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특허 상세정보

Multiple mode environmental control system for pressurized aircraft cabin

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B28B-009/00   
미국특허분류(USC) 62/172 ; 60/039.07 ; 62/402
출원번호 US-0925557 (1997-09-08)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Wood, Phillips, VanSanten, Clark & Mortimer
인용정보 피인용 횟수 : 29  인용 특허 : 9
초록

The need for engine bleed air in a cabin pressurizing/ventilation ECS system for aircraft is avoided in a construction including a pressurizable aircraft cabin (10) having a cabin air inlet (20) and a cabin air outlet (22). The system includes a ram air inlet (34) and an aircraft exhaust air outlet (42) along with a motor operated vapor compression cabin air cooling system (24) having an inlet (28) and an outlet (26). A turbomachine (40) includes a compressor (32) connected between the ram air inlet (34) and the cooling system inlet (28) along with a com...

대표
청구항

[ I claim:] [1.] A multiple-mode auxiliary power unit based environmental control system for a pressurizable-cabin aircraft having a cabin air inlet and a cabin air outlet comprising:a ram air inlet;an environmental control system exhaust outlet;a cabin air cooling system including an inlet and an outlet;said environmental control system exhaust outlet being connected to said cabin air inlet;a turbomachine including a compressor connected between said ram air inlet and said cooling system inlet, a combustion turbine and a power recovery turbine mechanica...

이 특허를 인용한 특허 피인용횟수: 29

  1. Brutscher,Norbert; Haas,Joachim. Air-conditioning system and a method for the preparation of air for the air-conditioning of a space. USP2008127467524.
  2. Klimpel, Frank; Schmidt, Stephan-Anton; Beier, Jens. Aircraft air conditioning system comprising a separate refrigeration cycle. USP2016119487300.
  3. Balan, Chellappa; Sheldon, Karl Edward. Aircraft auxiliary gas turbine engine and method for operating. USP2010057721554.
  4. Zhou, Rui; Winter, Stephen Francis; Kyriazopoulos, Athanasios; Muller, Jones Ricardo; Parilla, Javier Armando. Aircraft energy management system including engine fan discharge air boosted environmental control system. USP2016029254920.
  5. Loison, Renaud. Aircraft fuel storage device, management associated system and method. USP2016059340296.
  6. Snyder, Douglas J.. Aircraft system. USP2018039908635.
  7. Loison, Renaud. Autonomous electricity production and conditioning system for an aircraft, associated aircraft and method. USP2014118882030.
  8. Sheldon, Karl Edward; Seeley, Charles Erklin; Haber, Ludwig Christian. Auxiliary power unit assembly. USP2010057707838.
  9. Winslow, Christopher L.; Anduze, Alejandro. Bleed valve system for a gas turbine engine. USP2004026695578.
  10. Arthurs,Timothy R.; Horner,Darrell W.; Laing,Alastair R.; Rabon,Joaquin P.. Cabin pressure control system and method that accommodates aircraft take-off with and without a cabin pressurization source. USP2008127462098.
  11. Ernst, Jeffrey; Bibbins, Kenneth F.; Schroder, Bruce R.. Decoupling control architecture for pressure and flow controls in series. USP2013068463496.
  12. Asfia, Julie F.; Williams, Kenneth R.; Atkey, Warren A.; Fiterman, Charles J.; Loukusa, Steven M.; Ng, Casey Y.. Electric air conditioning system for an aircraft. USP2003036526775.
  13. Bruno, Louis J.; Lents, Charles E.; Sahm, Michael K.; Thresher, Wayne A.. Electric power and cooling system for an aircraft. USP2005016845630.
  14. Lents, Charles E.; Squier, Steven E.; Thresher, Wayne A.. Electrically driven aircraft cabin ventilation and environmental control system. USP2004016681592.
  15. Lents, Charles E.; Squier, Steven E.; Thresher, Wayne A.. Electrically driven aircraft cabin ventilation and environmental control system. USP2005086928832.
  16. Ullyott, Richard; Jones, Anthony; Julien, Andre; Thomassin, Jean. Engine assembly with direct drive of generator. USP2018069994332.
  17. Williams Samuel B. ; Jones John F. ; Thompson ; Jr. Robert S.. Environment control unit for turbine engine. USP2001026189324.
  18. Bruno, Louis J.; Christians, Douglas L.. Hybrid environmental conditioning system. USP2014128915095.
  19. Lui, Clarence W. T.; Derouineau, Jean Luc; Claeys, Henry M.. Integrated environmental control and auxiliary power system for an aircraft. USP2009107607318.
  20. Derouineau, Jean Luc; Schenk, Bjoern; Lui, Clarence. Integrated power and pressurization system. USP2009087578136.
  21. Ho, Yu-Hang. Magnetically coupled integrated power and cooling unit. USP2004086776002.
  22. Army Jr.,Donald E.; Christians,Douglas L.; Peacos, III,Frederick. Manifold for pack and a half condensing cycle pack with combined heat exchangers. USP2006027000425.
  23. Haillot, Jean-Michel. Method for optimizing the overall energy efficiency of an aircraft, and main power package for implementing same. USP2014108868262.
  24. Sanchez Perez, Arturo del Refugio; Ramos Coria, Daniel Andres; Felix, Rodrigo; Magaña, Artemio. Methods and systems for boost control. USP20180810047665.
  25. Thompson Robert George. Secondary power integrated cabin energy system for a pressurized aircraft. USP2001096283410.
  26. Army, Jr., Donald E.; Greenberg, Michael D.. Sensor manifold for a flow sensing venturi. USP2004026688184.
  27. Ronan, Michael. Single stage engine bleed. USP20180910071806.
  28. Wolfe, David; Minh, Nguyen Q.; Meister, Kurt; Matulich, Dan S.. Turbomachine-driven environmental control system. USP2004056735953.
  29. 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.