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특허 상세정보

Gas turbine engine assembly and methods of assembling same

특허상세정보
국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) F02K-003/02   
미국특허분류(USC) 060/268; 060/226.1; 415/061
출원번호 UP-0553571 (2006-10-27)
등록번호 US-7832193 (2011-01-16)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Louke, Marcella R.
인용정보 피인용 횟수 : 38  인용 특허 : 21
초록

A method of assembling a gas turbine assembly includes providing a core gas turbine engine including a high-pressure compressor, a combustor, and a turbine, coupling a low-pressure turbine to the core gas turbine engine, coupling a booster compressor to a gearbox, and coupling the gearbox to the low-pressure turbine such that the booster compressor is driven by the low-pressure turbine.

대표
청구항

What is claimed is: 1. A method of assembling a gas turbine assembly, said method comprising: providing a core gas turbine engine including a high-pressure compressor, a combustor, and a turbine; coupling a low pressure turbine to the core gas turbine engine; coupling a booster compressor to a gearbox; coupling the gearbox to the low-pressure turbine such that the booster compressor is driven by the low-pressure turbine; coupling a drive shaft to the low pressure turbine; and coupling the gearbox between the drive shaft and the booster compressor such t...

이 특허에 인용된 특허 (21)

  1. 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.
  2. Orlando, Robert Joseph; Moniz, Thomas Ory. Aircraft gas turbine engine with tandem non-interdigitated counter rotating low pressure turbines. USP2004036711887.
  3. 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.
  4. Orlando, Robert Joseph; Moniz, Thomas Ory. Counter rotating fan aircraft gas turbine engine with aft booster. USP2004076763653.
  5. Orlando,Robert Joseph; Moniz,Thomas Ory. Counter-rotating gas turbine engine and method of assembling same. USP2007037186073.
  6. Moniz, Thomas Ory; Orlando, Robert Joseph. Counterrotatable booster compressor assembly for a gas turbine engine. USP2004056739120.
  7. Moniz,Thomas Ory; Orlando,Robert Joseph. Gas turbine engine assembly and methods of assembling same. USP2009027493753.
  8. Moniz,Thomas Ory; Orlando,Robert Joseph. Gas turbine engine assembly and methods of assembling same. USP2009027490460.
  9. Moniz,Thomas Ory; Orlando,Robert Joseph. Gas turbine engine assembly and methods of assembling same. USP2009027490461.
  10. Moniz,Thomas Ory; Orlando,Robert Joseph. Gas turbine engine assembly and methods of assembling same. USP2009027493754.
  11. Orlando, Robert Joseph; Moniz, Thomas Ory. Gas turbine engine assembly and methods of assembling same. USP2009057526913.
  12. Orlando, Robert Joseph; Moniz, Thomas Ory. Gas turbine engine assembly and methods of assembling same. USP2009047513103.
  13. Orlando Robert J.. Gear driven booster. USP2000126158210.
  14. Adamson Arthur P. (Cincinnati OH) Butler Lawrence (Cincinnati OH). High bypass turbofan engine having a partially geared fan drive turbine. USP1990044916894.
  15. Anthony L. DiPietro, Jr.. Integrated fan-core twin spool counter-rotating turbofan gas turbine engine. USP2002016339927.
  16. Johnson,James Edward. Methods and apparatus for assembling a gas turbine engine. USP2006117140174.
  17. Rohra Alois (Munich DEX) Geidel Helmut A. (Karlsfeld DEX). Turbofan engine having a contrarotating low-pressure compressor. USP1994015274999.
  18. Adamson Arthur P. (Cincinnati OH) Wall Robert A. (Wyoming OH). Turbofan engine having a counterrotating partially geared fan drive turbine. USP1990114969325.
  19. Coplin John F. (Derby GB2). Turbofan gas turbine engine. USP1989054827712.
  20. Perry Derick A. (Derby GB2). Turbofan gas turbine engine. USP1988064751816.
  21. 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: 38

