The invention relates to an aircraft including a fuselage and a first measuring probe including means for measuring the local incidence, means for measuring the static pressure, and optionally means for measuring the total pressure. The fuselage includes at least one first zone where the pressure coefficient of the aircraft depends on the unique local incidence irrespective of the sideslip and incidence values of the aircraft, and the first measuring probe is arranged in said first zone


    Access

    Download


    Export, share and cite



    Title :

    Aéronef comprenant une sonde de mesure et procédé de détermination de paramètres de vol d'un tel aéronef


    Additional title:

    Aircraft including a measuring probe and method for determining flight parameters of such an aircraft
    Luftfahrzeug, das eine Messsonde umfasst, und Verfahren zur Bestimmung der Flugparameter eines solchen Luftfahrzeugs


    Contributors:

    Publication date :

    2017-08-09


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    French


    Classification :

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



    PROCEDE D'OPTIMISATION DES PARAMETRES DE DECOLLAGE D'UN AERONEF

    DEMORTIER JEAN PIERRE / HODGES COLIN / PETIT ERIC et al. | European Patent Office | 2017

    Free access

    PROCEDE D'OPTIMISATION DES PARAMETRES DE DECOLLAGE D'UN AERONEF

    DEMORTIER JEAN-PIERRE / HODGES COLIN / THIERS CYRILLE et al. | European Patent Office | 2019

    Free access

    Sonde de mesure aérodynamique pour aéronef

    LEBLOND HENRI / MANDLE JACQUES | European Patent Office | 2016

    Free access