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
WO2014055435(A3)
申请公布日期
2014.05.30
申请号
WO2013US62688
申请日期
2013.09.30
申请人
ALSTOM TECHNOLOGY LTD.;STUTTAFORD, PETER, JOHN;JORGENSEN, STEPHEN;CHEN, YAN
发明人
STUTTAFORD, PETER, JOHN;JORGENSEN, STEPHEN;CHEN, YAN