Pilot nozzle for a gas turbine combustor and supply path...

Details Pilot nozzle for a gas turbine combustor and supply path... Pilot nozzle for a gas turbine combustor and supply path...

F - Mech Eng,Light,Heat,Weapons

23

R

F23R 3/28 (2006.01) F23D 14/48 (2006.01) F23D 14/78 (2006.01) F23D 17/00 (2006.01) F23R 3/34 (2006.01)

Patent

CA 2379218

This pilot nozzle has a fuel oil supply pipe disposed at the center of a heat-shielding air layer that is provided along an axial core, and a plurality of atomizing-fluid supply paths are disposed in the circumferential direction of a cylinder unit that surrounds the outside of the heat-shielding air layer. The atomizing-fluid supply paths and the fuel gas supply paths are disposed alternately and uniformly. Based on this structure, it is possible to take a large thickness for the heat-shielding air layer to a maximum extent in a radial direction. Therefore, it is possible to protect the fuel oil supply pipe disposed at the center, from high temperature at the outside of the pilot nozzle.

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