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

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

Reexamination Certificate

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Details

C060S746000, C060S039463, C060S747000

Reexamination Certificate

active

06862888

ABSTRACT:
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 atomized-fluid supply paths are disposed in the circumferential direction of a cylinder unit that surrounds the outside of the heat-shielding air layer. The atomized-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.

REFERENCES:
patent: 5359847 (1994-11-01), Pillsbury et al.
patent: 5408825 (1995-04-01), Foss et al.
patent: 5647215 (1997-07-01), Sharifi et al.
patent: 5657632 (1997-08-01), Foss
patent: 5784875 (1998-07-01), Statler
patent: 6122916 (2000-09-01), Amos et al.
patent: 6282904 (2001-09-01), Kraft et al.
patent: 20030051478 (2003-03-01), Matsuyama et al.

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