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특허 상세정보

Electric power and cooling system for an aircraft

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) F25D-00900    B64D-01302   
미국특허분류(USC) 062/323.3; 062/402; 454/071
출원번호 US-0077281 (2002-02-14)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Bachman &
인용정보 피인용 횟수 : 17  인용 특허 : 12
초록

The present invention relates to an electrical power and cooling system for use in an aircraft having at least one engine. The electrical power and cooling system comprises a single shaft, a power turbine mounted on the shaft for receiving fresh pressurized air from the at least one engine, a cooling turbine mounted on the shaft and receiving the fresh pressurized air from the at least one engine, a generator mounted on the shaft, and a fan mounted on the shaft for creating a flow of cooling air. The system further has a condenser for removing moisture f...

대표
청구항

1. An electric power and cooling system for supplying electric power and conditioned air to an aircraft having at least one engine comprising a single shaft, a power turbine mounted on the shaft for receiving fresh pressurized air from said engine, a cooling turbine mounted on said shaft and receiving said fresh pressurized air from said engine, a generator mounted on said shaft, and a fan mounted on said shaft for creating a flow of air for cooling said fresh pressurized air.2. An electric power and cooling system according to claim 1, further comprisin...

이 특허를 인용한 특허 피인용횟수: 17

  1. Bruno, Louis J.; Hipsky, Harold W.; Army, Jr., Donald E.; Kline, Erin G.; Millot, Christina W.; D'Orlando, Paul M.. Aircraft environmental control system. USP20181210160547.
  2. Ho, YuHang; Knowles, Jeffrey A.. Apparatus for aircraft with high peak power equipment. USP2016059328661.
  3. Good, Jef William; Seagren, Robert L.; Berg, Joshua. Electrical power supply system having internal fault protection. USP2015049018799.
  4. Bruno, Louis J.; Army, Jr., Donald E.; Zywiak, Thomas M.; Kline, Erin G.; Millot, Christina W.; Hipsky, Harold W.; D'Orlando, Paul M.. Environmental control system utilizing parallel ram heat exchangers. USP2018069994322.
  5. Plattner, Wesley M.. Flow control system for an aircraft. USP2014098839641.
  6. Guering, Bernard; Durand, Yves. Heat exchanger incorporated into a wall of an aircraft. USP2016099446850.
  7. Bruno, Louis J.; Christians, Douglas L.. Hybrid cooling system for aircraft applications. USP2015018936071.
  8. Lui, Clarence W. T.; Derouineau, Jean Luc; Claeys, Henry M.. Integrated environmental control and auxiliary power system for an aircraft. USP2009107607318.
  9. Coons, Terry L.. Method and system for providing cooling and power. USP2011098019522.
  10. Bruno, Louis J.; Hipsky, Harold W.. Mixing bleed and ram air at a turbine inlet of a compressing device. USP20190310232948.
  11. Bruno, Louis J.; Hipsky, Harold W.. Mixing bleed and ram air using a two turbine architecture with an outflow heat exchanger. USP20181210144517.
  12. Bruno, Louis J.; Hipsky, Harold W.. Mixing bleed and ram air using an air cycle machine with two turbines. USP20181110137993.
  13. Maier, Josef; Beutel, Michael. Power distribution architecture for aircraft. USP2014118890355.
  14. Bruno, Louis J.; Zywiak, Thomas M.; Kline, Erin G.; Millot, Christina W.; Army, Jr., Donald E.; Hipsky, Harold W.. Recirculation system for parallel ram heat exchangers. USP2018029889938.
  15. Schiff, Peter. System and method for replacing an engine powered air conditioning unit with an electric air conditioning unit in an aircraft. USP2017049617005.
  16. Kelnhofer, Juergen. System for cooling a heat exchanger on board an aircraft. USP2016039284057.
  17. Brutscher, Norbert; Haas, Joachim. System for the preparation of compressed air. USP2010127845188.