发明名称 |
Turbomachine assembly with combustors having different flow directions and corresponding operating method |
摘要 |
<p>A turbomachine assembly includes a first combustor (30) configured to combust fuel and compressed air and a second combustor (32) configured to combust fuel and compressed air. Flow moves through the first combustor (30) in a first direction and flow moves though the second combustor (32) in a second direction different than the first direction. The first combustor (30) is axially spaced from the second combustor (32). A corresponding operating method is also provided.</p> |
申请公布号 |
EP2532857(A1) |
申请公布日期 |
2012.12.12 |
申请号 |
EP20120168699 |
申请日期 |
2012.05.21 |
申请人 |
UNITED TECHNOLOGIES CORPORATION |
发明人 |
KUPRATIS, DANIEL B. |
分类号 |
F02C3/14;F23R3/34;F23R3/54 |
主分类号 |
F02C3/14 |
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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