Various implementations directed to a cabin thermal management system are provided. In one implementation, an aircraft may include a passenger cabin configured to transport one or more passengers. The aircraft may also include a battery pack configured to power one or more electronic components of the aircraft. The aircraft may further include a cabin thermal management system configured to regulate a cabin temperature of the passenger cabin by transferring thermal energy from the battery pack to the passenger cabin.


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    Title :

    CABIN THERMAL MANAGEMENT SYSTEM


    Contributors:

    Publication date :

    2021-03-04


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

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



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