A method of controlling an engine for a propeller-driven aircraft, including setting an initial maximum power limit, wherein the initial maximum power limit is associated with a maximum allowable thrust for an aircraft, receiving an indication that a predetermined aircraft condition is satisfied, and setting an updated maximum power limit.


    Access

    Download


    Export, share and cite



    Title :

    POWER CONTROL FOR PROPELLER-DRIVEN AIRCRAFT


    Contributors:

    Publication date :

    2016-07-21


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

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



    POWER CONTROL FOR PROPELLER-DRIVEN AIRCRAFT

    MCWATERS MARK WAYNE / NIELSEN SCOTT RICHARD | European Patent Office | 2019

    Free access

    Power control for propeller-driven aircraft

    MCWATERS MARK WAYNE / NIELSEN SCOTT RICHARD | European Patent Office | 2018

    Free access

    Noise Control in Propeller-Driven Aircraft

    Rennison, D. C. / Wilby, J. F. | NTRS | 1983


    Propeller-driven helicopter and aircraft

    ZHU XIAOYI | European Patent Office | 2021

    Free access

    Vortex Wakes Behind Propeller-Driven Aircraft

    Ginevsky, A.S. / Zhelannikov, A.I. | Springer Verlag | 2009