To provide an aircraft environmental control system and a method for controlling temperature in an aircraft.SOLUTION: An airflow interleaver 300 comprises: a first airflow guide structure 302 configured to guide a second airflow 108 towards a central axis 226 of a mixing chamber 202; and a second airflow guide structure 304 configured to guide a first airflow 104 away from the central axis 226. A method includes introducing first and second airflows 104 and 108 to a mix manifold 200, and mixing the first and second airflows, which includes guiding the first airflow 104 away from the central axis 226 and guiding the second airflow 108 towards the central axis 226.SELECTED DRAWING: Figure 2

    【課題】航空機環境制御システム、及び航空機内の温度を制御する方法を提供する。【解決手段】気流インタリーバ300が、混合チャンバ202の中央軸226に向かって第2の気流108を案内するよう構成された第1の気流案内構造302と、中央軸226から遠ざけて第1の気流104を案内するよう構成された第2の気流案内構造304と、を備える。本方法は、混合マニフォールド200へと第1の気流及び第2の気流104、108を導き、混合することを含み、このことは、中央軸226から遠ざけて第1の気流104を案内することと、中央軸226に向かって第2の気流108を案内することと、を含む。【選択図】図2


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    Titel :

    AIRCRAFT ENVIRONMENTAL CONTROL SYSTEM HAVING AIRFLOW INTERLEAVER, AND METHOD FOR CONTROLLING AIRFLOW WITHIN AIRCRAFT


    Weitere Titelangaben:

    気流インタリーバを備えた航空機環境制御システム、及び航空機内の気流を制御する方法


    Beteiligte:
    NICHOLAS A JONES (Autor:in) / WILLIAM C HAAS (Autor:in)

    Erscheinungsdatum :

    15.06.2022


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Japanisch


    Klassifikation :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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