Turbine blade, erosion shield forming method, and turbine blade manufacturing method
A rotor blade includes: a blade main body having a tip as an upstream end in a rotation direction, and a blade surface in contact with the tip and which is an upstream surface in a flow direction of a work fluid; and an erosion shield formed as a cladding portion using laser welding on the tip and the blade surface. A boundary between the blade main body and the erosion shield is shaped to approach a surface opposite the blade surface from an end facing the blade surface towards the tip. The boundary includes a first arc that includes the end facing the blade surface and a second arc closer towards the tip than the first arc. The first arc is convex towards an inside of the blade main body and the second arc is convex towards an outside of the blade main body.
1. An erosion shield forming method for forming an erosion shield on at least part of a tip end and a blade surface of a blade main body, the erosion shield forming method comprising:
removing at least part of a tip end and an end surface of a base body which is formed as a turbine blade to form a boundary;
forming a cladding portion at the boundary by laser welding, the cladding portion being one layer gradually formed by cladding in one direction from a blade surface side to a side opposite the blade surface such that the cladding portion is formed firstly at the blade surface side and formed lastly at the side opposite the blade surface, and an entirety of the cladding portion from the blade surface side to the side opposite the blade surface is formed with one layer; and
performing finish processing to remove an excess thickness portion of the base body and part of the cladding portion,
wherein:
the boundary has a shape that approaches a surface opposite the blade surface from an end portion on the blade surface towards the tip end, and includes a first arc which includes the end portion on the blade surface, a second arc which is closer towards a tip end side than the first arc, and a third arc which is closer towards the tip end side than the second arc;
the first arc is convex towards an inside of the blade main body;
the second arc is convex towards an outside of the blade main body; and
the third arc is convex towards the outside of the blade main body.
2. The erosion shield forming method according to claim 1 , wherein, in the base body, the excess thickness portion on the blade surface has a thickness of 0.5 mm or more.
3. The erosion shield forming method according to claim 1 , wherein, in the base body, a thickness of the excess thickness portion on the surface opposite the blade surface is equal to or thicker than a thickness of the excess thickness portion on the blade surface.
4. The erosion shield forming method according to claim 1 , wherein the first arc and the second arc are smoothly connected in the boundary.
5. The erosion shield forming method according to claim 1 , wherein the second arc has a curvature radius which is larger than a curvature radius of the first arc.
6. The erosion shield forming method according to claim 1 , wherein a thickness of the erosion shield at the tip end is thicker than a thickness of the erosion shield between the first arc and the second arc.
7. A turbine blade manufacturing method, comprising:
manufacturing a base body by molding the base body with an excess thickness portion on a turbine blade; and
forming an erosion shield on at least part of a tip end and a blade surface of a blade main body by:
removing at least part of a tip end and an end surface of the base body which is formed as the turbine blade to form a boundary;
forming a cladding portion at the boundary by laser welding, the cladding portion being one layer gradually formed by cladding in one direction from a blade surface side to a side opposite the blade surface such that the cladding portion is formed firstly at the blade surface side and formed lastly at the side opposite the blade surface, and an entirety of the cladding portion from the blade surface side to the side opposite the blade surface is formed with one layer; and
performing finish processing to remove the excess thickness portion of the base body and part of the cladding portion,
wherein:
the boundary has a shape that approaches a surface opposite the blade surface from an end portion on the blade surface towards the tip end, and includes a first arc which includes the end portion on the blade surface, a second arc which is closer towards a tip end side than the first arc, and a third arc which is closer towards the tip end side than the second arc;
the first arc is convex towards an inside of the blade main body;
the second arc is convex towards an outside of the blade main body; and
the third arc is convex towards the outside of the blade main body.