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특허 상세정보

Endothermic fluid based thermal management method

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) F02C-003/20   
미국특허분류(USC) 60/3902
출원번호 US-0096631 (1993-07-22)
발명자 / 주소
출원인 / 주소
인용정보 피인용 횟수 : 14  인용 특허 : 0
초록

A thermal management system for a propulsion engine of a supersonic or hypersonic aircraft is provided that uses a single flow of endothermic fluid as engine fuel and as a heat sink for engine cooling. The system includes a plurality of heat exchangers in flow series arrangement. Each heat exchanger has a reactor portion, containing a catalyst, in heat exchange relation with a heat source portion. The single fluid flow flows through each of the reactor portions and heat source portions. The heat for the reaction in the reactor portions is provided by the...

대표
청구항

A method in which a single flow of an endothermic fluid is used as to fuel and cool a propulsion engine mounted on an aircraft operable at high Mach numbers, said aircraft having a stored source of said fluid in a liquid state; comprising the steps of: a) pressurizing said fluid; b) heating said fluid to a temperature at which an endothermic reaction can occur, by flowing it past a first portion of said engine requiring cooling; c) partially reforming said fluid by exposing it to a catalyst and heat; d) reheating said partially reformed fluid by flowing ...

이 특허를 인용한 특허 피인용횟수: 14

  1. Mhadeshwar, Ashish B.; Norton, Daniel; Perry, Robert James; Glaser, Paul; Pastecki, Patrick Edward. Catalytic alcohol dehydrogenation heat sink for mobile application. USP2015028961891.
  2. Mudawar, Issam; Visaria, Milan. Coiled and microchannel heat exchangers for metal hydride storage systems. USP2014078778063.
  3. Reuter, Charles E.. Dual pump fuel flow system for a gas turbine engine and method of controlling. USP2014118893466.
  4. Mudawar, Issam; Visaria, Milan; Zhang, Hui; Pourpoint, Timothee. Finned heat exchangers for metal hydride storage systems. USP2014018636836.
  5. Reuter, Charles E.; Price, Aaron V.; Haugsjaahabink, Todd; Sato, Yukinori; Wichowski, John J.. Flow control system and method for controlling two positive displacement pumps. USP2013048408233.
  6. Jarmon, David C.; Sillence, Mark A.; Attridge, Paul; Yamanis, Jean. Flowpath heat exchanger for thermal management and power generation within a hypersonic vehicle. USP2012038127555.
  7. Reuter, Charles; Dyer, Gerald P.; Haugsjaahabink, Todd; Shah, Satish. Fluid flow system for a gas turbine engine. USP2003116651441.
  8. Suzuki, Kenji; Kuroyanagi, Atsushi; Yasutake, Toshinobu. Fuel supply system, scramjet engine and method for operating the same. USP20190110190540.
  9. Thompson Jr.,Robert S.; Williams,Gregg. Gas turbine engine cooling system and method. USP2006016988367.
  10. Thompson, Jr., Robert S.; Williams, Gregg; Jarrell, David W.; Lynch, Curtis E.; Suchezky, Mark E.. Gas turbine engine cooling system and method. USP2014098820092.
  11. Thompson, Jr., Robert S; Williams, Gregg. Gas turbine engine cooling system and method. USP2011118057163.
  12. Norton, Daniel G.; Perry, Robert J.. High capacity heat sink. USP2013078496201.
  13. Huang, He. Liquid fuel with endothermic fuel-cracking catalyst. USP2014088814958.
  14. Huang, He; Kaslusky, Scott F.; Tillman, Thomas G.; DeValve, Timothy D.; Bertuccioli, Luca; Sahm, Michael K.; Spadaccini, Louis J.; Bayt, Robert L.; Lamm, Foster Philip; Sabatino, Daniel R.. System and method for thermal management. USP2005096939392.