Method and apparatus for deicing a leading edge

Valves and valve actuation – Fluid actuated or retarded – Pilot or servo type motor

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Details

60411, 244134A, F16K 3142

Patent

active

048652911

ABSTRACT:
An airfoil deicer and method for deicing an airfoil wherein the deicer has an outer skin 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.

REFERENCES:
patent: 604358 (1898-05-01), Alexander

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