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Gas turbine engine with fuel booster

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) F02C-006/08   
미국특허분류(USC) 060/782;
출원번호 US-0532853 (2008-03-27)
등록번호 US-8448447 (2013-05-28)
우선권정보 EP-07006445 (2007-03-28)
국제출원번호 PCT/EP2008/053586 (2008-03-27)
§371/§102 date 20090924 (20090924)
국제공개번호 WO2009/089921 (2009-07-23)
발명자 / 주소
출원인 / 주소
인용정보 피인용 횟수 : 0  인용 특허 : 16
초록
▼

A gas turbine engine including a compressor section, a combustor section including a combustor, a turbine section, a gaseous fuel supply conduit with an upstream section and a downstream section, a fuel booster, and a heat exchanger is provided. The fuel booster is located in the gaseous fuel supply conduit. The fuel booster has a driving expander with a driving fluid inlet and a driving fluid outlet for discharging expanded air and a fuel compressor with a low pressure fuel inlet connected to the upstream section of the gaseous fuel supply conduit and a...

대표
청구항
▼

1. A gas turbine engine, comprising: a compressor section;a combustor section including a combustor;a turbine section;a gaseous fuel supply conduit with an upstream section and a downstream section;a fuel booster located in the gaseous fuel supply conduit, the fuel booster comprising: a driving expander with a driving fluid inlet and a driving fluid outlet,a fuel compressor including a fuel inlet, the fuel inlet being connected to the upstream section, the fuel compressor also including a fuel outlet, the fuel outlet being connected to the downstream sec...

이 특허에 인용된 특허 (16)

  1. Glickstein Marvin R. (North Palm Beach FL). Aircraft cooling method. USP1995055414992.
  2. Stahl Charles R. (Scotia NY). Closed cycle gas turbine for gaseous production. USP1984034434613.
  3. Wright E. Scott (Mesa AZ). Endothermic fuel power generator and method. USP1992115161365.
  4. Fletcher,Paul; Oswald,James I. Gas fuel compression by liquification. USP2007097266946.
  5. Johnson David M. (Mainville OH). Gas turbine engine case thermal control flange. USP1993065219268.
  6. Althaus Rolf (Flawil CHX). Gas turbine plant. USP1994055313783.
  7. Olmes, Sven; Reiter, Wilhelm; Zierer, Thomas. Gas turbine with heat exchanger for cooling compressed air and preheating a fuel. USP2010107810332.
  8. Day William H. (Avon CT). High-efficiency gas turbine engine. USP1993085233823.
  9. Rao, Ashok. Humid air turbine cycle with carbon dioxide recovery. USP2009127637093.
  10. Dixon James T. (Jupiter FL) Glickstein Marvin R. (North Palm Beach FL). Integrated auxiliary power system. USP1994115363641.
  11. George E. Wilmot, Jr. ; Gregory M. Ott. Integrated thermal management and coolant system for an aircraft. USP2002076415595.
  12. Fetescu, Mircea; Liebig, Erhard; Rickli, Jean-Pierre; Stirnimann, Franz. Method for operating a power plant having turbine cooling. USP2003056560966.
  13. Yu, Hong. Re-fired gas turbine engine. USP2004116817187.
  14. Cloyd Scott T. (Lake Mary FL) Hindle Robert A. (Cocoa Beach FL) Brown Stephen W. (Oviedo FL). System for capturing heat transferred from compressed cooling air in a gas turbine. USP1993105255505.
  15. Droessler Kim J. ; Earleson Walter E. ; Smith Carol J.. Turbo compounded fuel supply system for a gaseous fuel engine. USP1999055899070.
  16. Faulkner Henry B. (Dover MA) Kesseli James B. (Mont Vernon NH) Swarden Michael C. (Cambridge MA) Jansen Willem (Weston MA). Turbocharger-based bleed-air driven fuel gas booster system and method. USP1994075329757.

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