一种飞机起落架试验装置
By using an automated design that combines chamfered blocks with guide grooves, and employing a servo motor to drive a rack and pinion mechanism, the automatic installation and disassembly of the landing gear is achieved. This solves the problem of manual intervention in connection and separation in existing technologies, and improves the convenience and safety of test operations.
Patent Information
- Authority / Receiving Office
- CN · China
- Patent Type
- Utility models(China)
- Current Assignee / Owner
- XIAN HANGFENG TESTING TECH CO LTD
- Filing Date
- 2025-07-07
- Publication Date
- 2026-07-17
AI Technical Summary
In existing aircraft landing gear testing equipment, the connection process between the gantry crane hook and the cantilever pulley track assembly requires manual intervention, and the hook is not easy to quickly separate after the assembly is hoisted to the specified height, which affects the convenience of the test operation.
The design employs a combination of chamfered blocks and guide grooves, and uses a servo motor to drive a rack and pinion mechanism to achieve automatic connection and separation. Combined with the lifting of cylinders and moving frames, the installation and disassembly of the landing gear are completed automatically.
This improved the ease of operation and efficiency of landing gear testing, reduced manual intervention, and enhanced the automation and safety of the testing process.
Smart Images
Figure CN224511469U_ABST