[특허]Unmanned vertical take-off and landing, horizontal cruise, air vehicle

Unmanned vertical take-off and landing, horizontal cruise, air vehicle 원문보기

IPC분류정보
국가/구분	United States(US) Patent 등록
국제특허분류(IPC7판)	B64C-027/22 B64C-029/02
출원번호	US-0997007 (1992-12-28)
발명자 / 주소	Ebbert Marvin D. (San Diego CA) Gustin Russell G. (Jamul CA) Horbett Edward G. (San Diego CA) Edwards Jack J. (El Cajon CA) Adcock Clifton L. (San Diego CA)
출원인 / 주소	Hughes Missile Systems Company (Los Angeles CA 02)
인용정보	피인용 횟수 : 63 인용 특허 : 0

초록 ▼

An unmanned air vehicle capable of vertical take-off and landing, hovering and high-speed horizontal cruise flight. A forward centerbody houses an engine and carries a single rotor assembly having a plurality of propellers lying in a plane substantially perpendicular to the centerline of the forward centerbody. A coaxial aft centerbody is secured to the aft end of the forward centerbody and typically houses the vehicle avionics. A plurality of stators extend outwardly of the aft centerbody, in a plane substantially parallel to the propellers. A single toroidal duct surrounds the rotor assembly and the stators and is secured to the stators. A plurality of movable control vanes are secured between the duct and aft centerbody aft of the stators. A flight control system, typically housed in the aft centerbody, controls the engine and the vanes to cause the vehicle to selectively move upwardly, downwardly, hover or translate to forward, horizontal, motion with the rotor in a plane within 80°of vertical. A sensor, cargo, or other payload may be carried at the forward end of the forward centerbody, extending well in front of the duct. The vehicle is highly maneuverable, light weight and safe for operation from a small area due to the ducted rotor.

대표청구항 ▼

An unmanned vertical take-off and landing, horizontal high-speed cruise, air vehicle which comprises: a forward centerbody; an engine housed within said forward centerbody; a single rotor assembly mounted on said forward centerbody and connected to said engine for rotation thereby; a plurality of spaced propellers extending outwardly from the rotor assembly; an aft centerbody having a forward end secured to an aft end of said forward centerbody, said forward and aft centerbodies being collinear and lying substantially along a vehicle centerline; a plurality of stators extending outwardly of said aft centerbody; a single toroidal duct assembly surrounding said rotor assembly and stators and secured to said stators; a plurality of control vanes extending between said duct and said aft centerbody aft of said stators; and flight control means for controlling said engine and control vanes to selectively cause the vehicle to move upwardly and downwardly with said rotor in a generally horizontal plane and to move horizontally with said rotor in a pane about 50 to 80 degrees to the horizontal.

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A62B-1/08	.. 윈치 또는 풀리에 제동기구가 있는 것

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Unmanned vertical take-off and landing, horizontal cruise, air vehicle 원문보기

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Unmanned vertical take-off and landing, horizontal cruise, air vehicle 원문보기

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