Process for local repair of a damaged thermomechanical part and part thus produced, in particular a turbine part
US-9221101-B2 · Dec 29, 2015 · US
US11167348B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-11167348-B2 |
| Application number | US-201816019403-A |
| Country | US |
| Kind code | B2 |
| Filing date | Jun 26, 2018 |
| Priority date | Jun 28, 2017 |
| Publication date | Nov 9, 2021 |
| Grant date | Nov 9, 2021 |
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A system may include a current source; a first metal or alloy component with a first major surface electrically coupled to the current source; a second metal or alloy component with a second major surface electrically coupled in series to the first component and the current source via an external electrical conductor, where the first and second major surfaces are positioned adjacent to each other to define a joint region; a metal or alloy powder disposed in at least a portion of the joint region; and a controller. The controller may be configured to cause the current source to output an alternating current that conducts through the first component and the second component to induce magnetic eddy currents, magnetic hysteresis, or both within at least a portion of the metal or alloy powder disposed in at least the first portion of the joint region.
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What is claimed is: 1. A system comprising: a current source; a first component comprising a first metal or alloy and a first major surface, wherein the first component is electrically coupled to the current source; a second component comprising a second metal or alloy and a second major surface, wherein: the first major surface and the second major surface are positioned adjacent to each other to define a joint region between adjacent portions of the first major surface and the second major surface, and the second component is electrically coupled in series to the first component and the current source via an external electrical conductor; a metal or alloy powder disposed in at least a portion of the joint region; and a controller configured to cause the current source to output an alternating current that: conducts through the first component adjacent to at least a first portion of the joint region and through the second component adjacent to at least the first portion of the joint region, and induces magnetic eddy currents, magnetic hysteresis, or both within at least a portion of the metal or alloy powder disposed in at least the first portion of the joint region. 2. The system of claim 1 , further comprising a first electrode electrically coupled to the current source and the first component and a second electrode electrically coupled to the current source and the second component, wherein the controller is further configured to control positions of the first and second electrodes relative to the respective first and second components. 3. The system of claim 1 , further comprising at least one electrode electrically coupled to the current source and at least one of the first component or the second component, wherein the at least one electrode is configured to induce within the metal or alloy powder magnetic eddy currents, magnetic hysteresis, or both over a surface area greater than sixteen square millimeters as measured from the first major surface or the second major surface. 4. The system of claim 1 , wherein the frequency of the alternating current is within a range from 1 kHz to 10 GHz. 5. The system of claim 1 , wherein at least one of the first component and the second component comprises a nickel based superalloy or a titanium based alloy. 6. The system of claim 1 , wherein the metal or alloy powder is free of a melting point depressant. 7. A method comprising: positioning a first component comprising a first metal or alloy and a first major surface, wherein the first component is electrically coupled to a current source, adjacent to a second component comprising a second metal or alloy and a second major surface, wherein the second component is electrically coupled in series to the first major component and the current source via an external electrical conductor, to define a joint region between adjacent portions of the first major surface of the first component and the second major surface of the second component; introducing a metal or alloy powder to at least a portion of the joint region; and controlling, by a controller, the current source to cause the current source to output an alternating current that: conducts through the first component adjacent to at least a first portion of the joint region and through the second component adjacent to at least the first portion of the joint region; and introduces magnetic eddy currents, magnetic hysteresis, or both within at least a portion of the metal or alloy powder in the at least first portion of the joint region. 8. The method of claim 7 , further comprising: controlling, by the controller: a first position of a first electrode electrically coupled to the current source and the first component; and a second position of a second electrode electrically coupled to the current source and the second component. 9. The method of claim 8 , wherein at least one electrode is configured to induce within the metal or alloy powder magnetic eddy currents, magnetic hysteresis, or both over a surface area greater than sixteen square millimeters as measured from the first major surface or the second major surface. 10. The method of claim 7 , wherein the frequency of the alternating current is within a range from 1 kHz to 10 GHz. 11. The method of claim 7 , wherein at least one of the first component and the second component comprises a nickel based superalloy or a titanium based alloy. 12. The method of claim 7 , wherein the metal or alloy powder is free of a melting point depressant.
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