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특허 상세정보

Integrated air and vapor cycle cooling system

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64D-037/34    B64D-013/06    F25B-025/00    B64D-013/08   
출원번호 US-0991155 (2016-01-08)
등록번호 US-10207809 (2019-02-19)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Shimokaji IP
인용정보 피인용 횟수 : 0  인용 특허 : 28
초록

A cooling system in which an ACS (air cycle system) turbine may be driven by high pressure air from a turbo-fan engine and a VCS (vapor cycle system) having an evaporator and a VCS refrigerant compressor may be driven by the ACS turbine. Fluid of the chilled fluid reservoir, which may be chilled fuel, may be circulated through and cooled in the evaporator. In some embodiments, the ACS turbine may be coupled to the VCS refrigerant compressor by a magnetic coupling.

대표
청구항

1. A cooling system, comprising: an air cycle system (ACS) comprising a two-stage turbine driven by air from a turbo-fan engine;a vapor cycle system (VCS) comprising an evaporator, a two-stage compressor driven by the turbine, and a condenser cooled by discharge from the turbine;wherein the evaporator receives a liquid refrigerant from the condenser;wherein the condenser receives a gas refrigerant from a second stage of the compressor;wherein a first stage of the compressor receives a liquid/gas refrigerant from the evaporator;a liquid coolant reservoir ...

이 특허에 인용된 특허 (28)

  1. Coffinberry, George Albert; Garrigan, Neil Richard. Adaptive power and thermal management system. USP2013098522572.
  2. Axe,Richard James; Hunt,Richard Grant. Air conditioning system. USP2006057040112.
  3. McAuliffe, Christopher; Merritt, Brent J.; Beers, Craig M.. Air cycle machine for an aircraft environmental control system. USP2013018347647.
  4. Fiterman, Charles J.; Atkey, Warren A.. Aircraft air conditioning systems and methods. USP2017069669936.
  5. Gagne, Steven; Rodriguez, Rigoberto; Siegel, William L.; Arvin, John R.. Aircraft and airborne electrical power and thermal management system. USP2015038967531.
  6. Mitani, Hisashi. Aircraft environment controller. USP2003036527228.
  7. Albero, Jose; Bruno, Louis J.; Dussault, Richard; Lents, Charles E.; Thresher, Wayne A.; Sahm, Michael K.; Thompson, Robert G.. Aircraft system architecture. USP2003106634596.
  8. Rosen, Seth E.; Struziak, Ronald M.. Bearing sleeve. USP2015018926182.
  9. Järlestål, Anders. Cooling of avionics using a fuel tank and refrigerant source. USP2011108042343.
  10. Anderson, Morris G.; Alford, William E.; Trego, Michael L.; Haugland, Ron; Winstanley, David K.. Cooling systems for use on aircraft. USP2010127856824.
  11. Ho, Yuhang. Environmental control system for an aircraft. USP2005096948331.
  12. Sarmiento Penuela, Oscar Eduardo; Burgmair, Raphael Rupert; Huber, Johannes; Satria, Medy; Selga, Rosa Castane; Srinivasan, Prashant. Gas dosage control for gas engine. USP2017029581089.
  13. Shnaid Isaac (Zalman Shneuz Stz. 36/10 Haifa 32545 ILX). Gas turbine with bottoming air turbine cycle. USP1995085442904.
  14. Mayer Arnold H. (Huber Heights OH). Heat management system for aircraft. USP1985034505124.
  15. Williams Kenneth R.. Integrated air conditioning and power unit. USP1999055899085.
  16. George E. Wilmot, Jr. ; Gregory M. Ott. Integrated thermal management and coolant system for an aircraft. USP2002076415595.
  17. Ho, Yu-Hang. Magnetically coupled integrated power and cooling unit. USP2004086776002.
  18. Coons, Terry L.. Method and system for providing cooling and power. USP2011098019522.
  19. Sommer, Steven T.. Method and system for rotor cooling. USP2013048424339.
  20. Murry, Roger P.. Method of heating for an aircraft electric environmental control system. USP2003106629428.
  21. Miazgowicz, Keith D.. Multiple spool turbocharger. USP2016119500198.
  22. Munoz, Jules Ricardo; Bertuccioli, Luca; Radomsky, Jr., Roger W.. Reduced bleed vapor compression cycle environmental control system for aircraft. USP2005066908062.
  23. Ro,Soo hyuk. Refrigerating apparatus with turbo compressor. USP2008117451616.
  24. Lee, Haeng-Bok; Jung, Daeyoon. Small-size and light-weight environmental control unit for aircraft-external stores. USP2014108863544.
  25. Niggemann Richard E. ; Nguyen Dam. Thermal and energy management method and apparatus for an aircraft. USP2001026182435.
  26. Atkey, Warren A.. Turbo-compressor system and method for extracting energy from an aircraft engine. USP2017059656756.
  27. Schlemmer-Kelling, Udo. Two-stage turbocharged engine. USP2015038978359.
  28. Munoz, Jules Ricardo; Bertuccioli, Luca; Sahm, Michael K.; Fletcher, Jay; Lents, Charles E.; Welch, Richard; Squier, Steve; Becker, Arthur Chris. Vapor compression cycle environmental control system. USP2003126663044.