发明名称 |
End-fed liquid fuel gallery for a gas turbine fuel injector |
摘要 |
A fuel injector for a gas turbine engine may include an injector housing extending along a longitudinal axis and configured to be fluidly coupled to a combustor of the turbine engine. The fuel injector may also include a flow path for a fuel air mixture to the combustor extending longitudinally within the injector housing, and a gallery for liquid fuel encircling the flow path. The gallery may include a plurality of fuel spokes that are configured to deliver liquid fuel from the gallery to the flow path. The gallery may extend from a feed end to a terminal end that overlaps the feed end. The feed end may be a region where liquid fuel enters the gallery and the terminal end may be a region where the gallery terminates. |
申请公布号 |
GB2499140(B) |
申请公布日期 |
2017.03.22 |
申请号 |
GB20130007681 |
申请日期 |
2011.10.12 |
申请人 |
Solar Turbines Incorporated |
发明人 |
John Frederick Lockyer;Christopher Zdzislaw Twardochleb;Mario E Abreu |
分类号 |
F02C7/232;F02C7/22;F23R3/28 |
主分类号 |
F02C7/232 |
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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