| 发明名称 |
GAS TURBINE ENGINE COMBUSTOR |
| 摘要 |
A swirler assembly for a gas turbine engine includes an outer annular injector which at least partially surrounds an inner injector and an air-assist atomizer upstream of said inner injector. |
| 申请公布号 |
WO2014197070(A2) |
申请公布日期 |
2014.12.11 |
| 申请号 |
WO2014US26189 |
申请日期 |
2014.03.13 |
| 申请人 |
UNITED TECHNOLOGIES CORPORATION |
发明人 |
CUNHA, FRANK;ERBAS-SEN, NURHAK |
| 分类号 |
F23R3/28;F02C7/04;F02C7/22;F23R3/22 |
主分类号 |
F23R3/28 |
| 代理机构 |
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代理人 |
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| 地址 |
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