An engine and propeller control system (EPECS) of an aircraft includes a propeller (30) with a plurality of blades (110) coupled to an aircraft engine. Each of the blades (110) are coupled to an actuator (111) configured to adjust the blades (110) between a first pitch to produce forward thrust and a second pitch to produce reverse thrust. The EPECS (200) further includes a controller (250) configured to control the actuator (111) to invoke the second pitch in response to receiving a reverse thrust command signal. The controller (250) is configured to alert that the reverse thrust command signal is generated prior to landing the aircraft.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    DISENGAGEMENT FOR REVERSE PROPELLER PROTECTION


    Weitere Titelangaben:

    ABKOPPLUNG FÜR UMKEHRPROPELLERSCHUTZ
    DÉBRAYAGE POUR LA PROTECTION CONTRE L'HÉLICE INVERSÉE


    Beteiligte:
    GHATTAS ANDREW (Autor:in)

    Erscheinungsdatum :

    18.06.2025


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / F02C Gasturbinenanlagen , GAS-TURBINE PLANTS



    DISENGAGEMENT FOR REVERSE PROPELLER PROTECTION

    GHATTAS ANDREW | Europäisches Patentamt | 2025

    Freier Zugriff

    Propeller thrust reverse

    Roosenboom, Eric W.M. / Schröder, Andreas | Tema Archiv | 2007


    Reverse stop folding propeller

    HE JUN / DU XINYANG / LI SHENGJUN et al. | Europäisches Patentamt | 2023

    Freier Zugriff

    Coaxial reverse propeller helicopter

    LUO JUN | Europäisches Patentamt | 2021

    Freier Zugriff

    DISENGAGEMENT DEVICE

    NASHIKO TADAHIRO / HITOMI ATSUSHI | Europäisches Patentamt | 2017

    Freier Zugriff