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>