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특허 상세정보

Gas turbine engine curved diffuser with partial impingement cooling apparatus for transitions

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) F02C-001/00   
미국특허분류(USC) 060/760; 060/752
출원번호 US-0345725 (2006-02-02)
등록번호 US7870739 (2011-01-03)
발명자 / 주소
출원인 / 주소
인용정보 피인용 횟수 : 1  인용 특허 : 23

A curved diffuser (210) in a gas turbine engine (201) directs a primary portion of air flow from a compressor (202) through a curved discharge opening (213) into a plenum (220). The curved diffuser (210) also comprises ports (217) through which a secondary portion of air passes into confined space (225) that is defined in part by a pressure boundary element that may be comprised of at least one plate (222) or at least one conduit (306). The at least one plate (222) and the at least one conduit (306) respectively comprise apertures (246, 312) through whic...


I claim as my invention: 1. A gas turbine engine comprising:a. an air compressor;b. a plurality of combustion chambers, each comprising an intake end and an outlet end, and connected in parallel with respect to airflow;c. a plurality of transitions, each comprising an inboard side, two lateral sides, and an outboard side, and each associated with a respective combustion chamber, providing fluid communication between the respective outlet end and an entrance port of a turbine;d. a curved diffuser in fluid communication between the compressor and a plenum ...

이 특허에 인용된 특허 (23)

  1. Geoffrey M Dailey GB; Anthony Pidcock GB; Desmond Close GB. Combuster arrangement. USP2002016334297.
  2. Kalbfuss Richard (Mannheim DEX). Combustion chamber for a gas turbine. USP1980074211069.
  3. Johnson Robert H. (Bolton Landing NY) Wilkes Colin (Scotia NY). Combustion control system. USP1981034255927.
  4. Daniel Mark Brown ; David Orus Fitts ; Stephen Hugh Black FR. Combustor liner cooling thimbles and related method. USP2002116484505.
  5. Sato Isao (Hitachi JPX) Kato Fumio (Hitachi JPX) Uchiyama Yoshihiro (Hitachi JPX) Iizuka Nobuyuki (Hitachi JPX) Hata Tsuneyuki (Hitachi JPX). Combustor of gas turbine with features for vibration reduction and increased cooling. USP1981114297843.
  6. Stuttaford, Peter; Fischer, Bernhard; Cowburn, David Edwin; Oskooei, Saeid; Fryer, Michael Andrew; Kojovic, Aleksandar; Acton, Jeffrey Scott. Combustor turbine successive dual cooling. USP2003036536201.
  7. Robert Harold Cromer ; William Theodore Bechtel ; Maz Sutcu. Cooling air recycling for gas turbine transition duct end frame and related method. USP2002076412268.
  8. Zimmermann Achim (Mlheim a.d. Ruhr DEX) Beck Karl-Erhard (Berlin DEX) Mohr Klaus D. (Wuppertal DEX). Cylindrical combustion chamber housing of a gas turbine. USP1994115363653.
  9. Moussa Zaher M.. Deswirler system for centrifugal compressor. USP2001086279322.
  10. Jorgensen, Stephen W.; Leahy, Jr., James H.. Effusion cooled transition duct. USP2003056568187.
  11. Coslow Billy Joe ; Whidden Graydon Lane. Gas turbine combustor transition. USP1999055906093.
  12. Butt Graham P. (Ancaster CAX). Gas turbine combustor transition duct forced convection cooling. USP1990024903477.
  13. Campbell David A. (Derby GB2). Gas turbine engine. USP1981094291531.
  14. Bland, Robert; Ellis, Charles; Tiemann, Peter. Gas turbine with a compressor for air. USP2004016672070.
  15. Kwan William,DEX. Heat shield for a gas turbine combustion chamber. USP1999075918467.
  16. Davis ; Jr. Lewis B. (Schenectady NY) Goodwin Walter W. (Loudonville NY) Steber Charles E. (Scotia NY). Impingement cooled transition duct. USP1988014719748.
  17. Eggmann Jean (Baden CHX) Graf Hans (Untersiggenthal CHX) Zaba Tadeusz (Ennetbaden CHX). Method and apparatus for cooling hot gas casings. USP1982074339925.
  18. Gerhold Bruce W. (Rexford NY) Wilkes Colin (Scotia NY). NOx suppressant stationary gas turbine combustor. USP1981114297842.
  19. Herman Avrum S. (Indianapolis IN) Reider Samuel B. (Indianapolis IN). Porous laminated combustor structure. USP1981014244178.
  20. Frutschi Hans U. (Riniken CHX) Wettstein Hans (Fislisbach CHX). Power plant. USP1996095557921.
  21. Vogt Robert L. (Schenectady NY). Sectoral combustor for burning low-BTU fuel gas. USP1980124236378.
  22. Lin Edward J. C. ; Warren ; Jr. Richard Edwin ; Vandervort Christian L.. Tri-passage diffuser for a gas turbine. USP1998045737915.
  23. Barbeau Dennis E. (Liberty Center OH). Turbine engine construction. USP1982024314443.