Gas turbine dual fuel nozzle

Power plants – Combustion products used as motive fluid – Combined with regulation of power output feature

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60746, F02C 100

Patent

active

052223574

ABSTRACT:
In a gas turbine dual fuel nozzle including a main nozzle body with a support flange having a liquid fuel and atomizing air nozzle structure centrally extending therethrough with a fuel and atomizing air discharge structure arranged at its free end and a fuel gas supply structure arranged around the free end of the fuel and atomizing air discharge structure wherein the fuel gas supply structure has a front face extending inwardly adjacent the fuel and atomizing air discharge structure and having a central opening permitting the discharge of liquid fuel and atomizing air therethrough, the front face has bores extending therethrough in radial symmetry in a circular array and radial slots formed therein between said bores and the central opening so as to eliminate hoop stresses in the front face around its central opening.

REFERENCES:
patent: 2968925 (1961-01-01), Blevans et al.
patent: 3777983 (1973-12-01), Hibbins
patent: 4154056 (1979-05-01), Emory
patent: 4337618 (1982-07-01), Hughes et al.
patent: 4566268 (1986-01-01), Hoffeins et al.
patent: 4977740 (1990-12-01), Madden et al.

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