United Technologies Corporation

United States of America As Represented by the Secretary of the Air Force

James E Fisher

George A Bonner

An improved vane platform feather seal is disclosed for use in turbine engines. This feather seal contains a flat, thin feather seal, which is attached by adhesive to ease assembly to an L-shaped retainer plate to result in a combined thickness of 0.032 inches. This new seal may be used to replace the inner vane platform seals which are currently used in F-100 turbine engines, which have a history of not bending easily to conform to seal slots. The new seal provides improved platform sealing without loss of platform retention in the event of vane burn through.

Vane platform sealing and retention means

Adjacent cylindrical bearings disposed within a wall are prevented from rotating and moving axially by a sheet metal tablock which simultaneously engages a slot in the external surfaces of each bearing. A cap fits around each bearing, and a flange on each cap overlies the tablock. Tab ends of the tablock are folded over the flange and trap the tablock in position.

Growing community of inventors

Palm Beach Gardens, FL, United States of America

James E Fisher