F - Mech Eng,Light,Heat,Weapons – 23 – R
Patent
F - Mech Eng,Light,Heat,Weapons
23
R
F23R 3/28 (2006.01) F23R 3/20 (2006.01)
Patent
CA 2614624
A pilot nozzle of a gas turbine combustor comprises a first structure, provided near a main nozzle of a combustor that injects fuel oil, having a flow channel for a fuel gas and an outlet for the fuel gas. The first structure diffusion-injecting the fuel gas obliquely forward through the outlet to maintain a flame and to aid ignition of the fuel oil injected from the main nozzle. There is further provided a second structure which circulates in whirls a combustion gas generated due to the combustion of the fuel gas.
Aoyama Kuniaki
Inada Mitsuru
Mandai Shigemi
Nishida Koichi
Ohta Masataka
Fetherstonhaugh & Co.
Mitsubishi Heavy Industries Ltd.
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