무인 항공기(UAV) 발사관(100)은, 관을 형성하기 위해 개구(106) 주위에 배치된 프리프레그 기판의 적어도 하나의 레이어와, 관(100)의 내부에 배치되고 제 1 걸쇠 탭(126)을 갖는 사봇(110)과, 제 1 걸쇠 탭에 탈착가능하게 연결되고 관(100)의 내주벽(102)과 접촉하는 걸쇠(124)를 포함하고, 걸쇠(124)는 내주벽(102)과 제 1 걸쇠 탭(126)에 의해 회전가능하게 구속된다.
A method of launching an unmanned aerial vehicle (UAV) launch, comprising:restraining a sabot in a launch tube (100);introducing gas to a high-pressure side of an expandable sabot skirt (132) of a sabot (110) to break said restraint of said sabot (110) in said launch tube (100); anddriving said sabot (110) up said launch tube (100) using said gas.
SYSTEM FOR DETACHABLY COUPLING AN UNMANNED AERIAL VEHICLE WITHIN A LAUNCH TUBE
발사관 내에서 무인 항공기를 탈착가능하게 연결시키는 시스템
2021-03-03
Patent
Electronic Resource
Korean
IPC: | B64C AEROPLANES , Flugzeuge |
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