发明名称 SWIRLER PASSAGE AND BURNER FOR A GAS TURBINE ENGINE
摘要 A swirler passage is provided for mixing fuel and compressor air with at least two side walls; at least first and second conduits arranged inside at least one of the at least two side walls, the first conduit forming a fuel gas conduit and the second conduit forming an air conduit, the fuel gas conduit connected to a gas fuel supply and the air conduit connected to an air supply; a tube connected to the fuel gas conduit and entirely traversing the air conduit inside the side wall; a fluid passage connected to the air conduit and surrounding the tube; at least one fuel outlet opening of the tube arranged on the side wall; and at least one air outlet opening of the fluid passage arranged on the side wall and surrounding the fuel outlet opening.
申请公布号 US2009277179(A1) 申请公布日期 2009.11.12
申请号 US20070310143 申请日期 2007.08.10
申请人 WILBRAHAM NIGEL 发明人 WILBRAHAM NIGEL
分类号 F02C7/22 主分类号 F02C7/22
代理机构 代理人
主权项
地址
您可能感兴趣的专利