A method and control system for controlling the thrust of an aircraft. A thrust request is input into a controller and the controller determines throttle, governor, and RPM setpoints to meet the input thrust request. The controller can determine minimum and maximum available thrust limits of the engine and can modify any of the setpoints if any setpoint violates the available thrust limit.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Direct Thrust Control Method for Aircraft Thruster


    Beteiligte:

    Erscheinungsdatum :

    13.03.2025


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / B64C AEROPLANES , Flugzeuge



    DIRECT THRUST CONTROL METHOD FOR AIRCRAFT THRUSTER

    SOIKKELI JOHANNES | Europäisches Patentamt | 2025

    Freier Zugriff

    Micro newton thruster development : direct thrust measurements and thruster downscaling

    Hey, Franz Georg / Springer Fachmedien Wiesbaden / Technische Universität Dresden | TIBKAT | 2018


    Electronegative Gas Thruster - Direct Thrust Measurement Project

    Dankanich, John / Aanesland, Ane / Polzin, Kurt et al. | NTRS | 2015


    Electronegative Gas Thruster - Direct Thrust Measurement Project

    J. Dankanich / A. Aanesland / K. Polzin et al. | NTIS | 2015


    Direct Thrust Measurement of Compact Hexapole ECR Thruster

    Chen, Kuo-Yi / Zhong, Bei-Jing | AIAA | 2022