发明名称 |
VARIABLE FLOW DIVIDER MECHANISM FOR A MULTI-STAGE COMBUSTOR |
摘要 |
The present invention discloses a novel apparatus and way for altering the airflow to a gas turbine combustion system. The apparatus comprises a flow divider mechanism which splits the airflow surrounding a combustion liner into two distinct portions, one directed towards a pilot and one directed towards a main stage combustion. The flow divider mechanism is interchangeable so as to provide a way of altering airflow splits between stages of the combustion system. |
申请公布号 |
US2014090400(A1) |
申请公布日期 |
2014.04.03 |
申请号 |
US201314038056 |
申请日期 |
2013.09.26 |
申请人 |
STUTTAFORD PETER JOHN;JORGENSEN STEPHEN;CHEN YAN |
发明人 |
STUTTAFORD PETER JOHN;JORGENSEN STEPHEN;CHEN YAN |
分类号 |
F23R3/26;F23R3/60 |
主分类号 |
F23R3/26 |
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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