A high damping thermal deformation releasing device

A release device and thermal deformation technology, applied in the direction of elastic shock absorbers, shock absorbers, shock absorbers, etc., can solve the problems of large displacement and high structural stress of flexible structural parts, and achieve reduced relative displacement, stable mechanical properties, Effect of High Damping Ratio

Active Publication Date: 2019-08-09
BEIJING INST OF SPACECRAFT SYST ENG
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Problems solved by technology

[0004] The technical solution of the present invention is to overcome the deficiencies of the prior art and provide a high-damping thermal deformation release device, which can solve the problem of thermal stress caused by thermal deformation caused by high-frequency vibration of two structural components connected by flexible structural components. , the relative displacement of flexible structural parts is relatively large, resulting in the problem of high structural stress

Method used

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  • A high damping thermal deformation releasing device
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  • A high damping thermal deformation releasing device

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Embodiment Construction

[0025] Combine below Figure 1-Figure 4 The device provided by the present invention is described in detail. The high-damping thermal deformation release device of the present invention includes a base 1 , an elastic element 2 , a shell 3 , a damping element 4 , and a connecting seat 5 . Wherein, the base 1 and the connecting seat 5 are flat plates made of metal. The lower end of the elastic element 2 is fixed to the base 1, the elastic element 2 is perpendicular to the base 1, the upper end of the elastic element 2 is fixed to the connecting seat 5, and the elastic element 2 is vertical to the base 1. The stiffness in the direction of the base 1 is greater than the stiffness of the elastic element 2 in a direction parallel to the base 1, the shell 3 is connected to the base 1, and the elastic element 2 is enclosed inside the shell 3; the damping element 4. Filling between the elastic element 2 and the housing 3, there is a gap on the contact surface between the damping eleme...

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Abstract

The invention relates to a high-damping heat deformation release device which comprises a base (1), an elastic element (2), a shell (3), a damping element (4) and a connection base (5). The lower end of the elastic element (2) is fixedly connected with the base (1), the elastic element (2) is perpendicular to the base (1), the upper end of the elastic element (2) is fixedly connected with the connection base (5), the rigidity of the elastic element (2) in the direction perpendicular to the base (1) is larger than the rigidity of the elastic element (2) in the direction parallel to the base (1), the shell (3) is connected with the base (1) and used for wrapping the elastic element (2), the space between the elastic element (2) and the shell (3) is filled with the damping element (4), a gap exists in the contact face between the damping element (4) and the elastic element (2), the gap is used for adjusting the contact area of the damping element (4) and the elastic element (2), and the volume ratio of the gap in the damping element (4) is inversely proportional to the damping coefficient of the damping element (4) and the rigidity of the elastic element (2).

Description

technical field [0001] The invention relates to the technical field of flexible connection, in particular to a high-damping thermal deformation releasing device. Background technique [0002] The large-scale flat-panel phased array antenna used by microwave remote sensing spacecraft is affected by the change of the sun's irradiation angle in the orbital environment, and the temperature will fluctuate to a certain extent. In order to ensure the light weight and high strength of the structure, the antenna mounting frame is mostly made of carbon fiber material. The antenna itself must use metal materials in order to ensure electrical performance. The thermal expansion characteristics of the two materials are quite different. When the temperature changes, the thermal deformation of the two materials is not coordinated, which will cause the structure to warp and deform, which will change the antenna beam pointing and affect the detection performance. Optical remote sensing sate...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): F16F7/00F16F7/12
CPCF16F7/00F16F7/12F16F2238/02F16F2238/022F16F2238/04
Inventor 王光远王建军杨双景管帅张庆君李延齐亚琳
Owner BEIJING INST OF SPACECRAFT SYST ENG
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