There is disclosed an aircraft configured to collect air data, the aircraft comprising: a wing structure; a forebody, forward of the wing structure; an afterbody, backward of the forebody; a skin covering the wing, the forebody and the afterbody; at least one recess formed at the skin, the recess being configured to affect the pressure of air flowing at the recess; at least one ambient sensor port for measuring ambient air pressure at the skin; and at least one recess sensor port for measuring the air pressure at the recess.


    Access

    Download


    Export, share and cite



    Title :

    Aircraft with skin layer air data sensor


    Contributors:

    Publication date :

    2023-10-03


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    G01P MEASURING LINEAR OR ANGULAR SPEED, ACCELERATION, DECELERATION OR SHOCK , Messen der Linear- oder Winkelgeschwindigkeit, der Beschleunigung, der Verzögerung oder des Stoßes / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



    Identifying Boundary-Layer Transitions on Aircraft Skin

    Holmes, B. J. / Croom, C. C. / Kelliher, W. C. et al. | NTRS | 1984


    Multi-layer de-icing skin for aircraft platforms

    BRUCE ALLAN JAMES / CYRUS MICHAEL / FROLOV SERGEY | European Patent Office | 2017

    Free access

    MULTI-LAYER DE-ICING SKIN FOR AIRCRAFT PLATFORMS

    BRUCE ALAAN JAMES / CYRUS MICHAEL / FROLOV SERGEY | European Patent Office | 2015

    Free access

    MULTI-LAYER DE-ICING SKIN FOR AIRCRAFT PLATFORMS

    BRUCE ALAAN JAMES / CYRUS MICHAEL / FROLOV SERGEY | European Patent Office | 2019

    Free access

    AIRCRAFT WITH AIR DATA SENSOR

    ELLISON WILLIAM FRANK | European Patent Office | 2024

    Free access