$\require{mediawiki-texvc}$

연합인증

연합인증 가입 기관의 연구자들은 소속기관의 인증정보(ID와 암호)를 이용해 다른 대학, 연구기관, 서비스 공급자의 다양한 온라인 자원과 연구 데이터를 이용할 수 있습니다.

이는 여행자가 자국에서 발행 받은 여권으로 세계 각국을 자유롭게 여행할 수 있는 것과 같습니다.

연합인증으로 이용이 가능한 서비스는 NTIS, DataON, Edison, Kafe, Webinar 등이 있습니다.

한번의 인증절차만으로 연합인증 가입 서비스에 추가 로그인 없이 이용이 가능합니다.

다만, 연합인증을 위해서는 최초 1회만 인증 절차가 필요합니다. (회원이 아닐 경우 회원 가입이 필요합니다.)

연합인증 절차는 다음과 같습니다.

최초이용시에는
ScienceON에 로그인 → 연합인증 서비스 접속 → 로그인 (본인 확인 또는 회원가입) → 서비스 이용

그 이후에는
ScienceON 로그인 → 연합인증 서비스 접속 → 서비스 이용

연합인증을 활용하시면 KISTI가 제공하는 다양한 서비스를 편리하게 이용하실 수 있습니다.

Engine nacelle outer cowl panel with integral track fairings 원문보기

IPC분류정보
국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판)
  • B64D-029/00
출원번호 US-0013993 (1998-01-27)
발명자 / 주소
  • Welch John M.
  • Benton William E.
  • Lobsinger Michael R.
출원인 / 주소
  • The Boeing Company
대리인 / 주소
    Christensen O'Connor Johnson & Kindness PLLC
인용정보 피인용 횟수 : 40  인용 특허 : 20

초록 ▼

An outer cowl panel (24) for an engine nacelle (20). The outer cowl panel (24) includes integral track fairings (30) at aft side edges of the outer cowl panel. The outer cowl panel (24) also includes a chamfered leading edge having outer face sheets (88A, 88B) that extend over the leading edges of a

대표청구항 ▼

[ The embodiments of the invention in which an exclusive property or privilege is claimed are defined as follows:] [8.] An outer cowl panel for a nacelle engine comprising:a carbon fiber reinforced laminate having a leading edge defined by stacking of a plurality of plies to form the laminate; anda

이 특허에 인용된 특허 (20)

  1. Anderson Robert E. (Huntington Station NY), Advanced composite aircraft cowl.
    상세보기
  2. Rolston Stephen C.,GBX ; Ashford Edward M.,GB5, Aerodynamic low drag structure.
    상세보기
  3. Dhoore Louis G. (Seattle WA) Schultz William H. (Bellevue WA), Combination bulk absorber-honeycomb acoustic panels.
    상세보기
  4. 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.
    상세보기
  5. Vetter Earl E. (Mercer Island WA), Common pod for housing a plurality of different turbofan jet propulsion engines.
    상세보기
  6. Chee Wan T. (Bellevue WA) Quigley George W. (Bellevue WA), Continuously wound filament structure for use in noise attenuation element.
    상세보기
  7. Mutch Henry (Chula Vista CA), Gas turbine engine compartment vent system.
    상세보기
  8. Nelsen Murray D. (Goddard KS) Kunze ; Jr. Robert K. (Wichita KS) Olsen Robert F. (Woodinville WA) Rushwald Ira B. (Seattle WA), High efficiency broadband acoustic resonator and absorption panel.
    상세보기
  9. Darfler Stephen C. (Castro Valley CA), High thermal conductivity non-metallic honeycomb.
    상세보기
  10. Beggs, Stanley L.; Riel, Frank J.; Lawson, Dale W. R., Honeycomb noise attenuation structure.
    상세보기
  11. Vermilye Michael L. (Redmond WA), Hybrid thrust reverser cascade basket and method.
    상세보기
  12. Gnagy Clayton C. (Enumclaw WA), Integrated insulation wall assembly.
    상세보기
  13. James Varnell L. (Auburn WA), Jet engine thrust reverser.
    상세보기
  14. Stachowiak Claude R. (Renton WA), Jet engine thrust reverser.
    상세보기
  15. Birbragher Fernando (Miami FL), Noise reduction nacelle.
    상세보기
  16. Pearson Kenneth A. (Henleaze GB2) Moorhouse Major D. (Stapleton GB2), Pressure relief panel for aircraft powerplant.
    상세보기
  17. Fischer Josef (Ried im Innkreis ATX) Stephan Walter A. (Braunau ATX), Structural panel.
    상세보기
  18. Vermilye Michael L. (Redmond WA), Thrust reverser blocker door assembly.
    상세보기
  19. Dorr John A. (Crofton MD), Ultrasonic sensor system.
    상세보기
  20. Bubello Robert (Meriden CT) Ream Jeffrey L. (Tollano CT), Ventilation system for a nacelle.
    상세보기

이 특허를 인용한 특허 (40)

