发明名称 Gas turbine combustor
摘要 <p>A combustor according to the present invention includes a combustion chamber (5) to which fuel and air are supplied; air holes (32) adapted to supply air to the combustion chamber (5); fuel nozzles (25) adapted to supply gaseous fuel to the air holes (32); and orifices (24) adapted to allow the gaseous fuel supplied to the air holes (32) to cause a pressure drop.</p>
申请公布号 EP2481986(A2) 申请公布日期 2012.08.01
申请号 EP20120152843 申请日期 2012.01.27
申请人 HITACHI LTD. 发明人 MIURA, KEISUKE;KOGANEZAWA, TOMOMI;DODO, SATOSHI;SAITO, TAKEO
分类号 F23R3/28 主分类号 F23R3/28
代理机构 代理人
主权项
地址