Nested channel ducts for nozzle construction and the like

Power plants – Combustion products used as motive fluid – Process

Reexamination Certificate

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Details

C060S734000, C060S742000, C285S124100

Reexamination Certificate

active

07028484

ABSTRACT:
A multiple conduit system for a gas turbine engine, the multiple conduit system extending between a plurality of conduit inlet and outlets. A channel is formed in a surface of a gas turbine engine component, and the channel is adapted for conveying a fluid flow from an inlet to an outlet. At least a first sealing member is disposed within the channel and divides the channel into at least a first discrete conduit and a second discrete conduit. A second sealing member encloses the channel to define the second discrete conduit. The first and second discrete conduits are each adapted to direct an independent fluid flow from respective inlets to respective outlets.

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