Seal system for an interturbine duct within a gas turbine...

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

Patent

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F02C 7/28 (2006.01) F02C 9/18 (2006.01) F02K 3/02 (2006.01) F16J 15/02 (2006.01)

Patent

CA 2598326

The interturbine duct (ITD) directs hot combustion gases from a high pressure turbine stage outlet to a low pressure turbine stage inlet in a gas turbine engine. The ITD comprises an outer wall and a heat resistant non-metallic resilient annular seal provided around an end of the outer wall that is adjacent to the high pressure turbine stage outlet.

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