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특허 상세정보

Apparatus for minimizing inlet airflow turbulence in a gas turbine engine

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) F01D-017/16    F01D-011/00   
미국특허분류(USC) 415/161 ; 415/160 ; 415/230 ; 415/231 ; 277/637 ; 277/645
출원번호 US-0993822 (1997-12-18)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Hayes
인용정보 피인용 횟수 : 33  인용 특허 : 3
초록

A seal, and method of using same, for an inlet guide vane in a gas turbine engine includes a longitudinally extending tubular portion that has a longitudinal axis defined therethrough, a dovetail portion including a rib portion and a retaining feature. The rib portion is integral with the tubular portion and extends parallel to the axis, and the rib portion extends in a direction radially outward from the axis. The retaining feature is integral with the rib portion and tapers toward the axis.

대표
청구항

[ We claim:] [1.] A method for preventing turbulence in air entering a fan of a gas turbine engine, said method comprising:providing an engine inlet, said inlet having an inner shroud, an annular casing spaced radially outward from the inner shroud, and a plurality of inlet guide vanes extending radially from the inner shroud to the casing, each of said guide vanes including a strut airfoil and a flap airfoil, said strut airfoil of each inlet guide vane in spaced relation to said flap airfoil thereof defining a gap therebetween, said flap airfoil of each...

이 특허를 인용한 특허 피인용횟수: 33

  1. Marrinan, Patrick Michael; Becker, Thomas Lee; Murrow, Kurt David. Aft engine for an aircraft. USP2018059957055.
  2. Tsou, Chi-Ling Michael; Holdren, Carl Francis; Bailey, William Andrew; Lenahan, Dean Thomas. Baffle seal for gas turbine engine thrust reverser. USP2012048157270.
  3. Sorokes, James M.; Maier, William C.. Compressor performance adjustment system. USP2014018632302.
  4. Vontell, John H.; Brush, Ronald W.. Fluid pressure operated fixture. USP2012018091419.
  5. Subramaniyan, Moorthi; Chengappa, Manjunath Bangalore; Patel, Pradeep. Gas turbine diffuser strut including a trailing edge flap and methods of assembling the same. USP20181210151325.
  6. Norris, James W.; Banks, Anton G.. Gas turbine engine having controllable inlet guide vanes. USP2013018348600.
  7. Bruce,Robert William; Distler,Timothy David. Inlet guide vane bushing having extended life expectancy. USP2006107121727.
  8. Carroll, Christian A.. Inlet guide vanes and gas turbine engine systems involving such vanes. USP2016029249736.
  9. Suciu, Gabriel L.; Merry, Brian D.; Brilliant, Lisa I.. Integrated inlet vane and strut. USP2015069068460.
  10. Yu, Hong; Dutton, Ronald. Integrated strut and IGV configuration. USP20181010094223.
  11. Paradis, Vincent; Pater, Chris. Integrated strut and turbine vane nozzle arrangement. USP2017019556746.
  12. Paradis, Vincent; Pietrobon, John Walter; Bouchard, Richard L.. Integrated strut and vane arrangements. USP20190310221711.
  13. Paradis, Vincent; Pietrobon, John Walter; Bouchard, Richard L.. Integrated strut and vane arrangements. USP2017129835038.
  14. Paradis, Vincent; Vlasic, Edward; Tsifourdaris, Panagiota. Integrated strut-vane. USP20190310221707.
  15. Tsifourdaris, Panagiota; Vlasic, Edward; Moradi, Niloofar; Doyon, Francois. Integrated strut-vane nozzle (ISV) with uneven vane axial chords. USP2018039909434.
  16. Howell,Stephen John; Jacobson,John Carl; McCaffrey,Timothy P.; Barnes,Barry Francis. Methods and apparatus for attaching swirlers to gas turbine engine combustors. USP2007127310952.
  17. Manteiga, John A.; Laidlaw, Gilbert J.. Methods and apparatus for controlling engine clearance closures. USP2005056886343.
  18. Howell,Stephen John; Danis,Allen Michael. Methods and apparatus for cooling turbine engine combustor exit temperatures. USP2006057036316.
  19. Howell,Stephen John; Jacobson,John Carl; McCaffrey,Timothy P.; Barnes,Barry Francis. Methods and apparatus for film cooling gas turbine engine combustors. USP2006057051532.
  20. McCaffrey, Timothy P.; Howell, Stephen John; Tingle, Walter J.; Barnes, Barry Francis; Jacobson, John Carl. Methods and apparatus for operating gas turbine engine combustors. USP2005106955038.
  21. McCaffrey,Timothy P.; Howell,Stephen John; Jacobson,John Carl; Barnes,Barry Francis. Methods and apparatus for operating gas turbine engine combustors. USP2006087093419.
  22. Manteiga,John A.; Tingle,Walter J.; White,Timothy A.; Canillas,Kevin F.. Methods and apparatus for supplying feed air to turbine combustors. USP2006057040096.
  23. Capozzi, Joseph; Zenon, Ruby Lasandra; Turner, Alan Glen; Wallis, Carol Vaczy; Szucs, Peter Nicholas. Methods and apparatus for varying gas turbine engine inlet air flow. USP2003096619916.
  24. Howell, Stephen John; Jacobson, John Carl; McCaffrey, Timothy P.; Barnes, Barry Francis. Methods for assembling gas turbine engine combustors. USP2010057721437.
  25. Firnhaber, Michael C. Rigid and rotatable vanes molded within variably shaped flexible airfoils. USP2017109789636.
  26. Firnhaber, Michael C.; DiBenedetto, Enzo. Seal assembly for a guide vane assembly. USP2017049617864.
  27. Winter, Michael. Systems and methods for altering inlet airflow of gas turbine engines. USP2015109169779.
  28. Wood, Peter John; Zenon, Ruby Lasandra; LaChapelle, Donald George; Mielke, Mark Joseph; Grant, Carl. Turbofan gas turbine engine with variable fan outlet guide vanes. USP2010067730714.
  29. Campbell, Christian X.. Vane assembly with metal trailing edge segment. USP2010117837438.
  30. Campbell,Christian X.. Vane assembly with metal trailing edge segment. USP2008017316539.
  31. Weaver Kevin J,GBX. Variable camber vane. USP2001016179559.
  32. Carroll, Christian A.; Eley, James Allen; Klinetob, Carl Brian. Variable geometry inlet guide vane. USP2009067549839.
  33. Burdick, Andrew D.; Praisner, Thomas J.; Aggarwala, Andrew S.; Hudson, Eric A.; McCaffrey, Michael G.. Variable vane and seal arrangement. USP2017109803559.