发明名称 Coaxial Fuel and Air Premixer for a Gas Turbine Combustor
摘要 <p>An air/fuel premixer (10) comprising a peripheral wall (12) defining a mixing chamber (14), a nozzle (20) disposed at least partially within the peripheral wall (12) comprising an outer annular wall (22) spaced from the peripheral wall (12) so as to define an outer air passage (23) between the peripheral wall (12) and the outer annular wall (22), an inner annular wall (24) disposed at least partially within and spaced from the outer annular wall (22), so as to define an inner air passage (25), and at least one fuel gas annulus (26) between the outer annular wall (22) and the inner annular wall (24), the at least one fuel gas annulus (26) defining at least one fuel gas passage (27), at least one air inlet for introducing air through the inner air passage (25) and the outer air passage (23) to the mixing chamber (14), and at least one fuel inlet for injecting fuel through the fuel gas passage (27) to the mixing chamber (14) to form an air/fuel mixture. </p>
申请公布号 EP2221541(A3) 申请公布日期 2014.07.09
申请号 EP20090178144 申请日期 2009.12.07
申请人 GENERAL ELECTRIC COMPANY 发明人 YORK, WILLIAM DAVID;ZIMINSKY, WILLY STEVE;LACY, BENJAMIN PAUL
分类号 F23R3/28;F23D14/64 主分类号 F23R3/28
代理机构 代理人
主权项
地址