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특허 상세정보

Cooling systems for use on aircraft

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) F02C-001/00   
미국특허분류(USC) 060/728; 060/226.1; 060/785
출원번호 UP-0767993 (2007-06-25)
등록번호 US-7856824 (2011-02-24)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Ingrassia Fisher & Lorenz PC
인용정보 피인용 횟수 : 17  인용 특허 : 15
초록

Cooling systems for an aircraft are provided. In an embodiment, a system includes an engine nacelle, an engine, a bypass duct, and a heat exchanger. The engine nacelle includes an airflow inlet. The engine is housed in the engine nacelle in flow communication with the airflow inlet. The bypass duct extends between the engine nacelle and the engine is in flow communication with the airflow inlet. The bypass duct includes an outer wall and an opening formed therein. The heat exchanger is integrated with the engine and is disposed over the opening of the by...

대표
청구항

We claim: 1. A cooling system for an aircraft comprising: an engine nacelle including an airflow inlet; an engine housed in the engine nacelle in flow communication with the airflow inlet; a bypass duct extending between the engine nacelle and the engine in flow communication with the airflow inlet, the bypass duct including an outer wall having an opening formed therein; and a heat exchanger integrated with the engine and disposed outside of the bypass duct over the opening of the bypass duct outer wall between the bypass duct outer wall and the engine...

이 특허에 인용된 특허 (15)

  1. Albero, Jose; Bruno, Louis J.; Dussault, Richard; Lents, Charles E.; Thresher, Wayne A.; Sahm, Michael K.; Thompson, Robert G.. Aircraft system architecture. USP2003106634596.
  2. Anthony I. Skur, III. Bleed air heat exchanger integral to a jet engine. USP2002096442944.
  3. Elovic Ernest (Cincinnati OH). Cooling air cooler for a gas turbofan engine. USP1981034254618.
  4. Rolt, Andrew M. Engine. USP2010057716913.
  5. Severson Mark Hamilton ; Squier Steven Eric. Environmental control system with energy recovery and bleed air assist. USP1999065911388.
  6. Colman Michael E. (Wakefield MA) Goeller Robert E. (Beverly MA). Gas turbine engine component cooling system. USP1986094608819.
  7. Parsons Franklin D. (Cincinnati OH). Heat exchange arrangement in a gas turbine engine fan duct for cooling hot bleed air. USP1993045203163.
  8. Glickstein Marvin R. (North Palm Beach FL) Dixon James T. (Jupiter FL) Podolsky Donald M. (Jupiter FL). High pressure air source for aircraft and engine requirements. USP1996045511374.
  9. Williams Kenneth R.. Integrated air conditioning and power unit. USP1999055899085.
  10. Christians Douglas L. ; Drew Diane G. ; Harris Mark L. ; Kline Erin G. ; Zager Michael. Integrated environmental control system. USP1998015704218.
  11. Munoz, Jules Ricardo; Bertuccioli, Luca; Sahm, Michael K.; Fletcher, Jay; Lents, Charles E.; Squier, Steven E.; Welch, Richard; Becker, Arthur Curtis. Integrated system for providing aircraft environmental control. USP2004116817575.
  12. Shah Anil D. (Seattle WA). Integrated thermal anti-icing and environmental control system. USP1976093981466.
  13. Aniekan Udobot ; Ron Brager ; Larry Reed. Method and apparatus for improved aircraft environmental control system utilizing parallel heat exchanger arrays. USP2002106460353.
  14. Miller Franklin E. (Cincinnati OH). Precooling heat exchange arrangement integral with mounting structure fairing of gas turbine engine. USP1992065123242.
  15. Yoshinaka Tsukasa. Turbine engine with intercooler in bypass air passage. USP2000106134880.

이 특허를 인용한 특허 피인용횟수: 17

  1. Cheong, Chee Yuen. Air recovery system for precooler heat-exchanger. USP2015089109514.
  2. Sennoun, Mohammed El Hacin. Bleed air and hot section component cooling air system and method. USP2015129222411.
  3. Suciu, Gabriel L.; Glahn, Jorn A.; Merry, Brian D.; Dye, Christopher M.. Bypass air-pump system within the core engine to provide air for an environmental control system in a gas turbine engine. USP2016079394803.
  4. Suciu, Gabriel L.; Glahn, Jorn A.; Merry, Brian D.; Dye, Christopher M.. Combined pump system for engine TMS AOC reduction and ECS loss elimination. USP2016109470153.
  5. 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. USP2018049932892.
  6. 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. USP2017109797297.
  7. 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. USP2018029896998.
  8. Strecker, Steven; Liu, Xiaoliu; Logan, Adam. Cooling system for engine and aircraft air. USP2016019239005.
  9. 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. USP2018019879591.
  10. Sennoun, Mohammed El Hacin; Dinsmore, Nicholas Rowe; Miller, Brandon Wayne. Environmental control system supply precooler bypass. USP2013038397487.
  11. Coffin, James B.; Davis, Todd A.; DiBenedetto, Enzo. Forward compartment service system for a geared architecture gas turbine engine. USP2016089410447.
  12. Suciu, Gabriel L.. Gas turbine engine thermal management system for heat exchanger using bypass flow. USP20180710036329.
  13. Marche, Herve. Heat exchanger unit for an aircraft. USP2012048161755.
  14. Koerner, Mike; MacKnight, Allen; Nikbin, Siamak; Quan, Myron; Robles, Daniel R. Integrated air and vapor cycle cooling system. USP20190210207809.
  15. Antel, Jr., William Joseph; Diaz, Carlos Enrique; Benignos, Jorge Carretero. Plate-like air-cooled engine surface cooler with fluid channel and varying fin geometry. USP2017039599410.
  16. Martinou, Jean-Marc; Marche, Herve. Propulsion unit for aircraft with heat exchanger having front inlet faces for cooling air flow and hot air flow. USP2013098522529.
  17. Lau, Andrea Chor Ying; Li, Xiaomei. Temperature control setpoint offset for ram air minimization. USP2013128612063.