[특허]Flying vehicle-launching apparatus and method

[미국특허] Flying vehicle-launching apparatus and method 원문보기

IPC분류정보
국가/구분	United States(US) Patent 등록
국제특허분류(IPC7판)	B64F-001/04 B64F-001/00 B60L-013/00
출원번호	UP-0763662 (2007-06-15)
등록번호	US-7594624 (2009-10-12)
우선권정보	JP-2003-359180(2003-10-20)
발명자 / 주소	Yamamoto, Masatada
출원인 / 주소	Central Japan Railway Company
대리인 / 주소	Burke, Margaret A.
인용정보	피인용 횟수 : 8 인용 특허 : 40

초록 ▼

A flying vehicle-launching apparatus and method for launching a winged flying vehicle by accelerating the vehicle in a predetermined direction includes a flying vehicle-supporting platform, a guide device, and a driving device. The flying vehicle-supporting platform supports the winged flying vehicle so that it can lift off therefrom. The guide device supports the flying vehicle-supporting platform across two or more separated and parallel guide ways and guides the flying vehicle-supporting platform along the guide ways. In the flying vehicle-launching method, a propulsive engine of the winged flying vehicle is started after initiating acceleration with a flying vehicle-accelerating device. The winged flying vehicle is released from the flying vehicle-accelerating device in a predetermined angle of attack that is positive to a direction of acceleration after reaching a predetermined velocity.

대표청구항 ▼

What is claimed is: 1. A flying vehicle-launching method for accelerating a winged flying vehicle in a specific direction by a flying vehicle-accelerating means, the method comprising: initiating acceleration of the winged flying vehicle by the flying vehicle-accelerating means to a predetermined velocity; starting a propulsive engine of the winged flying vehicle during acceleration; and releasing the winged flying vehicle in a condition of being tilted in a predetermined positive angle of attack to a direction of acceleration from the flying vehicle-accelerating means after being accelerated at the predetermined speed, wherein the flying vehicle-accelerating means comprises: a flying vehicle-supporting platform that supports the winged flying vehicle such that the winged flying vehicle can launch therefrom; two or more guide ways extending in parallel and separated from each other, each guide way comprising a track; a guide device comprising at least one carriage portion which travels along each track, the at least one carriage portion supporting the flying vehicle-supporting platform over the two or more guide ways and the guide device guiding the flying vehicle-supporting platform along the guide ways; and a driving device that drives the flying vehicle-supporting platform along the guide ways, wherein the driving device drives the at least one carriage portion to drive the flying vehicle supporting platform and comprises a linear motor, the linear motor comprising a stator provided along the tracks and an armature disposed on the at least one carriage portion, and wherein each carriage portion comprises two or more truck groups disposed along the traveling direction of the flying vehicle launching apparatus, the truck groups being fixed under the respective carriage portion so as to be rotatable around horizontal axes perpendicular to the traveling direction. 2. The flying vehicle-launching method of claim 1, wherein each truck group comprises a plurality of trucks. 3. The flying vehicle-launching method of claim 1, wherein the acceleration is started with the winged flying vehicle slanted in an angle of attack that is positive with respect to the direction of acceleration. 4. The flying vehicle-launching method of claim 1, wherein after the propulsive engine of the winged flying vehicle is started, a thrust from the flying vehicle-accelerating means is controlled so that the winged flying vehicle is accelerated in accordance with a predetermined acceleration pattern. 5. The flying vehicle-launching method of claim 4, wherein after initiating combustion in the propulsive engine of the winged flying vehicle, the winged flying vehicle is accelerated with the thrust from the flying vehicle acceleration means configured to be equal to a difference of an acceleration resistance of the winged flying vehicle accelerated at a predetermined acceleration and a thrust of the propulsive engine if the thrust of the propulsive engine is smaller than the acceleration resistance of the winged flying vehicle, wherein the acceleration resistance of the winged flying vehicle and the thrust of the propulsive engine act in opposite directions. 6. The flying vehicle-launching method of claim 1, wherein after acceleration, the winged flying vehicle is released by lifting of the winged flying vehicle using the flying vehicle-supporting platform as a runway. 7. The flying vehicle-launching method of claim 1, wherein after starting the propulsive engine of the winged flying vehicle, it is determined whether the propulsive engine is operating normally before releasing the winged flying vehicle from the flying vehicle-supporting platform, and if the propulsive engine is operating normally, the winged flying vehicle is released from the flying vehicle-supporting platform when reaching a predetermined speed, and if the propulsive engine is not operating normally, the flying vehicle-supporting platform is slowed to a halt with the winged flying vehicle supported thereon.

