发明名称 |
Gas turbine engines with fuel injector assemblies |
摘要 |
In accordance with an exemplary embodiment, a fuel injector assembly is provided for a gas turbine engine with a compressor section and a combustion section. The fuel injector assembly includes a stem (310) defining a fuel path for fuel and a flow guide (330) coupled to and extending along the stem. The flow guide receives an air flow (302). The assembly further includes a swirler apparatus (350) coupled to the stem and configured to receive the fuel. The swirler apparatus is further coupled to the flow guide and configured to receive the air flow. The swirler apparatus is configured to mix the fuel and the air flow and direct the mixture into a combustor of the combustor assembly. |
申请公布号 |
EP2806217(A3) |
申请公布日期 |
2015.04.01 |
申请号 |
EP20140167277 |
申请日期 |
2014.05.06 |
申请人 |
HONEYWELL INTERNATIONAL INC. |
发明人 |
ZUPANC, FRANK J.;PARDINGTON, RONALD B.;YANKOWICH, PAUL |
分类号 |
F23R3/14;F23R3/28 |
主分类号 |
F23R3/14 |
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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