发明名称 Combustion dynamics monitoring ignition system for a gas turbine
摘要 <p>A combustor (102) including a casing (104) surrounding a combustion zone (106), and an ignitor plug (108) including a tip (110), a base (112), and a body (114) extending therebetween, the body (114) extending through the combustor casing (104) such that the tip (110) is proximate the combustion zone (106), the ignitor plug (108) configured to receive ignition energy through the base (112) and generate an ignition source at the tip (110), the ignitor plug (108) further configured to sense combustion dynamics in the combustion zone (106) and generate a signal relative to the sensed combustion dynamics.</p>
申请公布号 EP2455661(A2) 申请公布日期 2012.05.23
申请号 EP20110188194 申请日期 2011.11.08
申请人 GE AVIATION SYSTEMS LLC 发明人 STEFFLER, JOSEPH BERNARD
分类号 F23N5/12;F02P17/12;F23N5/24 主分类号 F23N5/12
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