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Leading edge construction for an aerodynamic surface and method of making the same 원문보기

IPC분류정보
국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판)
  • B64C-001/00
  • B64C-003/00
  • B64C-005/00
출원번호 US-0977825 (1997-11-25)
우선권정보 DE-0049132 (1996-11-27)
발명자 / 주소
  • Kraenzien Peter,DEX
출원인 / 주소
  • DaimlerChrysler Aerospace Airbus GmbH, DEX
대리인 / 주소
    Fasse
인용정보 피인용 횟수 : 23  인용 특허 : 14

초록

A leading edge structure for an aerodynamic surface includes a support structure made of fiber-reinforced synthetic material and a skin structure made of metal mounted on the support structure. The support structure includes an inner laminate, an outer laminate, and longitudinally extending tubes an

대표청구항

[ What is claimed is:] [1.] A leading edge structure for an aerodynamic surface, comprising a support structure, a skin structure arranged on said support structure, and an adhesive that bonds said skin structure onto said support structure, wherein:said support structure comprises an inner laminate

이 특허에 인용된 특허 (14)

  1. Clites James L. (23301 Bocana Malibu CA 90265), Airfoil self energizing boundary layer control system.
  2. Isenberg Jack M. (Bellevue WA), Apparatus and method for manufacturing laminar flow control aircraft structure.
  3. Loebert Gerhard (Baldham DEX), Apparatus for reducing turbulent drag.
  4. Johnson Warren A. (San Diego CA) Harding Geoffrey A. (Chula Vista CA), Arrangement for maintaining laminar air flow over gaps in aircraft engine nacelle surfaces.
  5. Jackson Melvin R. (Niskayuna NY) Skelly David W. (Burnt Hills NY) Rowe Raymond G. (Schenectady NY) LaChapelle Donald G. (Cincinnati OH) Wilson Paul S. (Sharonville OH), Double-wall airfoil.
  6. Frosch Robert A. Administrator of the National Aeronautics and Space Administration ; with respect to an invention of ( Mercer Island WA) Robinson Robert K. (Mercer Island WA) Tomlinson Harry M. (Bel, Fuselage structure using advanced technology fiber reinforced composites.
  7. Gratzer Louis B. (Seattle WA), Laminar flow control airfoil.
  8. DeCoux Steven P. (Long Beach CA), Laminar flow control apparatus for aerodynamic surfaces.
  9. Ashton ; Larry J. ; Abildskov ; Dale P., Lightweight contoured load carrying structure.
  10. DeCoux Steven P. (Long Beach CA), Method and apparatus for laminar flow control.
  11. Hertzberg Paul E. (San Diego CA), Method of making delamination resistant composites.
  12. Hartwich Peter M. (Newport News VA), Porous airfoil and process.
  13. Saveker David R. (711 Hanford St. Pismo Beach CA 93449), Sinusoidal structural element.
  14. Yasui Ken K. (Huntington Beach CA), Superplastically formed structure having a perforated skin.

이 특허를 인용한 특허 (23)

  1. Teich, Benjamin, Aerodynamic component and method for producing an aerodynamic component.
  2. Schmidt, Eric Thomas, Aerodynamically efficient surfaces.
  3. Schmidt, Eric Thomas, Aerodynamically efficient surfaces.
  4. Teeter,Darrin Blake, Air intake manifold.
  5. Perez Rodriguez, David; Ballestero Mendez, Jorge, Fixing system for a leading edge to the structure of an aircraft lift plane.
  6. Brook, Kenneth L.; Keefe, Bonnie, Fluid dynamic vent dam.
  7. Brook, Kenneth L.; Keefe, Bonnie A., Fluid dynamic vent dam.
  8. Billman, Garrett M.; O'Neil, Patrick J., Forebody vortex alleviation device.
  9. Williams, Stewart W; Turner, Brian J, Laminar flow control system and suction panel for use therewith.
  10. Gerber, Martin, Leading edge nose structure on the vertical stabilizer of an aircraft.
  11. De Castro Nodal, Manuel; Cerezo Pancorbo, Carlos; Dominguez Casado, Rafael; Grueso Diez, Cesar; Huertas Garcia, Manuel; Robledo Sacristan, Bonifacio, Leading edge of supporting surfaces of aircraft.
  12. Schmidt,Eric T., Linear shock wave absorber.
  13. Debaisieux, Stéphane; Overbergh, Christian; Quets, Sébastien, Manufacturing process for a grooved structure and structure obtained by this process.
  14. Teeter, Darrin Blake, Method for making composite structures.
  15. Josef Mertens DE; Henri Lajain DE, Method of fabricating leading edge nose structures of aerodynamic surfaces.
  16. Tanner, Justin A.; Facinelli, William A.; Kang, Albert, Outflow valve having J-shaped bellmouth and cabin pressure control system employing the same.
  17. Porte, Alain; Chelin, Frédéric; Dida, Stéphane; Hormiere, Arnaud, Panel for an air intake of an aircraft nacelle that ensures optimized acoustic treatment and frost treatment.
  18. Bertolotti,Fabio P., Perforated skin structure for laminar-flow systems.
  19. Gerber, Martin; Syassen, Freerk, Profile plate portion for use as an outer wall of a flow body, method for manufacturing a profile plate portion and flow body component comprising a suction-extraction device for fluid.
  20. Chapman, Jr., W. Cullen, Tubular members integrated to form a structure.
  21. Chapman, Jr.,W. Cullen, Tubular members integrated to form a structure.
  22. Komoda, Ushio; Motohashi, Hideto, Vent member, wing panel, and main wing for aircraft.
  23. Wood, Norman, Wing leading edge venting.
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