CAPOT D'ENTREE TOURNANT POUR TURBOMACHINE, COMPRENANT UNE EXTREMITE AVANT EXCENTREE

摘要

A rotating inlet cowl for a turbine engine includes a rotation axis. The rotating inlet cowl includes a forward cone defining a forward end of the inlet cowl. The forward end is configured to be eccentric relative to the rotation axis of the inlet cowl. Furthermore, the forward cone is truncated by a truncation surface defining the forward end of the inlet cowl.