A system for heating an aircraft surface having a thermally disadvantaged zone includes a carbon nano-tube (CNT) sheet heating element having a power inlet configured to receive power from an external electrical power source and provide it to the CNT sheet heating element that extends across the thermally disadvantaged zone. The CNT sheet heating element is configured and arranged such upon application of power from the external electrical power source to the CNT sheet heating element, the CNT sheet heating element produces a first heat output in a first zone and a second heat output in the thermally disadvantaged zone with the second heat output being greater than the first heat output.


    Access

    Download


    Export, share and cite



    Title :

    AIRCRAFT HEATING SYSTEM FOR THERMALLY DISADVANTAGED ZONES


    Contributors:

    Publication date :

    2023-04-20


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

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



    AIRCRAFT HEATING SYSTEM FOR THERMALLY DISADVANTAGED ZONES

    GEORGE ADAM / ZADELL ALEX / BOTURA GALDEMIR et al. | European Patent Office | 2023

    Free access

    Aircraft heating system for thermally disadvantageous zones

    ASOK GEORGE / ZADER AVI / BOTURA GALDEMIR CEZAR et al. | European Patent Office | 2023

    Free access


    AIRCRAFT WITH SEPARATE ZONES

    NODA GLEN / SAVIAN SCOTT / SHIMIZU BRUCE | European Patent Office | 2020

    Free access

    THERMAL BARRIER CURTAIN SYSTEMS ESPECIALLY USEFUL FOR THERMALLY ISOLATING INTERIOR CABIN ZONES OF CARGO TRANSPORT AIRCRAFT

    DEMETRIUS ROCHA DE SOUZA / CARLOS EDUARDO CAETANO DE SOUZA / EVERTON LUIS SALLES et al. | European Patent Office | 2023

    Free access