Invention Grant
US08234872B2 Turbine air flow conditioner 失效
涡轮空气流量调节器

Turbine air flow conditioner
Abstract:
A system includes an air flow conditioner configured to mount in an air chamber separated from a combustion chamber of a turbine combustor. The air flow conditioner comprises a perforated annular wall configured to direct an air flow in both an axial direction and a radial direction relative to an axis of the turbine combustor. In addition, the air flow conditioner is configured to uniformly supply the air flow into air inlets of one or more fuel nozzles.
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