发明名称 |
Fuel injection assembly for a gas turbine |
摘要 |
<p>A gas turbine comprises a combustion unit (8), a flow sleeve (2) surrounding the combustion unit (8), wherein the flow sleeve (2) is positioned radially outward from the combustion unit (8). Further, the gas turbine includes a fuel injection assembly which is integrated with a flange means (4) which supports the combustion unit (8). The fuel injection assembly is provided with a hollow fuel supply casing having an outer wall (10). The fuel injection assembly comprises a plurality of dispensing tubes (12) coupled to the outer wall (10). The plurality of dispensing tubes (12) is adapted to discharge fuel into the annular cavity. The fuel injection assembly is disposed in the annular cavity between the flow sleeve (2) and a combustion unit (2) of the gas turbine.</p> |
申请公布号 |
EP2949999(A1) |
申请公布日期 |
2015.12.02 |
申请号 |
EP20140170275 |
申请日期 |
2014.05.28 |
申请人 |
SIEMENS AKTIENGESELLSCHAFT |
发明人 |
GUPTA, GAURAV;PFADLER, SEBASTIAN;SINGH, MANOJ;SINGH, RAM BAHADUR |
分类号 |
F23R3/28;F23R3/54;F23R3/60 |
主分类号 |
F23R3/28 |
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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