Aluminum-iron alloy-coated steel sheet for hot press forming, having excellent hydrogen delayed fracture resistance, peeling resistance, and weldability and hot-formed member using same
US-2019003029-A1 · Jan 3, 2019 · US
US11261514B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-11261514-B2 |
| Application number | US-201716326780-A |
| Country | US |
| Kind code | B2 |
| Filing date | Sep 22, 2017 |
| Priority date | Sep 30, 2016 |
| Publication date | Mar 1, 2022 |
| Grant date | Mar 1, 2022 |
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A method for producing a component made of a steel product coated with an Al—Si protective coating, includes: providing a substrate consisting of a steel produced coated with an Al—Si protective coating, heating the substrate to a temperature T 1 such that the Al—Si protective coating is only partially pre-alloyed with Fe of the steel product, cooling the pre-alloyed substrate to room temperature, applying a corrosion protection oil to the surface of the pre-alloyed substrate, wherein the oil consists of a composition containing fatty acid ester, transporting the pre-alloyed substrate to which the oil has been applied, heating the pre-alloyed substrate to which the oil has been applied to a temperature T 2 such that the Al—Si protective coating is fully alloyed with Fe of the steel product and the oil is removed without leaving residue, and shaping the re-heated substrate to form the component.
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The invention claimed is: 1. Method for producing a component made of a steel product coated with an Al—Si protective coating, comprising: providing a substrate consisting of a steel product coated with an Al—Si protective coating, heating the substrate to a temperature T 1 such that the Al—Si protective coating is only partially pre-alloyed with Fe of the steel product, cooling the pre-alloyed substrate to room temperature, applying a corrosion protection oil to the surface of the pre-alloyed substrate, wherein the corrosion protection oil contains fatty acid esters, transporting the pre-alloyed substrate to which the corrosion protection oil has been applied, heating the pre-alloyed substrate to which the corrosion protection oil has been applied to a temperature T 2 , wherein the corrosion protection oil is not removed from the substrate by cleaning the pre-alloyed substrate to which the corrosion protection oil has been applied before it is heated to T 2 and the heating is carried out to T 2 such that the Al—Si protective coating is fully alloyed with Fe of the steel product and the corrosion protection oil is removed without leaving residue, and shaping the re-heated substrate to form the component. 2. Method according to claim 1 , wherein the heating to T 2 takes place under a protective atmosphere. 3. Method according to claim 1 , wherein the composition contains at least 98% by weight of the fatty acid esters. 4. Method according to claim 1 , wherein the fatty acid esters is a C8-C16 compound. 5. Method according to claim 1 , wherein the composition has a sulfur content in the range of 0.1-2% by weight. 6. Method according to claim 1 , wherein the composition has a saponification number in the range of 150-265 mg KOH/g. 7. Method according to one of the preceding claim 1 , wherein the corrosion protection oil is applied to the substrate in a quantity of 0.5 to 2 g/m2. 8. Method according to claim 1 , wherein the temperature T 2 corresponds to a temperature range of 850° C. to 1000° C. 9. Method according to claim 1 , wherein the temperature T 1 corresponds to a temperature range of 550° to 780° C. 10. Method according to claim 1 , wherein the heating of the pre-alloyed substrate to which the corrosion protection oil has been applied to the temperature T 2 comprises: heating the substrate to the temperature range T 2 of 850° C. to 1000° C., holding the substrate in the temperature range T 2 , and cooling the substrate to a temperature range T 3 of 550° C. to 750° C. 11. Method according to claim 8 , wherein the temperature T 2 corresponds to a temperature range of 880° C. to 930° C. 12. Method according to 8, wherein the temperature T 1 corresponds to a temperature range of 600° to 700° C. 13. Method according to claim 10 , wherein the temperature T 2 is a temperature range of 880° C. to 930° C. and/or the temperature range T 3 is a temperature range of 600° C. to 700° C. 14. Method according to claim 10 , wherein the heating to T 2 is 60 to 210 s. 15. Method according to claim 10 , wherein the holding in the temperature range T 2 is 30 to 600 s. 16. Method according to claim 10 , wherein the cooling after the pre-alloying takes place occurs with a cooling rate in the range of 2 to 25 K/s. 17. Method according to claim 14 , wherein the heating to T 2 is 90 to 180 s. 18. Method according to claim 15 , wherein the holding in the temperature range T 2 is 30 to 120 s. 19. Method according to claim 16 , wherein the cooling after the pre-alloying takes place occurs with a cooling rate in the range of 8 to 20 K/s.
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