Electro-mechanical de-icer modeling with aeronautics application
Résumé
The development of a multi physics model, for
a new electro-mechanical de-icing solution, is presented in this
article. The technology proposed by aeronautics industry resides
in the principles of Laplace forces and plate elastic deformation.
Electro-magneto-mechanical modeling is intended for expressing
the interdependence between the mechanical response and the
electrical stimulus. The resulting expressions incorporate the
dynamics of the call and the particular topology of the structural
elements of the system. Measurements issue from previous
prototypes served to validate the final model. As the goal was to
obtain a model adapted for optimization process, some results
and perspectives are also discussed.