Patent ID: 9724785
Date: 2017-08-08
CPC Classifications: B23K,B23P,F01D,F05D,G01N,Y10T

Claim:
1. A weldment member foe a gas turbine engine comprising: a gas turbine having a forward welding member having an annular shape with a forward welding face formed at one end of the annular shape, the forward welding face having at least one forward radiographic marking hole formed therein; and an aft welding member having an annular shape with an aft welding face formed at one end of the annular shape, the aft welding face having at least one aft radiographic marking hole formed therein, wherein the forward welding face of the forward welding member is aligned with the aft welding face pf the aft welding member and the at least one forward radiographic marking hole is offset from the at least one aft radiographic marking hole angularly.