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Thermal management system for turbofan engines

IPC분류정보
국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판)
  • F02C-007/14
  • F28D-011/00
  • F28F-027/00
출원번호 US-0432111 (2006-05-11)
등록번호 US-8776952 (2014-07-15)
발명자 / 주소
  • Schwarz, Frederick M.
  • Gorbounov, Mikhail B.
출원인 / 주소
  • United Technologies Corporation
대리인 / 주소
    Kinney & Lange, P.A.
인용정보 피인용 횟수 : 9  인용 특허 : 20

초록

A heat exchange system for use in operating equipment in which a working fluid is utilized needing a heat exchange system to provide air and working fluid heat exchanges to cool the working fluid at selectively variable rates in airstreams. The system comprises a plurality of heat exchangers includi

대표청구항

1. A heat exchange system upstream of a turbofan bypass airstream nozzle to cool a liquid working fluid in turbofan airstreams, the system comprising: a lower bifurcation structure with moveable exit flaps;a first heat exchanger mounted stationary in the lower bifurcation structure with a plurality

이 특허에 인용된 특허 (20)

  1. Negulescu Dimitrie,DEX, Aircraft gas turbine engine with a liquid-air heat exchanger.
  2. Bruno,Vittorio; Olver,Bryan; Logan,John Adam, Bypass duct fluid cooler.
  3. Elovic Ernest (Cincinnati OH), Cooling air cooler for a gas turbofan engine.
  4. Jones, Alan R., Cooling systems.
  5. Burr Donald N. (Glastonbury CT) Danilowicz Paul S. (Manchester CT) Franz Thomas C. (Bolton CT) Mortimer Thomas P. (Bolton CT) Pero Edward B. (Somers CT), Fuel and oil heat management system for a gas turbine engine.
  6. Dreisbach ; Jr. Raymond A. (Old Saybrook CT) Griffin James G. (West Hartford CT) Cole Edward F. (Glastonbury CT), Fuel heating system for gas turbine engine.
  7. Vermejan Alexander E. (Mason OH) Daiber Paul C. (Cincinnati OH) Morton Scott C. (Cincinnati OH) Taylor Michelle L. (Cincinnati OH), Gas turbine engine fan cooled heat exchanger.
  8. Loxley Russell A. (Leicestershire GB2) Clarke Andrew (Nottingham GB2), Heat exchange apparatus for gas turbine fluids.
  9. Mortimer, Thomas P.; Suciu, Gabriel L., Heat exchange system.
  10. Griffin James G. (West Hartford CT) Singer Irwin D. (Glastonbury CT) Summers Roger L. (Lafayette IN), Lubrication cooling system for aircraft engine accessory.
  11. Butler Reginald J. (Derby GB2), Management system for heat generated by aircraft gas turbine installations.
  12. Butler Reginald J. (Derby GB2), Method for management of heat generated by aircraft gas turbine installations.
  13. Griffiths, James Alan; Smith, Mitchell Donald; Bartos, James William, Methods and apparatus for supplying cooling air to turbine engines.
  14. Zysman, Steven H.; Kohlenberg, Gregory A., Modulating flow through gas turbine engine cooling system.
  15. Parnes Marvin J. (Norwalk CT) Vogel Herman (Newtown CT), Oil cooler for fan jet engines.
  16. Coffinberry George A. (Cincinnati OH) Kast Howard B. (Fairfield OH), Oil cooling system for a gas turbine engine.
  17. Scott-Scott John L. (Warwick GB2) Belcher Bryan L. (Leamington Spa GB2) Bond Alan (Oxford GB2), Prevention of icing in the intakes of aerospace propulsors.
  18. Larkin,Michael J.; Eiler,Donald C., Supplemental oil cooler airflow for gas turbine engine.
  19. Beutin Bruno A. (Corbeil Essonnes FRX) Creti Joel (Ussy/Marne FRX) Donnadieu Jean-Pierre (Longueville FRX) Garnier Francis G. A. (Bombon FRX) Hugues Michel G. (Bois Le Roi FRX) Lecordix Jean-Loic H. , System for regulating oil and fuel temperatures of a turbojet engine.
  20. Adamson ; Arthur P., Variable thrust nozzle for quiet turbofan engine and method of operating same.

이 특허를 인용한 특허 (9)

  1. Thomassin, Jean; Bolduc, Sebastien; Villeneuve, Bruno; Berube, Stephane; Fontaine, Mike; Gagnon-Martin, David; Bilodeau, Jade; Julien, Andre; Legare, Pierre-Yves; Nichols, Jason, Compound engine assembly with coaxial compressor and offset turbine section.
  2. Thomassin, Jean; Bolduc, Sebastien; Villeneuve, Bruno; Berube, Stephane; Fontaine, Mike; Gagnon-Martin, David; Julien, Andre; Cunningham, Mark; Lafortune, Serge; Legare, Pierre-Yves, Compound engine assembly with common inlet.
  3. Thomassin, Jean; Bolduc, Sebastien; Villeneuve, Bruno; Berube, Stephane; Fontaine, Mike; Gagnon-Martin, David; Julien, Andre; Cunningham, Mark; Lafortune, Serge; Legare, Pierre-Yves, Compound engine assembly with modulated flow.
  4. Kupratis, Daniel Bernard; Hanrahan, Paul R., Cooled cooling air system for a gas turbine engine.
  5. Thomassin, Jean; Bolduc, Sebastien; Villeneuve, Bruno; Berube, Stephane; Fontaine, Mike; Gagnon-Martin, David; Julien, Andre; Cunningham, Mark; Lafortune, Serge; Legare, Pierre-Yves, Engine intake assembly with selector valve.
  6. Xu, JinQuan, Gas turbine engine fluid supply system having at least one airbag, and method for maintaining non-interrupted circulating turbomachine fluid flow during a non-positive G-force event.
  7. Phillips, Kathleen R.; Phillips, Thomas G.; Stearns, Ethan K., Gas turbine engine with geared turbofan and oil thermal management system.
  8. Suciu, Gabriel L.; Chandler, Jesse M.; Staubach, Joseph Brent; Merry, Brian D., Intercooled cooling air tapped from plural locations.
  9. Miller, Brandon Wayne; Anstead, Duane Howard; Sennoun, Mohammed El Hacin; Fang, Ning; Snow, Kyle Robert, Thermal management system.
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