Internal fuel manifold with turned channel having a variable...

B - Operations – Transporting – 23 – B

Patent

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B23B 5/36 (2006.01) B23P 15/00 (2006.01) F02C 7/22 (2006.01)

Patent

CA 2643325

A method of manufacturing an internal manifold of a gas turbine engine (10) including machining an annular channel (36) in a ring (22) by a turning process, and varying a position of a tool bit (80) relative to the surface (38) of the ring as a function of a relative circumferential location of the tool bit (80) around the ring (22) such that the channel (36) has a cross-sectional area that varies around a circumference of the ring.

L'invention concerne un procédé de fabrication d'un collecteur interne d'une turbine à gaz (10) comprenant l'étape consistant à usiner un profilé annulaire (36) dans un anneau (22) par un processus de tournage, et l'étape consistant à varier une position d'un outil rapporté (80) par rapport à la surface (38) de l'anneau en fonction d'un emplacement circonférentiel relatif de l'outil rapporté (80) autour de l'anneau (22) de telle manière que le profilé (36) a une surface de coupe transversale qui varie sur une circonférence de l'anneau.

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