To provide launch tubes and canisters, report-suppressing launch tubes, and sabots, for an unmanned aerial vehicle (UAV).SOLUTION: An unmanned aerial vehicle (UAV) launch tube (100) comprises at least one layer of a prepreg substrate disposed about an aperture (106) to form a tube, a sabot (110) disposed in an interior of the tube (100) and having a first clasp tab (126), and a clasp (124) detachably coupled to the first clasp tab and contacting an inner circumferential wall (102) of the tube (100), where the clasp (124) is rotationally constrained by the inner circumferential wall (102) and the first clasp tab (126).SELECTED DRAWING: Figure 1
【課題】無人航空機(UAV)用の発射管とキャニスタ、静音型発射管、および発射筒を提供する。【解決手段】無人航空機(UAV)の発射管(100)であって、開口(106)の周りに設けられ管を形成するプリプレグ基材の少なくとも1つの層と、前記管(100)の内部に配置されて、第1止め具タブ(126)を有する発射筒(110)と、前記第1止め具タブに脱着可能に連結されて、前記管(100)の内周壁(102)に接している止め具(124)とを具え、前記止め具(124)が、前記内周壁(102)および前記第1止め具タブ(126)により回転拘束されている。【選択図】図1
SYSTEM FOR DETACHABLY COUPLING UNMANNED AERIAL VEHICLE WITHIN LAUNCH TUBE
発射管内で無人航空機を脱着可能に連結するシステム
2020-12-24
Patent
Electronic Resource
Japanese
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