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System for combining flow from compressor bleeds of an industrial gas turbine for gas turbine performance optimization 원문보기

IPC분류정보
국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판)
  • F02C-007/18
  • F02C-007/00
출원번호 US-0482946 (2000-01-14)
발명자 / 주소
  • Marks, Paul T.
출원인 / 주소
  • General Electric Co.
대리인 / 주소
    Nixon & Vanderhye
인용정보 피인용 횟수 : 32  인용 특허 : 8

초록

A gas turbine cooling and sealing air supply system design for an industrial gas turbine is provided which effectively eliminates the need to dissipate bleed pressure across an orifice or similar device, thereby to optimize full load ISO performance. This flow system is realized by providing cross o

대표청구항

A gas turbine cooling and sealing air supply system design for an industrial gas turbine is provided which effectively eliminates the need to dissipate bleed pressure across an orifice or similar device, thereby to optimize full load ISO performance. This flow system is realized by providing cross o

이 특허에 인용된 특허 (8)

  1. Schulze Wallace M. (West Chester OH), Auxiliary air system for gas turbine engine.
  2. Bruun Eugene R. (Simsbury CT) Kos Joseph M. (Holyoke MA), Control of aircraft bleed air stage mixing.
  3. Brockett Walter D. (North Haven CT), Ejector assisted compressor bleed.
  4. Smith Alan W. (Cincinnati OH), Engine bleed air supply system.
  5. Nishijima Tsunemasa (Hitachi JPX), Gas turbine system.
  6. Hines William R. (Montgomery OH), Hot day M & I gas turbine engine and method of operation.
  7. Kumata Kazuhiko (Katsuta JPX) Iizuka Nobuyuki (Hitachi JPX) Kunihiro Masashi (Hitachi JPX) Kurosawa Soichi (Hitachi JPX), Method and apparatus for controlling temperatures of turbine casing and turbine rotor.
  8. Guimier Michel (Mormant FRX) Paris Philippe M. (Le Mee Sur Seine FRX), System for ventilating the turbine disks and stator of a turbo jet engine.

이 특허를 인용한 특허 (32)

  1. Weber, David Wayne, Blade cooling circuit feed duct, exhaust duct, and related cooling structure.
  2. Lacy, Benjamin Paul; Johnson, Thomas Edward; York, William David; Zuo, Baifang, Coannular oil injection nozzle.
  3. York, William D.; Ziminsky, Willy S.; Lacy, Benjamin P., Coaxial fuel and air premixer for a gas turbine combustor.
  4. Scipio, Alston Ilford; Ekanayake, Sanji, Compressor bellmouth with a wash door.
  5. Bozzi, Luca; Mantero, Marco; Bonzani, Federico, Control method for cooling a turbine stage in a gas turbine.
  6. Laster,Walter Ray; Bandaru,Ramarao V.; Baer,Joan Mae, Control of gas turbine for catalyst activation.
  7. Golden, Christopher Lee; Earnhardt, Dustin Michael; Iduate, Michelle Jessica; Lewis, Bryan David; Porter, Christopher Donald; Weber, David Wayne, Cooling structure for stationary blade.
  8. Weber, David Wayne; Earnhardt, Dustin Michael; Foster, Gregory Thomas; Iduate, Michelle Jessica, Cooling structure for stationary blade.
  9. Ciofini, Maurizio; Rossin, Stefano; DeProsperis, Roberto, Cooling system for a gas turbine and corresponding operation method.
  10. Douglas, Jonathan D.; Bianchi, Marcus V. A.; Rossi, Todd M., Estimating evaporator airflow in vapor compression cycle cooling equipment.
  11. Zhang, Hua; Ball, Jr., David Wesley; Eluripati, Ravi Praveen; Pompey, Christina Renee; Whaling, Kenneth Neil, Gas turbine ejector and method of operation.
  12. Schwarz, Frederick M.; Forcier, Matthew P., High temperature disk conditioning system.
  13. Jonqueres, Michel A.; Araki, Roy, Low-pressure bleed air aircraft environmental control system.
  14. Feigl, Markus; Itzel, Gary Michael, Method and system for controlling gas turbine performance with a variable backflow margin.
  15. Weber, Kent; Kyriazopoulos, Athanasios; Hightower, Peter C.; Burie, Bradley J., Method and systems for bleed air supply.
  16. Arias Chao, Manuel; Wippel, Bernhard; Balmer, Christian; Jakoby, Ralf, Method for operating a gas turbine plant and gas turbine plant for implementing the method.
  17. Doebbeling, Klaus; Nemet, Anton; Zajadatz, Martin; Waelchli, Rene, Method of operating a gas turbine assembly and the gas turbine assembly.
  18. Eluripati, Ravi Praveen S.; Ball, Jr., David W.; Whaling, Kenneth N.; Davis, James L.; Saravanan, Nattamai V.; Sengar, Ajit S., Mixer for cooling and sealing air system for turbomachinery.
  19. Ekanayake, Sanji; Kim, Kihyung; Scipio, Alston Ilford; Tong, Leslie Yung Min; Yarnold, Michael Wesley, Power generation system having compressor creating excess air flow and turbo-expander using same.
  20. Ekanayake, Sanji; Freeman, Thomas John; Memmer, John David; Rehg, Timothy Joseph; Scipio, Alston Ilford, Power generation system having compressor creating excess gas flow for supplemental gas turbine system.
  21. Scipio, Alston Ilford; Ekanayake, Sanji; Shaffer, Jason Brian; Klosinski, Joseph Philip; Mathai, George Vargese, Power plant including a static mixer and steam generating system via turbine extraction and compressor extraction.
  22. Klosinski, Joseph Philip; Scipio, Alston Ilford; Ekanayake, Sanji; Mathai, George Vargese, Power plant including an ejector and steam generating system via turbine extraction.
  23. Klosinski, Joseph Philip; Cocca, Michael Anthony; Scipio, Alston Ilford; Ekanayake, Sanji, Power plant including an ejector and steam generating system via turbine extraction and compressor extraction.
  24. Klosinski, Joseph Philip; Cocca, Michael Anthony; Scipio, Alston Ilford; Ekanayake, Sanji; Shaffer, Jason Brian, Power plant including exhaust gas coolant injection system and steam generating system via turbine extraction.
  25. Klosinski, Joseph Philip; Scipio, Alston Ilford; Ekanayake, Sanji, Power plant with steam generation via combustor gas extraction.
  26. Patel, Kaushal Vishnubhai; Farrar, James Stewart; Maki, William Eric, Reheat steam bypass system.
  27. Rhoden, William E.; Jalbert, Peter L.; Beaupre, Rudolph Thomas; Scott, David Russell, Small engine cooled cooling air system.
  28. Saha, Rajarshi; Donkada, Santhosh; Mazumder, Indrajit; Pemmi, Bhaskar, System for controlling a cooling flow from a compressor section of a gas turbine.
  29. Roush, Eric David; Parker, William Andrew, System for delivering air from a multi-stage compressor to a turbine portion of a gas turbine engine.
  30. Laurello, Vincent P.; Tham, Kok-Mun, Vane carrier temperature control system in a gas turbine engine.
  31. Whaling, Kenneth Neil; Erickson, Dean Matthew; Zhang, Hua; Ball, David Wesley; Pompey, Christina Renee, Variable geometry ejector.
  32. Wolfe, Christopher E.; Beadie, Douglas F.; Whaling, Kenneth N.; Ball, David W.; McGovern, Kevin T.; Eluripati, Ravi Praveen; Samudrala, Omprakash, Variable motive nozzle ejector for use with turbine engines.
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