Method of fabricating a steam turbine blade equipped with erosion shield
A technology for steam turbines, manufacturing methods, applied in the direction of supporting elements of blades, turbines, manufacturing tools, etc., capable of solving problems such as manufacturing cost defects
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Embodiment 1
[0024] figure 1 (a) to (d) show the manufacturing process of the steam turbine rotor blade according to the first embodiment of the present invention. Shows the leading edge portion of the tip portion of the steam turbine rotor blade. As a raw material for steam turbine moving blades, such as figure 1 As shown in (a), it is composed of a blade portion 1 of a steam turbine rotor blade, an erosion protection sheet 2 , and a spacer 3 arranged between the blade portion 1 and the erosion protection sheet 2 . As the turbine rotor blades, Ti alloys (for example, Ti alloys including A16% and V4%), 12Cr stainless steel, and the like are used. As an anti-corrosion sheet, when the turbine rotor blade is a Ti alloy, use a corrosion-resistant Ti alloy (for example, a Ti alloy including Mo15%, Zr5%, and Al13%), and when the turbine rotor blade is 12Cr stainless steel, use Co-based alloys. As the spacer, a Ti spacer or a Ni-based alloy having hardness lower than that of the turbine rotor...
Embodiment 2
[0032] use figure 2 (a) to (d) illustrate the second embodiment of the present invention. The description of the same parts as those in the first embodiment is omitted.
[0033] In this embodiment, a part of the raw material of the blade portion 1 is used as the burn-through prevention mechanism provided on the electron beam exit side, that is, on the back surface of the slot. In the present embodiment, the joint portion of the material of the blade portion 1 and the corrosion protection sheet 2 is formed in an L-shape. The spacer 3 and the corrosion protection sheet 2 are attached to the L-shaped protruding part (base) of the blade part 1 . The L-shaped protrusion functions as a burn-through prevention mechanism. In addition, as in the first embodiment, after electron beam welding, machining is performed so that the L-shaped protruding portion of the blade portion 1 is also removed to obtain the target rotor blade shape.
[0034] Even in this embodiment, the same effect ...
Embodiment 3
[0036] use image 3 (a) to (d) illustrate the third embodiment of the present invention. The description of the same parts as those in the first embodiment is omitted.
[0037] In this embodiment, a part of the raw material of the erosion resist sheet 2 is used as the burn-through prevention mechanism provided on the electron beam exit side, that is, on the back surface of the slot. In this embodiment, the material of the corrosion protection sheet 2 is formed in an L-shape at the junction with the blade portion 1 . A spacer 3 and an erosion protection sheet 2 having an L-shaped protrusion (base) are attached to the blade portion 1 . The L-shaped protrusion functions as a burn-through prevention mechanism. In addition, as in the first embodiment, after electron beam welding, machining is performed so that the L-shaped protruding portion of the erosion resist sheet 2 is also removed to obtain the target rotor blade shape.
[0038] Even in this embodiment, basically the same...
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