Method to determine the crater end location of a cast metal product
11883877 · 2024-01-30
Assignee
Inventors
- Thomas BRULLOT (Rombas, FR)
- Thomas LAVALARD (Metz, FR)
- Jean-Marc HEMMEN (Verny, FR)
- Jean-Noël FOULIGNY (Norroy-Les-pont-à-Mousson, FR)
Cpc classification
B22D11/16
PERFORMING OPERATIONS; TRANSPORTING
B22D11/22
PERFORMING OPERATIONS; TRANSPORTING
B22D11/207
PERFORMING OPERATIONS; TRANSPORTING
International classification
B22D11/16
PERFORMING OPERATIONS; TRANSPORTING
Abstract
A method to determine the crater end location of a cast metal product during its casting, the crater end location being the location at which the cast metal product becomes fully solidified. A continuous casting method and a continuous casting machine are also provided.
Claims
1. A method to determine a crater end location of a cast metal product during casting, the crater end location being the location at which the cast metal product becomes fully solidified, the method comprising the steps of: casting molten metal in a continuous casting machine including a plurality of upper and lower segment frames bearing rolls, the upper and lower segment frames being located respectively above and below the cast metal product; estimating a location P.sub.est within the continuous casting machine where the metal product becomes fully solidified; at least measuring a bending of the nearest upper segment frame of the estimated location P.sub.es, wherein the bending is measured at least on two ends of the nearest upper segment frame; and calculating a location P.sub.mes of the crater end based on the measured bending.
2. The method as recited in claim 1 wherein the estimating of the location P.sub.est is performed with a model.
3. A method of casting a metal product at a casting speed S, the method comprising monitoring the casting speed S according to the crater end location as determined by the method as recited in claim 1.
4. The method of casting as recited in claim 3 wherein the casting speed S is monitored so as to minimize a distance between the crater end location and an output end of the continuous casting machine.
5. The method of casting as recited in claim 3 further comprising applying a dynamic soft reduction to the metal product and the casting speed is monitored so that the dynamic soft reduction is applied to the metal product before the crater end position is reached.
6. The method as recited in claim 1, wherein the bending is measured at a plurality of locations, and wherein the location P.sub.mes calculated as between two locations of the plurality of locations having a biggest bending variation in respective signals.
7. The method recited in claim 1, wherein the bending is measured at locations on the nearest segment frame which are between vertical support beams.
Description
BRIEF DESCRIPTION OF THE DRAWINGS
(1) Other characteristics and advantages of the invention will appear at the reading of the following description.
(2) In order to illustrate the invention, trials have been performed and will be described by way of non-limitative examples, notably in reference to figures which represent:
(3)
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DETAILED DESCRIPTION
(7)
(8) Once the bending is measured it is possible to calculate the location P.sub.mes of the crater end based on said bending. When only one bending measurement is performed the measured signal can be compared with a predefined value of bending in a mushy state, if the measured bending is below said value it means that the load applied to the segment frame is lower than expected in a mushy state and so that the metal product is already solidified. The crater end is thus located before the bending measurement means location. If the measured bending is above or equal to the predefined value it means the crater end is located after said measurement mean. Depending on the difference between the bending measured value and the predefined value it is possible to calculate the distance between the position of the sensor and the crater end location.
(9) When several bending measurement means are used it is possible to compare the bending measured by each one, the crater end being located between the two positions of the measurement sensors having the biggest bending variations in their respective signals. This is illustrated in
(10) By multiplying the casting speed variations and calculation of the crater end location with a method and processor 100 (shown schematically in
(11)
(12) Using a method according to the invention it is possible to accurately and robustly detect the crater end location. Indeed, the measurement being performed on the upper segment frame, the measurement means are positioned on said frames and may perform the measurement as long as they work and there is no need to wait for a caster stop and part replacement to replace a defective sensor.