高线速度对锥齿轮喷油特性影响规律不清的问题,建立了航空弧齿锥齿轮
喷油润滑热-流耦合分析模型,研究了高达160 m/s线速度的航空弧齿锥齿轮流场和温度场特性. 发现线速度从
40 m/s升高到160 m/s,齿面油液体积分数下降83.5%,润滑效果显著降低,且在120 m/s后齿面出现乏油状态,啮合区
对流换热降低. 随转速升高齿轮风阻损失呈指数增长,在80 m/s后成为齿轮副的主要功率损失来源. 随线速度升高,
齿轮不同部位温差不断增加,致使热应力和变形增大. 该研究为高速齿轮传动润滑和高承载设计提供支撑.
关键词: 高线速度; 弧齿锥齿轮; 喷油润滑; 热-流耦合; 风阻损失
中图分类号: TH117.2;TH132.41;V233 文献标志码: A 文章编号: 1004-0595(2025)04–0525–12
Influence of the Impact of Velocity on Oil Injection Lubrication
Flow Field and Temperature Field in High-Speed
Aeronautical Bevel Gears
1 1 2 1 1*
WEN Wuyi , LIN Qinjie , WANG Zhongrong , ZHU Caichao , LIU Huaiju
(1. State Key Laboratory of Mechanical Transmission for Advanced Equipment, Chongqing
University, Chongqing 400044, China;;
2. AEEC Sichuan Gas Turbine Establishment, Sichuan Chengdu 610500, China)
Abstract: The gear transmission system in aircraft engines often operates under high-speed and heavy-load conditions.
Reliable lubrication is crucial to ensure that the spiral bevel gears do not experience gear scuffing or pitting. In aircraft
accessory gearboxes, spiral bevel gears often rely on oil jet lubrication. However, the oil spray parameters designed
empirically do not consider the lubrication degradation caused by jet breakup due to rotational speed, making it difficult
to meet the design requirements of aircraft gear transmission. A Finite Volume-based thermal-fluid coupling simulation
model of spiral bevel gears has been established to consider the influence of actual conditions such as gear speed, oil
spray velocity, spray angle on lubrication and heat dissipation effects, supporting the high-reliability and high-power
Received 18 January 2024, revised 30 April 2024, accepted 30 April 2024, available online 8 August 2024.
*Corresponding author. E-mail: huaijuliu@cqu.edu.cn, Tel: +86-18883873165.
This project was supported by the National Natural Science Foundation of China (52322504, U2141247) and Chongqing Outstanding
Youth Science Fund (CSTB2023NSCQ-JQX0016).
国家自然科学基金项目(52322504, U2141247)和重庆市杰出青年科学基金项目(CSTB2023NSCQ-JQX0016)资助.