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특허 상세정보

Gas generators

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) F02C-003/16    F02C-003/14   
미국특허분류(USC) 60/3914 ; 60/3935
출원번호 US-0489063 (1974-07-16)
우선권정보 UK-0006158 (1972-02-09)
발명자 / 주소
인용정보 피인용 횟수 : 26  인용 특허 : 0
초록

Improvements in a gas generator having a “rambine”rotor on which compression, combustion and expansion take place. The improvements include a counter rotating compressor rotor with blades shaped to impart a component of velocity in the direction of rotation of the compressor rotor, hence increasing the whirl velocity of inlet air to the rambine rotor. Preferred embodiments include a plurality of compressor rotors for successively increasing the relative whirl velocity; a rambine rotor having a combustion zone with increasing cross-sectional area over an ...

대표
청구항

In a gas generator including housing means having an air inlet and an exhaust gas outlet, bearing means mounted inwardly of said housing means, a rambine rotor; said rambine rotor being rotatably mounted on said bearing means and having a plurality of blades, each of said blades and a next adjacent one of said blades defining an inlet passage for compressing air induced from said air inlet, there being an axially extending region downstream of said inlet passages, and means for dispensing fuel into said axially extending region for combustion with air re...

이 특허를 인용한 특허 피인용횟수: 26

  1. Bland, Robert J.. At least one combustion apparatus and duct structure for a gas turbine engine. USP2010117836677.
  2. Bland, Robert J.. Axially staged combustion system for a gas turbine engine. USP2009127631499.
  3. Levesque Jean-Paul (P.O. Box 568 Schefferville ; County of Duplessis CAX G0G 2T0). Centrifugal chambers gas turbine. USP1983014368619.
  4. Kendrick, Donald W.. Combustion cavity layouts for fuel staging in trapped vortex combustors. USP2014048689562.
  5. Anatoly Rakhmailov RU. Gas turbine engine. USP2002106460343.
  6. Anatoly Rakhmailov RU. Gas turbine engine. USP2002106460324.
  7. Anatoly Rakhmailov RU. Gas turbine engine. USP2002046363708.
  8. Anatoly Rakhmailov RU. Gas turbine engine. USP2002096442945.
  9. Rakhmailov Anatoly,RUX. Gas turbine engine. USP2001106305157.
  10. Rakhmailov Anatoly,RUX ; Yaishnikov Valentin,UAX ; Kolotilenko Mikhail,UAX ; Rakhmailov Oleg,RUX ; Drozd Igor,RUX ; Kalin Martin. Gas turbine engine. USP2001026189311.
  11. Rakhmailov, Anatoly. Gas turbine engine. USP2003056557337.
  12. Rakhmailov Anatoly,RUX ; Yaishnikov Valentin,UAX ; Kolotilenko Mikhail,UAX ; Rakhmailov Oleg,RUX ; Drozd Igor,RUX. Gas turbine engine having a bladed disk. USP2001086272844.
  13. Rakhmailov Anatoly,RUX. Gas turbine engine having counter rotating turbines and a controller for controlling the load driven by one of the turbines. USP2000116145296.
  14. Anatoly Rakhmailov RU. Gas turbine engine with exhaust compressor having outlet tap control. USP2002066397576.
  15. Lawlor,Shawn P.; Novaresi,Mark A.; Cornelius,Charles C.. Gas turbine power plant with supersonic shock compression ramps. USP2008107434400.
  16. Kendrick, Donald W.. Method of fuel staging in combustion apparatus. USP2013108549862.
  17. Rakhmailov Anatoly,RUX. Method of operation of a gas turbine engine and a gas turbine engine. USP2001046212871.
  18. Shawn P. Lawlor. Ramjet engine for power generation. USP2002086434924.
  19. Brouillette,Martin; Plante,Jean S��bastien. Rotary ramjet engine. USP2008037337606.
  20. Lawlor, Shawn P.; Steele, Robert C.; Kendrick, Donald. Rotary ramjet engine with flameholder extending to running clearance at engine casing interior wall. USP2004026694743.
  21. Lawlor,Shawn P.; Novaresi,Mark A.; Cornelius,Charles C.. Supersonic compressor. USP2008027334990.
  22. Lawlor,Shawn P.; Novaresi,Mark A.; Cornelius,Charles C.. Supersonic gas compressor. USP2007117293955.
  23. Kendrick,Donald; Lawlor,Shawn P.; Steele,Robert C.. Trapped vortex combustor. USP2006027003961.
  24. Steele, Robert C.; Edmonds, Ryan G.; Williams, Joseph T.; Baldwin, Stephen P.. Vortex combustor for low NOX emissions when burning lean premixed high hydrogen content fuel. USP2012118312725.
  25. Steele, Robert C.; Edmonds, Ryan G.; Williams, Joseph T.; Baldwin, Stephen P.. Vortex combustor for low NOx emissions when burning lean premixed high hydrogen content fuel. USP2009107603841.
  26. Kendrick, Donald W.. Vortex premixer for combustion apparatus. USP2014048689561.