[특허]One-piece closed-shape structure and method of forming same

One-piece closed-shape structure and method of forming same 원문보기

IPC분류정보
국가/구분	United States(US) Patent 등록
국제특허분류(IPC7판)	H02K-012/02
출원번호	US-0712041 (2003-11-14)
발명자 / 주소	Anderson,Alan H. Bowman,Kathlene K. Teufel,Paul D.
출원인 / 주소	Toyota Motor Sales, U.S.A., Inc.
대리인 / 주소	Finnegan, Henderson, Farabow, Garrett &
인용정보	피인용 횟수 : 9 인용 특허 : 37

초록 ▼

The present invention relates to a one-piece closed-shape structure and a method for manufacturing a one-piece closed-shape structure. In particular, the present invention relates to a one-piece fuselage and a method for manufacturing a one-piece fuselage. One embodiment of the method of the invention involves the use of molding technology, tooling technology, the integration of the molding and tooling technology, and fiber placement to manufacture a one-piece closed shape structure.

대표청구항 ▼

What is claimed is: 1. A one-piece closed shape structure, comprising an outer skin formed of a composite material; an inner skin formed of a composite material; a frame located on an interior portion of the inner skin; and a core material located between the inner and outer skin, wherein the outer skin, inner skin, frame, and core material have been simultaneously co-cured to form the one-piece closed shape structure. 2. A one-piece airplane fuselage, comprising an outer skin formed of a composite material; an inner skin formed of a composite material; a frame located on an interior portion of the inner skin; and a core material located between the inner and outer skin; wherein the outer skin, inner skin, frame, and core material have been simultaneously co-cured to form the one-piece airplane fuselage. 3. The airplane fuselage of claim 2, further comprising at least one integrally formed flange that has been simultaneously co-cured with the outer skin, inner skin, frame, and core material. 4. The airplane fuselage of claim 3, further comprising at least one integrally formed wing attachment pocket that has been simultaneously co-cured with the outer skin, inner skin, frame, core material, and flange.

이 특허에 인용된 특허 (37)

