Turbo engine inlet bullet fairing

Details Turbo engine inlet bullet fairing Turbo engine inlet bullet fairing

F - Mech Eng,Light,Heat,Weapons

02

C

F02C 7/042 (2006.01) F02C 7/05 (2006.01)

Patent

CA 2513783

Cône d'entrée d'une turbomachine, telle en particulier qu'un turboréacteur, ce cône étant monté en bout d'un arbre (10) portant des aubes de soufflante (18) et associé à des moyens commandés (42) de déplacement axial permettant de modifier sa position axiale par rapport aux aubes de soufflante (18).

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