|국가/구분||United States(US) Patent 등록|
|미국특허분류(USC)||244/012; 054/055; 054/053.B|
|발명자 / 주소|
|출원인 / 주소|
|대리인 / 주소||
|인용정보||피인용 횟수 : 6 인용 특허 : 52|
An integrated and/or modular high-speed aircraft and method of design and manufacture. The aircraft can have a supersonic or near-sonic cruise Mach number. In one embodiment, the aircraft can include an aft body integrated with a delta wing and a rearwardly tapering fuselage to define a smooth forward-to-rear area distribution. A propulsion system, including an engine, inlet, and exhaust nozzle can be integrated into the aft body to be at least partially hidden behind the wing. In one embodiment, the entrance of the inlet can be positioned beneath the wi...
1. An aircraft, comprising:a fuselage portion configured to carry a payload; a wing portion depending from the fuselage portion, the wing portion having a forward region with a leading edge and an aft region with a trailing edge, the wing portion further having an upper surface and a lower surface; a propulsion system mounted to the wing portion, the propulsion system having at least one generally fixed inlet aperture projecting upwardly from the wing portion upper surface and aft of the wing leading edge, at least one engine positioned aft of the at lea...