  1. Carter, Bruce Alan; Ganiger, Ravindra Shankar; Mondal, Bhaskar Nanda; Miller, Jacob Patrick; Mahesh, Sivakumar; Kirkeng, Kevin L.; Vanapalli, Veeraraju. Bearing assembly for supporting a rotor shaft of a gas turbine engine. USP2018039909451.
  2. Wallace, Thomas Tracy; Simpson, William Joseph; List, John Howard; Tao, Jason Jianxin; Steen, Tod Robert. Dynamic load reduction system. USP2015109169728.
  3. Sheridan, William G.. Fan drive planetary gear system integrated carrier and torque frame. USP2015069068629.
  4. Schilling, Jan Christopher; Kray, Nicholas Joseph. Fiber composite reinforced aircraft gas turbine engine drums with radially inwardly extending blades. USP2011098011877.
  5. Sheridan, William G.. Fundamental gear system architecture. USP20190310221770.
  6. 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.
  7. Suciu, Gabriel L.; Merry, Brian D.; Dye, Christopher M.; Johnson, Steven B.. Gas turbine engine compressor arrangement. USP2014048684303.
  8. Johnson, Steven Douglas; Miller, Brandon Wayne; Gonyou, Craig Alan. Gas turbine engine dual sealing cylindrical variable bleed valve. USP20190210208676.
  9. Merry, Brian D.; Suciu, Gabriel L.. Gas turbine engine shaft bearing arrangement. USP20181210145266.
  10. Merry, Brian D.; Suciu, Gabriel L. Gas turbine engine shaft bearing configuration. USP2013088511061.
  11. Merry, Brian D.; Suciu, Gabriel L.. Gas turbine engine shaft bearing configuration. USP2013038402741.
  12. Merry, Brian D.; Suciu, Gabriel L.; Hasel, Karl L.. Gas turbine engine shaft bearing configuration. USP2015119194329.
  13. Merry, Brian D.; Suciu, Gabriel L.; Hasel, Karl L.. Gas turbine engine shaft bearing configuration. USP2014108863491.
  14. Merry, Brian D.; Suciu, Gabriel L.; Hasel, Karl L.. Gas turbine engine shaft bearing configuration. USP20190210215094.
  15. Menheere, David; Kostka, Richard; Dubreuil, Jean. Gas turbine engine with transmission. USP2016059347373.
  16. Sheridan, William G.. Gear system architecture for gas turbine engine. USP2017129840969.
  17. 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.
  18. 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.
  19. 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.
  20. 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.
  21. Magowan, John W.. Geared fan with inner counter rotating compressor. USP2016019228535.
  22. Magowan, John W.. Geared fan with inner counter rotating compressor. USP20181110125694.
  23. Houston, David P.; Kupratis, Daniel Bernard; Schwarz, Frederick M.. Geared turbofan gas turbine engine architecture. USP2017089739206.
  24. Houston, David P.; Kupratis, Daniel Bernard; Schwarz, Frederick M.. Geared turbofan gas turbine engine architecture. USP2017119828944.
  25. Kupratis, Daniel Bernard; Schwarz, Frederick M.. Geared turbofan gas turbine engine architecture. USP2015018935913.
  26. Kupratis, Daniel Bernard; Schwarz, Frederick M.. Geared turbofan gas turbine engine architecture. USP2014118887487.
  27. Kupratis, Daniel Bernard; Schwarz, Frederick M.. Geared turbofan gas turbine engine architecture. USP2015129222417.
  28. Kupratis, Daniel Bernard; Schwarz, Frederick M.. Geared turbofan gas turbine engine architecture. USP20180710030586.
  29. Merry, Brian D.; Suciu, Gabriel L.; Brilliant, Lisa I.; Rose, Becky E.; Dong, Yuan; Balamucki, Stanley J.. LPC flowpath shape with gas turbine engine shaft bearing configuration. USP2015059038366.
  30. Sabnis, Jayant. Thrust efficient turbofan engine. USP20180810047699.
  31. Sabnis, Jayant. Thrust efficient turbofan engine. USP20180810047700.
  32. Sabnis, Jayant. Thrust efficient turbofan engine. USP20180810047701.
  33. Sabnis, Jayant. Thrust efficient turbofan engine. USP20180810060391.
  34. Sabnis, Jayant. Thrust efficient turbofan engine. USP20180810047702.
  35. Sabnis, Jayant. Thrust efficient turbofan engine. USP2017049624827.
  36. Sabnis, Jayant. Thrust efficient turbofan engine. USP2015069051877.
  37. Sabnis, Jayant. Thrust efficient turbofan engine. USP2017049624828.
  38. Kupratis, Daniel B.. Turbofan with gear-driven compressor and fan-driven core. USP2015049003808.