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Defect detection method and system applied to OSR adhesive layers on surface of spacecraft

A defect detection and glue sticking technology, applied in the direction of optical testing defects/defects, instruments, measuring devices, etc., can solve the problems of eye irritation, waste of time and manpower, impossible online system, etc., to enhance accuracy and stability , The effect of reducing labor costs and improving reliability

Active Publication Date: 2018-05-04
SHANGHAI INST OF SATELLITE EQUIP
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  • Abstract
  • Description
  • Claims
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Problems solved by technology

At present, we use specific cotton swabs for piece-by-piece inspection, which is inefficient and wastes time and manpower
Different operators and the pressure of each pressing are different, resulting in different defect detection standards
At the same time, OSR has a strong reflective effect, and long-term detection of light will sting the eyes and cause harm to the human body
Although equipment such as X-ray diffraction and high-precision infrared thermal imaging cameras can detect these defects, they are expensive and cannot be used in online systems

Method used

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  • Defect detection method and system applied to OSR adhesive layers on surface of spacecraft

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Embodiment Construction

[0019] 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 changes and improvements without departing from the concept of the present invention. These all belong to the protection scope of the present invention.

[0020] Such as figure 1 As shown, the embodiment of the present invention provides a defect detection system applied to the OSR adhesive layer on the surface of the spacecraft, including a vacuum pump assembly, a pressure bag film, a sealing tape, an industrial camera and a cloth map, and the vacuum pump group includes a vacuum pump , suction pipeline and vacuum valve, the vacuum degree is not less than 0.092Mpa when working; the pressure bag film is made of polyvinyl chloride, polyethylene, polypropyle...

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Abstract

The invention discloses a defect detection system applied to OSR adhesive layers on the surface of a spacecraft. The system comprises a vacuum pump assembly, pressurizing bag film, a sealing rubber strip, an industrial camera and a cloth map, wherein the vacuum pump assembly comprises a vacuum pump, an air suction pipeline and a vacuum valve, and the vacuum degree of the vacuum pump assembly is not lower than 0.092MPa during working; and the pressurizing bag film is a film with a thickness of 40-80 microns, and the film has good translucency and is prepared from polyvinyl chloride, polyethylene, polypropylene or other resin. According to the detection system and method, OSRs at defected parts of adhesive layers sink in a vacuum pressure lamination process, elastic pieces are elastically bent through the pressure lamination on the OSRs, the surface state heights are inconsistent, and the sizes, shapes and the positions of the defected regions are reflected, so that the influences causedto the product quality can be judged, the defect detection of the adhesive layers can be rapidly and efficiently realized, the time and the labor can be substantially saved, the cost is low, and thereliability is high.

Description

technical field [0001] The invention relates to a pressure-type defect detection system and detection method, in particular to a method and system for detecting defects of an OSR adhesive layer applied to the surface of a spacecraft, and belongs to the technical field of aerospace product detection. Background technique [0002] OSR is one of the most ideal thermal control materials for long-lived satellites to adjust the temperature of the spacecraft surface through its own thermal radiation performance, namely solar absorption ratio (αs) and hemispherical emissivity (εh). The OSR structure is generally coated with an ITO layer and a metal silver film on both sides of a thin glass substrate (size 40mm*40mm, thickness <0.2mm). When in use, paste it directly on the outer heat dissipation surface of the satellite with conductive glue. In the production process, there are often "voids" in the OSR adhesive, which affects the adhesive strength of the OSR on the one hand, and ...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G01N21/88
CPCG01N21/8803G01N21/8851
Inventor 孙敬文陈砚朋张红梅任晓雯隋微微彭聪
Owner SHANGHAI INST OF SATELLITE EQUIP