POWER SYSTEM
    6.
    发明公开
    POWER SYSTEM 审中-公开

    公开(公告)号:EP4414268A1

    公开(公告)日:2024-08-14

    申请号:EP23156399.0

    申请日:2023-02-13

    CPC classification number: B64D27/24 B64D35/00 B64D35/02 B64D27/026

    Abstract: A power system for an aircraft comprises: a motor-generator component; a shaft, wherein the motor-generator component is connectable to the shaft, the shaft connectable to an additional component of the aircraft to for torque transfer with the additional component; and a de-coupler operable to disconnect the motor-generator component from the shaft, wherein the motor-generator component is located between the de-coupler and the additional component in use.

    PROPULSION SYSTEM, AIRCRAFT HAVING A PROPULSION SYSTEM, AND METHOD OF MANUFACTURING AN AIRCRAFT

    公开(公告)号:EP4410679A2

    公开(公告)日:2024-08-07

    申请号:EP24183634.5

    申请日:2021-05-03

    CPC classification number: B64D29/00 B64D27/02

    Abstract: A propulsion system for an aircraft is taught herein. The propulsion system includes, but is not limited to, an engine. The propulsion system further includes, but is not limited to, an outer cover associated with the engine. The engine and the outer cover are configured for coupling to the aircraft. The propulsion system further includes, but is not limited to, an external engine component. The propulsion system still further includes, but is not limited to, a coupler that operatively couples the external engine component to the engine. The external engine component is configured to be coupled to the aircraft at a location spaced apart from the engine.

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