发明名称 Aircraft capable of takeoff/landing via the fuselage thereof, and takeoff/landing system for the aircraft
摘要 The aircraft capable of takeoff/landing via the fuselage thereof and the takeoff/landing system of the aircraft according to the present invention are configured such that multiple takeoff/landing rollers are arranged in a sliding direction such that the aircraft fuselage having a landing surface formed at the bottom thereof can safely land and slide in a sliding direction, thus enabling the aircraft fuselage to contact a running surface and takeoff/land without separate landing gear. Thus, not only can the weight of the aircraft be reduced, but the fuel consumption of the aircraft can be reduced as well, the useful space in the aircraft can be broadened, the length of the runway can be shortened due to the frictional force generated by the takeoff/landing device, and the safety during the takeoff/landing of the aircraft can be improved.
申请公布号 US9302768(B2) 申请公布日期 2016.04.05
申请号 US201214415438 申请日期 2012.07.17
申请人 Donggyu Yang 发明人 Yang Donggyu
分类号 B64C25/32;B64C25/04;B64F1/02;B64F1/04;B64C25/14;B64C25/62 主分类号 B64C25/32
代理机构 代理人
主权项 1. A fuselage takeoff and landing enabled aircraft, wherein a landing surface is formed at a bottom surface of the aircraft fuselage such that the aircraft fuselage is placed on a virtual runway surface to allow takeoff and landing, wherein a rail catcher assembly docked with a guide rail provided on the virtual runway surface to support the aircraft fuselage to maintain the center line of movement is provided on the aircraft fuselage.
地址 Seoul KR