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Piezo-actuator de-icing array design is an important aspect when inducing the mechanical vibrational de-icing system on aviation equipment. We introduced a de-icing array design framework considering the positioning laws of actuators and adhesive bonding layer thickness control. Successful de-icing results in ice wind tunnel show the feasibility of the piezo-actuator array design framework.
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This page is a summary of: Piezoelectric-Actuator De-Icing Array Design Based on Structural Vibration Modes, Journal of Aircraft, May 2024, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.c037448.
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