Williams Sam B. (Bloomfield Hills MI), Aircraft.
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Willden Kurtis S. (Kent WA) Goodno Kenneth N. (Federal Way WA), Caul and method for bonding and curing intricate composite structures.
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Lallo Arthur J. (Edgmont PA) Falasco Thomas J. (Broomall PA), Co-cured composite fan blade and method.
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Carter Glenn T. (Fort Worth TX) Paniszczyn Thomas F. (Fort Worth TX), Combination airbrake and pitch control device.
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Giannetti, William B.; Chuang, Hsing-Yen; Chauvin, Dewey, Composite baseball bat having an interface section in the bat barrel.
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Kay, Bruce Frederic; Goodworth, Alan Roy, Composite tail cone assembly.
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Noto Vincent H., Continuous laminating or molding process.
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Cronkhite James D. (Hurst TX) Haas Thomas J. (Grand Prairie TX) Mort Raymond W. (Hurst TX), Energy absorbing composite aircraft structure.
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Nakamura Wayne H. (San Jose CA), Fabrication by filament winding with an elastomeric material.
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Vaniglia Milo M. (Southgate KY), Fiber placement machine.
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Vaniglia Milo M. (Southgate KY), Fiber placement machine.
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Barr Roy L. ; Bloch Daniel D. ; Mallow Andrew R. ; Rhodes Charles A., Fiber placement mid-span redirect.
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Cogburn Jimmie W. (Fort Worth TX) Chitwood Billie E. (Fort Worth TX) Howeth Marvin S. (Fort Worth TX), Filament reinforced structural shapes.
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Corbett Darrell H. (Kent WA) Speelmon C. Robert (Redmond WA), Filament winding feed system.
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Weingart Oscar (Riverside CA) Lunde Gerald A. (Norco CA) Taylor Clark D. (Riverside CA), Filament winding mechanism for forming and winding a shingled gap free band.
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Weingart Oscar (Riverside CA) Lunde Gerald A. (Norco CA) Taylor Clark D. (Riverside CA), Filament winding process.
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Carbone Pat. J. (Maplewood NJ) Willson Raleigh E. (Flanders NJ) Petruccelli Frank (Boonton NJ), Filament winding using a rotationally molded inner layer.
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Crane Roger M. (Arnold MD), High-damping rib-stiffened composite hollow cylinder core configuration.
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Davis Kevin (Ogden UT) Yorgason James A. (Ogden UT), Method for constructing an inflatable mandrel.
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Youngkeit Dean C. (Willard UT), Method for making a composite component using a transverse tape.
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Murphy James C. ; Boyce Gerald S.,GBX ; Coeckelbergs Erik,BEX, Method for making thermoplastic composite pressure vessels.
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Darrieux Jean-Louis (Saint Medard En Jalles FRX) Picosson Christian (Macau FRX) Canfranc Hugues (Saint Aubin De Medoc FRX), Method for producing hollow composite articles by winding/laying down on an expansible mandrel.
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Halcomb Ronald G. (Tulsa OK), Method for producing integrally stiffened fiber reinforced plastic panels.
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Hamamoto Kenji (Tokyo JPX) Amaoka Kazuaki (Tokyo JPX) Takizawa Naoya (Utsunomiya JPX) Hosoi Masanori (Shimotsuga JPX), Method of fabricating aircraft fuselage structure.
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Goodno Kenneth T. (31232 - 28th Ave. S. Federal Way WA 98003), Method of making and using flexible mandrel.
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Stettler Andreas (Lutzenberg CHX) Anderegg Kurt (Rheineck CHX), Method of manufacturing integral railway coach bodies.
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Arenas Gabriel N. (39 St. Jude La. Scotia NY 12302), Method of molding eggshell thin bodies.
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Russell, Mark C.; Doyle, Sean P.; Russell, Charles T., Method of producing a channeled wall fluid control apparatus.
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Benson Vernon M. ; Gill Dee R. ; Nielsen James P. ; Mansouri Hosein ; Shepherd Noel I., Multiple axes fiber placement machine.
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Cappa James O. ; Dursch Harry W., One piece spacecraft frame.
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Mowbray Donald Fredrick ; Fitzgerald John James ; Bachrach William Elliot ; Lin Wendy Wen-Ling ; Finn Scott Roger, Poly-component blade for a steam turbine.
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Greenwood Mark Edward ; Gauchel James Vincent ; Beckman Jay Joseph ; Hankin Anthony Grenville,GBX, Process for filament winding composite workpieces.
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Martin Andrew McG., Reclosable storage bag and method for making the same.
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Hollingsworth Ritch D. (8579 Mortenson Dr. Fair Oaks CA 95628), Rigid segmented mandrel with inflatable support.
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Meyer Gero,DEX, Separating device for winding devices for material webs, longitudinally divided into several partial webs.
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Maro Tsuyoshi (Ibaraki JPX) Kitakami Osamu (Toride JPX) Fujiwara Hideo (Ibaraki JPX) Wakai Kunio (Ibaraki JPX), Soft magnetic materials comprising 9 to 15 atomic percent carbon atoms.
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Kam ; Clifford Y. ; Freeman ; Vernon L. ; Penton ; Allen P., Stiffened composite structural member and method of fabrication.
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이 특허를 인용한 특허 (9)

Robinson, Mike; Schrag, Allan; Harrell, Matthew, Cabin headliner.
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Kismarton, Max U.; Andrews, Francis E.; Koch, William J., Compliant stiffener for aircraft fuselage.
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Novikov, Dmitri; Furrer, David Ulrich; Burlatsky, Sergei F; Huttenhower, Hillary Anne; Atrazhev, Vadim; Sultanov, Vadim; Dmitriev, Dmitry; Riehl, John D; Watson, Charles R, High performance polymer and process therefor.
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Coleman, Robert Alexander; King, Timothy Dean; Hanson, Steven Fillmore; Baca, Leonard Lloyd, Method and system for forming a complex monolithic thermoset part.
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Tessier, Sylvain; Gingras, Richard; Dionne, Jacques; Bednar, Felix, Modular mandrel for monolithic composite fuselage.
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Longo, Curtis, Vibration apparatus and methods of vibration.
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Longo, Curtis, Vibration apparatus and methods of vibration.
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Longo, Curtis, Vibration apparatus and methods of vibration.
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Longo,Curtis, Vibration apparatus and methods of vibration.
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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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One-piece closed-shape structure and method of forming same 원문보기