To achieve improvement in cargo loading property and inspection property, and multiuse of an unmanned rotary-wing aircraft.SOLUTION: An airframe body of an unmanned rotary-wing aircraft is covered with a fiber material, a fastener 3 is provided on a surface of an airframe cover which is made of the fiber material, the fastener is opened, and a large opening is formed in the aircraft body by utilization of flexibility of the fiber material, whereby loading of a cargo 7 into an airframe, inspection of an airframe interior and part replacement can be easily performed. The cover of the fiber material, which covers the airframe, is replaced as clothes changing, and thus, heat-resistant performance, chemical-resistant performance, blade-resistant performance, waterproof performance and a design thereof is changed according to uses and use environments of the aircraft.SELECTED DRAWING: Figure 2
【課題】無人の回転翼航空機の荷物の積載性、点検性の向上、ならびに多用途化。【解決手段】回転翼航空機の機体胴体部を繊維素材で覆い、繊維素材で作られた機体被覆の表面にファスナー3を設け、ファスナーを開き繊維素材の柔軟性を利用して機体胴体部に大きな開口部をつくり機体内部への荷物7の積載、機体内部の点検、部品交換を容易に行えるようにし、機体を覆う繊維素材の被覆は服を着せ替えるように交換し機体の用途や使用環境にあわせて耐熱性能、耐薬品性能、耐刃性能、防水性能やデザインを変更する。【選択図】図2
AIRFRAME BODY COVER OF UNMANNED ROTARY-WING AIRCRAFT WITH USE OF FIBER MATERIAL AND FASTENER
繊維素材とファスナーを用いた無人の回転翼航空機の機体胴体被覆
2019-08-01
Patent
Electronic Resource
Japanese
IPC: | B64C AEROPLANES , Flugzeuge |
UNMANNED ROTARY WING AIRCRAFT, AND GAS STORAGE BODY MOUNTED ON UNMANNED ROTARY WING AIRCRAFT
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