A method converts an aircraft takeoff trim setting that would be a function of several parameters to a value that is a function of CG position only. In this way, it is possible to create a direct simple equivalence between Stabilizer angle and CG. The equivalent CG can be presented in real time to the pilot,


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    Titel :

    ENHANCED TAKE-OFF TRIM INDICATION


    Weitere Titelangaben:

    VERBESSERTE TAKE-OFF TRIMMUNG ANZEIGE
    INDICATION DE COMPENSATEUR AU DÉCOLLAGE AMELIORÉE



    Erscheinungsdatum :

    31.03.2021


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    G01M TESTING STATIC OR DYNAMIC BALANCE OF MACHINES OR STRUCTURES , Prüfen der statischen oder dynamischen Massenverteilung rotierender Teile von Maschinen oder Konstruktionen / B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



    Enhanced takeoff trim indication

    DE SOUZA SÉRGIO LUIZ MIRANDA / MENINI EDUARDO ALVES / MORIMITSU LUMI GALADRIEL SILVA | Europäisches Patentamt | 2020

    Freier Zugriff

    ENHANCED TAKEOFF TRIM INDICATION

    DE SOUZA SÉRGIO LUIZ MIRANDA / MENINI EDUARDO ALVES / MORIMITSU LUMI GALADRIEL SILVA | Europäisches Patentamt | 2019

    Freier Zugriff

    Use of trim-angle indicator for seaplane take-off

    Gough, M.N. | Engineering Index Backfile | 1937


    The effect of trim angle on the take-off performance

    Shoemaker, James M / Dawson, John R | NTRS | 1934


    Effect of trim angle on take-off performance of flying boat

    Shoemaker, J.M. / Dawson, J.R. | Engineering Index Backfile | 1934