Rotor disk weld inspection method and arrangement therefore

Details Rotor disk weld inspection method and arrangement therefore Rotor disk weld inspection method and arrangement therefore

B - Operations, Transporting

23

K

B23K 31/00 (2006.01) B23K 31/12 (2006.01) F01D 5/02 (2006.01)

Patent

CA 2681277

A method for inspecting a weld (25) joining a first rotor disk (10) made of nickel alloy and having an inner surface (12) and an outer surface (11) concentric with the rotor's longitudinal axis (LA) to a second rotor disk (15) comprising an inner surface (17) and an outer surface (16) concentric with the rotor's longitudinal axis (LA). The weld (25) made of nickel alloy fills a radial gap between the rotor disks (10,15), and has a dissimilar microstructure to either of the rotor disks (10,15), the method including the steps of; forming at least one slot (20) in the first rotor disk (10) extending through either the inner surface (12) or the outer surface (11) of the first rotor disk (10) terminating in the first rotor disk; and passing an inspection signal from the first slot (20), to the weld (25) so as to inspect the weld (25) for defects (27).

Affiliated with

Also associated with

Rating

Rotor disk weld inspection method and arrangement therefore does not yet have a rating. At this time, there are no reviews or comments for this patent.

If you have personal experience with Rotor disk weld inspection method and arrangement therefore, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Rotor disk weld inspection method and arrangement therefore will most certainly appreciate the feedback.

Rate now

Comments { 0 }

Profile ID: LFCA-PAI-O-1435663