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Combustion chamber for gas turbine engines - has flame tube and inlet formed by diffusor coupled to external wall by diverging wall sections
Combustion chamber for gas turbine engines - has flame tube and inlet formed by diffusor coupled to external wall by diverging wall sections
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机译:用于燃气涡轮发动机的燃烧室-具有火焰管和由扩散器形成的进气口,扩散器通过发散壁段连接到外壁
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摘要
The combustion chamber for a gas turbine engine has an external housing holding a flame tube. The combustion chamber inlet is formed by an inlet diffuser which diverges in conical form in the direction of the axial compressed air flow. The diffuser is connected with the combustion chamber external housing by conically expanding inner and external wall sections. The wall parts are two conical guide baffles connected at the downstream end of the outlet plane of the inlet diffuser. They also project up to the combustion chamber external housing. A cross section change occurs in the outlet plane of the inlet diffusor.
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