Axial loading element for turbine vane

Details Axial loading element for turbine vane Axial loading element for turbine vane

F - Mech Eng,Light,Heat,Weapons

01

D

F01D 9/02 (2006.01) F01D 25/04 (2006.01)

Patent

CA 2638527

A vane assembly for a gas turbine engine comprising an axial loading element disposed between a mounting element of the vane ring and a cooperating portion of the supporting structure, such as to generate a load force therebetween in an axial direction. The axial load force limits unwanted relative movement between the vane ring and the supporting structure during operation of the gas turbine engine.

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