发明名称 Multimode fuel injector for combustion chambers, in particular of a jet engine
摘要 A fuel injector including a peripheral atomisation system having a plurality of fuel ejection orifices distributed at regular intervals along the circumference and an annular air eddy deflector. The deflector includes air ejection channels such that, for each fuel ejection axis defined by an ejection orifice, there is a corresponding air ejection channel of which at least the radially most internal part has a median substantially intersecting this fuel ejection axis.
申请公布号 US8033114(B2) 申请公布日期 2011.10.11
申请号 US20070620314 申请日期 2007.01.05
申请人 SNECMA 发明人 HERNANDEZ DIDIER HIPPOLYTE;NOEL THOMAS OLIVIER MARIE
分类号 F02C1/00;B05B7/10 主分类号 F02C1/00
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