# US 2024/0198413 A1 · Nosetip design for high-performance continuous casting

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- Number: US 2024/0198413 A1
- Document ID: US20240198413A1
- Status: Published application
- Kind: A1
- Application number: 18/555,401
- Filed: 2022-06-01
- Published: 2024-06-20
- Earliest claimed: 2021-06-02
- Assignees: Novelis Inc.
- Applicants: Novelis Inc.
- Inventors: Samuel Robert Wagstaff; Simon William Barker
- Web page: https://patentgrep.com/patent/US20240198413A1

## CPC

- B22D 11/064: {for supplying molten metal (supplying molten metal to open-ended moulds B22D11/10)}
- B22D 11/0605: {formed by two belts, e.g. Hazelett-process}
- B22D 11/0622: {formed by two casting wheels}
- B22D 11/0642: {Nozzles (nozzles used in open-ended moulds B22D41/50)}
- B22D 11/115: by using magnetic fields
- B22D: CASTING OF METALS; CASTING OF OTHER SUBSTANCES BY THE SAME PROCESSES OR DEVICES (shaping of plastics or substances in a plastic state B29C; metallurgical processing, selection of substances to be added to metal C21, C22)

## Abstract

Described are nosetips for continuous casting of a metal alloy. The nosetip may include a first portion having a first surface parallel to a second surface opposite the first surface. The nosetip may include a second portion having a third surface directed toward an extended first surface. The extended first surface may be in a common plane with the first surface. The nosetip may include a third portion having an arcuate surface connecting the third surface to the extended first surface. The arcuate surface may include a point of curvature at a vertical distance from the extended first surface. The vertical distance may be configured to limit a maximum meniscus height for liquid metal, cast using the nosetip, between the nosetip and a continuous casting surface. Also described are methods of continuous casting a metal alloy at a casting speed of greater than 12 m/min.

## Claims

### Claim 1

A nosetip for continuous casting of a metal alloy, the nosetip comprising:
a first portion having a first surface parallel to a second surface, the second surface opposite the first surface;
a second portion having a third surface directed toward an extended first surface, the extended first surface in a common plane with the first surface; and
a third portion having an arcuate surface connecting the third surface to the extended first surface.

### Claim 2 (depends on 1)

The nosetip of claim 1, wherein the arcuate surface includes a point of curvature.

### Claim 3 (depends on 2)

The nosetip of claim 2, wherein the point of curvature is a vertical distance from the extended first surface, the vertical distance configured to limit a maximum meniscus height for liquid metal, cast using the nosetip, between the nosetip and a continuous casting surface.

### Claim 4 (depends on 2)

The nosetip of claim 2, wherein the third portion includes a cutback between the point of curvature and the extended first surface.

### Claim 5 (depends on 1)

The nosetip of claim 1, wherein the third portion includes a turbulence generating mechanism.

### Claim 6 (depends on 5)

The nosetip of claim 5, wherein the turbulence generating mechanism is at least one chosen from a plurality of dimples, a plurality of ribs, a plurality of piers, or a surface roughness greater than a surface roughness of the first surface, the second surface, or the extended first surface.

### Claim 7 (depends on 1)

The nosetip of claim 1, wherein the nosetip comprises a refractory material.

### Claim 8

A method of continuous casting a metal alloy, the method comprising:
providing an arcuate nosetip, the arcuate nosetip including:
a first portion having a first surface parallel to a second surface, the second surface opposite the first surface;
a second portion having a third surface directed toward an extended first surface, the extended first surface in a common plane with the first surface; and
a third portion having an arcuate surface connecting the third surface to the extended first surface; and
flowing liquid metal, through the arcuate nosetip, to a casting cavity to form a cast product.

### Claim 9 (depends on 8)

The method of claim 8, wherein a meniscus length of the liquid metal flowing through the arcuate nosetip is at most equal to a distance from a point of curvature to a casting surface partially defining the casting cavity.

### Claim 10 (depends on 9)

The method of claim 9, wherein the meniscus length is from 0.5 mm to 2.0 mm.

### Claim 11 (depends on 8)

The method of claim 8, wherein the third portion of the arcuate nosetip further comprises a turbulence generating mechanism.

### Claim 12 (depends on 11)

The method of claim 11, wherein the turbulence generating mechanism is at least one chosen from a surface roughness, a plurality of dimples, a plurality of ribs, a plurality of piers, and combinations thereof.

### Claim 13 (depends on 8)

The method of claim 8, further comprising generating turbulence in the liquid metal at the arcuate surface using a magnetic oscillation technique.

### Claim 14 (depends on 8)

The method of claim 8, wherein the nosetip is a refractory material.

### Claim 15 (depends on 8)

The method of claim 8, wherein the cast product has a surface roughness of at most 10 μm.

### Claim 16 (depends on 8)

The method of claim 8, wherein the cast product has a composition near the surface having a decrease in Fe and Mn at the cast surface as compared with a reference conventionally cast standard.

### Claim 17 (depends on 16)

The method of claim 16, wherein the composition is characterized by Glow Discharge Optical Emission Spectroscopy.

### Claim 18 (depends on 8)

The method of claim 8, wherein the cast product has an exudate frequency of at most 30 exudates/cm2.

### Claim 19 (depends on 18)

The method of claim 18, wherein the exudate frequency is determined by 3D image analysis.

### Claim 20 (depends on 8)

The method of claim 8, wherein the method provides a casting speed of greater than 12 m/min.
