发明名称 |
Transition with a linear flow path for use in a gas turbine engine |
摘要 |
A transition duct for routing a gas flow from a combustor to the first stage of a turbine section in a combustion turbine engine is disclosed. The transition duct may have an internal passage extending between an inlet to an outlet. An axis of the transition duct body may be generally linear such that gases expelled from the transition duct body flow in a proper direction into the downstream turbine blades.
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申请公布号 |
US8113003(B2) |
申请公布日期 |
2012.02.14 |
申请号 |
US20080190074 |
申请日期 |
2008.08.12 |
申请人 |
CHARRON RICHARD;MONTGOMERY MATTHEW;SNYDER GARY;SIEMENS ENERGY, INC. |
发明人 |
CHARRON RICHARD;MONTGOMERY MATTHEW;SNYDER GARY |
分类号 |
F02G3/00;F02C1/00 |
主分类号 |
F02G3/00 |
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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