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특허 상세정보

Nested core gas turbine engine

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) F02C-003/073   
미국특허분류(USC) 060/039.43; 060/723; 060/805; 060/268; 415/068; 415/069
출원번호 US-0947002 (2001-09-05)
발명자 / 주소
대리인 / 주소
    Perman & Green, LLP
인용정보 피인용 횟수 : 25  인용 특허 : 5
초록

A gas turbine engine comprising a combustion chamber section, a turbine section, and a compressor section. The turbine section surrounds the combustion chamber and the compressor section surrounds the turbine section.

대표
청구항

A gas turbine engine comprising a combustion chamber section, a turbine section, and a compressor section. The turbine section surrounds the combustion chamber and the compressor section surrounds the turbine section. a length of extension of at least 0.25 inch. 11. A track arrangement according to claim 10 wherein: (a) said stud ridge receiver trough of said first bent extension has: (i) a front bend having an inside angle within the range of 75° to 85°, inclusive; (ii) a center bend having an inside angle within the range of 15° to 25°, inclusi...

이 특허를 인용한 특허 피인용횟수: 25

  1. Engle, Darren T.; Wilson, Jody W.. Compressor-less micro gas turbine power generating system. USP2012118302403.
  2. Nawrocki, Gilles. Diaphragm with passive flow rate control for compression stage. USP2016099447784.
  3. Vanderspurt, Thomas Henry; Dardas, Zissis A.. Endothermic cracking aircraft fuel system. USP20181010099797.
  4. Vanderspurt, Thomas Henry; Dardas, Zissis A.. Endothermic cracking aircraft fuel system. USP2015109150300.
  5. Vanderspurt, Thomas Henry; Dardas, Zissis A.. Endothermic cracking aircraft fuel system. USP2011098015823.
  6. McCune, Michael E.; Husband, Jason. Flexible support structure for a geared architecture gas turbine engine. USP20190310227893.
  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. Schwarz, Frederick M.; Suciu, Gabriel L.. Gas turbine engine for long range aircraft. USP2018059976489.
  11. Dale, Mark R.. Gas turbine engine with dual compression rotor. USP2014058726635.
  12. Sheridan, William G.. Gear system architecture for gas turbine engine. USP2017129840969.
  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. USP2014128899915.
  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. USP2017099752511.
  15. 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.
  16. 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.
  17. Schwarz, Frederick M.; Kupratis, Daniel Bernard. Geared turbofan engine with a high ratio of thrust to turbine volume. USP20181110138809.
  18. Gaia, Mario; Bini, Roberto. Method and turbine for expanding an organic operating fluid in a rankine cycle. USP2017089726047.
  19. Dev,Sudarshan Paul. Nested core gas turbine engine. USP2007057219490.
  20. Intile, John Charles. Power generation system including afirst turbine stage structurally incorporating a combustor. USP2012128322141.
  21. Platts,David A.. Radial-radial single rotor turbine. USP2006057044718.
  22. Plante, Jean-Sebastien; Rancourt, David; Picard, Mathieu. Rotor assembly having a concentric arrangement of a turbine portion, a cooling channel and a reinforcement wall. USP2017069670840.
  23. Mutou, Yoshihiko; Tanaka, Ryozo. Seal mechanism for use with turbine rotor. USP2016069359958.
  24. Collette, Daniel. UAV pod cooling using integrated duct wall heat transfer. USP2012028123460.
  25. Norris, James W.; Nordeen, Craig A.; Raver, Bernard J.. Variable bypass turbine fan. USP2011108028513.