CAPACITANCE BASED WEAR INDICATOR
    12.
    发明申请

    公开(公告)号:US20190186285A1

    公开(公告)日:2019-06-20

    申请号:US15846859

    申请日:2017-12-19

    Abstract: A wear indicator for detecting blade clearance in a gas turbine engine includes a capacitor connected to a first conductor and a second conductor. The capacitor includes a multiple of layers arranged transverse to a rub direction, each layer separated by an insulator and including a first plate, a second plate, and a dielectric between the first plate and the second plate. A method of detecting blade clearance in a gas turbine engine, includes determining a change in capacitance between the first and second capacitance and determining an amount of material removed from the wear indicator by the blade corresponding to the change in capacitance.

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