Low-density clad steel sheet having excellent formability and fatigue property and manufacturing method therefor
US-2024326399-A1 · Oct 3, 2024 · US
US10906128B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-10906128-B2 |
| Application number | US-201815989830-A |
| Country | US |
| Kind code | B2 |
| Filing date | May 25, 2018 |
| Priority date | Feb 17, 2016 |
| Publication date | Feb 2, 2021 |
| Grant date | Feb 2, 2021 |
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A method for forming an impact weld used in an additive manufacturing process is provided. The method includes providing a metallic material for impact welding to a substrate. The metallic material is propelled toward the substrate with a sufficient velocity to form an impact weld for welding the metallic material to the substrate. Further, the method includes traversing the substrate in a direction relative to a direction from which the metallic material is propelled and repeating the propelling so that a layer of additive material is deposited on the substrate as desired. In addition, a method for forming an impact welding used in an additive manufacturing process via discharge actuated arrangement is provided.
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What is claimed is: 1. A method for forming an impact weld used in an additive manufacturing process, comprising: providing a metallic material for impact welding to a substrate; propelling the metallic material toward the substrate with a discharge velocity to form an impact weld for welding the metallic material to the substrate; traversing the substrate 34 in a direction relative to a direction from which the metallic material is propelled and repeating the propelling so that a lyaer of additive material is deposited on the substrate 34 as desired, providing a wire having a powder filler metal core located within a sheath; inserting the wire within a conduit 18 having an opening; and providing at least one laser energy pulse through the opening 20 , wherein the laser energy pulse interacts with the sheath 16 to ablate the sheath 16 and pinch off at least one segment of the wire, wherein the ablation generates gas pressure propelling the segment toward a substrate with the discharge velocity to form an impact weld for welding the metal core and sheath to the substrate. 2. The method as claimed in claim 1 , wherein the opening exposes a circumferential portion of the sheath. 3. The method as claimed in claim 1 , wherein a plurality of segments are continuously deposited on the substrate to form a plurality of layers on the substrate. 4. The method as claimed in claim 2 further comprising: providing a wire having a powder filler metal core located within a sheath having a consumable foil; inserting the wire within a conduit having an opening; providing at least one pulse of high electric current to the foil, wherein the current pulse vaporizes the foil to pinch off at least one segment of the wire and wherein vaporization of the foil generates gas pressure that propels the segment toward a substrate with the discharge velocity to form an impact weld for welding the metal core and sheath to the substrate. 5. The method as claimed in claim 4 , wherein the opening exposes a circumferential portion of the sheath. 6. The method as claimed in claim 4 , wherein a plurality of segments are continuously deposited on the substrate to form a plurality of layers on the substrate. 7. A method for forming an impact weld used in an additive manufacturing process via a discharge actuated arrangement, comprising: providing a discharge actuated device having an opening; loading a metallic shot material into a magazine of the discharge actuated device; discharging the metallic shot particle from the device through the opening wherein the discharged metallic particle is propelled toward a substrate with a discharge velocity to form an impact weld for welding the metallic shot particle to the substrate, traversing the substrate in a direction relative to the discharge actuated device and repeating the propelling so that a layer of additive material is deposited on the substrate and/or underlaying layer respectively as desired. 8. The method as claimed in claim 7 , further comprising loading a charge into the magazine, wherein the discharging is created by a chemical reaction of the charge. 9. The method as claimed in claim 7 , wherein the discharging is created by a quick release of a compressed gas. 10. The method as claimed in claim 7 , wherein the discharging includes discharging the metallic particle from the opening 150 at the discharge velocity of 100 to 500 m/sec. 11. The method as claimed in claim 7 , wherein the discharging includes automatically activating a discharge at least times per second, wherein each discharge comprises a single metallic shot 140 . 12. The method as claimed in claim 7 , wherein the metallic shot material is a nickel-based superalloy material. 13. The method as claimed in claim 7 , wherein the metallic shot material includes a diameter in the range of 0.5 to 35 mm. 14. The method as claimed in claim 13 , wherein the metallic shot material includes a diameter in the range of 1 to 4 mm. 15. The method as claimed in claim 7 , further comprising traversing the discharge actuated device in a direction relative to the substrate and repeating the propelling so that a layer of additive material is deposited on the substrate and/or underlying layer respectively as desired. 16. The method as claimed in claim 7 , wherein a successive layer is built on top of the deposited layer of additive material. 17. The method as claimed in claim 15 , wherein a successive layer is built on top of the deposited layer of additive material.
Preliminary treatment · CPC title
by means of high energy impulses, e.g. magnetic energy · CPC title
Direct deposition of metal particles, e.g. direct metal deposition [DMD] or laser engineered net shaping [LENS] · CPC title
Process efficiency · CPC title
Processes of additive manufacturing · CPC title
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