Annular gas turbine engine case and method of manufacturing

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

Patent

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Details

F01D 25/24 (2006.01) B21H 7/00 (2006.01) F01D 21/04 (2006.01) F02C 7/00 (2006.01) B21B 17/02 (2006.01)

Patent

CA 2602981

The method is used for making an annular gas turbine engine case, the method comprises flowforming a first area of the preform to provide a first annular case portion having a first thickness and a second area having a second thickness, the first and the second average thickness being different.

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