Blade for an axial compressor and manufacturing method thereof

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

Patent

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Details

F01D 5/16 (2006.01) F01D 5/14 (2006.01) F01D 9/02 (2006.01)

Patent

CA 2698465

The invention provides blades, and the modification thereof, for stages 18-22 of an axial compressor wherein the blades have reduced susceptibility to tip cracking. The blades and blades manufactured by the provided method have a thickened profile that results in reduced stress in response to multi frequency impulses and preferably increased frequency response of the chord wise bending mode.

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