Natural gas fuel nozzle for gas turbine engine

Power plants – Combustion products used as motive fluid – Using special fuel or oxidizer

Reexamination Certificate

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Details

C060S740000

Reexamination Certificate

active

06871488

ABSTRACT:
A gas fuel nozzle for mounting in a combustor wall of a gas turbine engine, with an at least partially radially-directed array of gas fuel outlets extending beyond an air flow head having an array of compressed air jet apertures around the gas fuel outlets. The air flow head also has a deflector for creating an axial flow of air for deflecting in an axial direction the radially-injected gas fuel.

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patent: 532086 (1954-10-01), None

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