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Method for gluing two seams of spatial reflector

A reflector and double stop technology, applied in the field of space optical remote sensing, can solve the problems of space reflector surface shape accuracy drop, unstable stress distribution, uneven glue layer thickness, etc., to achieve the best engineering feasibility and small residual stress , The effect of uniform thickness of the glue layer

Inactive Publication Date: 2015-07-01
CHANGCHUN INST OF OPTICS FINE MECHANICS & PHYSICS CHINESE ACAD OF SCI
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Problems solved by technology

[0004] In order to solve the problems of low positioning accuracy, uneven adhesive layer thickness, and residual stress after the adhesive layer is cured in the existing method of using three jackscrews to complete the space mirror and the inlay, the surface shape accuracy of the space mirror is reduced, and the stress In order to solve the problem of unstable distribution, the present invention proposes a simple and reliable double-stop gluing method for space mirrors that can realize high-precision positioning between the space mirror and the inlay, and has a uniform thickness of the glue layer.

Method used

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  • Method for gluing two seams of spatial reflector
  • Method for gluing two seams of spatial reflector
  • Method for gluing two seams of spatial reflector

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Embodiment Construction

[0036] The present invention will be described in further detail below in conjunction with the accompanying drawings.

[0037] A method for gluing a space reflector with double seams according to the present invention, the method is realized by the following steps:

[0038] (1) First, use gauze dipped in acetone solution to wipe off the glue position on the side wall of the inner hole 11 of the space mirror 1 and the glue position on the outer side wall of the inlay 5 respectively, and then wipe the glue on the side wall of the space mirror 1 respectively. Apply epoxy resin glue with a thickness of 0.01 mm to 0.03 mm on the adhesive position on the side wall of the inner hole 11 and the adhesive position on the outer side wall of the inlay 5; the thickness of the applied epoxy resin adhesive is preferably 0.02 mm ;

[0039] (2) Place the space mirror 1 flat on the workbench, such as figure 1 As shown, first the bottom adhesive protective film 4 is tiled and pasted on the bot...

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Abstract

The invention provides a method for gluing two seams of a spatial reflector, relates to the technical field of spatial optical remote sensing, and aims at solving the problems of small positioning precision, non-uniform glue layer thickness, reduction of surface figure accuracy of the spatial reflector caused by residual stress after solidifying of a glue layer, and unstable stress distribution in the existing method of gluing the spatial reflector and an embedded part through three jackscrew. The method is that glue coats the lower side of the inner hole wall of the spatial reflector; the upper side of the inner hole wall of the spatial reflector is in match with a large seam of a double-seam adhering tool; meanwhile, the glue coats the outer wall of the embedded part; the inner wall of the embedded part is in match with a small seam of the double-seam adhering tool to finish the adhering of the spatial reflector and the embedded part; the large seam and the small seam of the double-seam adhering tool are processed based on the same reference, so that the coaxiality of the two seams can be ensured, and the uniformity of the glue layer thickness can be greatly improved; the glue layer is uniform in thickness; the residual stress is small after the solidifying of the glue layer; therefore, the surface figure accuracy of the spatial reflector can be fully ensured. The method is simple and reliable to operate.

Description

technical field [0001] The invention relates to the technical field of space optical remote sensing, in particular to a method for gluing a space reflector with double seams. Background technique [0002] The surface shape accuracy requirement of the space mirror 1 is very high, and its surface shape accuracy directly affects the imaging quality of the space camera. The space reflector 1 is usually made of glass or ceramic material, and the characteristics of the material make the space reflector 1 unable to be threaded, so that the thread cannot be used to connect and fix the inlay 5 . The space mirror 1 and the inlay 5 are usually connected by epoxy resin. However, due to the uneven thickness of the adhesive layer 2 bonded between the space mirror 1 and the inlay 5, the space mirror 1 Greater stress is generated between the mosaic 5 and the surface shape accuracy of the space mirror 1, thereby reducing the imaging quality of the space camera. [0003] At present, the glu...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G02B7/182
CPCG02B7/182
Inventor 鲍赫魏君成杨之音袁野庞新源
Owner CHANGCHUN INST OF OPTICS FINE MECHANICS & PHYSICS CHINESE ACAD OF SCI
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