B - Operations – Transporting – 23 – P
Patent
B - Operations, Transporting
23
P
B23P 6/00 (2006.01) B23P 15/00 (2006.01) F01D 9/04 (2006.01) F01D 25/24 (2006.01)
Patent
CA 2453026
A method facilitates replacing a portion of a gas turbine engine turbine support (100). The turbine support includes a body (102) including a forward leg (114), an aft leg (120), and a mounting flange (108) that each extend radially outwardly from the body. The forward leg is axially upstream from the aft leg and the mounting flange. The mounting flange is substantially axially aligned with respect to the aft leg. The method comprises cutting through at least one of the body, the aft leg, and the mounting flange, removing the forward leg and at least a portion of the body that is upstream from the cut (140) from the engine, and coupling a replacement spad to the portion of the turbine support that is downstream from the cut.
Gupta Bhupendra K.
Steplewski Marek
Company General Electric
Craig Wilson And Company
LandOfFree
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