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Composite panel having a built-in duct

IPC분류정보
국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판)
  • B32B-003/24
  • B64D-033/02
  • B64D-029/00
  • B64C-007/02
  • B64C-001/00
  • F02C-007/20
  • B64D-033/08
  • F02C-007/04
  • F01D-025/24
  • B29L-031/00
  • B29L-031/30
  • B32B-003/26
  • F02C-006/08
출원번호 US-0272884 (2014-05-08)
등록번호 US-9410485 (2016-08-09)
우선권정보 FR-11 60243 (2011-11-10)
발명자 / 주소
  • Laurant, Franck
  • Bellet, Francois
  • Joret, Jean-Philippe
출원인 / 주소
  • AIRCELLE
대리인 / 주소
    Burris Law, PLLC
인용정보 피인용 횟수 : 0  인용 특허 : 37

초록

A composite panel includes an inner skin and an outer skin and has an opening for receiving a sampling scoop, which forms a channel and the sampling opening of which is in communication with the outer skin. In particular, the outer skin is shaped such that, at the opening, same forms at least a port

대표청구항

1. A composite sandwich panel of a structure of a turbojet engine nacelle comprising a core surrounded by an inner skin and an outer skin, the core and the inner and outer skins defining a thickness of the composite sandwich panel, the composite sandwich panel having at least one air flow duct, the

이 특허에 인용된 특허 (37)

  1. Vauchel, Guy Bernard; Ruckert, Guillaume, Acoustic attenuation panel for aircraft for engine nacelle.
  2. Chiou, Song; Yu, Jia; Hubert, Claude; Layland, Michael, Acoustic barrel for aircraft engine nacelle including crack and delamination stoppers.
  3. Anderson Robert E. (Huntington Station NY), Advanced composite aircraft cowl.
  4. Tuan, Yen, Aero-acoustic aviation engine inlet for aggressive noise abatement.
  5. Alecu, Daniel T., Air-cooled oil cooler for turbofan engine.
  6. Powell, Arthur G.; Vijgen, Paul M., Apparatus and method for passive purging of micro-perforated aerodynamic surfaces.
  7. Bagnall,Adam M; Freeman,Christopher, Arrangement for bleeding the boundary layer from an aircraft engine.
  8. Sheaf, Christopher T J; Hussain, Zahid M, Breather duct shielding.
  9. Monhardt Richard J. (Glastonbury CT) Kudlacik Louis (Glastonbury CT) Nikkanen John P. (West Hartford CT) Niiler Juri (Glastonbury CT), Combined surge bleed and dust removal system for a fan-jet engine.
  10. Perry Derick A. (Derby), Deicing of a geared gas turbine engine.
  11. Dai, Charles M.; Tseng, Carol L., Design of a flush inlet as integrated with a ship hull for waterjet propulsion.
  12. Masoero Marco (Fiano ITX) Garrone Angelo (Cascine Vica-Rivoli ITX), Device for preventing the rear light units of motor vehicles from becoming dirty.
  13. Welch John M. ; Benton William E. ; Lobsinger Michael R., Engine nacelle outer cowl panel with integral track fairings.
  14. Hebert Leonard J. ; Miller Wendell R. ; Nesbitt Eric H. ; Piro Jerry ; Sangwin Michael L., Flow control device to eliminate cavity resonance.
  15. Vermejan Alexander E. (Mason OH) Daiber Paul C. (Cincinnati OH) Morton Scott C. (Cincinnati OH) Taylor Michelle L. (Cincinnati OH), Gas turbine engine fan cooled heat exchanger.
  16. Liu Hsin-Tuan (West Chester OH) Hines William R. (Montgomery OH), Gas turbine engine variable bleed pivotal flow splitter.
  17. Ferguson, Stanley D.; Eastman, Donald W., High performance submerged air inlet.
  18. Holman Wesley L. (Renton WA) Knoll Frederick L. (Kent WA), High temperature insulation system.
  19. Lahti Daniel J. (Cincinnati OH) Yates David E. (Cincinnati OH) Mungur Parmanand (West Chester OH) Stockman Norbert O. (Batavia OH), Hybrid laminar flow nacelle.
  20. Holland ; Charles L. ; Nicoloff ; George B., Inflatable air inlet duct.
  21. Binks, Alan; James, Norman John; Layland, Michael John, Inlet section of an aircraft engine nacelle.
  22. Bichler Bartholomus (Raubling DEX) Jost Michael (Munich DEX), Inlet system for supersonic or hypersonic aircraft.
  23. Riou, Georges Jean Xavier; Verseux, Philippe, Inner wall for a turbomachine nacelle.
  24. Layland Michael J. (Bonita CA), Integrated engine shroud for gas turbine engines.
  25. Benedetti, Brenda; Farrell, Robert S.; Leon, Luis R.; Lan, Justin H.; Booker, Garry A., Metallic sandwich structure having small bend radius.
  26. Moe, Jeffrey W.; Wunsch, John J.; Sperling, Michael S., Method and apparatus for noise abatement and ice protection of an aircraft engine nacelle inlet lip.
  27. Welch John M. ; Popp Thomas D. ; Baca Leonard L., Method for forming a composite acoustic panel.
  28. Scanlon John F. (Okemos MI) Saatchi Hossein (Rockford IL) Okey David W. (Rockford IL) Church John S. (Wilmington DE) Wigell Gary A. (Lansing MI), Method of fabricating composite structures.
  29. Birbragher Fernando (Miami FL), Nacelle anti-icing system.
  30. Zysman, Steven H.; Lord, Wesley K.; Miller, Robert M.; Atassi, Oliver V., Passive boundary layer bleed system for nacelle inlet airflow control.
  31. Wood, Joshua V.; Murphy, Michael Joseph, Retrofitable auxiliary inlet scoop.
  32. Vanderleest Siebold (Seattle WA), Scoop and inlet for auxiliary power units and method.
  33. Porte Alain,FRX ; Marche Herve,FRX, Sealing device between an air inlet and a fan frame of a turbofan engine.
  34. Peters, Jeffrey T.; Mickelsen, Justin C.; Romano, Robert; Greenman, Matthew D., Turbine engine bypass fan-bleed noise reduction.
  35. Eleftheriou,Andreas; Lobo,Kevin Walter; Weinberg,Maurice; Liu,Quantai, Turbofan case and method of making.
  36. Frantz John J. (Fairfield OH), Variable double lip quiet inlet.
  37. Hussain, Zahid M., Ventilation inlet.
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