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특허 상세정보

Counter-rotating turbine engine and method of assembling same

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) F01D-001/24    F01D-001/00   
미국특허분류(USC) 415/065; 415/068; 415/069; 415/229
출원번호 US-0976496 (2004-10-29)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Armstrong Teasdale LLP
인용정보 피인용 횟수 : 19  인용 특허 : 17
초록이 없습니다.
대표청구항이 없습니다

이 특허에 인용된 특허 (17)

  1. Seda, Jorge F.; Dunbar, Lawrence W.; Gliebe, Philip R.; Szucs, Peter N.; Brauer, John C.; Johnson, James E.; Moniz, Thomas; Steinmetz, Gregory T.. Aircraft engine with inter-turbine engine frame supported counter rotating low pressure turbine rotors. USP2003096619030.
  2. Orlando, Robert Joseph; Moniz, Thomas Ory; Baughman, John Lewis. Aircraft gas turbine engine having variable torque split counter rotating low pressure turbines and booster aft of counter rotating fans. USP2004076763654.
  3. Orlando, Robert Joseph; Moniz, Thomas Ory. Aircraft gas turbine engine with control vanes for counter rotating low pressure turbines. USP2004026684626.
  4. Orlando, Robert Joseph; Moniz, Thomas Ory. Aircraft gas turbine engine with tandem non-interdigitated counter rotating low pressure turbines. USP2004036711887.
  5. Moniz Thomas ; Hauser Ambrose A. ; Seda Jorge F.. Bearing lubrication configuration in a turbine engine. USP1998095813214.
  6. Jones Allen M. (Novi MI). Compliant foil bearing. USP1990084950089.
  7. Seda, Jorge F.; Dunbar, Lawrence W.; Szucs, Peter N.; Brauer, John C.; Johnson, James E.. Counter rotating aircraft gas turbine engine with high overall pressure ratio compressor. USP2004056732502.
  8. Orlando, Robert Joseph; Moniz, Thomas Ory. Counter rotating fan aircraft gas turbine engine with aft booster. USP2004076763653.
  9. Moniz, Thomas Ory; Orlando, Robert Joseph. Counterrotatable booster compressor assembly for a gas turbine engine. USP2004056739120.
  10. Ciokajlo John J. (Henderson NV) Hauser Ambrose A. (Wyoming OH). Counterrotating turbine support assembly. USP1994055307622.
  11. Marsh David N. (Phoenix AZ). Gas turbine engine rear magnetic or foil bearing cooling using exhaust eductor. USP1995095450719.
  12. Paul, Marius. High efficiency gas turbine power generator systems. USP2004046725643.
  13. Pfligler John J. ; Larson Carl A. ; Cunnington George R.. Impingement cooled foil bearings in a gas turbine engine. USP2001096286303.
  14. Giffin ; III Rollin G. ; Johnson James E. ; Crall David W. ; Salvage John W. ; Szucs Peter N.. Turbofan engine with a core driven supercharged bypass duct. USP1998095809772.
  15. Johnson James E.. Turbofan engine with a core driven supercharged bypass duct and fixed geometry nozzle. USP1998095806303.
  16. Bartos James W.. Turbofan engine with a low pressure turbine driven supercharger in a bypass duct operated by a fuel rich combustor and a. USP1999025867980.
  17. Baughman, John Lewis; Orlando, Robert Joseph; Moniz, Thomas Ory. Variable torque split aircraft gas turbine engine counter rotating low pressure turbines. USP2004076763652.

이 특허를 인용한 특허 피인용횟수: 19

  1. Arar, Malath Ibrahim. Active clearance control system and method for gas turbine. USP2015038973373.
  2. Vetters, Daniel K.; Cedoz, Robert W.. Apparatus and method for transmitting a rotary input into counter-rotating outputs. USP2011128075438.
  3. Cracco, Cedric. Compressor for an axial turbine engine with double contra-rotating rotors. USP20190410260348.
  4. Vetters, Daniel K.; Cedoz, Robert W.. Coupling assembly. USP2011098021267.
  5. Copeland, Andrew D.. Dual clutch arrangement and method. USP2013098534074.
  6. Schilling, Jan Christopher; Kray, Nicholas Joseph. Fiber composite reinforced aircraft gas turbine engine drums with radially inwardly extending blades. USP2011098011877.
  7. Sheridan, William G.. Fundamental gear system architecture. USP20190310221770.
  8. Sheridan, William G.; McCune, Michael E.; Schwarz, Frederick M.; Kupratis, Daniel Bernard; Suciu, Gabriel L.; Ackermann, William K.; Husband, Jason. Fundamental gear system architecture. USP2014068756908.
  9. Suciu, Gabriel L.; Merry, Brian D.; Dye, Christopher M.; Johnson, Steven B.. Gas turbine engine compressor arrangement. USP2014048684303.
  10. Sheridan, William G.. Gear system architecture for gas turbine engine. USP2017129840969.
  11. McCune, Michael E.; Husband, Jason; Schwarz, Frederick M.; Kupratis, Daniel Bernard; Suciu, Gabriel L.; Ackermann, William K.. Geared architecture for high speed and small volume fan drive turbine. USP2014128899915.
  12. McCune, Michael E.; Husband, Jason; Schwarz, Frederick M.; Kupratis, Daniel Bernard; Suciu, Gabriel L.; Ackermann, William K.. Geared architecture for high speed and small volume fan drive turbine. USP2017099752511.
  13. McCune, Michael E.; Husband, Jason; Schwarz, Frederick M.; Kupratis, Daniel Bernard; Suciu, Gabriel L.; Ackermann, William K.. Geared architecture for high speed and small volume fan drive turbine. USP2017049631558.
  14. McCune, Michael E.; Husband, Jason; Schwarz, Frederick M.; Kupratis, Daniel Bernard; Suciu, Gabriel L.; Ackermann, William K.. Geared architecture for high speed and small volume fan drive turbine. USP2014068747055.
  15. Snyder, Tony; Blake, Gregory; Copeland, Andrew D.. Gearing arrangement. USP2013078480527.
  16. Haskin, Jay. Power transmission system for turbine or compressor having counter-rotating blades. USP2017089745860.
  17. Haskin, Jay. Power transmission system for turbine, a turbocharger, a compressor, or a pump. USP20190110190436.
  18. Haskin, Jay. Power transmission system for turbines or compressors having counter-rotating blades. USP20190410260367.
  19. Haskin, Jay. Turbine apparatus with counter-rotating blades. USP2016089410430.