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US08397510B2 Combustor for gas turbine 失效
燃气轮机燃烧器

Combustor for gas turbine
Abstract:
A combustor for a gas turbine capable of performing stable combustion even by using high temperature air, comprising a first burner (5) jetting fuel and air into a combustion chamber (2) and a second burner (8) causing the circulating jet of the fuel and air installed at a position corresponding to the tip part of a flame caused by the first burner (5).
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