[특허]Double-pivoting deployment system for aerosurfaces

[미국특허] Double-pivoting deployment system for aerosurfaces 원문보기

IPC분류정보
국가/구분	United States(US) Patent 등록
국제특허분류(IPC7판)	F42B-010/14 B64C-003/56
출원번호	US-0749316 (1991-08-23)
발명자 / 주소	Moorefield William J. (St. Peters MO)
출원인 / 주소	McDonnell Douglas Corporation (St. Louis MO 02)
인용정보	피인용 횟수 : 28 인용 특허 : 0

초록 ▼

A double-pivoting deployment system for aerosurfaces, such as wings or fins, for use on aerospace vehicles. Each aerosurface has an inner segment and an outer segment. The inner segment is pivotally connected at a first axis of rotation to the support structure of the aerospace vehicle. An outer side portion of the inner segment is pivotally connected at a second axis of rotation to an inner side portion of the outer segment. In operation, the outer segment is stowed adjacent to the body of the aerospace vehicle such that the surface plane of the outer segment is longitudinally aligned with the longitudinal axis of the aerospace vehicle, and the aerosurface span is longitudinally aligned with, the longitudinal axis of the aerospace vehicle. From the stowed position, the outer segment is first rotated substantially 90°about the second axis of rotation so that the surface plane of the outer segment is generally horizontal; subsequently, the entire aerosurface is rotated about the first axis of rotation so that aerosurface span projects outwardly from the body of the aerospace vehicle.

대표청구항 ▼

In combination with a support structure of an aerospace vehicle, an aerosurface deployment assembly, comprising: (a) an actuating means; (b) a plurality of aerosurfaces, each having an inner segment and an outer segment, wherein each said inner segment is pivotally connected to said support structure at an axis of rotation substantially perpendicular to the longitudinal axis of the aerospace vehicle, and wherein an outer side portion of each said inner segment is pivotally connected to an inner side portion of each said outer segment at an axis of rotation parallel to said longitudinal axis when said aerosurfaces are in the stowed position; (c) a yoke means, operably connected to said actuating means, for translational travel along said support structure; and (d) a plurality of linkage rods for interconnecting said yoke means and said aerosurfaces, wherein a single linkage rod interconnects said yoke means to each said aerosurface, and wherein translational travel of said yoke means, initiated by said actuating means, moves said plurality of linkage rods to rotate said aerosurfaces about each of said axes of rotation substantially perpendicular to said longitudinal axis and each of said axes of rotation parallel to said longitudinal axis thereby deploying said aerosurfaces.

이 특허를 인용한 특허 (28) 인용/피인용 타임라인 분석

O'Shea, Hank, Aerial vehicle with variable aspect ratio deployable wings.
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Afanasyev, Sergey Nikolaevich, Aircraft.
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Cleveland, Kenneth D.; Pietrzak, Amy; Butland, Adam G.; Steenson, Jr., James H.; Schorr, David J.; Borysthen-Tkacz, Joseph, Apparatus for deploying stowed control surfaces of a projectile.
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Cleveland, Kenneth; Pietrzak, Amy; Butland, Adam; Steenson, Jr., James H.; Schorr, David; Borysthen-Tkacz, Joseph, Apparatus for deploying stowed control surfaces of a projectile.
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Clark Walter Dennis, Augmented wing tip drag flap.
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Shimovetz Ralph, Configurable aerial vehicle aerosurface.
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Russom,Jeffery D.; White,Lawrence R.; Greenwood,James, Control surface assemblies with torque tube base.
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Cohe, Patrick; Boissiere, Bruno; Clech, Loïc, Device for opening and locking a tail unit for ammunition.
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Shmoldas John D. (Thousand Oaks CA) Hutchings Michael B. (Westlake Village CA) Barlow Christopher W. (Newbury Park CA), Extendable wing for guided missles and munitions.
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Scott, Aaron Michael; Aberer, Philip Thomas; Japp, Neil Randall; McGaha, Nicholas Cody, Folding articulating wing mechanism.
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Santini, Gregory M.; Sakurai, Seiya, Horizontal folding wingtip.
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Mikhail Ameer G. (Bel Air MD), Kinetic energy projectile with fin leading edge protection mechanisms.
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Hawthorne,Dana D., Locking device with solenoid release pin.
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Eisentraut, Rudolph A.; Melkers, Edgar R., Method for designing a deployment mechanism.
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Hsu William W. ; Bragg Duncan D., Missile fin locking mechanism.
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Banks John Edward, Multi-axis unfolding mechanism with rate controlled synchronized movement.
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Sokolovsky Gennady Alexandrovich,RUX ; Belyaev Vladimir Nikolaevich,RUX ; Bogatsky Vladimir Grigorievich,RUX ; Bychkov Evgeny Alexandrovich,RUX ; Vatolin Valentin Vladimirovich,RUX ; Grachev Alexei V, Rocket with lattice control surfaces and a lattice control surface for a rocket.
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Smith Brian E., Secondary wing system for use on an aircraft.
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Kenneth E. Zoeller ; Matthew E. Byers ; William V. West ; Jason Fletcher, Septic tank filtering system.
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Zoeller Kenneth E. ; Byers Matthew E. ; West William V. ; Fletcher Jason, Septic tank filtering system.
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Zoeller Kenneth E. ; Byers Matthew E. ; West William V. ; Fletcher Jason, Septic tank filtering system.
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Banks Johnny E., Single axis fold actuator and lock for member.
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Torre, Christopher N., Stowable and deployable unmanned aerial vehicle.
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Hsu,William W.; Wiseman,Robert A., Techniques for controlling a fin with unlimited adjustment and no backlash.
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Gionta, Matthew; Crocoll, James; Karkow, Jon; Nicholas, Paul; Bledsoe, Scott, Two-motion wing-fold mechanism with independent load path.
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Petrov, Val, Vertical takeoff and landing airframe.
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Lassen, Matthew August; Good, Mark Steven, Wing fold controller.
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Fox, Stephen John; Kordel, Jan A.; Townsend, Keith; Lassen, Matthew August; Gardner, Mark John; Good, Mark Steven, Wing fold system rotating latch.
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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] Double-pivoting deployment system for aerosurfaces 원문보기