发明名称 |
Transition duct having airfoil and hot gas path assembly for turbomachine |
摘要 |
<p>A hot gas path assembly (30) includes an outer support ring (36), an inner support ring (40), and a transition duct (32) coupled to the outer support ring (36) and the inner support ring (40). The transition duct (32) includes a conduit (50) defining a passage (52) extending between an inlet (54) and an outlet (56). The inlet (54) and the outlet (56) are generally aligned along a longitudinal axis (60). The transition duct (32) further includes an airfoil (70) disposed within the conduit (50) and configured to alter a hot gas flow direction (72).</p> |
申请公布号 |
EP2730747(A1) |
申请公布日期 |
2014.05.14 |
申请号 |
EP20130191951 |
申请日期 |
2013.11.07 |
申请人 |
GENERAL ELECTRIC COMPANY |
发明人 |
DAVI, MICHAEL ALAN;GENGHIS KHAN, KHAN MOHAMED KHIRULLAH;FARRELL, THOMAS RAYMOND |
分类号 |
F01D9/02 |
主分类号 |
F01D9/02 |
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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