A stiffness simulation test device actively applying a support reaction force and deformation

CN117451286BActive Publication Date: 2026-10-20CHINA AIRPLANT STRENGTH RES INST
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Patent Information

Application Number
CN202311358626.5
Authority / Receiving Office
CN · China
Patent Type
Patents(China)
Current Assignee / Owner
Filing Date
2023-10-19
Publication Date
2026-10-20
Estimated Expiration
2043-10-19

AI Technical Summary

Technical Problem

[0005]本申请的目的是提供了一种主动施加支反力和变形的刚度模拟试验装置,以解决或减轻背景技术中的至少一个问题

Benefits of technology

[0017]本申请针对多站位、多方向刚度的机翼边界支持条件模拟而提出的基于主动施加载荷和位移相结合的刚度模拟试验装置,既保证了机翼/襟翼/副翼等试验件的刚度变形模拟的真实性,也解决了以往襟翼等试验件刚度标定困难、标定周期长、测量难、误差大的问题,通过对试验测量的支反力反馈数值分析,该试验装置及方法精准有效。

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Abstract

The application provides a rigidity simulation test device for actively applying counterforce and deformation, comprising: an active displacement control actuating cylinder connected with a flap through an adapter; a connecting section connected with a certain group of joints on the flap through a connecting piece; a supporting beam installed on a supporting column, wherein a vertical sliding rail is arranged on the supporting beam, and a guide block capable of relative movement is arranged in the sliding rail; a following section, one side of the following section being connected with the guide block, and the other side of the following section being provided with a bending moment actuating cylinder connected with the connecting section, wherein the bending moment actuating cylinder is connected with the connecting section through a force sensor; and a following deformation actuating cylinder, which is arranged in parallel with the active displacement control actuating cylinder and connected with the following section. The simulation test device can ensure the authenticity of the rigidity deformation simulation of the aileron and other test pieces, and solve the problems of difficulty in rigidity calibration of the flap and other test pieces and large measurement error.
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Citation Information

Patent Citations

  • Universal device for comparing stiffness of rotor blades or helm rotors for bending in thrust plane

    RU2704753C1

  • Stand for calibration and determination of rigidity of rotational dynamometers and strain-measuring shafts

    SU1749737A2