发明名称 |
FUEL MANIFOLD INLET TUBE |
摘要 |
An inlet tube supplies fuel to a manifold of a combustor in a gas turbine engine, the manifold defining a manifold plane. The inlet tube comprises a tube body having a channel providing fluid flow communication between first and second ends of the tube body. At least a portion of the channel defines a tube body plane which is spaced apart from the manifold plane.
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申请公布号 |
US2007163265(A1) |
申请公布日期 |
2007.07.19 |
申请号 |
US20070669493 |
申请日期 |
2007.01.31 |
申请人 |
FISH JASON;PATEL BHAWAN B |
发明人 |
FISH JASON;PATEL BHAWAN B. |
分类号 |
F02C7/26;F02C7/22;F23R3/28 |
主分类号 |
F02C7/26 |
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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