Solar array installation structure
An installation structure and solar array technology, which is applied in the field of satellite solar array installation methods, can solve the problems of solar array installation structure, such as large mass, complex structure form, and poor adaptability of the position of the pressing point of the solar array, so as to achieve light weight and good application prospects Broad, Simple Effects
Active Publication Date: 2017-11-24
SHANGHAI SATELLITE ENG INST
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Problems solved by technology
[0008] In order to solve the deficiencies in the prior art, such as the large mass of the solar array installation structure, the complex structure, and the poor adaptability to the position of the pressing point of the solar array, the purpose of the present invention is to provide a solar array installation structure
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[0022] In order to make the technical means, creative features, objectives and effects of the present invention easy to understand, the present invention will be further explained below in conjunction with specific embodiments.
[0023] Such as figure 1 As shown, this specific embodiment adopts the following technical solutions: a solar array installation structure, including a compression seat 1, an upper hinge at the root 2, a mounting beam 3, and a lower hinge 4 at the root, the compression seat 1 and the The mounting beam 3 is glued together to connect with the satellite star body, and the root upper hinge 2 and the root lower hinge 4 are both connected to the satellite star body by glue connection.
[0024] Such as figure 2 As shown, the material of the pressing seat 1 is 2A12T4 aluminum alloy, which is connected to the mounting beam 3 by Redux420 adhesive, and the position and number of the pressing seat 1 are adjustable according to requirements.
[0025] Such as image 3 As ...
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The invention discloses a novel solar array mounting structure. The novel solar array mounting structure comprises a compressing seat, an upper root hinge, a mounting beam and a lower root hinge; the compressing seat is integrally cemented with the mounting beam and is also connected with a satellite body; the upper root hinge and the lower root hinge are both connected with the satellite body by cementing. With the adoption of the novel solar array mounting structure, the problems like complex structure form of the solar array mounting frame, large mass, and poor adaption to the positions of compressing points of a solar array can be solved; the novel solar array mounting structure has the beneficial effects that the structure is simple, the mass is light, the mounting is convenient, and the adaption is high.
Description
Technical field [0001] The invention relates to an installation method of a satellite solar array, in particular to a solar array installation structure applied to a satellite. Background technique [0002] The installation structure of the solar array provides the installation surface for the solar array to withstand the impact of the explosion of the solar array pyrotechnics. With the development of aerospace technology, solar arrays have increasingly higher and diversified structural installation requirements. [0003] Before the application of the present invention, the solar array installation structure adopts the following methods: [0004] One is the solar array frame structure, the solar array is directly connected with the frame, its mass is heavier, and the frame structure is more complicated. [0005] One is that the solar array is directly connected to the side plate, and the internal connection of the plate needs to be reinforced, and the structure of the side plate is m...
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IPC IPC(8): H02S20/00
CPCY02E10/50
Inventor 顾志悦满孝颖王舒楠吕凯
Owner SHANGHAI SATELLITE ENG INST