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A preparation device and method for a large-scale heat-fit structure for carbon fiber filaments

A technology of carbon fiber filaments and preparation devices, which is applied in the direction of manufacturing tools, stamping machines, presses, etc., can solve the problems that thermal deformation cannot be completely eliminated, the range of material selection is limited, and the warping deformation of the detector is solved, so as to solve the problem of thermal mismatch deformation , simple structure, and the effect of small flexural section modulus

Active Publication Date: 2021-07-09
BEIJING RES INST OF SPATIAL MECHANICAL & ELECTRICAL TECH
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  • Summary
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  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

The working temperature of the detector is 60 ~ 80K, but the temperature of its assembly environment, storage environment and non-working state is generally at room temperature. It can be seen that there is a temperature fluctuation of about 200K in the environment where the detector and the carrier board assembly are located. When the temperature fluctuates, Inconsistencies in the linear expansion coefficients of the detector and the bearing plate and other structures will cause the detector to warp and deform, and in severe cases will cause the detector to be damaged
[0003] When the size of the detector is small (such as 320X256), the matching design of the linear expansion coefficient can be used to reduce the thermal deformation and warpage of the detector. The matching of expansion coefficients cannot completely eliminate thermal deformation, especially for detectors with large area arrays (such as 2560X2560), and the problem of detector warpage caused by thermal deformation appears again.

Method used

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  • A preparation device and method for a large-scale heat-fit structure for carbon fiber filaments
  • A preparation device and method for a large-scale heat-fit structure for carbon fiber filaments
  • A preparation device and method for a large-scale heat-fit structure for carbon fiber filaments

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preparation example Construction

[0026] The device for preparing carbon fiber thermally adapted structure of the present invention uses a metal mold to press and compress carbon fibers. The pressure can be adjusted so that the carbon fibers can be compressed without too much pressure and the carbon fibers are not damaged. The structure is simple and the implementability is good.

[0027] The present invention will be further described in detail below in conjunction with the accompanying drawings and specific embodiments.

[0028] Such as figure 1 As shown, the present invention is a preparation device for a large-size thermally adapted structure of carbon fiber filaments, including: a base 1 , a fixing block 2 , a pressing slider 3 , a pressure plate 4 , carbon fiber filaments 5 and screws 6 . The base 1 is placed on the platform, the fixed block 2 is installed in the slot 11 of the base 1, and the carbon fiber filament 5 is placed in the right-angled opening 22 of the fixed block 2. The carbon fiber filament...

Embodiment

[0043] According to the preparation device of the large area array detector thermal adaptation structure based on carbon fiber of the present invention, a carbon fiber filament thermal adaptation structure with a length of 50mm, a width of 40mm, and a thickness of 5mm has been successfully prepared, and the thermal adaptation structure glues the detector on the cold On the finger, under the temperature fluctuation of about 200K, the thermal deformation and warpage of the detector is only 3um, which solves the problem of thermal mismatch deformation between the large area array detector and the cold finger.

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Abstract

A preparation device and method for a large-scale heat-adaptive structure of carbon fiber filaments, comprising: a base, a fixing block, a pressing slide block, a pressure plate, carbon fiber filaments and screws. The pressure plate, the compression slider, the fixed block, and the base are fixedly connected in sequence, and a plurality of carbon fiber filaments are inserted between the compression slider and the fixed block, so that the cross-sectional shape of the carbon fiber filament is the same as that of the heat-fitting structure. The invention uses a metal mold to press and compress the carbon fiber, and the pressure can be adjusted so that the carbon fiber can be compressed without too much pressure to damage the carbon fiber. The structure is simple and the implementability is good.

Description

technical field [0001] The invention relates to a preparation device and method for a large-scale thermal adaptation structure of carbon fiber filaments, which belongs to the technical field of space camera large-area infrared focal plane structure, and particularly relates to a carbon fiber filament thermal adaptation applied to a large-scale infrared focal plane. A processing method and a manufacturing device for an adaptive structure. Background technique [0002] In order to obtain good imaging quality for space infrared remote sensing cameras, the area array detectors need to work in a cryogenic environment, and generally need to be cooled to 60-80K. Reduce the thermal resistance between the cold finger and the detector. The working temperature of the detector is 60 ~ 80K, but the temperature of its assembly environment, storage environment and non-working state is generally at room temperature. It can be seen that there is a temperature fluctuation of about 200K in th...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B30B1/00B30B15/00
CPCB30B1/00B30B15/00
Inventor 陈芳罗世魁高超杜建祥岳聪董科孙熠璇白杰
Owner BEIJING RES INST OF SPATIAL MECHANICAL & ELECTRICAL TECH
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