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Patent Searching and Data


Title:
LAUNCH VEHICLE AND MULTI-STAGE PNEUMATIC SUPPORT CYLINDER FOR RECOVERING LAUNCH VEHICLE
Document Type and Number:
WIPO Patent Application WO/2020/151718
Kind Code:
A1
Abstract:
Disclosed are a launch vehicle and a multi-stage pneumatic support cylinder for recovering a launch vehicle. The multi-stage pneumatic support cylinder comprises: a cylinder tube (1), comprising a main cylinder tube (10) and a plurality of sub-cylinder tubes (11) nested together and provided in the main cylinder tube (10), the main cylinder tube (10) forming a fixed portion of the cylinder tube (1), the plurality of sub-cylinder tubes (11) forming a telescopic portion of the cylinder tube (1); a gas generator (2) provided inside the main cylinder tube (10); and a buffering device (3) provided on the telescopic portion. The multi-stage pneumatic support cylinder for recovering a launch vehicle has the advantages of safety, reliability, and light overall weight, and can meet, during use, the requirements of quick opening, supporting, shock absorption, stabilization and tilt correction of a rocket landing device.

Inventors:
ZHANG YANJIE (CN)
ZHAO LIQIAO (CN)
ZHANG YU (CN)
WU XUE (CN)
LI YONGJUN (CN)
HAN ZHAOYANG (CN)
ZHANG YAMIN (CN)
NAN TIELING (CN)
Application Number:
PCT/CN2020/073597
Publication Date:
July 30, 2020
Filing Date:
January 21, 2020
Export Citation:
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Assignee:
LANDSPACE SCIENCE & TECH CO LTD (CN)
International Classes:
F15B15/16; F15B15/22; F15B15/24
Foreign References:
CN109764025A2019-05-17
CN209892546U2020-01-03
CN109229429A2019-01-18
CN205876852U2017-01-11
CN208278353U2018-12-25
CN105240343A2016-01-13
JP2002323012A2002-11-08
Attorney, Agent or Firm:
BEIJING BEIHUI LAW FIRM (CN)
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