发明名称 ROTATING INLET COWL FOR A TURBINE ENGINE, INCLUDING AN ECCENTRIC FRONT END
摘要 <p>The present invention relates to a rotating inlet cowl (30) for a turbine engine, having a rotational axis (34) and the front end of which is eccentric to said rotational axis (34). Further, a front cone (32) of the cowl is truncated by a truncating surface (70) that defines the front end (44) of the inlet cowl.</p>
申请公布号 WO2010112453(A1) 申请公布日期 2010.10.07
申请号 WO2010EP54080 申请日期 2010.03.29
申请人 SNECMA;DELAPIERRE, MICKAEL;GIGNOUX, HERVE;LORO, GAEL;WINTENBERGER, SYLVIE 发明人 DELAPIERRE, MICKAEL;GIGNOUX, HERVE;LORO, GAEL;WINTENBERGER, SYLVIE
分类号 F02C7/047;B64C11/14;B64D15/16;F02K3/06 主分类号 F02C7/047
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