Heat shield for a compressor/stator structure

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

Patent

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Details

F01D 5/00 (2006.01) F01D 25/14 (2006.01)

Patent

CA 2070521

ABSTRACT OF THE DISCLOSURE A heat shield mechanism for thermally protecting a casing located in a turbine engine having a plurality of honeycomb cells which are connected to a support plate. A spring in contact with the support plate and in contact with a vane liner exerts a force on the support plate which causes at least one of the plurality of honeycomb cells to be pressed against the casing.

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Profile ID: LFCA-PAI-O-2007850

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