Method and apparatus for deicing a leading edge.

摘要

An airfoil deicer (10) and method for deicing an airfoil wherein the deicer has an outer skin (12) having an elevated modulus of elasticity and a means for introducing a small deflection into the outer skin thereby creating substantial chord-wise tension in the outer skin, the deflection being induced in less than 0.250 seconds. In the method of deicing, the deflection is induced periodically and being completed within a time span of about 0.250 seconds to remove accumulations of ice as thin as 0.06 centimeters.