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Combustion chamber for gas turbine with precise fuel injection to increase the homogeneity of the air-fuel mixture
Combustion chamber for gas turbine with precise fuel injection to increase the homogeneity of the air-fuel mixture
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机译:用于燃气轮机的燃烧室,具有精确的燃油喷射功能,以提高混合气的均质性
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摘要
A gas turbine combustion chamber comprises a burner (7) fuel inlet and atomizer (6). The fuel injection inlet is positioned in the region of maximum air flow velocity. An Independent claim also included for a chamber as above in which the fuel injection inlet is positioned in the region of the highest local air mass stream.
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