专利名称：Combustor for gas turbine engine发明人：Morenko, Oleg申请号：EP14158791.5申请日：20140311公开号：EP2778370A1公开日：20140917
专利附图：
摘要：A gas turbine engine comprises a combustor (16). The combustor (16)comprises an annular combustor chamber formed between an inner liner (20) and anouter liner (30) spaced apart from the inner liner (20). An annular fuel manifold (40) hasfuel nozzles distributed circumferentially on the fuel manifold, the fuel manifold (40) and
fuel nozzles positioned entirely inside the combustion chamber.
申请人：PRATT & WHITNEY CANADA CORP.
地址：1000 Marie Victorin, (01BE5) Longueuil, Quebec J4G 1A1 CA
国籍：CA
代理机构：Leckey, David Herbert
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