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Carrier rocket external camera mounting structure

A carrier rocket and installation structure technology, which is applied in transportation and packaging, aerospace safety/emergency devices, space vehicle heat protection devices, etc., can solve problems such as inconvenient installation and easy damage of cameras, and achieve convenient installation and improved heat insulation effect , good protective effect

Inactive Publication Date: 2021-06-25
BEIJING XINGJI RONGYAO SPACE TECH CO LTD +1
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] Therefore, the technical problem to be solved in the present invention is to overcome the disadvantages of easy damage and inconvenient installation of the external camera of the launch vehicle in the prior art, thereby providing a mounting structure for the external camera of the launch vehicle that is not easily damaged, and is firmly and conveniently installed.

Method used

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  • Carrier rocket external camera mounting structure
  • Carrier rocket external camera mounting structure
  • Carrier rocket external camera mounting structure

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Embodiment Construction

[0029] The technical solutions of the present invention will be clearly and completely described below in conjunction with the accompanying drawings. Apparently, the described embodiments are some of the embodiments of the present invention, but not all of them. Based on the embodiments of the present invention, all other embodiments obtained by persons of ordinary skill in the art without making creative efforts belong to the protection scope of the present invention.

[0030] In addition, the technical features involved in the different embodiments of the present invention described below may be combined with each other as long as there is no conflict with each other.

[0031] like Figures 1 to 5 A specific implementation of the installation structure of the external camera of the launch vehicle shown, the installation structure of the external camera is installed on the outer wall of the second-stage rear section of the launch vehicle, the outer surface of the second-stage...

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Abstract

The invention relates to the technical field of camera mounting and fixing, in particular to a carrier rocket external camera mounting structure which comprises a mounting plate, a first mounting surface and a second mounting surface, the first mounting surface is fixed to the outer wall of a cabin of a carrier rocket in a matched mode, the second mounting surface is fixed to a camera in a matched mode, and a third mounting hole is formed in the cabin, the cable of the camera penetrates through the third mounting hole and is electrically connected with equipment in the cabin body; and a shell which is arranged on the periphery of the mounting plate in a covering manner and covers the camera. According to the carrier rocket external camera installation structure, the camera is not prone to being damaged, and installation is firm and convenient.

Description

technical field [0001] The invention relates to the technical field of camera installation and fixing, in particular to an installation structure for an external camera of a launch vehicle. Background technique [0002] During the entire flight process of the launch vehicle from launching to entering space, it has to go through severe force and thermal environment tests. After launch, the speed of the launch vehicle can reach several kilometers per second. When the high-speed moving rocket body passes through the dense atmosphere, it is not only affected by aerodynamic force, but also generates a lot of heat due to intense friction with the air. As a sensitive electrical device, the camera has strict requirements on the installation and use environment. Direct exposure to the external environment will cause damage to the camera and affect its use. Contents of the invention [0003] Therefore, the technical problem to be solved in the present invention is to overcome the d...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64G1/66B64G1/58
CPCB64G1/66B64G1/58
Inventor 彭小波崔深山张骁飞黄至诚刘鹏程杨小顺
Owner BEIJING XINGJI RONGYAO SPACE TECH CO LTD