Composite leading edge for aircraft

Details Composite leading edge for aircraft Composite leading edge for aircraft

B - Operations, Transporting

64

D

244/108

B64D 15/00 (2006.01) B64D 15/16 (2006.01) H01Q 1/42 (2006.01)

Patent

CA 1161014

ABSTRACT A mold-formed, replaceable nonmetallic aircraft leading edge portion comprises an inner, rigid member and an outer, flexible, elastomeric member. The outer member may be a deicer or erosion shoe while the inner member may be of suitable plastic.

359080

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