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특허 상세정보

Integrated system for providing aircraft environmental control

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64D-013/08   
미국특허분류(USC) 244/118.5; 060/039.07; 454/076
출원번호 US-0251721 (2002-09-20)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Bachman & LaPointe, P.C.
인용정보 피인용 횟수 : 20  인용 특허 : 12
초록

The present invention relates to an integrated enviromental control system for an aircraft. The system uses bleed air from a propulsion engine to drive an air turbine which provides power to at least one aircraft component such as an aircraft mounted accessory drive. The system uses the bleed air exiting the air turbine as an air source for the cabin and/or flight deck enviromental control system.

대표
청구항

1. An integrated environmental control system for an aircraft comprising:means for using engine bleed air to provide power to at least one aircraft component and to provide cooling to at least one of a flight deck and a cabin;said bleed air using means comprising an aircraft mounted accessory drive, a turbine connected to said aircraft mounted accessory drive for providing power to said aircraft mounted accessory drive, and means for delivering said engine bleed air to an inlet of said turbine;means for delivering bleed air exiting said turbine to means ...

이 특허를 인용한 특허 피인용횟수: 20

  1. Zawilinski, David J.; Makulec, Jeffrey M.; Ryan, Bradley Thomas; Slayter, Matthew. Air turbine starter. USP2014038672638.
  2. Zawilinski, David J.; Makulec, Jeffrey M.; Slayter, Matthew. Air turbine starter inlet housing assembly airflow path. USP2014028651806.
  3. Zawilinski, David J.; Makulec, Jeffrey M.; Slayter, Matthew. Air turbine starter turbine blade airfoil. USP2014038672637.
  4. Zawilinski, David J.; Makulec, Jeffrey M.; Ryan, Bradley Thomas; Slayter, Matthew. Air turbine starter turbine nozzle airfoil. USP2015059028208.
  5. Zawilinski, David J.; Makulec, Jeffrey M.; Slayter, Matthew. Air turbine starter turbine nozzle airfoil. USP2014038672620.
  6. Markwart, Michael; Scherer, Thomas; Schaumann, Oliver. Arrangement and method for utilizing the heat of waste air for heating the bilge area of aircraft. USP2011077980928.
  7. Markwart, Michael; Scherer, Thomas; Schaumann, Oliver. Arrangement and method for utilizing the heat of waste air for heating the bilge area of aircraft. USP2012038137169.
  8. Kesseli, James B.; Nash, James S.. Ceramic-to-metal turbine shaft attachment. USP2015069051873.
  9. Baldwin, Matthew Stephen. Ceramic-to-metal turbine volute attachment for a gas turbine engine. USP20181010094288.
  10. Army, Donald E.. Condenser with recirculation air mixer. USP2016129527594.
  11. Strecker, Steven; Liu, Xiaoliu; Logan, Adam. Cooling system for engine and aircraft air. USP2016019239005.
  12. Anderson, Morris G.; Alford, William E.; Trego, Michael L.; Haugland, Ron; Winstanley, David K.. Cooling systems for use on aircraft. USP2010127856824.
  13. Ernst, Jeffrey; Bibbins, Kenneth F.; Schroder, Bruce R.. Decoupling control architecture for pressure and flow controls in series. USP2013068463496.
  14. Donnelly, Frank Wegner; Dewis, David William. Dispatchable power from a renewable energy facility. USP2014108866334.
  15. Dewis, David William; Kesseli, James; Donnelly, Frank Wegner; Wolf, Thomas; Upton, Timothy; Watson, John D.. Gas turbine energy storage and conversion system. USP2013088499874.
  16. Dewis, David William; Kesseli, James; Donnelly, Frank Wegner; Wolf, Thomas; Watson, John D.. Gas turbine energy storage and conversion system. USP2014048708083.
  17. Donnelly, Frank Wegner; Dewis, David William. Gas turbine engine configurations. USP2014038669670.
  18. Kesseli, James B.; Baldwin, Matthew Stephen. Metallic ceramic spool for a gas turbine engine. USP2015038984895.
  19. Weber, Kent I.; Kyriazopoulos, Athanasios; Hightower, Peter C.; Miller, Lance F.; Soave, Ronald J.. Method and system for vehicle thermal management. USP2015089114877.
  20. Shell, Sidney D.; Atkey, Warren A.; Trent, Michael. Systems and methods for cargo compartment air conditioning using recirculated air. USP2012128336821.