Cooling system for a transition bracket of a transition in a...

Power plants – Combustion products used as motive fluid – Plural combustion products generators in ring coaxial with...

Reexamination Certificate

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C060S752000, C060S800000

Reexamination Certificate

active

11044766

ABSTRACT:
A heat shield for a transition of a turbine engine for coupling a transition component of a turbine engine to a turbine vane assembly to direct combustor exhaust gases from the transition into the turbine vane assembly. The heat shield may be capable of reducing the temperature differential across a transition bracket extending from a transition component, thereby reducing the likelihood of premature failure of the bracket or the transition, or both. The heat shield may reduce the temperature differential by insulating the transition bracket and transition bracket rib from cooling gases. The heat shield may be formed from a tubular elongated body having first and second end attachments configured to attach the elongated heat shield body to the transition.

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patent: 2003-322337 (2003-11-01), None

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