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US08966910B2 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
摘要:
A turbine assembly includes a fuel nozzle configured to mix fuel and air and a transition nozzle oriented to receive the fuel and air mixture from the fuel nozzle. The transition nozzle includes a transition portion and a nozzle portion integrally formed with the transition portion. The transition nozzle includes a plurality of openings oriented to channel air to facilitate cooling the transition portion and/or the nozzle portion. The transition portion is oriented to channel combustion gases towards the nozzle portion.
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