[특허]Equipment carrying remote controlled aircraft

[미국특허] Equipment carrying remote controlled aircraft 원문보기

IPC분류정보
국가/구분	United States(US) Patent 등록
국제특허분류(IPC7판)	B64C-029/00
출원번호	US-0855254 (1992-03-23)
우선권정보	ES-0003414 (1989-10-10)
발명자 / 주소	Del Campo Aguilera Juan (Avenida de Baviera 4. 28028 Madrid ESX)
인용정보	피인용 횟수 : 44 인용 특허 : 0

초록 ▼

It works like a helicopter in vertical flight or like an airplane in horizontal flight, being able to land accurately on a small area. It is equipped with a rotor, a couple of wings fitted with ailerons and other control surfaces actuated differentially, with support wheels at their ends. It has a vertical stabilizer at the end of which there is a wheel. It has a horizontal stabilizer with elevators that are actuated simultaneously or differentially. It incorporates a propeller ahead of the rotor.

대표청구항 ▼

An equipment carrying, remote controlled aircraft designed to operate like a helicopter in vertical flight and like an airplane in horizontal flight, and which can also land accurately on a small area; said aircraft including a fuselage: a variable pitch propeller and a helicopter type, counter-rotating rotor fitted with hinged blades mounted near the front of said fuselage, said rotor acting as a thruster propeller during horizontal flight; engine means for driving said propeller and said rotor including throttle means for controlling the same; a set of sweptback wings spaced further back on said fuselage from said propeller and rotor extending laterally outwardly of said fuselage and forming a large dihedral angle therewith and with a horizontal plane while the airplane is in horizontal flight; ailerons on said wings and other control surfaces which can be actuated differentially for controlling the direction of flight of said aircraft; wheels to support said aircraft upon a landing area mounted at the end of said wings; a vertical stabilizer of large span similar to that of said wings having a third wheel cooperating with said wheels on said wings and set in such a way that all three of said wheels are positioned at the corners of an imaginary equilateral triangle, whose apothem is equal to or larger than the height of a center of gravity of said aircraft over a landing surface, while landing, said wheels being placed on a plane normal to the longitudinal axis of the aircraft and centered in relation to said axis; elevators between said wings and said rotor that can be actuated simultaneously or differentially; a ventral cupola for housing observation and detection instruments; an electric motor powered winch inside said fuselage for releasing and rewinding a cable adapted to be fastened to a point on the ground to improve the precision of a landing, said cable protruding through a guide cone and a hole at the back of said fuselage; variable power means for driving said winch to release and rewind said cable without the necessity of actuating said combination of said propeller and rotor or said throttle means of said engine; a generator driven by said engine means actuating said electrical motor of said winch so that an increment of power administered to said winch will be subtracted from engine power destined to provide lift for said aircraft in a vertical position during landing for obtaining a greater and more rapid control effect on the variation of sinking speed when the generator is only connected to said electric motor of said winch during landing.

