PROBLEM TO BE SOLVED: To provide a launch tube for an unmanned aerial vehicle UAV, a canister, a silent launch tube, and a launch cylinder.SOLUTION: A launch tube 100 of an unmanned aerial vehicle UAV includes: at least one layer of a prepreg substrate disposed around an aperture 106 to form a tube; a launch cylinder 110 disposed in an interior of the launch 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 launch tube 100. 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、発射管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、第1止め具タブに脱着可能に連結されて、発射管100の内周壁102に接している止め具124とを具え、止め具124が、内周壁102および第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
2018-03-15
Patent
Electronic Resource
Japanese
IPC: | B64F GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT , Boden- oder Flugzeugträgerdeckeinrichtungen besonders ausgebildet für die Verwendung in Verbindung mit Luftfahrzeugen / F41F APPARATUS FOR LAUNCHING PROJECTILES OR MISSILES FROM BARRELS, e.g. CANNONS , Vorrichtungen zum Abschießen von Geschossen oder Flugkörpern aus Rohren, z.B. Geschütze |
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