Rotating inlet cowl for a turbine engine, including an...

F - Mech Eng,Light,Heat,Weapons – 02 – C

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Details

F02C 7/047 (2006.01) B64C 11/14 (2006.01) B64D 15/16 (2006.01) F02K 3/06 (2006.01)

Patent

CA 2756845

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.

La présente invention se rapporte à un capot d'entrée tournant (30) pour tarbomachine, présentant un axe de rotation (34) et dont l'extrémité avant (44) est agencée de manière excentrée par rapport à cet axe de rotation (34). De plus, un cône avant (32) du capot est tronqué par une surface de troncature (70) définissant l'extrémité avant (44) du capot d'entrée.

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