An attachable electro-impulse de-icer for de-
icing an aircraft structural member includes an
inductor coil disposed in proximity with the outer surface of the structural member. The coil is supported by a flexible, ice-accumulating support member (surface ply) that permits the coil to move relative to the structural member. Preferably the coil and support member are formed in an integral construction that can be attached to the
leading edge of the structural member. The coil and support member are rapidly, and forcefully, displaced away from the structural member upon passing a short-duration, high-
current pulse through the coil. The current flow creates an
electromagnetic field that induces eddy currents in the support member (if made of
metal), and the structural member (if made of
metal). Upon collapse of the
electromagnetic field in the coil the support member is pulled rapidly to its
rest position adjacent the structural member. Alternative arrangements are provided wherein (1) a
metal target is disposed in proximity with the outer surface of the coil, (2) a metal target is disposed in proximity with the outer surface of the structural member, and (3) an additional target (doubler) is attached to the inner surface of the structural member.