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특허 상세정보

Endothermic fuel energy management system

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) F02C-003/28    F02C-007/224   
미국특허분류(USC) 60/3902 ; 60/3912 ; 60/736
출원번호 US-0103603 (1993-08-06)
발명자 / 주소
출원인 / 주소
인용정보 피인용 횟수 : 21  인용 특허 : 0
초록

A method for managing the energy produced by a gas turbine engine, which includes utilizing an endothermic fuel to cool the combustion products in the exhaust section of the gas turbine engine prior to burning the fuel in the combustion section of the engine.

대표
청구항

A method of recovering thermal energy from combustion products of a vehicle, said method comprising: providing at least one gas turbine engine in said vehicle, said engine having in serial flow arrangement a compressor section having in serial flow arrangement a low pressure compressor and a high pressure compressor, said compressor section for compressing ambient air thereby producing compressed air, a combustion section for mixing fuel with said compressed air and igniting said fuel and compressed air to produce said combustion products, a turbine sect...

이 특허를 인용한 특허 피인용횟수: 21

  1. Fowler, Robert B.; Joyner, Claude R.. Catalytically enhanced gas generator system for rocket applications. USP2015129200596.
  2. Cloyd Scott Thorsten ; Bohinsky Brian Joseph ; Paprotna Hubertus Edward. Coal fuel gas turbine system. USP1999075918466.
  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. Horner Michael W.. Extracted, cooled, compressed/intercooled, cooling/ combustion air for a gas turbine engine. USP2000046050080.
  7. Horner Michael W.. Extracted, cooled, compressed/intercooled, cooling/combustion air for a gas turbine engine. USP1998035724806.
  8. Minick, Alan B.. Fuel-cracking diesel engine system. USP2014048695540.
  9. Karam, Michael Abraham; Donovan, Eric Sean; Krautheim, Michael Stephen; Vetters, Daniel Kent; Chouinard, Donald G.. Gas turbine engine with air/fuel heat exchanger. USP2017099771867.
  10. Fujioka Masanori,JPX ; Sakata Teruaki,JPX ; Dilao Carmelo Osmena,JPX. Gas turbine fuel heating apparatus. USP1998085794448.
  11. Taguchi, Hidetoshi; Nishiwaki, Fumitoshi; Komori, Kou; Tamura, Tomoichiro; Matsumoto, Subaru. Gas turbine system with cooling fluid generator. USP20190210215095.
  12. Taguchi, Hidetoshi; Nishiwaki, Fumitoshi; Komori, Kou; Tamura, Tomoichiro; Matsumoto, Subaru. Gas turbine system with cooling fluid generator. USP2016019239009.
  13. George E. Wilmot, Jr. ; Gregory M. Ott. Integrated thermal management and coolant system for an aircraft. USP2002076415595.
  14. Nielsen Henrik,CHX. Method of operating a gas-turbine group. USP1999025873233.
  15. Wang, Yu; Ghanime, George Hanna; Tang, Chi; DeLeonardo, Guy Wayne. Methods and apparatus for heating a fluid. USP2011017874156.
  16. Mazumder, Indrajit; Saha, Rajarshi; Lokanath, Shivaprasad; Baikampady Gopalkrishna, Vinod Kumar. Optimization of low-BTU fuel-fired combined-cycle power plant by performance heating. USP2012028117821.
  17. Norton, Daniel G.; Perry, Robert J.; Allen, Edward H.; Glaser, Paul B.. System and method for rejecting heat from equipment via endothermic isomerization. USP2014078765070.
  18. Kelnhofer, Juergen. System for cooling a heat exchanger on board an aircraft. USP2016039284057.
  19. Norton, Daniel G.; Perry, Robert J.; Osaheni, John; Pastecki, Patrick; Glaser, Paul; Mhadeshwar, Ashish B.. Systems and methods for using an endothermic fuel with a high heat sink capacity for aircraft waste heat rejection. USP2015038978353.
  20. Watkins, William B.; Fowler, Robert B.. Three component injector for kerosene-oxygen rocket engine. USP2010037685807.
  21. Callas, James John. Turbine engine having fuel-cooled air intercooling. USP2012078220268.