Bladed disk repair process with shield
In some examples, systems and techniques for repairing or otherwise forming a blade of a bladed disk. In one example, a method including positioning a shield member around a perimeter of a partial blade extending from a rotor disk of a bladed disk, the shield member being positioned adjacent to a build surface of the partial blade; and depositing, with the shield member around the perimeter of the partial blade, a material on the build surface using an additive manufacturing technique to form a repaired portion on the build surface of the partial blade.
1. A method comprising:
positioning a shield member including an aperture, the aperture surrounding an entire outer a perimeter of a partial blade extending from a rotor disk of a bladed disk, the shield member being positioned adjacent to a build surface of the partial blade, wherein the partial blade extends through the aperture of the shield member in a radial direction from a rotor of the bladed disk; and
depositing, with the shield member around the entire outer perimeter of the partial blade, a material on the build surface using an additive manufacturing technique to form a repaired portion on the build surface of the partial blade.
2. The method of claim 1 , wherein the shield member defines at least one cooling passageway, the method further comprising:
cooling the shield member by passing a fluid through the cooling passageway while depositing the material on the build surface of the blade.
3. The method of claim 2 , wherein cooling the shield member comprising controlling the flow of the fluid through the cooling passageway to control a temperature of the partial blade during the deposition of the material on the build surface.
4. The method of claim 2 , wherein the fluid comprises a compressed gas.
5. The method of claim 1 , wherein a portion of the aperture is chamfered such that a gap exists between a top surface of the shield member and the partial blade when the partial blade extends through the aperture in the shield member.
6. The method of claim 1 , wherein the shield member is formed of composition including at least one of aluminum, copper, titanium alloy, nickel alloy, or a ceramic.
7. The method of claim 1 , wherein the shield member includes a plurality of discrete sections each formed of a different composition.
8. The method of claim 7 , wherein the plurality of discrete sections includes a first section that defines the aperture, the first section being formed of a composition including a ceramic.
9. The method of claim 7 , wherein the plurality of discrete sections includes a first section that defines a top surface of the shield member, the first section being formed of a composition including at least one of copper or aluminum.
10. The method of claim 1 , wherein the shield member includes a first portion and a second portion, wherein positioning the shield member around the entire outer perimeter of a partial blade includes assembling the first portion and the second portion of the shield member around the perimeter of the partial blade.
11. The method of claim 1 , further comprising adjusting a position of the shield member relative to the partial blade periodically during the formation of the repaired portion.
12. The method of claim 1 , wherein the additive manufacturing technique comprises a directed energy deposition technique.
13. The method of claim 1 , wherein depositing, with the shield member around the perimeter of the partial blade, the material on the build surface comprises:
forming a melt pool on the build surface; and
delivering the material to the melt pool to form a respective layer of material on the build surface when the melt pool cools.
14. The method of claim 1 , wherein the shield member includes a shield substrate defining an opening, and an insert that fits within the opening of the shield substrate, wherein positioning the shield member around the entire outer perimeter of the partial blade includes:
positioning the partial blade within an aperture in the insert; and
positioning the opening of the shield substrate around the insert with the partial blade within the aperture of the insert.
15. The method of claim 1 , wherein the shield member includes a shield substrate and a vertical wall around a perimeter of the shield substrate.
16. The method of claim 15 , wherein the shield member includes at least one cooling structure including cooling fins located on the vertical wall of the substrate.
17. The method of claim 14 , wherein the shield substrate is formed from a first material and the insert is formed of a second material that is different from the first material.
18. A method comprising:
positioning a shield member that includes an aperture around a perimeter of a partial blade extending from a rotor disk of a bladed disk, the shield member being positioned adjacent to a build surface of the partial blade; and
depositing, with the shield member around the perimeter of the partial blade, a material on the build surface using an additive manufacturing technique to form a repaired portion on the build surface of the partial blade, wherein a portion of the aperture is chamfered such that a gap exists between a top surface of the shield member and the partial blade when the partial blade extends through the aperture in the shield member.
19. A method comprising:
positioning a shield member around a perimeter of a partial blade extending from a rotor disk of a bladed disk, the shield member being positioned adjacent to a build surface of the partial blade; and
depositing, with the shield member around the perimeter of the partial blade, a material on the build surface using an additive manufacturing technique to form a repaired portion on the build surface of the partial blade, wherein the shield member includes a shield substrate and a vertical wall around a perimeter of the shield substrate, and wherein the shield member includes at least one cooling structure including cooling fins located on the vertical wall of the substrate.