이 특허를 인용한 특허 (44) 인용/피인용 타임라인 분석

Johnson,Samuel A., Aerial robot.
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Johnson, Samuel Alan; Burkard, William Dennis; Mimlitch, III, Robert H.; Mimlitch, Jr., Robert Henry; Norman, David Anthony, Aerial robot with dispensable conductive filament.
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Barrett, Ronald M.; Honea, Robert B.; Bramlette, Richard B., Aerial vehicle.
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Barrett, Ronald M.; Honea, Robert B.; Bramlette, Richard B., Aerial vehicles and methods of use.
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David Barry Ingram GB, Aircraft.
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Hothi, Inderpal Singh; Stoackley, Jon Robert; Stoackley, Steven John, Aircraft.
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Darrow, Jr., David A.; Bertolotti, Fabio P.; Sbabo, Thomas L.; D'Anna, Frank P., De-rotation system for a counter-rotating, coaxial rotor hub shaft fairing.
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Darrow, Jr., David A.; D'Anna, Frank P.; Sbabo, Thomas L., De-rotation system suitable for use with a shaft fairing system.
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Lawrence, John M., Dual rotor vertical takeoff and landing rotorcraft.
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Parks, Robert, Ducted spinner for engine cooling.
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Blevio, Sr., Henry L., Five-piece fuselage, including engines and wings, for a aerodynamically stable, high-lift, vertical takeoff aircraft.
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Barrett, Ronald M.; Bramlette, Richard B.; Honea, Robert B., Flat-stock aerial vehicles and methods of use.
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Kawaguchi, Hiroshi, Flying object.
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Fisher, Christopher Eugene; Mukherjee, Jason Sidharthadev; Lott, William Arden, Geographic survey system for vertical take-off and landing (VTOL) unmanned aerial vehicles (UAVs).
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Claridge, Jerry Daniel; Manning, Charles Fischer, High speed multi-rotor vertical takeoff and landing aircraft.
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Parks,Robert, Inbound transition control for a tail-sitting vertical take off and landing aircraft.
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McDonnell William R., Landing and take-off assembly for vertical take-off and landing and horizontal flight aircraft.
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Sirohi, Jayant; Lauder, Timothy Fred, Magnetic de-rotation system for a shaft fairing system.
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Kinsey, Lloyd E.; Kranking, Patrick, Methods and apparatus for transforming unmanned aerial vehicle.
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Reynolds, John; Young, Eric P.; Wurts, Joseph; Knutson, Eric, Miniature vertical takeoff and landing aircraft.
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Lauder, Timothy Fred, Planetary de-rotation system for a shaft fairing system.
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Lauder, Timothy Fred, Planetary de-rotation system for a shaft fairing system.
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Howard, John V., Remotely controlled co-axial rotorcraft for heavy-lift aerial-crane operations.
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Howard, John V., Remotely controlled co-axial rotorcraft for heavy-lift aerial-crane operations.
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Bertolotti, Fabio P.; Scott, Mark W.; Wake, Brian E.; Egolf, T. Alan; McCormick, Duane C.; Usta, Ebru; Ochs, Stuart S., Rotor hub fairing system for a counter-rotating, coaxial rotor system.
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Bertolotti,Fabio P.; Scott,Mark W.; Wake,Brian E.; Egolf,T. Alan; McCormick,Duane C., Rotor hub fairing system for a counter-rotating, coaxial rotor system.
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Fisher, Christopher Eugene; Mukherjee, Jason Sidharthadev; Lott, William Arden; Aagaard, Eric James, Survey migration system for vertical take-off and landing (VTOL) unmanned aerial vehicles (UAVS).
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Parks,Robert, System and method for controlling a roll rate of a torsionally-disconnected freewing aircraft.
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Parks,Robert; Led��,Jean Charles; Drela,Mark, System and method for controlling engine RPM of a ducted fan aircraft.
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Paduano, James Donald; Dahlstrand, Paul Nils; Wissler, John Brooke; Woodworth, Adam, System, apparatus and method for long endurance vertical takeoff and landing vehicle.
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Paduano, James Donald; Dahlstrand, Paul Nils; Wissler, John Brooke; Woodworth, Adam, System, apparatus and method for long endurance vertical takeoff and landing vehicle.
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Cherepinsky, Igor; Sane, Harshad S., Tail-sitter flight management system.
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Karem, Abe, Tilt outboard wing for tilt rotor aircraft.
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Chan, Keen Ian, Unmanned aerial vehicle.
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Chan, Keen Ian, Unmanned aerial vehicle.
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Johnson, Jonathon Thomas; Johnson, Elizabeth V. M., VTOL symmetric airfoil fuselage of fixed wing design.
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Alber, Mark R., Vertical take-off and landing aircraft with variable wing geometry.
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Taylor, Dana J.; Tokumaru, Phillip T.; Hibbs, Bart Dean; Parks, William Martin; Ganzer, David Wayne; King, Joseph Frederick, Vertical takeoff and landing (VTOL) air vehicle.
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Taylor, Dana J.; Tokumaru, Phillip T.; Hibbs, Bart Dean; Parks, William Martin; Ganzer, David Wayne; King, Joseph Frederick, Vertical takeoff and landing (VTOL) air vehicle.
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Taylor, Dana J.; Tokumaru, Phillip T.; Hibbs, Bart Dean; Parks, William Martin; Ganzer, David Wayne; King, Joseph Frederick, Vertical takeoff and landing (VTOL) air vehicle.
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Creasman, Son F., Vertical takeoff and landing (VTOL) unmanned aerial vehicle (UAV).
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Sanders, II, Stanley Gordon, Vertical takeoff and landing aircraft.
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Patrick John Muldoon, Vertical/short take-off and landing aircraft.
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Parks, Robert; Ledé, Jean-Charles, Vibration isolation engine mount system and method for ducted fans.
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IPC	Description
A	생활필수품
A62	인명구조; 소방(사다리 E06C)
A62B	인명구조용의 기구, 장치 또는 방법(특히 의료용에 사용되는 밸브 A61M 39/00; 특히 물에서 쓰이는 인명구조 장치 또는 방법 B63C 9/00; 잠수장비 B63C 11/00; 특히 항공기에 쓰는 것, 예. 낙하산, 투출좌석 B64D; 특히 광산에서 쓰이는 구조장치 E21F 11/00)
A62B-1/08	.. 윈치 또는 풀리에 제동기구가 있는 것

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[미국특허] Equipment carrying remote controlled aircraft 원문보기