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Gravity balancing device for large-aperture space camera

A space camera and gravity balance technology, applied in the field of space remote sensing, can solve problems such as the inapplicability of large-caliber space-based space cameras, and achieve the effect of repeating tests, eliminating influences, and ensuring accuracy

Active Publication Date: 2021-03-09
CHANGCHUN INST OF OPTICS FINE MECHANICS & PHYSICS CHINESE ACAD OF SCI
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  • Abstract
  • Description
  • Claims
  • Application Information

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Problems solved by technology

[0003] At present, the commonly used gravity balance scheme for space cameras is to set multiple gravity balance points on one side of the space camera, and achieve gravity balance by unloading the deformation of the support structure. The essence of this method is to achieve gravity balance through the "over-design" of the support structure. Not suitable for large aperture space-based space cameras

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Embodiment Construction

[0025] In order to make the object, technical solution and advantages of the present invention clearer, the present invention will be further described in detail below in conjunction with the accompanying drawings. It should be understood that the specific embodiments described here are only used to explain the present invention, but not to limit the present invention.

[0026] The gravity balance device for a large-aperture camera in space provided by the present invention will be described in detail below.

[0027] figure 1 A structural diagram showing the overall structure of a large-aperture space camera gravity balance device of the present invention

[0028] Such as figure 1 As shown, it is a space large-diameter gravity balance device provided by the embodiment of the present invention, and the whole device has two left-right symmetrical structures. Including: space camera support structure 1, kinematic support structure 2, single-degree-of-freedom gravity balance de...

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Abstract

The invention provides a gravity balancing device for a large-aperture space camera. The gravity balancing device comprises a space camera supporting structure, a kinematics supporting structure, a single-degree-of-freedom gravity balancing device and a tool structure, wherein the space camera supporting structure is used for fixing an optical lens group of the large-aperture space camera; the space camera supporting structure is hinged to the tool structure through the kinematics supporting structure to unload bending moment. The single-degree-of-freedom gravity balance device is hinged to the space camera supporting structure through the adapting piece to adjust balance, the weight and bending moment of the whole machine are independently unloaded instead of unloading deformation, the single-degree-of-freedom gravity balance device and the space camera supporting structure do not interfere with each other, gravity balance of the space camera is achieved, and it is guaranteed that therelative positions of all the reflectors meet the index requirements. In addition, the gravity balancing device can eliminate the influence of a test environment on a test result, and repeated testscan be achieved.

Description

technical field [0001] The invention relates to the technical field of space remote sensing, in particular to a gravity balance device for a large-diameter space camera. Background technique [0002] Space cameras have the characteristics of no borders in sky observation and earth observation, and more comprehensive and accurate information collection. Therefore, they play a very important role in many fields such as astronomy, earth science, military applications, and civilian production. With the development of space remote sensing technology, space cameras are developing in the direction of large aperture, long focal length, and diversification, which leads to the increase in volume and quality of their supporting structures. To reduce the cost of scientific research and launch costs, the space camera structure must be lightweight designed. A high lightweight rate will lead to a reduction in the cross-sectional size of the space camera structure, which in turn will lead t...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G01C25/00H04N17/00
CPCG01C25/00H04N17/00
Inventor 安明鑫薛闯董吉洪徐抒岩
Owner CHANGCHUN INST OF OPTICS FINE MECHANICS & PHYSICS CHINESE ACAD OF SCI