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 in particular to an injector element (201) having at least one first helical channel (204) and at least one second helical channel (205), each of said helical channels (204, 205) following a respective helix (204a, 205a) centered on a central axis (X) of the injector element (201). The helix (205a) of the at least one second helical channel (205) is situated inside the helix (204a) of the at least one first helical channel (204).</p>
申请公布号 EP2923059(A1) 申请公布日期 2015.09.30
申请号 EP20130803160 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
代理机构 代理人
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