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Magic cube type modularization satellite

A modular and block technology, applied in the field of modular satellites, can solve the problems of not being able to give full play to the speed, flexibility, and adaptability of micro-spacecraft, and achieve on-orbit maintenance, reduce thermal control measures, and realize functional expansion. Effect

Active Publication Date: 2017-03-22
AEROSPACE DONGFANGHONG DEV LTD
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AI Technical Summary

Problems solved by technology

[0002] Since the main feature of micro-spacecraft is a wide variety of payload systems and flexible and diverse satellite mission requirements, the traditional spacecraft design method is still used, and the payload system must adapt to the constraints of the platform, which cannot give full play to the fast, flexible, and Adaptable Features

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  • Magic cube type modularization satellite
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  • Magic cube type modularization satellite

Examples

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Embodiment Construction

[0018] The preferred embodiments of the present invention will be further described in detail below in conjunction with the accompanying drawings.

[0019] This example provides a modular satellite in magic mode, including the central shaft and N 3 -(N-2) 3 a Rubik's cube, N is a natural number, N≥2, and each Rubik's cube is provided with an independent functional module of the spacecraft; The inner surface of the face center cube is provided with a first arc groove, and the face center cube is rotationally connected with the central shaft through the first arc groove; the inner surface of the face center cube is provided with There is a second arc surface groove, and the face center cube is slidably installed around the surface center cube through the second arc surface groove; the inner surface of the corner cube is provided with a third arc surface concave groove, and the corner cube is slidably installed at the corner position between the center cubes of the facets throu...

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Abstract

The invention provides a magic cube type modularization satellite which comprises a center rotating shaft and N<3>-(N-2)<3> magic cube blocks, and N is larger than or equal to 2. Each magic cube block is provided with an independent spacecraft functional module. The magic cube blocks comprise the face center magic cube blocks, the edge face center magic cube blocks and the corner magic cube blocks. First arc surface grooves are formed in the inner side faces of the face center magic cube blocks. The face center magic cube blocks are rotatably connected with the center rotating shaft through the first arc surface grooves. Second arc surface grooves are formed in the inner side faces of the edge face center magic cube blocks. The edge face center magic cube blocks are arranged around the face center magic cube blocks in a sliding mode through the second arc surface grooves. Third arc surface grooves are formed in the inner side faces of the corner magic cube blocks. The corner magic cube blocks are arranged on the corners among the edge face center magic cube blocks in a sliding mode through the third arc surface grooves. By means of modularization design, the combinations and replacement of modules with different functions are achieved, and the orientations of the magic cube block surfaces can be configured adaptively.

Description

technical field [0001] The invention relates to a modular satellite, in particular to a magic modular satellite. Background technique [0002] Since the main characteristics of micro-spacecraft are a wide variety of payload systems and flexible and diverse satellite mission requirements, the traditional spacecraft design method is still used, and the payload system must adapt to the constraints of the platform, which cannot give full play to the fast, flexible, and Features of strong adaptability. For micro-spacecraft, modular satellites are of great significance in the fields of how to achieve rapid construction and recovery of space systems, on-orbit maintenance and function expansion of satellites, and tactical satellites that support rapid response to ground information. Contents of the invention [0003] The technical problem to be solved by the present invention is to provide a flexible and effective miniaturized modular satellite, and to realize the rational config...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64G1/10
CPCB64G1/10
Inventor 陈琦高鸽孙日思唐心春韩飞李春
Owner AEROSPACE DONGFANGHONG DEV LTD
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