Gas turbine engine thermal expansion joint

F - Mech Eng,Light,Heat,Weapons – 02 – C

Patent

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Details

F02C 7/28 (2006.01) F01D 25/14 (2006.01) F01D 25/24 (2006.01) F01D 25/28 (2006.01) F02C 7/12 (2006.01)

Patent

CA 2715591

A thermal expansion joint apparatus includes an insert extending passages passing through respective first and second components to loosely restrain the first component between the second component and an enlarged head of the insert thereby allowing thermal expansion of the respective first and second components relative to each other. The insert is secured to the second component by a fastener which can be removed, for example, when the insert is to be removed from the engine.

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