Ground vibration test fixture for large-scale spacecraft

A space vehicle and vibration test technology, which is applied in vibration test, machine/structural component test, measuring device, etc., can solve the problems of weak stiffness, low first-order frequency, and low strength, so as to improve safety and reliability, improve The Effect of Stiffness and Strength

Active Publication Date: 2013-04-17
SHANGHAI YUDA IND
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AI Technical Summary

Problems solved by technology

[0003] Aiming at defects such as low structural strength, weak stiffness, low first-order frequency, and large mass of the solid-type large-scale vibration test fixture in the prior art when the interface expansion is nearly doubled and the fixture height is required to be not less than 900mm, the purpose of the present invention is to It is to provide a large interface rib type vibration test fixture

Method used

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  • Ground vibration test fixture for large-scale spacecraft
  • Ground vibration test fixture for large-scale spacecraft

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Embodiment Construction

[0020] The present invention will be described in detail below in conjunction with specific embodiments. The following examples will help those skilled in the art to further understand the present invention, but do not limit the present invention in any form. It should be noted that those skilled in the art can make several modifications and improvements without departing from the concept of the present invention. These all belong to the protection scope of the present invention.

[0021] Such as figure 1 and figure 2 Shown, specifically, a kind of fixture 1 for ground vibration test of large space vehicle provided by the present invention is mainly used in the vibration test of large space vehicle, the interface size of vibration table φ990mm, φ1600mm is nearly doubled to adapt to φ3000mm above For the installation of large-interface products, the first-order resonance frequency of the vibration test fixture 1 can reach 137 Hz, which can meet the requirements of vibration...

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Abstract

The invention provides a ground vibration test fixture for a large-scale spacecraft. The ground vibration test fixture comprises a fixture main body, a first interface, a second interface, an upper end surface outer wall lug boss, a position limiting block and an upper end surface inner wall lug boss, wherein the first interface is arranged at the bottom of the fixture main body, the second interface is arranged at the top of the fixture main body, the upper end surface of the fixture main body is provided with the upper end surface outer wall lug boss and the upper end surface inner wall lug boss, and the position limiting block is arranged on the upper end surface outer wall lug boss and is used for limiting the transverse sliding of a limiting product. The ground vibration test fixture solves the problems of great weight, low intensity, low rigidity, low first-order base frequency and the like under the condition that an interface of an entity type large-scale vibration test fixture is enlarged. The fixture structure form adopts the rib plate type, the rigidity and the intensity of the large-scale vibration test fixture are greatly improved, the first-order frequency of the fixture is 3 to 5 times higher than that of an aircraft, and the safety and the reliability of the vibration test are greatly improved.

Description

technical field [0001] The invention relates to a vibration test fixture, especially a vibration test fixture with a large interface, in particular to a ground vibration test fixture for a large space vehicle. Background technique [0002] Vibration test is an important part of environmental test, and fixture plays an extremely important role in vibration test. The vibration test fixture transmits the vibration energy of the mechanical connection to the test piece from the vibration table, and it cannot be distorted during the energy transmission process. In the entire test frequency range of the vibration table, it is difficult to transmit the vibration energy of the moving coil to the table without distortion. Unreasonable fixture design, manufacture, installation and use are prone to "overvibration" and "undervibration". Even if the requirements of the control spectrum are barely met, the load on the control system will be increased, especially when the dynamic response ...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G01M7/02
Inventor 王继虎张利付国庆张逸波姚煜中
Owner SHANGHAI YUDA IND
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