Gas turbine dual fuel nozzle

F - Mech Eng,Light,Heat,Weapons – 02 – C

Patent

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F02C 9/20 (2006.01) F23D 17/00 (2006.01)

Patent

CA 2087693

57,214 ABSTRACT OF THE DISCLOSURE 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 extend- ing 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.

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