Secondary fuel nozzle with readily customizable pilot fuel...

Power plants – Combustion products used as motive fluid – Combustion products generator

Reexamination Certificate

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C060S748000, C239S399000

Reexamination Certificate

active

06857271

ABSTRACT:
An improved secondary fuel distribution system having a readily adjustable premix pilot nozzle for use in a gas turbine combustor is disclosed. The secondary fuel nozzle assembly has a premix fuel nozzle comprising an annular tubular manifold and a premix pilot nozzle. Multiple embodiments of premix pilot nozzles are disclosed that have a fuel flow rate that can be controlled and adjusted as required, including a plate and feed hole combination, a pressfit premix pilot nozzle, and a premix pilot nozzle that is threaded into the secondary fuel nozzle assembly.

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patent: 6609376 (2003-08-01), Rokke

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