Invention Grant
US09243506B2 Methods and systems for cooling a transition nozzle 有权
用于冷却过渡喷嘴的方法和系统

Methods and systems for cooling a transition nozzle
Abstract:
A transition nozzle for use with a turbine assembly is provided. The transition nozzle includes a liner defining a combustion chamber therein, a wrapper circumscribing the liner such that a cooling duct is defined between the wrapper and the liner, a cooling fluid inlet configured to supply a cooling fluid to the cooling duct, and a plurality of ribs coupled between the liner and the wrapper such that a plurality of cooling channels are defined in the cooling duct.
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