Unison Industries, Inc.

Daniel Scott McCann

Derek Thomas Dreischarf

Bernard Albert Luschek

Joseph Richard Schmitt

Dennis Alan McQueen

David William Millward

Anthony Lynn Lighthill

A turbine engine with a casing including opposing surfaces and a manifold opening passing through the surfaces. A surface cooler is provided adjacent one of the surfaces. A cooler manifold passes through the manifold opening. A seal is provided between the surface cooler and the casing. At least one bolt is used to secure the surface cooler to the casing with the seal in between.

Turbine engine thermal seal

A fan casing assembly for a turbine engine including a casing having an annular fan cooler. The annular fan cooler includes first and second connection assemblies to fix movement of the fan cooler during engine operation, while permitting circumferential thermal growth of the fan cooler without suffering from high cycle fatigue.

Turbine engine cooler assembly

Growing community of inventors

Centerville, OH, United States of America

Daniel Scott McCann