Abstract System for repairing worn surfaces of steam turbine components and especially high pressure turbine rotors, are disclosed. These systems include depositing a first layer of weld metal on a worn surface of the component, whereby a heat-affected zone is created. A second layer of weld metal is then deposited over the first layer using a greater amount of heat to temper at least a portion of the heat-affected zone produced by the first layer. The preferred embodiments include the use of gas tungsten arc welding for providing fine-grain size and more creep resistance, especially in the weld and heat-affected zone. The resulting build-up can be machined, for example into a blade fastening to produce a component having properties equal to or better than the base-metal alloy. The invention also provides a longer lasting turbine system, including rotors which have serrated steeples that are more resistant to failure.
In a steam turbine system of the type having a ferrous steam turbine component, said component having a worn surface thereon, the improvement comprising: (a) a first layer of weld metal deposited on said worn surface, said deposition of said first layer producing a heat-affected zone in said component; and (b) a second layer of weld metal deposited to said first layer, said deposition of said second layer tempering at least a portion of said heat-affected zone in said component, wherein said turbine component comprises about 1.05% to 1.35% by weight Cr, about 1.00% to about 1.30% by weight Mo, and about 0.21% to 0.29% by weight V.
Claim 2
Dependent Claim
108 words
In a steam turbine system of the type having a ferrous steam turbine component, said component having a worn surface thereon, the improvement comprising: (a) a first layer of weld metal deposited on said worn surface, said deposition of said first layer producing a heat-affected zone in said component; and (b) a second layer of weld metal deposited to said first layer, said deposition of said second layer tempering at least a portion of said heat-affected zone in said component, wherein said turbine component comprises about 1.05% to 1.35% by weight Cr, about 1.00% to about 1.30% by weight Mo, and about 0.21% to 0.29% by weight V.
Claim 3
Dependent Claim
12 words
The system of claim 1 wherein said turbine component comprises a rotor.
Claim 4
Dependent Claim
23 words
The system of claim 2 wherein said first layer of weld metal comprises a plurality of weld beads disposed transversely across said rotor.
Claim 5
Dependent Claim
23 words
The system of claim 3 wherein said second layer of weld metal comprises a plurality of weld beads disposed transversely across said rotor.
Claim 6
Dependent Claim
25 words
The system of claim 4 further comprising steeples machined from a weld build up comprising at least said first and second layers of weld metal.
Claim 7
Dependent Claim
21 words
The system of claim 1 wherein said steeple has a higher creep resistance than that of the ferrous steam turbine component.