A hover-capable aircraft includes a body including a tubular strut, a first rotor assembly rotatably coupled to the body and positioned about the strut, wherein the first rotor assembly includes a first plurality of circumferentially-spaced blades, a first actuation assembly including a first plurality of electronically controlled actuators coupled to a first swashplate and configured to control the movement of the first swashplate relative to the body, and a control system coupled to the body and configured to control the first plurality of actuators, wherein the control system includes a cable extending through a passage formed in the tubular strut and in signal communication with the first plurality of actuators.


    Access

    Download


    Export, share and cite



    Title :

    HOVER-CAPABLE AIRCRAFT


    Contributors:

    Publication date :

    2021-08-19


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge / B60L PROPULSION OF ELECTRICALLY-PROPELLED VEHICLES , Antrieb von elektrisch angetriebenen Fahrzeugen / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



    HOVER-CAPABLE AIRCRAFT

    BIANCHI ANDREA / SARTORI SERGIO | European Patent Office | 2021

    Free access

    HOVER-CAPABLE AIRCRAFT

    ANDREA GABRIELLI / GASPARINI GIUSEPPE | European Patent Office | 2019

    Free access

    HOVER-CAPABLE AIRCRAFT

    PISANI PAOLO / MONTAGNA FEDERICO / REGONINI ROBERTO et al. | European Patent Office | 2023

    Free access

    HOVER-CAPABLE AIRCRAFT

    BIANCHI ANDREA / SARTORI SERGIO | European Patent Office | 2020

    Free access

    HOVER-CAPABLE AIRCRAFT

    BIANCHI ANDREA / SARTORI SERGIO | European Patent Office | 2020

    Free access