发明授权
US08984855B2 Rotating inlet cowl for a turbine engine, comprising an eccentric forward end 有权
用于涡轮发动机的旋转入口罩,包括偏心的前端

Rotating inlet cowl for a turbine engine, comprising an eccentric forward end
摘要:
A rotating inlet cowl for a turbine engine, having a rotation axis and for which the forward end is arranged to be eccentric relative to this rotation axis. Furthermore, a forward cone of the cowl is truncated by a truncation surface defining the forward end of the inlet cowl.
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