发明名称 FUEL LANCE FOR A GAS TURBINE ENGINE
摘要 A fuel lance (7) for introducing fuel into a gas flow in a combustor (1) of a gas turbine engine includes a region of the lance (7) through which the fuel is introduced into the gas flow having a generally helical formation (12).
申请公布号 US2010077756(A1) 申请公布日期 2010.04.01
申请号 US20080241223 申请日期 2008.09.30
申请人 POYYAPAKKAM MADHAVAN NARASIMHAN;EROGLU ADNAN;KELSALL GREGORY JOHN 发明人 POYYAPAKKAM MADHAVAN NARASIMHAN;EROGLU ADNAN;KELSALL GREGORY JOHN
分类号 F02C7/22;F23R3/28 主分类号 F02C7/22
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