A large-load flexible and controllable landing buffer device and method

A buffer device and flexible technology, applied in the landing buffer field of aerospace vehicles, can solve the problems of small buffer weight, uncontrollable buffer process, poor adaptability to landing environment, etc., and achieve the effect of improving buffer capacity and reliability

Active Publication Date: 2019-01-15
BEIJING RES INST OF SPATIAL MECHANICAL & ELECTRICAL TECH
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  • Application Information

AI Technical Summary

Problems solved by technology

[0004] Aiming at the disadvantages of the existing domestic traditional airbag cushioning devices, such as small cushioning weight, uncontrollable cushioning process, and poor adaptability to the landing environment, the present invention provides a large-load flexible and controllable landing cushioning device and method, realizing a new generation of multi-purpose The landing buffer of the spacecraft's return capsule, and the control of the buffering process, can better adapt to the landing environment

Method used

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  • A large-load flexible and controllable landing buffer device and method
  • A large-load flexible and controllable landing buffer device and method
  • A large-load flexible and controllable landing buffer device and method

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Embodiment Construction

[0051] The basic idea of ​​the present invention is to propose a large-load flexible and controllable landing buffer device and method, which can be realized by the combination of a pressure cylinder group, an addition and exhaust valve, an electric explosion valve, a filter, a pressure monitoring device, a shunt, and a buffer airbag The landing buffer for the return cabin of a new generation of multi-purpose spacecraft has reached a buffer capacity of 7000kg; it has realized the switching of the landing mode of the return cabin in the land and sea landing environments, and improved the airbag landing buffer device to the plateau. Adaptability under air pressure environment and slope environment conditions; realized the active control of the buffer process, which can control the landing buffer overload within the required range; realized the anti-rollover and overturning functions of the return cabin during landing.

[0052] The present invention will be described in detail below ...

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Abstract

The invention discloses a large-load flexibility-controllable landing buffering device and method. Due to the combination of an air bottle set, charging and exhausting valves, electric explosion valves, filters, pressure monitoring devices, diverters and buffering air bags, landing buffering of a new-generation multi-purpose airship re-entry capsule is achieved, and the buffering capability reaches the magnitude of 7000 kg; switching of the landing work modes of the re-entry capsule in two landing environments is achieved, and adaptability of the air bag landing buffering device to the highland low-pressure environment condition and the slope environment condition is improved; initiative control over the buffering process is achieved, and the landing buffering overload can be controlled in the required range; and a rollover preventing function and a toppling preventing function of the re-entry capsule in the landing process are achieved.

Description

Technical field [0001] The invention relates to a large-load flexible and controllable landing buffer device and method, belonging to the technical field of landing buffers for aerospace vehicles. Background technique [0002] When the new generation multi-purpose spacecraft is landing on the return module, it is necessary to carry out landing buffer protection for the return module to reduce the landing overload of the return module and protect the safety of the astronauts. Therefore, the landing buffer device of the return cabin of the multi-purpose spacecraft is one of the key technologies. [0003] Commonly used landing buffer devices include reverse thrust rockets, landing legs, and buffer airbags. Reverse rockets and landing legs have been more developed for the landing buffer of the return module of the new generation of multi-purpose spacecraft, so they are not suitable for the landing buffer of the return module of the new generation of multi-purpose spacecraft. Because ...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B64G1/62
CPCB64G1/62
Inventor 徐诚方竺梅芳雷江利廖航刘靖雷王飞邓黎
Owner BEIJING RES INST OF SPATIAL MECHANICAL & ELECTRICAL TECH
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