Transition reinforcement of composite blade dovetails

Details Transition reinforcement of composite blade dovetails Transition reinforcement of composite blade dovetails

F - Mech Eng,Light,Heat,Weapons

04

D

154/121, 170/84

F04D 29/38 (2006.01) C22C 47/00 (2006.01) F01D 5/28 (2006.01)

Patent

CA 1042350

Abstract The composite filament laminates of a composite blade are splayed at the root thereof to receive metallic inserts therebetween. A transition material having a modulus of elasticity greater than that of the inserts and less than that of the laminates is bonded therebetween to more uniformly distribute the blade loadings into the root region.

266622

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