发明名称 |
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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申请公布号 |
US2012328421(A1) |
申请公布日期 |
2012.12.27 |
申请号 |
US201113164887 |
申请日期 |
2011.06.21 |
申请人 |
MCMAHAN KEVIN WESTON;CHILA RONALD JAMES;JOHNS DAVID RICHARD |
发明人 |
MCMAHAN KEVIN WESTON;CHILA RONALD JAMES;JOHNS DAVID RICHARD |
分类号 |
F01D25/24;B23P15/04 |
主分类号 |
F01D25/24 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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