Method for continuously casting slab containing titanium or titanium alloy
US-2017197243-A1 · Jul 13, 2017 · US
US12083589B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-12083589-B2 |
| Application number | US-202118254966-A |
| Country | US |
| Kind code | B2 |
| Filing date | Dec 2, 2021 |
| Priority date | Dec 3, 2020 |
| Publication date | Sep 10, 2024 |
| Grant date | Sep 10, 2024 |
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.
A method for obtaining a product made of titanium alloy or a titanium-aluminum intermetallic compound by plasma torch melting, the alloy having an oriented structure, the method including heating the molten alloy surface in a casting ring with a plasma torch; cooling a cold zone of the casting ring over a length L1, the cooling forming a semi-solid crown of alloy; heating a hot zone of the casting ring over a length L2, thereby forming a solidification front, the flatness of which relative to a plane perpendicular to a drawing direction is less than 10°; and drawing the solidified alloy at a speed of more than 10−4 m/s in the drawing direction. The present disclosure also relates to a plant having one or more devices for implementing the method.
Opening claim text (preview).
The invention claimed is: 1. A method for obtaining a product made of a titanium alloy or a TiAl intermetallic compound by plasma torch melting, the alloy having an oriented structure, the method comprising: heating, with a plasma torch, a molten alloy or compound surface at a casting ring; cooling a cold area at the casting ring below the molten alloy or compound surface, over a length L 1 at a temperature comprised between 0 and 50° C., thereby forming a semi-solid alloy or compound crown; heating, downstream of the cold area, a hot area over a length L 2 at a temperature between T f ×0.8 and T f ×1.25, T f representing the melting temperature of the molten alloy or compound, thereby enabling control of an alloy or compound solidification front at an outlet of the hot area, the alloy or compound solidification front having a flatness with respect to a plane perpendicular to a drawing direction of less than 10°; and drawing the solidified alloy or compound at a drawing speed higher than 10 −4 m/s along the drawing direction. 2. The method of claim 1 , wherein the length L 1 is between 0.065 m and 0.09 m. 3. The method of claim 1 , wherein the length L 2 is between 0.17 m and 0.3 m. 4. The method of claim 1 , wherein a [L 2 /L 1 ] ratio of the length L 2 to the length L 1 is between 4 and 6. 5. The method of claim 1 , further comprising selecting a power of the plasma torch based on the drawing speed governed by a control law represented by: V = P * h * L * Δ T 1 - η * Q * ( 1 - e x p ( - 3 * R 2 σ 2 ) ) ρ * S * ( C p * Δ T 2 + L M ) wherein V is the drawing speed (m/s), S is the section of the drawn ingot (m 2 ), R the radius of the drawn ingot (m), η the efficiency of the plasma torch, Q the power of the plasma torch (W), σ the radius of action of the plasma torch (m), P the perimeter of the casting ring (m), L the total length of the casting ring (m), ρ the volumetric mass of the cast alloy (kg·m −3 ), h the exchange coefficient of the casting ring (W·m −2 ·° C. −1 ), C p the specific heat (J·kg −1 ·° C. −1 ), L M the specific latent heat of fusion of the cast alloy (J·kg −1 ), ΔT 2 the thermal gradient between the inlet and the outlet of the ring (° C.), and ΔT 1 is the thermal gradient between the metal temperature at the hot area and its preheating temperature. 6. The method of claim 1 , further comprising cooling a second cold area over a length L 3 downstream of the hot area. 7. The method of claim 6 , wherein the length L 3 is larger than 0.03 m.
Alloys based on titanium · CPC title
by melting {(C22C1/1036 takes precedence)} · CPC title
Influencing the temperature of the metal, e.g. by heating or cooling the mould · CPC title
with high melting point, e.g. Be 1280 degrees C, Ti 1725 degrees C · CPC title
for vertical casting · CPC title
Related publications grouped by family.
Answers are generated from the same data shown on this page.