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Application of a Broadband Active Vibration Control System to a Helicopter Trim Panel

Abstract : This paper discusses testing of a broadband active vibration control concept on an interior trim panel in a helicopter cabin mockup located at ONERA's Centre de Toulouse. The control system consisted of twelve diamond-shaped piezoelectric actuators distributed around a 1.2m x 1.2m trim panel. Accelerometers were mounted at the four vertices of each diamond. The aspect ratio of the diamond was based on the dielectric constants of the piezoelectric material in order to create an actuator-sensor pair that was collocated over a broad frequency range. This allowed robust control to be implemented using simple, low power analog electronics. Initial testing on a thick acrylic window demonstrated the capability of the controller, but actuator performance was less satisfactory when mounted on a composite sandwich trim panel. This may have been due to the orthotropic nature of the trim panel, or due to its much higher stiffness relative to the acrylic window. Insights gained from a finite element study of the actuator-sensor-structural system are discussed.
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Submitted on : Tuesday, August 26, 2014 - 4:55:09 PM
Last modification on : Tuesday, March 16, 2021 - 3:44:16 PM
Long-term archiving on: : Thursday, November 27, 2014 - 4:26:09 PM


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  • HAL Id : hal-01058383, version 1



R.H. Cabell, N.H. Schiller, F. Simon. Application of a Broadband Active Vibration Control System to a Helicopter Trim Panel. Noise-Con 2013, Aug 2013, DENVER, United States. ⟨hal-01058383⟩



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