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특허 상세정보

Methods and apparatus for sealing variable area fan nozzles of jet engines

특허상세정보
국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) F02K-001/00    F02K-001/06    F02K-001/30    F02K-001/34    B64C-015/02    F02K-001/12    F02K-001/80    F16J-015/02    F02K-001/78    F02K-001/70    F16J-015/00    F02K-001/72   
출원번호 US-0665188 (2012-10-31)
등록번호 US-9989009 (2018-06-05)
발명자 / 주소
  • Bakken, David Alan
출원인 / 주소
  • THE BOEING COMPANY
대리인 / 주소
    Hanley, Flight & Zimmerman, LLC
인용정보 피인용 횟수 : 0  인용 특허 : 43
초록

Methods and apparatus for sealing variable area fan nozzles of jet engines are disclosed. An apparatus in accordance with the teachings of this disclosure includes a frame and a seal to be coupled to the frame. The seal to enclose petals of a variable area fan nozzle to substantially prevent airflow between the petals.

대표
청구항

1. An apparatus, comprising: a frame; anda single seal coupled to the frame, the single seal and the frame to fully enclose petals of a variable area fan nozzle to substantially prevent airflow between the petals, wherein the single seal is an elastomeric material to enable the petals to flex the single seal as the petals move between a first position and a second position. 2. The apparatus of claim 1, wherein the single seal comprises an elongate projection that extends along a perimeter edge of the single seal, the frame comprises an elongate groove th...

이 특허에 인용된 특허 (43)

  1. Anderson Robert E. (Huntington Station NY), Advanced composite aircraft cowl.
  2. Renshaw Kevin J., Apparatus for a variable area nozzle.
  3. Bush,Robert H.; Zamora,Sean; Culver,Harry; Peters,Donald William, Axial divergent section slot nozzle.
  4. Barcza M. Kevin (Palm City FL), Axisymmetric convergent/divergent nozzle with external flaps.
  5. Hauer Thomas A. (Westchester OH), Axisymmetric vectoring exhaust nozzle.
  6. Lippmeier William C. (Cincinnati OH), Axisymmetric vectoring exhaust nozzle seal.
  7. Wood Jonathan M. (West Chester OH) Hauer Thomas A. (West Chester OH) Lippmeier William C. (Cincinnati OH), Axisymmetric vectoring exhaust nozzle thermal shield.
  8. Holowach Joseph (Cincinnati OH) Lee George D. (West Palm Beach FL), Bimetallic air seal for exhaust nozzles.
  9. Levasseur, Glenn, Bladder type variable area fan nozzle.
  10. Ward Eric J., C/D nozzle with synchronizing ring link suspension.
  11. Jasklowski, Christopher; Sangwin, Michael L.; Foutch, David William; Alkislar, Mehmet Bahadir; Dilligan, Matthew Anthony, Cable-actuated variable area fan nozzle with elastomeric seals.
  12. Barcza W. Kevin (Stuart FL), Convergent/divergent nozzle with seal centering.
  13. Nesbitt, Eric H.; Butler, George W.; Reed, David H., Deployable segmented exhaust nozzle for a jet engine.
  14. Lippmeier William C. (Cincinnati OH), Exhaust nozzle flap seal.
  15. Dijoud, Delphine Edith; Fauvelet, Benoit Marc Michel; Vincent, Thomas Alain Christian, Fan nozzle of adjustable section.
  16. Baran, Kenneth C., Fan variable area nozzle for a gas turbine engine fan nacelle with cam drive ring actuation system.
  17. Chaudhry, Zaffir, Fan variable area nozzle with cable actuator system.
  18. Chanez, Philippe Gerard; Zeggai, Kamel, Gas exhaust nozzle for a bypass turbomachine having an exhaust or throat section that can be varied by moving the secondary cowl.
  19. Birch,Nigel T; Webster,John R, Gas turbine engine exhaust nozzle having a noise attenuation device driven by shape memory material actuators.
  20. Thayer Edward B. (Palm Beach Gardens FL), Gas turbine vectoring exhaust nozzle.
  21. Butler,George W.; Reed,David H.; Calkins,Frederick T.; Davis,Christopher L.; Mabe,James H., High frequency jet nozzle actuators for jet noise reduction.
  22. Seiner,John M., Method and device for reducing engine noise.
  23. Gowda,Srinivasa Range; Early,Kevin Sean; Martens,Steven, Methods and apparatus for operating gas turbine engines.
  24. Wood, Jeffrey H.; Dunne, James P., Morphing structure and method.
  25. Nightingale Douglas J. (Thornbury GB2), Nozzles for gas turbine engines.
  26. Urruela Jose R. (Las Arenas ESX), Orientable axisymmetric nozzle of variable geometry of gas turbine propulsors.
  27. Curtis C. Cowan ; George F. Leblanc, Sealing means for a multi-axis nozzle.
  28. Wood,Jeffrey H, Shape changing structure.
  29. Brown, John Joseph; Keith, William Preston, Stave and ring CMC nozzle.
  30. Lippmeier William C. (Cincinnati OH) Wilkinson Todd T. (Chester OH) Ausdenmoore Robert M. (Chester OH), Support for a translating nozzle vectoring ring.
  31. Bhatt, Jay, Thrust reverser for a gas turbine engine with moveable doors.
  32. Jurich Umberto (Kirkland WA), Thrust reverser for high bypass jet engines.
  33. Ibarreche Mendia Jose I. (Gorliz ESX) Rivacoba Urruela Jose (Las Arenas ESX), Thrust vectoring variable geometry exhaust nozzle for gas turbines.
  34. Lair,Jean Pierre, Turbofan variable fan nozzle.
  35. Johnston Everett A. (Mason OH), Variable area exhaust nozzle.
  36. Lair Jean-Pierre (100 W. El Prado ; Suite 308 San Antonio TX 78212), Variable area exhaust nozzle.
  37. Duesler Paul W. ; Loffredo Constantino V. ; Prosser ; Jr. Harold T. ; Jones Christopher W., Variable area fan exhaust nozzle having mechanically separate sleeve and thrust reverser actuation systems.
  38. Atassi, Oliver V.; Petrenko, Oleg, Variable area fan nozzle with wall thickness distribution.
  39. Rey Nancy M. ; Miller Robin M. ; Tillman Thomas G. ; Rukus Robert M. ; Kettle John L. ; Dunphy James R. ; Chaudhry Zaffir A. ; Pearson David D. ; Dreitlein Kenneth C. ; Loffredo Constantino V. ; Wyno, Variable area nozzle for gas turbine engines driven by shape memory alloy actuators.
  40. Arnold,Steven M.; Penney,Nicholas, Variable area nozzle including a plurality of convexly vanes with a crowned contour, in a vane to vane sealing arrangement and with nonuniform lengths.
  41. Berg Paul H. (Simi Valley CA), Variable area turbine.
  42. Cariola Roy E. ; Aten Michael R., Variable fan exhaust area nozzle for aircraft gas turbine engine with thrust reverser.
  43. James Varnell L. (Kent WA), Variable geometry convergent divergent exhaust nozzle.