发明名称 TURBINE FUEL NOZZLE HAVING PREMIXER WITH AUXILIARY VANE
摘要 A fuel nozzle auxiliary vane comprising a vane mountable base comprising a fuel inlet, wherein the vane mountable base is configured to mount to a surface of a main vane disposed in an airflow path of a fuel nozzle. The fuel nozzle auxiliary vane also includes a body extending from the vane mountable base, wherein the body comprises a fuel passage that turns from the fuel inlet to a fuel outlet, and the fuel outlet has a fuel outlet direction generally crosswise to a fuel inlet direction through the fuel inlet.
申请公布号 US2010293956(A1) 申请公布日期 2010.11.25
申请号 US20090470293 申请日期 2009.05.21
申请人 GENERAL ELECTRIC COMPANY 发明人 NADKARNI VAIBHAV
分类号 F02C7/22 主分类号 F02C7/22
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