An apparatus includes a transmission system for an aircraft structure, in which the aircraft structure includes a first propeller assembly and a second propeller assembly, and an engine assembly. The transmission system is configured to (A) be coupled to the engine assembly, (B) be coupled to the first propeller assembly and the second propeller assembly. The transmission system is also configured to urge, in use, the first propeller assembly and the second propeller assembly to (i) operatively rotate in opposite directions relative to each other, and (ii) operatively rotate at different rotational speeds relative to the rotational speed of the engine assembly. The different rotational speeds of the first propeller assembly and the second propeller assembly, in use, urge the aircraft structure to move along a desired flight path.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    TRANSMISSION SYSTEM FOR AIRCRAFT STRUCTURE


    Beteiligte:

    Erscheinungsdatum :

    22.08.2019


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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



    TRANSMISSION SYSTEM FOR AIRCRAFT STRUCTURE

    CORREA HAMILL JUAN MANUEL | Europäisches Patentamt | 2021

    Freier Zugriff

    TRANSMISSION SYSTEM FOR AIRCRAFT STRUCTURE

    CORREA HAMILL JUAN MANUEL | Europäisches Patentamt | 2019

    Freier Zugriff

    Aircraft transmission structure

    SUN YUFEI / LIU ZHIQIANG / HU QIANG et al. | Europäisches Patentamt | 2024

    Freier Zugriff

    Aircraft transmission mechanism, transmission system and aircraft

    TAO FEI | Europäisches Patentamt | 2024

    Freier Zugriff

    Hybrid power transmission system for aircraft and aircraft

    GIANNINI FRANCESCO | Europäisches Patentamt | 2024

    Freier Zugriff