Dual fuel injection method and apparatus with multiple air blast

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

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Details

60 3906, 60737, 60746, 60747, 60748, 2394245, 2394193, F02C 320, F02G 300

Patent

active

058264230

ABSTRACT:
A dual fuel injector for injecting liquid and/or gaseous fuel into a gas turbine engine includes a plurality of hollow spoke members for injecting gaseous fuel that are located upstream of a plurality of main air swirling vanes that are in turn upstream of a plurality of air-blast atomizers for injecting main liquid fuel. A pilot fueling arrangement is provided that is capable of starting the gas turbine engine using either gaseous or liquid fuel. The injector includes a labyrinth-shaped cooling passage capable of providing cooling air to cylindrical walls of an injector centerbody.

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patent: 5218824 (1993-06-01), Cederwall et al.
patent: 5404711 (1995-04-01), Rajput
patent: 5408825 (1995-04-01), Foss et al.
patent: 5660044 (1997-08-01), Bonciani et al.

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