An aircraft drive shaft system (100) includes a generator shaft (102) extending along a longitudinal axis (A) with a longitudinal bore (104) defined through the generator shaft (102). A thru shaft (106) extends through the longitudinal bore (104) of the generator shaft (102). The thru shaft (106) includes a front coupler mount (108) at a first end (110) operative to receive torque input, and a rear coupler mount (112) at a second end (114) opposite the first end (110). The generator shaft (102) includes a rear coupler mount (116) at a second end (118) of the generator shaft (102) that is coupled to the rear coupler mount (112) of the thru shaft (106) operative to transmit torque from the front coupler mount (108) of the thru shaft (106), through the thru shaft (106), and into the generator shaft (102).


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    Titel :

    MECHANICAL DRIVE SHAFT ARRANGEMENTS FOR TAIL CONE GENERATORS


    Weitere Titelangaben:

    MECHANISCHE ANTRIEBSWELLENANORDNUNGEN FÜR HECKKEGELGENERATOREN
    AGENCEMENTS D'ARBRE D'ENTRAÎNEMENT MÉCANIQUE POUR GÉNÉRATEURS DE CÔNE ARRIÈRE


    Beteiligte:
    MENHEERE DAVID (Autor:in)

    Erscheinungsdatum :

    21.05.2025


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    F02C Gasturbinenanlagen , GAS-TURBINE PLANTS / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / F01D Strömungsmaschinen [Kraft- und Arbeitsmaschinen oder Kraftmaschinen], z.B. Dampfturbinen , NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES



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