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Microsatellite quality characteristic bidirectional testing equipment and method

A technology for quality characteristics and testing equipment, applied in the testing of mechanical equipment, machine/structural components, static/dynamic balance testing, etc., to achieve the effect of reducing volume and mass, reducing impact, and improving test accuracy

Active Publication Date: 2011-02-16
AEROSPACE DONGFANGHONG SATELLITE
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  • Abstract
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  • Claims
  • Application Information

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Problems solved by technology

[0006] The technical solution problem of the present invention is: to overcome the deficiencies of the prior art, provide a kind of microsatellite high-precision quality characteristic two-way test equipment and method, solve the problem of coordinate transformation when microsatellite quality characteristic test, improve the microsatellite quality characteristic The test accuracy and test efficiency

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  • Microsatellite quality characteristic bidirectional testing equipment and method
  • Microsatellite quality characteristic bidirectional testing equipment and method
  • Microsatellite quality characteristic bidirectional testing equipment and method

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Embodiment Construction

[0035] The structure of the micro-satellite mass characteristic two-way testing equipment of the present invention is as figure 1 , figure 2 , image 3 As shown, a U-shaped symmetrical inner and outer support frame structure is adopted, and the main body of the structure is made of lightweight aluminum, including an outer support frame 1, an inner support frame 2, a deceleration mechanism 4, a docking ring 5, a counterweight section 6, a positioning mechanism 7, and eyebolt screws 9. Both the outer support frame 1 and the inner support frame 2 are U-shaped symmetrical structures, the two sides of the inner support frame 2 and the outer support frame 1 are installed and connected by the positioning mechanism 7 and the reduction mechanism 4 respectively, and the inner support frame 2 can rotate on the outer support frame 1 , the positioning mechanism 7 is used for the positioning of the inner support frame 2, and the reduction mechanism 4 is used for driving and rotating the ...

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Abstract

The invention discloses microsatellite quality characteristic bidirectional testing equipment. A U-shaped symmetrical inner and outer supporting frame structure is adopted; an inner supporting frame is driven to rotate around a rotating shaft by a speed-reducing mechanism and is easily positioned in vertical and horizontal directions through a positioning mechanism; and the problem of rapid coordinate conversion in a vertical state and a horizontal state through one-time hoisting is solved. The quality characteristic data in two states is tested through one-time hoisting and clamping in the field of microsatellites, the quality characteristic testing time is shortened, the testing efficiency and testing effect are improved, the safety and reliability of the quality characteristic testing are enhanced, and the labor intensity of personnel is greatly lightened. The microsatellite quality characteristic bidirectional testing equipment has a simple structure, is convenient to operate, and can be used for quality characteristic testing of spacecrafts and other miniature equipment.

Description

technical field [0001] The invention relates to a test device for measuring satellite quality characteristics and a method for using the device to test the quality characteristics. Background technique [0002] Through the mass characteristic test, the mass characteristic data of the satellite can be obtained, and these data include: the satellite mass M, in the star coordinate system (the origin is the center of the docking ring, the Z axis is perpendicular to the docking ring surface, points vertically upward to the star, and the X axis is horizontal In any direction, determine the Y-axis according to the right-hand rule, the position of the center of mass (X, Y, Z) in ), and measure the moment of inertia lxx, lyy, lzz. When measuring the center of mass of the satellite, first measure the center of mass of the X-axis and Y-axis in the vertical state of the satellite, and then measure the center of mass of the Z-axis in the horizontal state. The measurement sequence of sa...

Claims

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Application Information

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IPC IPC(8): F16H1/16F16H57/02G01M1/12G01M1/10F16H57/032F16H57/039
Inventor 刘江梁小峰张名毅王凤彬梁飞
Owner AEROSPACE DONGFANGHONG SATELLITE
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