发明名称 Fuel Lance for a Gas Turbine Engine
摘要 <p>The invention relates to a fuel lance (7) for introducing fuel into a gas flow in a combustor (1) of a gas turbine engine, whereby a region of the lance (7) through which the fuel is introduced into the gas flow comprises a generally helical formation (12).</p>
申请公布号 EP2169313(A2) 申请公布日期 2010.03.31
申请号 EP20090171054 申请日期 2009.09.23
申请人 ALSTOM TECHNOLOGY LTD 发明人 POYYAPAKKAM, MADHAVAN NARASIMHAN;EROGLU, ADNAN;KELSALL, GREGORY JOHN
分类号 F23R3/28 主分类号 F23R3/28
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