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특허 상세정보

Mixing bleed and ram air at a turbine inlet of a compressing device

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) F01D-005/06    B64D-013/02    B64D-013/06    B64D-013/08    F01D-017/10    F04D-025/04    F04D-029/32    F04D-029/053   
출원번호 US-0604506 (2017-05-24)
등록번호 US-10232948 (2019-03-19)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Cantor Colburn LLP
인용정보 피인용 횟수 : 0  인용 특허 : 22
초록

An air conditioning system for an aircraft is provided. The air conditioning system includes a first rotating component and a second rotating component. The first rotating component includes a compressor and a turbine. The compressor pressurizes a first medium. The first turbine receives a mixture of a second medium and a pressurized form of the first medium. The second rotating component includes a fan.

대표
청구항

1. An air cycle machine for an environmental control system for an aircraft, the air cycle machine comprising: a compressor configured to pressurize a first medium;a first turbine configured to receive a mixture of a second medium and a pressurized form of the first medium;a second turbine configured to receive a third medium; anda fan,wherein the first medium comprises fresh air sourced from outside the aircraft, andwherein the second medium comprises bleed air sourced from a turbine engine or an auxiliary power unit,wherein the first and second mediums...

이 특허에 인용된 특허 (22)

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  11. Atkey, Warren A.; Bernier, Alan T.; Bowman, Michael D.; Campbell, Thomas A.; Cruse, Jonathan M.; Fiterman, Charles J.; Meis, Charles S.; Ng, Casey; Nozari, Farhad; Zielinski, Edward. Electric-based secondary power system architectures for aircraft. USP2011057950606.
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