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특허 상세정보

Electricity generating system having an annular combustor

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) F02C-003/06   
미국특허분류(USC) 600/393.6 ; 600/390.8 ; 600/392.81 ; 600/395.11 ; 600/734
출원번호 US-0319478 (1999-08-18)
국제출원번호 PCT/US97/22007 (1997-12-03)
§371/§102 date 19990818 (19990818)
국제공개번호 WO-9825082 (1998-06-11)
발명자 / 주소
출원인 / 주소
인용정보 피인용 횟수 : 25  인용 특허 : 9
초록

An electricity generating system having a body (159), an annular combustor (14), a turbine (16), a compressor chamber and a compressor (102) positioned within the compressor chamber. An inlet port is in fluid communication with the compressor chamber and an exit port is in fluid communication with the turbine. A plurality of magnets (MG) is secured to the rotor (18) and a stator (22) made of mangnetically attracted material, such as iron, and having a stator winding provided in the body (159). The stator winding is positioned in close proximity to the pl...

대표
청구항

[ We claim:] [1.]1. An electricity generating system, comprising:a body;a combustor provided in said body;a turbine made of a plurality of turbine blades secured to a rotor, provided in said body and in fluid communication with said combustor;a compressor chamber provided in said body and in fluid communication with said combustor;a plurality of compressor blades secured to said rotor, said compressor blades positioned within a compressor chamber;an air inlet port in fluid communication with said compressor chamber;an exit port in fluid communication wit...

이 특허를 인용한 특허 피인용횟수: 25

  1. Kesseli, James B.; Nash, James S.. Ceramic-to-metal turbine shaft attachment. USP2015069051873.
  2. Baldwin, Matthew Stephen. Ceramic-to-metal turbine volute attachment for a gas turbine engine. USP20181010094288.
  3. Vandale, Daniel D.; Simons, Girard A.. Combustor with staged fuel premixer. USP2010117836698.
  4. Alexander, Eric; Jones, Anthony; Harris, Mark; Barkley, Robert. Damping system for an expendable gas turbine engine. USP2005096942451.
  5. Donnelly, Frank Wegner; Dewis, David William. Dispatchable power from a renewable energy facility. USP2014108866334.
  6. Parsons, Douglas A.; Semyanko, Constantine. Fuel supply control for a gas turbine including multiple solenoid valves. USP2004096786049.
  7. Dewis, David William; Kesseli, James; Donnelly, Frank Wegner; Wolf, Thomas; Upton, Timothy; Watson, John D.. Gas turbine energy storage and conversion system. USP2013088499874.
  8. Dewis, David William; Kesseli, James; Donnelly, Frank Wegner; Wolf, Thomas; Watson, John D.. Gas turbine energy storage and conversion system. USP2014048708083.
  9. Cunha, Frank J.; Erbas-Sen, Nurhak. Gas turbine engine combustor liner assembly with convergent hyperbolic profile. USP20190110174949.
  10. Dierberger, James A.. Gas turbine engine component with upstream-directed cooling film holes. USP2018059958160.
  11. Donnelly, Frank Wegner; Dewis, David William. Gas turbine engine configurations. USP2014038669670.
  12. Grote, Holger; Kollenberg, Wolfgang; Tertilt, Marc. Heat shield element, in particular for lining a combustion chamber wall. USP2014108857190.
  13. Teets, Joseph Michael; Teets, Jon William. Hybrid microturbine for generating electricity. USP2009087574867.
  14. Hagshenas, Buzz; Alexander, Eric; Jones, Anthony; Harris, Mark. Long term storage capable damping system for an expendable gas turbine engine. USP2005056896480.
  15. Kesseli, James B.; Baldwin, Matthew Stephen. Metallic ceramic spool for a gas turbine engine. USP2015038984895.
  16. Dewis, David. Method for gas turbine light-off. USP2004116810677.
  17. Lam, Kam-Kei. Method for starting a combustion system. USP20190410260368.
  18. Teets, Joseph Michael; Teets, Jon William. Microturbine with CHP system having a distillation apparatus. USP2009087574853.
  19. Hartzheim, Anthony A.. Multiple control loop acceleration of turboalternator after reaching self-sustaining speed previous to reaching synchronous speed. USP2004126834226.
  20. Hartzheim, Anthony A.. Multiple control loop acceleration of turboalternator previous to self-sustaining speed. USP2004116819999.
  21. Hartzheim, Anthony A.. Offload control of turboalternator with rich burn quick quench lean burn combustor to prevent blowout of combustor. USP2004126836720.
  22. Jones, Anthony; Harris, Mark; Alexander, Eric; Lydon, Patrick. Rotational system for an expendable gas turbine engine. USP2013058438858.
  23. Jones,Anthony; Harris,Mark; Alexander,Eric; Lydon,Patrick. Static structure for an expendable gas turbine engine. USP2007037194866.
  24. Snyder, Daniel A.; Lana, Kyle Charles; Sandoval, Jonathan Perry; Virkler, Scott Daniel; Taraskevich, Jaimie; Otero, Edwin. Turbine blade damper seal. USP20181010113434.
  25. Bouiller,Philippe; Morreale,Serge; Rousselin,Stephane. Turbomachine including an integrated electricity generator. USP2007057224082.