  1. Bouchet,Eric; Mahieu,Benjamin; Juillen,Lionel; Vinches,Frederic, Aircraft partition designed to separate a cargo part from a cockpit or from a passenger compartment.
    상세보기
  2. Calder, David P.; Howarth, Graham F., Apparatus for facilitating access to a nacelle interior.
    상세보기
  3. Calder, David P.; Howarth, Graham F., Apparatus for facilitating access to a nacelle interior and method of assembling the same.
    상세보기
  4. McMillan, Alison J., Composite material hollow axisymmetric body.
    상세보기
  5. Laurant, Franck; Bellet, Francois; Joret, Jean-Philippe, Composite panel having a built-in duct.
    상세보기
  6. Dawson, Stacie M.; Wiley, Richard, Core reflex nozzle for turbofan engine.
    상세보기
  7. Winter, Michael, Fan nacelle flow control.
    상세보기
  8. Emmelmann, Claus; Klaukien, Frank-Michael; Kranz, Jannis; Wycisk, Eric; Sassmannshausen, Jan, Force introduction fitting for lightweight components.
    상세보기
  9. Klaukien, Frank-Michael, Force transmission fitting for lightweight components.
    상세보기
  10. Morford, Stephen A.; Larkin, Michael J., Gas turbine engine having slim-line nacelle.
    상세보기
  11. Morford, Stephen A.; Larkin, Michael J., Gas turbine engine having slim-line nacelle.
    상세보기
  12. Morford, Stephen A.; Larkin, Michael J., Gas turbine engine having slim-line nacelle.
    상세보기
  13. Morford, Stephen A.; Larkin, Michael J., Gas turbine engine having slim-line nacelle.
    상세보기
  14. Winter, Michael; Jain, Ashok K., Gas turbine engine providing simulated boundary layer thickness increase.
    상세보기
  15. Winter, Michael; Jain, Ashok K., Gas turbine engine system providing simulated boundary layer thickness increase.
    상세보기
  16. Welch, John M.; Popp, Thomas D., Integral composite slider for aircrafts.
    상세보기
  17. Latorre Plaza, Teresa; Garcia Vázquez, Luis Miguel; Recio Melero, Manuel, Manufacturing procedure of a part made out of a composite material introducing a geometric change in one of its faces.
    상세보기
  18. Benedetti, Brenda; Farrell, Robert S.; Leon, Luis R.; Lan, Justin H.; Booker, Garry A., Metallic sandwich structure having small bend radius.
    상세보기
  19. Chillapalli, Durga Srinivas; Kumar, Hemanth Gudibande Sathyakumar; Mondal, Bhaskar Nanda; Pal, Kishanjit; Shevakari, Sushilkumar Gulabrao; Moniz, Thomas Ory, Method and system for controlling core cowl vent area.
    상세보기
  20. Wunsch, John Joseph; Franks, Michael John; Greenfield, Danielle Marie; Bodey, Michael Stephens; Prather, Randall Maurice, Method and system for improving structural characteristics of composite component corners.
    상세보기
  21. Vail, III, William Banning; Skerl, Tomislav, Methods and apparatus for monitoring and fixing holes in composite aircraft.
    상세보기
  22. Vail, III, William Banning, Methods and apparatus to prevent failures of fiber-reinforced composite materials under compressive stresses caused by fluids and gases invading microfractures in the materials.
    상세보기
  23. Calder, David P.; Howarth, Graham F., Nacelle and method of assembling the same.
    상세보기
  24. Jain, Ashok K.; Winter, Michael, Nacelle assembly having inlet airfoil for a gas turbine engine.
    상세보기
  25. Haas, Martin, Nacelle assembly having inlet bleed.
    상세보기
  26. Haas, Martin, Nacelle assembly with turbulators.
    상세보기
  27. Jain, Ashok K., Nacelle flow assembly.
    상세보기
  28. Jain, Ashok K., Nacelle flow assembly.
    상세보기
  29. Jain, Ashok K., Nacelle flow assembly.
    상세보기
  30. Murphy, Michael J.; Malecki, Robert E., Non-circular aft nacelle cowling geometry.
    상세보기
  31. Murphy, Michael Joseph; Malecki, Robert E., Non-circular aft nacelle cowling geometry.
    상세보기
  32. Klahn, Christoph; Gysemberg, Rüdy; Rehme, Olaf, Supporting pillar for an aircraft's structural component manufactured by a selective laser melting process.
    상세보기
  33. Klahn, Christoph; Gysemberg, Rüdy; Rehme, Olaf, Supporting pillar for an aircraft's structural component manufactured by a selective laser melting process.
    상세보기
  34. Bellanger, Alexandre; Bouillon, Florent; Dubois, Laurent, Thrust reverser supporting structure including composite reinforcements and a base having an unclosed cross section.
    상세보기
  35. Jain, Ashok K.; Winter, Michael, Variable contour nacelle assembly for a gas turbine engine.
    상세보기
  36. Jain, Ashok K.; Winter, Michael, Variable contraction ratio nacelle assembly for a gas turbine engine.
    상세보기
  37. Jain, Ashok K., Variable geometry nacelle assembly for a gas turbine engine.
    상세보기
  38. Jain, Ashok K.; Chaudhry, Zaffir A., Variable shape inlet section for a nacelle assembly of a gas turbine engine.
    상세보기
  39. Eberth, Ulrich; Koeber, Mario, Window replacement for filling a window frame.
    상세보기
  40. Eberth, Ulrich; Koeber, Mario, Window replacement for filling a window frame.
    상세보기

관련 콘텐츠

섹션별 컨텐츠 바로가기

AI-Helper ※ AI-Helper는 오픈소스 모델을 사용합니다.

AI-Helper 아이콘
AI-Helper
안녕하세요, AI-Helper입니다. 좌측 "선택된 텍스트"에서 텍스트를 선택하여 요약, 번역, 용어설명을 실행하세요.
※ AI-Helper는 부적절한 답변을 할 수 있습니다.

선택된 텍스트

맨위로