Thrust bearing housing for a gas turbine engine

F - Mech Eng,Light,Heat,Weapons – 01 – D

Patent

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Details

F01D 25/16 (2006.01) F02C 7/06 (2006.01) F16C 35/04 (2006.01)

Patent

CA 2659823

The thrust bearing housing (20) comprises two opposite annular end members (36, 38) and a cone member (34) extending between the two end members (36, 38). The cone member (34) is connected to each end member at a circular junction (42, 44), each circular junction (42, 44) having a medial line which borders a respective end of a virtual conical plane (50). At least a major portion of the cone member (34) is provided inside the virtual conical plane (50).

L'invention porte sur un carter de butée (20) qui comprend deux éléments terminaux annulaires opposés (36, 38) et un élément conique (34) s'étendant entre les deux éléments terminaux (36, 38). L'élément conique (34) est relié à chaque élément terminal en une jonction circulaire (42, 44), chaque jonction circulaire (42, 44) possédant une ligne médiane qui borde une extrémité respective d'un plan conique virtuel (50). Au moins une majeure partie de l'élément conique (34) est située à l'intérieur du plan conique virtuel (50).

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