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특허 상세정보

Carbon seal contaminant barrier system

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) F04D-029/08   
미국특허분류(USC) 415/170.1 ; 415/174.2 ; 415/229 ; 277/058 ; 277/192
출원번호 US-0599028 (1996-02-09)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Woodard, Emhardt, Naughton, Moriarty & McNett
인용정보 피인용 횟수 : 18  인용 특허 : 0
초록

A carbon seal contaminant barrier system for a gas turbine engine including a lip seal for wiping the surface of a rotating seal runner, and a baffle spaced from the rotating seal runner to prevent the impingement of the contaminants on the lip seal. The lip seal and the baffle are spaced axially and cooperate to minimize the contaminants passed to a carbon sealing system. The circumferential carbon sealing ring having a plurality of passages therethrough for delivering pressurized gas adjacent the carbon sealing ring. The pressurized gas being utilized ...

대표
청구항

[ What is claimed is:] [1.] In combination:a gas turbine engine;a mechanical housing within said gas turbine engine;a shaft rotatably mounted within said housing;a carbon seal connected to said housing;a seal runner connected to said shaft, said seal runner arranged adjacent to said carbon seal to form a substantially fluid tight seal therebetween;a lip seal contacting said seal runner; anda baffle spaced from said lip seal and positioned around said seal runner.

이 특허를 인용한 특허 피인용횟수: 18

  1. Litis, Paul T.; Avery, David J.; Smith, Gregory P.; Gunn, John R.; Kurtz, IV, David L.; Brut, Kevin. Carbon seal O-ring cavity sizing. USP2018019869391.
  2. DiBenedetto, Enzo; NguyenLoc, Fred. Forward compartment baffle arrangement for a geared turbofan engine. USP2018029896968.
  3. Bruce, Robert William; Schell, Jerry Donald; Beall, Charles J.. High temperature rod end bearings. USP2009067543992.
  4. Blais, Daniel; Lewis, Alain; Martel, Alain C.. Internally cooled seal runner. USP2017049631508.
  5. Gockel,Richard R.; Robinson,John D.. Internally-cooled seal housing for turbine engine. USP2008087410341.
  6. Liu, Xiaoliu. Method and device for minimizing oil consumption in a gas turbine engine. USP2005046877950.
  7. Alvanos, Ioannis. Non-mechanically fastened TOBI heat shield. USP2014128899924.
  8. Olennikov, Alexander Yurievich. Oil cooled runner. USP2014038678741.
  9. Gildea Greg G. ; Galvin Joseph D. ; Davis Brian. Plenum oil seal. USP2000086109615.
  10. Ullah, M. Rifat; Miller, Jonathan Logan; Kurz, Leslie Charles. Runner for circumferential seals. USP2016069359912.
  11. Labbe, Michel. Seal and bearing assembly for a gas turbine engine and method of assembling same. USP2018069989083.
  12. Desjardins, Michel. Seal assembly for a bearing assembly in a gas turbine engine. USP2018049944399.
  13. Huppe, Roger; Caron, Jean-Francois. Seal runner. USP2018029896953.
  14. Simmers,Douglas Evan. Stretched membrane device. USP2008057374301.
  15. Berry, Jonathan Dwight. System for injecting fuel in a gas turbine combustor. USP2016109476592.
  16. van Kalken, Christian; Agrawal, Sanjay. Uninterruptible power supply apparatus for receiving power from different electrical utility configurations. USP2016069373978.
  17. Bruce,Robert William; Schell,Jerry Donald. Wear resistant variable stator vane assemblies. USP2007057220098.
  18. Roche, Brian; Garrison, Glenn; Patel, Hiren; Eppehimer, John; Vasagar, Manik; Sanville, Mark; Pillai, Saji. Windback device. USP2013078490982.