Single-step process for selective heat treatment of metals using multiple heating sources
US-2024254611-A1 · Aug 1, 2024 · US
US2016201155A1 · US · A1
| Field | Value |
|---|---|
| Publication number | US-2016201155-A1 |
| Application number | US-201514877532-A |
| Country | US |
| Kind code | A1 |
| Filing date | Oct 7, 2015 |
| Priority date | Aug 27, 2014 |
| Publication date | Jul 14, 2016 |
| Grant date | — |
A practical reading order for non-experts. Skip the full description unless you need deep technical detail.
What the patent document calls the invention.
A short plain-language summary of the technical disclosure.
Who owns or filed the patent and who is credited as inventor.
Filing, priority, publication, and grant dates set the timeline.
The legal scope of protection — read this for what is actually claimed.
Technology tags used to group this patent with similar filings.
Prior art links and similar publications in this corpus.
Official abstract text for this publication.
In a method for manufacturing a component containing an iron alloy material, a pulverulent pre-alloy is provided. The pre-alloy comprises, in wt. %, 0.01 to 1% C, 0.0.01 to 30% Mn, ≦6% Al, and 0.05 to 6.0% Si, the remainder being Fe and usual contaminants. The pulverulent pre-alloy is mixed with at least one of elementary Ag powder, elementary Au powder, elementary Pd powder and elementary Pt powder so as to produce a powder mixture containing 0.1 to 20% of at least one of Ag, Au, Pd and Pt. The powder mixture is applied onto a carrier ( 16 ) by means of a powder application device ( 14 ). Electromagnetic or particle radiation is selectively irradiated onto the powder mixture applied onto the carrier ( 16 ) by means of an irradiation device ( 18 ) so as to generate a component from the powder mixture by an additive layer construction method.
Opening claim text (preview).
1 . A method for manufacturing a component containing an iron alloy material, the method comprising the steps: providing a pulverulent pre-alloy, the pre-alloy comprising in wt. %: 0.01 to 1% C 0.0.01 to 30% Mn ≦6% Al, and 0.05 to 6.0% Si, the remainder being Fe and usual contaminants, mixing the pulverulent pre-alloy with at least one of elementary Ag powder, elementary Au powder, elementary Pd powder and elementary Pt powder so as to produce a powder mixture containing 0.1 to 20% of at least one of Ag, Au, Pd and Pt, applying the powder mixture onto a carrier by means of a powder application device, and selectively irradiating electromagnetic or particle radiation onto the powder mixture applied onto the carrier by means of an irradiation device so as to generate a component from the powder mixture by an additive layer construction method. 2 . The method according to claim 1 , wherein the pulverulent pre-alloy further comprises at least one of Cr at a content of ≦2%, Cu at a content of ≦2%, Ti at a content of ≦2%, Co at a content of ≦2%, Zr at a content of ≦2%, V at a content of ≦2%, Nb at a content of ≦2%, Ta at a content of ≦2% and B at a content of ≦0.2%. 3 . The method according to claim 1 , wherein the pulverulent pre-alloy is mixed with at least one of elementary Ag powder, elementary Au powder, elementary Pd powder and elementary Pt powder so as to produce a powder mixture containing ≦15%, in particular ≦10% and more particular ≦5% of at least one of Ag, Au, Pd and Pt. 4 . The method according to claim 1 , wherein the pulverulent pre-alloy is mixed with at least one of elementary Ag powder, elementary Au powder, elementary Pd powder and elementary Pt powder so as to produce a powder mixture containing ≦0.5%, in particular ≦1% and more particular ≦2% of at least one of Ag, Au, Pd and Pt. 5 . The method according to claim 1 , wherein the operation of the powder application device and the irradiation device is controlled in such a manner that local melt pools are formed in the powder mixture upon being irradiated with electromagnetic or particle radiation, and that the melt in the local melt pools solidifies at a solidification rate of approximately 7×10 6 K/s. 6 . The method according to claim 1 , wherein the generated component is heat-treated in an inert atmosphere for 1 minute to 24 hours at a temperature between 200° C. and 1100° C. 7 . An iron alloy material, comprising in wt. %: 0.01 to 1% C 0.01 to 30% Mn ≦6% Al, 0.05 to 6.0% Si, and 0.1 to 20% Ag, the remainder being Fe and usual contaminants. 8 . The iron alloy material according to claim 7 , further comprising at least one of Cr at a content of ≦2%, Cu at a content of ≦2%, Ti at a content of ≦2%, Co at a content of ≦2%, Zr at a content of ≦2%, V at a content of ≦2%, Nb at a content of ≦2%, Ta at a content of ≦2% and B at a content of ≦0.2%. 9 . The iron alloy material according to claim 7 , wherein the Ag content of the iron alloy material is ≦15%, in particular ≦10% and more particular ≦5%. 10 . The iron alloy material according to claim 7 , wherein the Ag content of the iron alloy material is ≧0.5%, in particular ≧1% and more particular ≧2%. 11 . The iron alloy material according to claim 7 , wherein, in the microstructure of the iron alloy material, Ag is present in the form of Ag particles dispersed in an iron alloy matrix. 12 . The iron alloy material according to claim 7 , wherein, in the microstructure of the iron alloy material, an iron alloy matrix is present which, upon plastic deformation of the iron alloy material, shows twinning induced plasticity and/or transformation induced plasticity. 13 . Component, in particular implant component, containing an iron alloy material according to claim 7 .
Carbon {; Graphite} · CPC title
containing titanium or zirconium · CPC title
Using a mixture of pre-alloyed powders or a master alloy · CPC title
Processes characterised by the sequence of their steps · CPC title
Iron or iron alloys · CPC title
Related publications grouped by family.
Answers are generated from the same data shown on this page.