发明名称 INJECTION ELEMENT FOR THE COMBUSTION CHAMBER OF A ROCKET ENGINE
摘要 <p>The invention relates to the field of injectors, and especially to an injection element (201) comprising at least one first spiral channel (204) and at least one second spiral channel (205), each of said spiral channels (204, 205) following a helix (204a, 205a) centered on a central axis (X) of the injection element (201). The helix (205a) of the at least one second spiral channel (205) is arranged inside the helix (204a) of the at least one first spiral channel (204).</p>
申请公布号 WO2014080126(A1) 申请公布日期 2014.05.30
申请号 WO2013FR52803 申请日期 2013.11.20
申请人 SNECMA 发明人 TALIERCIO, LAETITIA;INDERSIE, DOMINIQUE
分类号 F02K9/52 主分类号 F02K9/52
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