Turbine blade manufacturing method
View Patent ↗A method of manufacturing a turbine blade, the method comprising forming a forging by forging stainless steel; heat treating the forging; and cooling the forging after the heat treatment; wherein in the heat treatment and the cooling, a plurality of the forgings are arranged in alignment, and adjacent forgings of the plurality of forgings are disposed so that at least respective portions of portions of the adjacent forgings corresponding to a region from a portion corresponding to a platform of a turbine blade to a center in a longitudinal direction of the turbine blade face each other and warm each other via radiant heat.
1. A method of manufacturing a turbine blade, the method comprising:
forming a forging by forging stainless steel;
heat treating the forging; and
cooling the forging after the heat treatment; wherein:
in the heat treatment and the cooling,
a plurality of the forgings are arranged in alignment, and
adjacent forgings of the plurality of forgings are disposed so that: (i) at least respective portions of portions of the adjacent forgings corresponding to a region from a portion corresponding to a platform of a turbine blade to a center in a longitudinal direction of the turbine blade face each other and warm each other via radiant heat, and (ii) non-uniformity in a cooling rate between a large surface area portion with a large surface area per unit mass and a small surface area portion with a small surface area per unit mass is suppressed.
2. The method of manufacturing a turbine blade according to claim 1 , wherein:
the plurality of forgings are accommodated in an accommodating structure to carry out the heat treatment and the cooling; and
a heat insulation shield is disposed between the forging accommodated opposite to an inner wall of the accommodating structure and the accommodating structure.
3. The method of manufacturing a turbine blade according to claim 1 , wherein:
the heat insulation shield is a plate member; and
a thickness of the heat insulation shield is identical to a cross-sectional maximum thickness in the portion of the forging corresponding to the region from the portion corresponding to the platform of the turbine blade to the center in the longitudinal direction of the turbine blade.
4. The method of manufacturing a turbine blade according to claim 3 , wherein
the cross-sectional maximum thickness is a cross-sectional maximum thickness at a starting point of bending of the forging occurring after the heat treatment.
5. The method of manufacturing a turbine blade according to claim 1 , wherein
in the cooling, rectified cooling gas is supplied to the plurality of forgings.
6. The method of manufacturing a turbine blade according to claim 1 , wherein
the stainless steel is precipitation hardening stainless steel.
7. The method of manufacturing a turbine blade according to claim 1 , wherein
the plurality of forgings are arranged in alignment in a row with suction sides of the plurality of forgings opposing pressure sides of the plurality of forgings.
8. The method of manufacturing a turbine blade according to claim 7 , wherein
the plurality of forgings form a plurality of rows.
9. The method of manufacturing a turbine blade according to claim 1 , wherein:
the plurality of forgings include first forgings and second forgings,
the first forgings are arranged in alignment in a row with suction sides of the first forgings opposing pressure sides of the first forgings, and
the second forgings are not arranged in alignment.
10. The method of manufacturing a turbine blade according to claim 1 , wherein
the plurality of forgings are accommodated in a structure for accommodation to be heat treated and cooled, and the plurality of forgings are disposed in a radial manner around a center of the structure.