Gas turbine fuel nozzle manufacturing

B - Operations – Transporting – 23 – P

Patent

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Details

B23P 15/00 (2006.01) B23Q 3/00 (2006.01) F23R 3/42 (2006.01)

Patent

CA 2590056

A method and a pre-shaped workpiece (20) for making at least a portion of a gas turbine fuel nozzle (20') are disclosed having opposed gripping tabs (22, 24) which can be secured to machine tool holders (32, 34) during manufacturing by a machine tool (30).

La présente invention concerne un procédé et une pièce de fabrication préformée (20) pour fabriquer au moins une partie d~un injecteur de carburant de turbine à gaz (20 ~) présentant des pattes de serrage opposées (22, 24) qui peuvent être fixées à des supports de machine-outil (32, 34) pendant la fabrication par une machine-outil (30).

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