Gas turbine engine failure detection system
    1.
    发明授权
    Gas turbine engine failure detection system 失效
    燃气轮机发动机故障检测系统

    公开(公告)号:US5411364A

    公开(公告)日:1995-05-02

    申请号:US172465

    申请日:1993-12-22

    摘要: An electro optic sensor for sensing unwanted axial motion of the turbine of a gas turbine engine away from its normal position, includes a pair of fiber optic wave guides interconnected through a frangible member disposed axially adjacent the turbine rotor. Upon axial movement of the rotor away from its normal position, the frangible element is broken to open the optical circuit associated with the guides. Associated electronic circuitry generates an output signal indicative of failure of the gas turbine rotor.

    摘要翻译: 用于感测燃气涡轮发动机的涡轮机远离其正常位置的不期望的轴向运动的电光传感器包括通过轴向邻近涡轮机转子布置的易碎构件相互连接的一对光纤波导。 当转子轴向移动远离其正常位置时,易碎元件被破坏以打开与引导件相关的光学回路。 相关的电子电路产生指示燃气轮机转子故障的输出信号。