Electronic module mounting to vibration isolating structure

    公开(公告)号:US10267236B2

    公开(公告)日:2019-04-23

    申请号:US15137640

    申请日:2016-04-25

    Abstract: An electromechanical component arrangement for a gas turbine engine includes a mechanical component located at a first side of a firewall of a gas turbine engine and an electronic module of the electromechanical component in communication with the mechanical component separated from the mechanical component by a firewall, the firewall comprising a first side and a second side, the second side having a lower operating temperature than the first side. A vibration isolation structure is located at the second side. The electronic module is connected thereto and includes at least one vibration isolator secured to the firewall to vibrationally isolate the electronic module from gas turbine engine vibrations.

    SYSTEM AND METHOD FOR CONTROLLING AN ENVIRONMENTAL CONDITION OF AN ENGINE ELECTRONIC COMPONENT
    6.
    发明申请
    SYSTEM AND METHOD FOR CONTROLLING AN ENVIRONMENTAL CONDITION OF AN ENGINE ELECTRONIC COMPONENT 审中-公开
    用于控制发动机电子部件的环境条件的系统和方法

    公开(公告)号:US20160177781A1

    公开(公告)日:2016-06-23

    申请号:US14974808

    申请日:2015-12-18

    Abstract: The present disclosure relates generally to a gas turbine engine that includes a fan configured to generate a fanstream and a fanstream duct configured to receive the fanstream flowing therethrough. An engine electronic component is positioned in flow communication with the fanstream. A heating element is positioned in the fanstream upstream from the engine electronic component and is operative to heat at least a portion of the fanstream in flow communication with the engine electronic component. The position of the engine electronic component passively thermally conditions the engine electronic component and the heating element actively thermally conditions the engine electronic component.

    Abstract translation: 本公开一般涉及一种燃气涡轮发动机,其包括被配置为产生风扇流的风扇和被配置为接收流过其中的风扇流的风扇流管。 发动机电子部件被定位成与风扇流动地流动连通。 加热元件位于发动机电子部件上游的风扇流中,并且可操作地加热与发动机电子部件流动连通的风扇流的至少一部分。 发动机电子部件的位置被动地热调节发动机电子部件和加热元件,使发动机电子部件发热。

    Conditioned low pressure compressor compartment for gas turbine engine

    公开(公告)号:US10927763B2

    公开(公告)日:2021-02-23

    申请号:US15091186

    申请日:2016-04-05

    Abstract: A low pressure compressor for a gas turbine engine includes a low pressure compressor case extending circumferentially around a central axis of the gas turbine engine. The low pressure compressor case includes an inner radial wall surrounding a low pressure compressor rotor and an outer radial wall at least partially defining a fan bypass passage of the gas turbine engine. A low pressure compressor compartment is located between the inner radial wall and the outer radial wall and an electrical component is located in the low pressure compressor compartment. An inlet port at the outer radial wall is configured to admit a cooling airflow into the low pressure compressor compartment from the fan bypass passage to cool the electrical component.

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