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Ceramic vane drive jointA variable geometry gas turbine has an array of ceramic composition vanes positioned by an actuating ring coupled through a plurality of circumferentially spaced turbine vane levers to the outer end of a metallic vane drive shaft at each of the ceramic vanes. Each of the ceramic vanes has an end slot of bow tie configuration including flared end segments and a center slot therebetween. Each of the vane drive shafts has a cross head with ends thereof spaced with respect to the sides of the end slot to define clearance for free expansion of the cross head with respect to the vane and the cross head being configured to uniformly distribute drive loads across bearing surfaces of the vane slot.
Document ID
20080004236
Acquisition Source
Headquarters
Document Type
Other - Patent
Authors
Smale, Charles H.
Date Acquired
August 24, 2013
Publication Date
November 24, 1981
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
Patent Number: US-PATENT-4,302,149
Patent Application Number: US-PATENT-APPL-SN-122475
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Patent
US-PATENT-4,302,149
Patent Application
US-PATENT-APPL-SN-122475
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