이 특허에 인용된 특허 (40) 인용/피인용 타임라인 분석

Young Manley A. (Issaquah WA), Air vehicle launching device.
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Siegel Moses (Cheltenham PA) Cahall Everett (Medford NJ) Dunning David (Bayville NJ) Hammond Joseph (Cornwells Heights PA), Aircraft launcher.
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Thorby Douglas C. (Shepperton GB2) Johnson John (Chertsey GB2), Aircraft launching techniques.
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Lipponen,Pentti, Arrangement in catapult.
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Evans, WIlliam P., Automatic control of air vehicle during catapult launch.
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Higuchi Toshiro (Yokohama JPX) Kamei Shigeki (Nishinomiya JPX) Kawaguchi Kojiro (Osaka JPX), Conveying system utilizing a linear pulse motor.
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Sakamoto Shunji (Hiroshima JPX) Hoshino Toshihiko (Hiroshima JPX), Conveyor means using linear motor.
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Martin Monkewitz (Luzern CHX), Device for the acceleration of bodies, especially a mobile catapult for flying bodies.
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Minovitch Michael A. (2832 St. George St. Los Angeles CA 90027), Electromagnetic transportation system for manned space travel.
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Yamamoto,Masatada, Flying vehicle-launching apparatus and method.
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Palmer William R. (Melbourne FL), High altitude launch platform payload launching apparatus and method.
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Palmer William R. (Melbourne FL), High altitude launch platform payload launching apparatus and method.
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Giuliani Robert L. (1456 Thurston Ave. A-1204 Honolulu HI 96822) Giuliani Mark A. (45-310 Akimala Pl. Kaneohe HI 96744) Giuliani Karen A. (45-310 Akimala Pl. Kaneohe HI 96744), Launch and ascent system.
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Griffin Dennis (Guildford GB2), Launcher for remotely piloted aircraft.
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Mayhew ; Harry E. ; Nissley ; William J. ; Widdekind ; Leonard R., Launching apparatus for flying device.
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Schlegel William R. (Wilmington DE) Hennessey John J. (Springfield PA), Launching apparatus for flying device.
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Krefta, Mark Peter; Hall, David Jonathan; Eichler, Kenneth Martin; Wu, Jiing-Liang; Strickler, Robert E.; Brennen, Michael Barnaby, Linear position sensing system and coil switching methods for closed-loop control of large linear induction motor systems.
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Scott Harry ; Wurst Stephen G., Low earth orbit payload launch system.
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J. Kirston Henderson, Magnetic levitation transport system.
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Roeseler,Cory; McGeer,Brian T.; von Flotow,Andreas H., Methods and apparatuses for launching airborne devices along flexible elongated members.
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Dennis,Brian D.; von Flotow,Andreas H., Methods and apparatuses for launching unmanned aircraft, including methods and apparatuses for transmitting forces to the aircraft during launch.
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Young, Eric P.; Reynolds, John; Curran, Mathew; Wurts, Joseph; Gast, Danny, Miniature aircraft catapult.
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Steve Miller, Mobile aircraft launcher.
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Rich Hubert A. (Westminster CA) Saffer Gary M. (Torrance CA) Woolington John C. (Harbor City CA), Paper-airplane-making and launching device.
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Rosenbaum, Bernard J.; Petter, George E.; Gessler, Joseph A.; Hughes, Michael G., Portable catapult launcher for small aircraft.
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Thomas Ernest D. R. (Banstead GB2), Ramp for aircraft take-off.
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Nissley ; Jr. William J. (Wilmington DE), Rocket-powered apparatus for launching a flying device.
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Elias Antonio L. (Fairfax VA), Rocket-powered, air-deployed, lift-assisted booster vehicle for orbital, supraorbital and suborbital flight.
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Gregory Thomas J. (Saratoga CA), Rotating launch device for a remotely piloted aircraft.
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Wood, John R.; Wood, Jeff S.; Wood, Travis, Short runway aircraft launching and landing system.
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Kelly Michael S., Space launch vehicles configured as gliders and towed to launch altitude by conventional aircraft.
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Bourlett Steven P. (Tiverton RI), Submarine launched unmanned aerial vehicle.
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Harrison, Richard G, System for airborne launch of an aircraft from a larger carrier aircraft.
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Witte Earl L. (Rte. 6 ; Clinton Rd. Paducah KY 42001), Toy aircraft.
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Johnson Lonnie (1640 Roswell St. ; Ste. A Smyrna GA 30080) Applewhite John T. (138 Belmont Dr. SW. Atlanta GA 30311), Toy airplane and launcher.
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Hirtle Michael O\Hara (Torrance CA) Morse James Edward (Lawndale CA), Toy airplane launcher.
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Amamoto Kenneth I. (Los Angeles CA) Fekete Ferenc (Huntington Beach CA) Halford Wayne R. (Manhattan Beach CA) Kilroy Eugene J. (Palos Verdes Estates CA) Hirtle Michael O. (East Aurora NY), Toy spring-type projectile launcher having directional controlling joy stick.
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Rudell Elliot (1619 Gramercy Ave. Torrance CA 90501) Foster George (2700 Panorama Dr. #404 Signal Hill CA 90806), Toy vehicle launcher with pivoting linear propulsion members.
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Cox,Beverly; Dews,Hampton; Nyroth,Nicholas, Unmanned airborne reconnaissance system.
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Hppner Heinz-Jochen (Bremen DEX) Krmer Ulrich (Syke-Barrien DEX) Sgarz Hugo (Bremen DEX) Sadowski Herbert (Bremen DEX), Unmanned craft.
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이 특허를 인용한 특허 (8) 인용/피인용 타임라인 분석

Endres, Steven P., Aircraft thrust, assembly, and methods.
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Endres, Steven P., Airport capacity from takeoff assist.
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Endres, Steven P., Airport capacity from takeoff assist.
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Endres, Steven P., Airport capacity from takeoff assist.
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Tully, Andrew; Page, Dennis; Withers, Robert; Neeld, Kenneth; Orner, Jr., Richard L., Electric unmanned aerial vehicle launcher.
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Tully, Andrew; Page, Dennis; Withers, Robert; Neeld, Kenneth; Orner, Jr., Richard L.; Schneider, Kirk F.; Whitsel, Scott J., Electric unmanned aerial vehicle launcher.
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Binnebesel, Jan, Ground-based apparatus for the take-off, landing and taxiing of aircraft.
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Miller, Stephen W., Sliding frame aircraft launcher.
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[미국특허] Flying vehicle-launching apparatus and method 원문보기

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