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특허 상세정보

Gas turbine engine nacelle

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64D-033/02   
미국특허분류(USC) 137/151 ; 181/214 ; 244/53B
출원번호 US-0850644 (1986-04-11)
발명자 / 주소
출원인 / 주소
인용정보 피인용 횟수 : 34  인용 특허 : 1
초록

A nacelle structure (14) for a gas turbine engine (4) extends upstream from the engine air inlet (10) and includes an external surface (18) and an internal surface (16). The external surface (18) is concentric about a linear centerline (22) which is disposed parallel to the free airflow stream (6) encountered by the nacelle (14) in flight. The internal surface (16) is concentric about a curved centerline (30), the curved centerline (30) being parallel to the free airflow stream (6) at the nacelle inlet (12) and parallel to the engine centerline (26) at t...

대표
청구항

A nacelle structure extending upstream of the air inlet opening of an aircraft gas turbine engine, comprising: an external surface defined by end points of radii extending perpendicularly to a linear, external surface centerline; an internal surface defined by end points of radii extending perpendicularly to a curved internal surface centerline; wherein the external surface centerline is oriented parallel with an external free flow of air encountering the nacelle structure, the external surface centerline further forming a droop angle with respect to the...

이 특허를 인용한 특허 피인용횟수: 34

  1. Marrinan, Patrick Michael; Becker, Thomas Lee; Murrow, Kurt David; Yao, Jixian. AFT engine nacelle shape for an aircraft. USP2017119815560.
  2. Becker, Thomas Lee; Murrow, Kurt David; Marrinan, Patrick Michael; Miller, Brandon Wayne. Aft engine for an aircraft. USP2017119821917.
  3. Becker, Thomas Lee; Murrow, Kurt David; Marrinan, Patrick Michael; Miller, Brandon Wayne. Aft engine for an aircraft. USP20180710017270.
  4. Marrinan, Patrick Michael; Becker, Thomas Lee; Murrow, Kurt David. Aft engine for an aircraft. USP2018059957055.
  5. Marrinan, Patrick Michael; Becker, Thomas Lee; Murrow, Kurt David; Yao, Jixian. Aircraft having an aft engine. USP2017059637217.
  6. McConachie James M. ; Curtin Margaret M. ; Dougherty Robert P. ; Sangwin Michael L.. Biplanar scarfed nacelle inlet. USP1999065915403.
  7. Hendricks, Gavin. Cambered aero-engine inlet. USP2012098261530.
  8. Hendricks, Gavin. Cambered aero-engine inlet. USP2013098528318.
  9. Weinstein James N. Cooker die and rotary cutter removably securing mechanism. USP2001026189439.
  10. Weinstein James N. ; Cremers Thomas G.. Cooker die and rotary cutter removably securing mechanism. USP2000116152021.
  11. Weinstein James N. ; Cremers Thomas G. ; Smith Thomas L. ; Robie Steven C.. Cooker die and rotary cutter removably securing mechanism. USP2001016167798.
  12. Hurd Ronald D. (Minnetonka MN). Cooker die removably securing mechanism. USP1996115577437.
  13. Winter, Michael. Fan nacelle flow control. USP2013098529188.
  14. Morford, Stephen A.; Larkin, Michael J.. Gas turbine engine having slim-line nacelle. USP2010097797944.
  15. Morford, Stephen A.; Larkin, Michael J.. Gas turbine engine having slim-line nacelle. USP2014098844294.
  16. Morford, Stephen A.; Larkin, Michael J.. Gas turbine engine having slim-line nacelle. USP2013018353164.
  17. Morford, Stephen A.; Larkin, Michael J.. Gas turbine engine having slim-line nacelle. USP2014058726632.
  18. Mosley, Christopher Alan; Smith, Angus Roy; Sheaf, Christopher Thomas John; Wells, John Richard. Gas turbine engine nacelle. USP2018029885285.
  19. Winter, Michael; Jain, Ashok K.. Gas turbine engine providing simulated boundary layer thickness increase. USP2011017870721.
  20. Winter, Michael; Jain, Ashok K.. Gas turbine engine system providing simulated boundary layer thickness increase. USP2012078209953.
  21. Lahti Daniel J. (Cincinnati OH) Yates David E. (Cincinnati OH) Mungur Parmanand (West Chester OH) Stockman Norbert O. (Batavia OH). Hybrid laminar flow nacelle. USP1991024993663.
  22. Jain, Ashok K.; Winter, Michael. Nacelle assembly having inlet airfoil for a gas turbine engine. USP2013048408491.
  23. Haas, Martin. Nacelle assembly having inlet bleed. USP2012068192147.
  24. Haas, Martin. Nacelle assembly with turbulators. USP2012058186942.
  25. Jain, Ashok K.. Nacelle flow assembly. USP2013128596573.
  26. Jain, Ashok K.. Nacelle flow assembly. USP2012108282037.
  27. Jain, Ashok K.. Nacelle flow assembly. USP2015049004399.
  28. Marrinan, Patrick Michael; Becker, Thomas Lee; Murrow, Kurt David; Yao, Jixian. Non-axis symmetric aft engine. USP2018029884687.
  29. Weinstein, James N.; Cremers, Thomas G.; Smith, Thomas L.. Rotary cutter assembly. USP2004076767198.
  30. Howarth,Nicholas; Freeman,Christopher. Turbine engine arrangements. USP2007017165744.
  31. Jain, Ashok K.; Winter, Michael. Variable contour nacelle assembly for a gas turbine engine. USP2016019228534.
  32. Jain, Ashok K.; Winter, Michael. Variable contraction ratio nacelle assembly for a gas turbine engine. USP2014058727267.
  33. Jain, Ashok K.. Variable geometry nacelle assembly for a gas turbine engine. USP2012068205430.
  34. Jain, Ashok K.; Chaudhry, Zaffir A.. Variable shape inlet section for a nacelle assembly of a gas turbine engine. USP2013038402739.