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Semi-enclosed split manned lunar rover

A split-type, lunar rover technology, applied in the field of manned moon landing, can solve the problems of not much content and few achievements of independent innovation, and achieve the effect of reducing the envelope space and avoiding damage

Active Publication Date: 2016-08-24
SHANGHAI AEROSPACE SYST ENG INST
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0005] At present, the research on manned lunar vehicles in China is still in its infancy, and it is still in the stage of tracking and research on the Apollo manned lunar vehicles and NASA's new concept manned lunar vehicles. The concept plan is mainly a wheeled open manned lunar vehicle. , the content of independent innovation is not much, and the published results are also few

Method used

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  • Semi-enclosed split manned lunar rover
  • Semi-enclosed split manned lunar rover
  • Semi-enclosed split manned lunar rover

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Embodiment Construction

[0024] The following will combine Figure 1 to Figure 5 The semi-enclosed split-type manned lunar vehicle provided by the present invention is described in detail, which is an optional embodiment of the present invention. It can be considered that those skilled in the art can make it without changing the spirit and content of the present invention. Make revisions and polish.

[0025] Please refer to Figure 1 to Figure 5 , the present embodiment provides a semi-enclosed split-type manned lunar vehicle, including a vehicle body structure, the vehicle body structure includes an open structure of the middle chassis 1, the front chassis 2 and the front chassis 1 located at both ends of the middle chassis 1 The rear chassis 3 and the box structures 19 and 16 detachably mounted on the front chassis 2 and the rear chassis 3, the front chassis 2 and the rear chassis 3 are all connected to the middle chassis 1 through a rotating shaft It is connected by rotation and can be folded on ...

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Abstract

The invention provides a semi-closed split manned lunar vehicle. The semi-closed split manned lunar vehicle comprises a vehicle body structure; the vehicle body structure comprises a middle chasse of an open structure, a front chassis and a rear chassis both arranged at the two ends of the middle chassis, and box structures detachably mounted on the front chassis and the rear chassis; the front chassis and the rear chassis both are rotatably connected with the middle chassis by use of rotating shafts, and can be folded on the middle chassis by being turned; the lunar vehicle further comprises a cambered flexible solar cell array serving as an upper cover structure; the cambered flexible solar cell array can be folded on the vehicle body structure; after the cambered flexible solar cell array is unfolded and mounted, the size and the position of the cambered flexible solar cell array at least cover the upper side of the middle chassis; at least a power controller and a storage battery pack are arranged in the box structure on the front chassis; the cambered flexible solar cell array is connected with the storage battery pack by use of the power controller.

Description

technical field [0001] The invention relates to the technical field of manned lunar landing, in particular to a semi-enclosed split type manned lunar vehicle. Background technique [0002] The manned lunar vehicle is responsible for expanding the range of activities of astronauts, transporting scientific payloads, sampling tools and various lunar samples, and ensuring the safe and efficient completion of lunar surface exploration by astronauts. Therefore, the manned lunar rover needs to have good lunar surface mobility, human-computer interaction capabilities, loading and transportation capabilities, and safety assurance capabilities. [0003] The United States achieved manned moon landings in the early 1970s. At the beginning of the 21st century, the United States proposed a "return to the moon plan", planning to manned moon landings again and establishing a lunar base. According to the needs of manned lunar vehicles in different mission stages of manned lunar landing, NAS...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B64G1/16
Inventor 邱宝贵曾令斌胡震宇丁亮亮袁卫文肖杰李毅姬鸣罗小桃张晓伟贾巍
Owner SHANGHAI AEROSPACE SYST ENG INST
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