An aircraft morphable aerodynamic surface structure including an elastomeric material having a glass transition temperature, a temperature management system for heating or cooling the elastomeric material, and a controller to control the temperature management system, the controller configured to control the temperature management system on the basis of a command received at the controller.


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    Title :

    AIRCRAFT SURFACE STRUCTURE


    Contributors:

    Publication date :

    2025-01-30


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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