Structural airfoil having integral expulsive system

Details Structural airfoil having integral expulsive system Structural airfoil having integral expulsive system

B - Operations, Transporting

64

D

244/105, 244/34,

B64D 15/18 (2006.01) B64C 3/00 (2006.01) B64C 3/52 (2006.01) B64D 15/16 (2006.01)

Patent

CA 2028972

STRUCTURAL AIRFOIL HAVING INTEGRAL EXPULSIVE SYSTEM ABSTRACT A structural member having integral surf ace de-icing capability and method of manufacture are described. The structural member includes a non-metallic high tensile modulus fiber-reinforced matrix structural backing, thin force and displacement generation means, and a thin high tensile modulus outer skin bonded to said backing and said force and displacement generation means which is postponed between the backing and the skin. The force and displacement generation means may include one or more inflatable tubular members and/or electromagnetic apparatus. The structural member may be substituted for the aluminum alloy leading edge structural skin typically employed on modern aircraft. 1484E

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