Flutter damper for a turbofan engine

    公开(公告)号:US10578016B2

    公开(公告)日:2020-03-03

    申请号:US15452619

    申请日:2017-03-07

    Abstract: Disclosed is a flutter damper, including an acoustic liner configured for peak acoustical energy absorption at a frequency range that is greater than a frequency range associated with fan flutter, a chamber, and a piezoelectric element disposed within a first surface of the chamber, and the chamber being configured for peak acoustical energy absorption at a frequency range that is associated with one or more fan flutter modes, and wherein the piezoelectric element is operatively connected to an electronic engine control.

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