A multi-degree-of-freedom support mechanism for a high-speed wind tunnel
By designing a multi-degree of freedom support mechanism for high-speed wind tunnels, using a full-scisor three-degree of freedom mechanism and hollow motor rolling assembly, the problems of biased load and poor load-bearing capacity of the existing support mechanism are solved, and efficient and symmetrical aerodynamic test is achieved.
Patent Information
- Application Number
- CN202411864303.8
- Authority / Receiving Office
- CN · China
- Patent Type
- Patents(China)
- Current Assignee / Owner
- Filing Date
- 2024-12-18
- Publication Date
- 2025-03-28
- Estimated Expiration
- 2044-12-18
AI Technical Summary
The existing high-speed wind tunnel model support mechanism has a bias load problem in aerodynamic tests, which affects the symmetry and stability of the model and flow field, and has poor load-bearing capacity and low test efficiency.
A high-speed wind tunnel multi-degree of freedom support mechanism is designed, including the main load-bearing skeleton, side sliding assembly, angle of attack assembly and rolling assembly. It adopts a full scimitar three-degree of freedom mechanism to realize rolling motion through a hollow motor and a rolling bracket to improve the stiffness and symmetry of the overall structure.
The continuous free movement of the model in the angle of attack, side slip and rolling directions is achieved, the test efficiency is improved, the stiffness and airflow symmetry of the support mechanism are enhanced, and the impact of electromagnetic interference on the sensor is reduced.