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특허 상세정보

Cooling system

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) F02C-007/06    F02C-007/14    F02C-007/18    F02C-007/224    F02C-007/16    F25B-001/00    F25B-041/06    F28D-015/00    F28F-027/02    F28D-021/00   
출원번호 US-0814546 (2015-07-31)
등록번호 US-10260419 (2019-04-16)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    General Electric Company
인용정보 피인용 횟수 : 0  인용 특허 : 13
초록

A thermal management system for a gas turbine engine and/or an aircraft is provided including a thermal transport bus having a heat exchange fluid flowing therethrough. The thermal management system also includes a plurality of heat source exchangers and at least one heat sink exchanger. The plurality of heat source exchangers and the at least one heat sink exchanger are in thermal communication with the heat exchange fluid in the thermal transport bus. The plurality of heat source exchangers are arranged along the thermal transport bus and configured to...

대표
청구항

1. A thermal management system for incorporation at least partially into at least one of a gas turbine engine or an aircraft, the thermal management system comprising: a thermal transport bus having a heat exchange fluid flowing therethrough;a pump for generating a flow of the heat exchange fluid in the thermal transport bus;a plurality of heat source exchangers in thermal communication with the heat exchange fluid in the thermal transport bus, the plurality of heat source exchangers arranged along the thermal transport bus;at least one heat sink exchang...

이 특허에 인용된 특허 (13)

  1. Coffinberry, George Albert; Garrigan, Neil Richard. Adaptive power and thermal management system. USP2013098522572.
  2. Glickstein Marvin R. (North Palm Beach FL). Aircraft cooling method. USP1995055414992.
  3. Lui Clarence ; Wong Wai-Pak ; Meyer Richard. Dual expansion energy recovery (DEER) air cycle system with mid pressure water separation. USP2001066250097.
  4. Horner Michael W.. Extracted, cooled, compressed/intercooled, cooling/combustion air for a gas turbine engine. USP1998035724806.
  5. Chen, Alexander G.. Flame stability enhancement. USP2011027882704.
  6. Mayer Arnold H. (Huber Heights OH). Heat management system for aircraft. USP1985034505124.
  7. George E. Wilmot, Jr. ; Gregory M. Ott. Integrated thermal management and coolant system for an aircraft. USP2002076415595.
  8. Rannenberg, George C.. Multiple load, high efficiency air cycle air conditioning system. USP1985114550573.
  9. Bystry, Jr., Mark Denton; Simonetti, Joseph; Tarascio, Matthew J.; Strauss, Michael Peter; Kasprzyk, Adam; Lauder, Timothy Fred. Rotary wing aircraft propulsion system. USP2015028944367.
  10. Bulin, Guillaume; Pugliese, Stephane; Christian, Fabre; Oberle, Patrick. System for cooling and adjusting the temperature of apparatuses in the propulsion assembly of an aircraft. USP2013088499822.
  11. Niggemann Richard E. ; Nguyen Dam. Thermal and energy management method and apparatus for an aircraft. USP2001026182435.
  12. Sabatino,Daniel; Spadaccini,Louis J.; Kaslusky,Scott. Thermal management system for an aircraft. USP2007087260926.
  13. Xu, James Jun; Scharl, Albert Andreas; Imani, Shamim. Waste heat recovery systems. USP2015038984884.