一种航空活塞发动机力学性能测试实验台
By designing an experimental rig for testing the mechanical performance of aero-piston engines and adopting a combined structure of power shaft and bushing, simultaneous tensile and torque testing was achieved, solving the problem of single testing systems in existing technologies and improving testing efficiency and accuracy.
Patent Information
- Authority / Receiving Office
- CN · China
- Patent Type
- Patents(China)
- Current Assignee / Owner
- UNIV OF ELECTRONICS SCI & TECH OF CHINA
- Filing Date
- 2023-05-12
- Publication Date
- 2026-07-17
AI Technical Summary
Existing technologies can only test one of the mechanical properties of aircraft piston engines, namely tension or torque, and the testing system is limited and the results are not accurate enough.
An experimental rig for testing the mechanical performance of an aero-piston engine was designed, comprising a rig, an engine propeller assembly, a tensile testing assembly, and a torque testing assembly. The design of the power shaft and bushing enables simultaneous tensile and torque testing, and a locking assembly constrains the motion degrees of freedom of the power shaft and bushing before testing to avoid mismeasurement.
This allows for simultaneous tensile and torque testing without interference, improving testing efficiency and the accuracy of measurement data, avoiding false measurements, and ensuring the accuracy of test results.
Smart Images
Figure CN116481818B_ABST