Method and system for testing performance of flight control surface systems
The remote control loading method using a framework and linkage system solves the problem of multiple reconfigurations required for testing flight control surface devices in existing technologies, enabling rapid and accurate load simulation and testing, and improving testing efficiency.
Patent Information
- Authority / Receiving Office
- CN · China
- Patent Type
- Patents(China)
- Current Assignee / Owner
- THE BOEING CO
- Filing Date
- 2021-01-15
- Publication Date
- 2026-07-17
AI Technical Summary
Existing testing methods and systems require multiple reconfigurations to adapt to different load conditions when testing flight control surface devices, which increases complexity and time costs, and cannot accurately apply loads with the desired size and orientation.
The system employs a frame and linkage system, including support components, actuation components, and load components, to remotely control and adjust the load distribution, thereby enabling rapid and accurate loading of the flight control surface devices and ensuring the repeatability and predictability of the load distribution.
It reduces testing time and complexity, enables rapid and accurate simulation of various load conditions in a laboratory environment, ensures load repeatability and accuracy, reduces unwanted load vectors, and improves testing efficiency.
Smart Images
Figure CN113138090B_ABST