Repair of dual walled metallic components using directed energy deposition material addition
A technique for repairing a dual walled component comprising a spar comprising a plurality of pedestals and a coversheet attached to the plurality of pedestals may include removing a damaged portion of the coversheet from the dual walled component to expose a plurality of exposed pedestals and define a repair location and an adjacent coversheet portion. The technique also may include attaching a material to the plurality of exposed pedestals and adjacent coversheet portion using directed energy deposition material addition to form a repaired coversheet portion.
1. A method for repairing a dual walled component comprising a spar comprising a plurality of pedestals and a coversheet attached to the plurality of pedestals, the method comprising:
removing a damaged portion of the coversheet from the dual walled component to expose a plurality of exposed pedestals and define a repair location and an adjacent coversheet portion, wherein the plurality of pedestals comprises the plurality of exposed pedestals, and wherein the coversheet is attached to the plurality of pedestals;
positioning a preformed replacement coversheet portion at the repair location;
directing energy at each of a plurality of locations at which the preformed replacement coversheet portion is adjacent to the plurality of exposed pedestals to join the preformed replacement coversheet portion to the plurality of exposed pedestals; and
providing a powder to a side of the preformed replacement coversheet portion opposite of the plurality of exposed pedestals, wherein the energy joins at least some of the powder to the preformed replacement coversheet portion at at least one location adjacent to an exposed pedestal of the plurality of exposed pedestals.
2. The method of claim 1 , wherein the powder substantially fills a depression in the preformed replacement coversheet portion made from joining the preformed replacement coversheet portion to the exposed pedestal.
3. The method of claim 1 , further comprising:
filling a space between the plurality of exposed pedestals with a stop material, wherein the stop material defines a surface substantially aligned with a pedestal-contacting surface of the adjacent coversheet portion;
directing the powder to the surface of the stop material;
directing energy to the powder at locations adjacent to the stop material, the plurality of exposed pedestals, and the adjacent coversheet portion to form the repaired coversheet portion by directed energy deposition material addition.
4. The method of claim 1 , wherein the repaired coversheet portion comprises a first alloy, wherein the adjacent coversheet portion comprises a second alloy substantially similar to the first alloy.
5. The method of claim 1 , wherein the repaired coversheet portion comprises a first alloy, wherein the adjacent coversheet portion comprises a second, different alloy.
6. The method of claim 1 , wherein removing the damaged portion of the coversheet comprises removing at least a damaged portion of at least one pedestal of the plurality of pedestals, wherein the coversheet is attached to the at least one pedestal prior to removing the damaged portion of the coversheet.
7. The method of claim 1 , wherein removing the damaged portion of the coversheet comprises removing an undamaged portion of the coversheet, wherein the undamaged portion of the coversheet is adjacent to the damaged portion of the coversheet.
8. The method of claim 1 , further comprising:
forming at least one film cooling hole in the repaired portion of the coversheet.
9. The method of claim 1 , further comprising:
forming a thermal barrier coating on at least the repaired portion of the coversheet.