一种双弹翼气动加载载荷模拟装置
By using a tensioner and thrust sensor to adjust the loading force of the upper wing in the aerodynamic loading simulation device, and combining a roller assembly and a linear geared motor to adjust the loading force of the lower wing, the structural complexity and the problem of the invariable loading force of the traditional device are solved, and accurate wing loading simulation is achieved.
Patent Information
- Authority / Receiving Office
- CN · China
- Patent Type
- Patents(China)
- Current Assignee / Owner
- BEIJING RES INST OF SPATIAL MECHANICAL & ELECTRICAL TECH
- Filing Date
- 2023-11-28
- Publication Date
- 2026-07-17
AI Technical Summary
Traditional aerodynamic loading simulation devices for warheads cannot apply variable loading forces to two pairs of warheads simultaneously, and they also have risks such as complex structure, low accuracy, easy damage to thrust sensors, and mutual interference during warhead deployment.
The system employs components such as a support frame, test bench, fixed frame, projectile body, roller assembly, and thrust sensor. The loading force on the upper wing is adjusted by the tensioner and thrust sensor, while the loading force on the lower wing is adjusted by the roller assembly and linear gear motor, thus achieving variable load application on the two pairs of wings.
The device's structural complexity has been reduced, the accuracy of loading force adjustment and the device's applicability have been improved, the impact on the projectile has been reduced, the loading conditions of the projectile wings can be accurately simulated, the interference of the projectile wings has been avoided, and the data can be monitored in real time.
Smart Images
Figure CN117663920B_ABST