发明授权
US4149373A Combustion chamber stress reducing means 失效
燃烧室减压装置

Combustion chamber stress reducing means
摘要:
A gas turbine engine is shown having an annular burner casing with an annular burner therein. A conventional fuel and air supply can be provided. The burner is formed of conventional louver construction at the forward part thereof with the last louver of both the inner and outer burner wall being welded to its upstream louver with a curled forward end being curled to extend away from the upstream louver. This connection is formed on the louvers which restrict the flow through the burner.
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