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"" 따옴표 내의 구문과 완전히 일치하는 문서만 검색 예) "Transform and Quantization"

특허 상세정보

Flexible power and thermal architectures using a common machine

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) F25D-009/00   
미국특허분류(USC) 062/402; 060/224
출원번호 UP-0435997 (2006-05-17)
등록번호 US-7624592 (2009-12-16)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Stetina Brunda Garred & Brucker
인용정보 피인용 횟수 : 13  인용 특허 : 5
초록

A power and cooling management system configured to flexibly couple various adaptive modules to an integrated power and cooling unit to suit any aircraft platform is provided. The integrated power and cooling unit has a compressor(s), power turbine(s), cooling turbine(s) and integral starter generator(s) mounted to the shaft of the power and cooling turbine. The integrated power and cooling unit may be pneumatically and/or pneumatically coupled to an adaptive module that comprises an additional compressor and an additional turbine or electrically coupled...

대표
청구항

What is claimed is: 1. A power and cooling system, comprising: an integrated power and cooling unit, comprising: a first compressor connected to a discharged air inlet of an engine; a power turbine located at downstream of the compressor; a cooling turbine connected to the engine discharged air; and a first starter generator mounted to a common shaft of the power and cooling turbine; and an adaptive module pneumatically coupled to the integrated power and cooling unit, the adaptive module comprising: a second compressor pneumatically coupled to downstr...

이 특허를 인용한 특허 피인용횟수: 13

  1. Coffinberry, George Albert; Garrigan, Neil Richard. Adaptive power and thermal management system. USP2013098522572.
  2. 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.
  3. Ho, YuHang; Knowles, Jeffrey A.. Apparatus for aircraft with high peak power equipment. USP2016059328661.
  4. Coffinberry, George Albert. Flade duct turbine cooling and power and thermal management. USP2014078789376.
  5. Taguchi, Hidetoshi; Nishiwaki, Fumitoshi; Komori, Kou; Tamura, Tomoichiro; Matsumoto, Subaru. Gas turbine system with cooling fluid generator. USP20190210215095.
  6. Taguchi, Hidetoshi; Nishiwaki, Fumitoshi; Komori, Kou; Tamura, Tomoichiro; Matsumoto, Subaru. Gas turbine system with cooling fluid generator. USP2016019239009.
  7. Bruno, Louis J.; Jones, Anthony C.; Spierling, Todd A.; DeFrancesco, Gregory L.. Hybrid power system architecture for an aircraft. USP2014038662445.
  8. Leamy, Kevin Richard; Breig, Benjamin Paul; Epstein, Michael Jay; Parrilla, Javier Armando; Hurt, Matthew John; Brinson, Thomas Edward; Fleming, Andrew James. Jet engine cold air cooling system. USP20190410247100.
  9. Barkowsky, Jan; Dittmar, Jan. Main engine start by means of an aircraft air conditioning system. USP2014098844296.
  10. Agrawal, Giridhari L.; Buckley, Charles W.; Rajendran, Muthusamy. Mechanically-coupled turbomachinery configurations and cooling methods for hermetically-sealed high-temperature operation. USP2018049951784.
  11. Gagne, Steven; Rodriguez, Rigoberto J.; Siegel, William L.; Arvin, John R.. Phase change material cooling system for a vehicle. USP2017019534537.
  12. Cerny, Matthew Robert. Systems and methods for integrated power and thermal management in a turbine-powered aircraft. USP2017019534538.
  13. Agrawal, Giridhari L.; Buckley, Charles W.; Shakil, Ali; Coward, Andrew Hamilton. Ultra high pressure turbomachine for waste heat recovery. USP2016109476428.