一种新型桨轴轴承试验加载装置

By designing a novel propeller shaft bearing test loading device, which utilizes a test bearing, a radial force load loading component, and a simulated load loading unit, the complex stress conditions of aero-engine propeller shaft bearings are realistically simulated, solving the problem of insufficient accuracy of existing devices and achieving high-precision test results.

CN116164968BActive Publication Date: 2026-07-17AECC HUNAN AVIATION POWERPLANT RES INST

Patent Information

Authority / Receiving Office
CN · China
Patent Type
Patents(China)
Current Assignee / Owner
AECC HUNAN AVIATION POWERPLANT RES INST
Filing Date
2023-03-27
Publication Date
2026-07-17

AI Technical Summary

Technical Problem

Existing bearing testing equipment cannot realistically simulate the complex stress conditions of aero-engine propeller shaft bearings in actual applications, resulting in poor testing accuracy.

Method used

A novel propeller shaft bearing test loading device is designed, comprising a housing, multiple first bearing seats, a test shaft, a first radial force load loading component, and a simulated load loading unit. Radial and axial forces are applied through the test shaft to simulate the complex working conditions of the intermediate gear on the propeller shaft, forming bending moment force and realistically simulating the stress condition of the bearing.

Benefits of technology

It improves the accuracy of bearing testing, ensures test quality, and can realistically simulate the stress conditions of bearings under actual working conditions, thereby improving the accuracy and stability of the test.

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Abstract

本发明涉及航空发动机桨轴轴承试验技术领域,具体涉及一种新型桨轴轴承试验加载装置,包括:箱体;多个第一轴承座,多个第一轴承座沿水平方向间隔设置在箱体内,适于同轴安装多个试验轴承;试验轴,沿试验轴承的轴线依次穿设在多个试验轴承内,且试验轴的两端伸出试验轴承;第一径向力载荷加载组件,固定设置在箱体内,且位于试验轴的中间位置对试验轴施加径向力载荷;模拟载荷加载单元,固定设置在箱体内,与试验轴的一端连接,用于给试验轴的一端施加径向力载荷以及轴向力载荷;其中,径向力载荷和轴向力载荷均通过试验轴施加到试验轴承。解决了现有的试验装置不能真实模拟实际轴承的受力情况,对轴承考核的精准度较差的技术问题。
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