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특허 상세정보

Power generation system having compressor creating excess air flow and turbo-expander to increase turbine exhaust gas mass flow

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) F02C-006/00    F01K-023/10    F01D-013/00    F02C-003/10    F02C-003/13    F02C-006/02    F02C-006/08    F02C-009/18    F02C-003/04   
출원번호 US-0662805 (2015-03-19)
등록번호 US-9828887 (2017-11-28)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Cusick, Ernest G.
인용정보 피인용 횟수 : 0  인용 특허 : 16
초록

A power generation system may include: a first gas turbine system including a first turbine component, a first integral compressor and a first combustor to which air from the first integral compressor and fuel are supplied. The first integral compressor has a flow capacity greater than an intake capacity of the first combustor and/or the first turbine component, creating an excess air flow. A second gas turbine system may include similar components to the first except but without excess capacity in its compressor. A turbo-expander may be operatively coup...

대표
청구항

1. A power generation system, comprising: a first gas turbine system including a first turbine component, a first integral compressor and a first combustor to which air from the first integral compressor and fuel are supplied, the first combustor arranged to supply hot combustion gases to the first turbine component, and the first integral compressor having a flow capacity greater than an intake capacity of at least one of the first combustor and the first turbine component, creating an excess air flow,a second gas turbine system including, a second turb...

이 특허에 인용된 특허 (16)

  1. Anand, Ashok Kumar; Berrahou, Philip Fadhel; Jandrisevits, Michael. Compressor discharge bleed air circuit in gas turbine plants and related method. USP2003046543234.
  2. Ashok Kumar Anand ; Philip Fadhel Berrahou ; Michael Jandrisevits. Compressor discharge bleed air circuit in gas turbine plants and related method. USP2002096442941.
  3. Benjamin C. Wiant ; Dennis A. Horazak. Flow balanced gas turbine power plant. USP2002086430915.
  4. Kopko, William L.. Gas turbine operative at high ambient temperatures. USP2004046718771.
  5. Santini, Marco. Gas turbines in mechanical drive applications and operating methods. USP2016119488102.
  6. Schlak, Daniel Keith. Integral gas turbine, flywheel, generator, and method for hybrid operation thereof. USP2017019540998.
  7. Dixon James T. (Jupiter FL) Glickstein Marvin R. (North Palm Beach FL). Integrated auxiliary power system. USP1994115363641.
  8. George E. Wilmot, Jr. ; Gregory M. Ott. Integrated thermal management and coolant system for an aircraft. USP2002076415595.
  9. Scipio, Alston I.; Freeman, Thomas John; Obenhoff, Ryan Eric; Ekanayake, Sanji; Cocca, Michael Anthony; Yarnold, Mike; Warwick, Douglas Corbin; Klosinski, Joseph. Method and apparatus for optimizing the operation of a turbine system under flexible loads. USP2016039297316.
  10. Berry, Jacob. Method for gas turbine operation during under-frequency operation through use of air extraction. USP2013078479523.
  11. Wichmann, Lisa Anne; Snook, Daniel David; Draper, Samuel David; Dion Ouellet, Noémie; Rittenhouse, Scott Allen. Method of operating a stoichiometric exhaust gas recirculation power plant. USP2013068453462.
  12. Childers, Scott A.. Methods relating to gas turbine control and operation. USP2013018355854.
  13. Berman Paul A. (Plymouth Meeting PA). Power generating plant employing a reheat pressurized fluidized bed combustor system. USP1984104476674.
  14. Minto, Karl Dean. Power plant and control method. USP2012088245493.
  15. Houghton James (Newport Beach CA) Lamprecht Dieter G. (Huntington Beach CA). Process and economic use of excess compressed air when firing low BTU gas in a combustion gas turbine. USP1995075433069.
  16. Kesseli James B.. Turbine engine with turbocompressor for supplying atomizing fluid to turbine engine fuel system. USP1999115992139.