Radial loading element for turbine vane

F - Mech Eng,Light,Heat,Weapons – 01 – D

Patent

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Details

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

Patent

CA 2638542

A vane assembly for a gas turbine engine comprising a number of radial loading elements disposed between lugs of the vane ring and the vane support, such as to generate a radial load force against the vane ring. The radial load force prevents unwanted relative movement between the vane ring and the vane support during operation of the gas turbine engine.

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