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특허 상세정보

Autonomous electricity production and conditioning system for an aircraft, associated aircraft and method

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64D-041/00    B64D-013/06   
미국특허분류(USC) 244/058; 244/053A
출원번호 US-0471801 (2012-05-15)
등록번호 US-8882030 (2014-11-11)
우선권정보 FR-11 01511 (2011-05-18)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Dowell & Dowell, PC
인용정보 피인용 횟수 : 2  인용 특허 : 14
초록

An environmental control system including an upstream assembly supplying outside air to a rotary system of an aircraft, the air not having passed through a propulsion engine of the aircraft, and wherein the rotary system includes a rotary shaft, a power turbine, a compressor and a cold turbine, and wherein the upstream supply assembly is connected to an inlet of the compressor mounted with the rotary shaft that is rotated by the power turbine and wherein the shaft is supplied with compressed gas from the compressor toward the cold turbine.

대표
청구항

1. An autonomous electricity production and conditioning system for an aircraft, including: a rotary shaft;a main compressor mounted integral with the rotary shaft;a power turbine for rotating the rotary shaft; anda cold expansion turbine rotated by the rotary shaft and supplied with a compressed gas from the main compressor;wherein the system comprises an upstream assembly supplying outside air to the aircraft, which outside air has not passed through a propulsion engine of the aircraft, the upstream assembly being connected to an inlet of the main comp...

이 특허에 인용된 특허 (14)

  1. Friedrich Helmut (Bremen DT). Apparatus for starting aircraft engines and for operating auxiliary on-board power generating equipment. USP1976063965673.
  2. Gerhard Konrad DE; Arnold Lamm DE. Auxiliary power unit for an aircraft. USP2002096450447.
  3. Fucke, Lars; Daggett, David L.. Combined fuel cell aircraft auxiliary power unit and environmental control system. USP2011098016228.
  4. Fucke,Lars; Daggett,David L.. Combined fuel cell aircraft auxiliary power unit and environmental control system. USP2008067380749.
  5. Atkey,Warren A.; Bernier,Alan T.; Bowman,Michael D.; Campbell,Thomas A.; Cruse,Jonathan M.; Fiterman,Charles J.; Meis,Charles S.; Ng,Casey Y. K.; Nozari,Farhad; Zielinski,Edward. Electric-based secondary power system architectures for aircraft. USP2007047207521.
  6. Atkey,Warren A.; Bernier,Alan T.; Bowman,Michael D.; Campbell,Thomas A.; Cruse,Jonathan M.; Fiterman,Charles J.; Meis,Charles S.; Ng,Casey Y. K.; Nozari,Farhad; Zielinski,Edward. Electric-based secondary power system architectures for aircraft. USP2007057210653.
  7. Woodhouse Geoffrey D. (Prescott AZ). Fully integrated environmental and secondary power system. USP1996025490645.
  8. Shnaid Isaac (Zalman Shneuz Stz. 36/10 Haifa 32545 ILX). Gas turbine with bottoming air turbine cycle. USP1995085442904.
  9. Young ; Richard N.. Independent power generator. USP1978054091613.
  10. Vershure ; Jr. Roy W. (Escondido CA) Rodgers Colin (San Diego CA) Shekleton Jack R. (San Diego CA). Integrated power unit. USP1989034815277.
  11. Vershure ; Jr. Roy W. (Escondido CA) Rodgers Colin (San Diego CA) Shekleton Jack R. (San Diego CA). Integrated power unit. USP1989044819423.
  12. Williams Kenneth R.. Multi-mode secondary power unit. USP1998095813630.
  13. Cronin Michael J. (Sherman Oaks CA). Multifunction power system for an aircraft. USP1987084684081.
  14. Niggeman Richard E.. Multiple mode environmental control system for pressurized aircraft cabin. USP1999095956960.