Component made of metallic composite material and method for the manufacture of the component by hot forming

Patent metadata

Field	Value
Publication number	US-10974485-B2
Application number	US-201615769917-A
Country	US
Kind code	B2
Filing date	Oct 31, 2016
Priority date	Oct 30, 2015
Publication date	Apr 13, 2021
Grant date	Apr 13, 2021

Abstract

A component made of metallic composite material having high corrosion resistance and scale resistance. The metallic composite material contains as a core material an uncoated hardenable steel on which surface a corrosion resistance and scaling resistance layer is provided using heat resistant stainless steel, and has a yield strength Rp 0,2 of at least 1000 MPa and a tensile strength R m of at least 1500 MPa for the core material and a critical scaling resistance temperature in air for the layer material is at least 850° C.

First claim

The invention claimed is:

1. A component made of a metallic composite material having high corrosion resistance and scale resistance, wherein the metallic composite material comprises as a core material an uncoated hardenable steel on which surface a corrosion resistant and scaling resistant layer is provided using heat resistant stainless steel as a layer material,
wherein the core material comprises in mass %: up to 0.48% C, up to 0.4% N, 10.5-18% Cr, up to 8% Ni, up to 18% Mn, up to 3.0% Mo, up to 1.0% Si, up to 0.65% Cu, up to 0.005 B, and the remainder being Fe and inevitable impurities and has a yield strength Rp 0,2 of at least 1000 MPa and a tensile strength R m of at least 1500 MPa, and
wherein the layer material is austenitic heat resistant stainless steel comprising by mass % 18-25% Cr, 10-19% Ni, Mn≥0.5% and Si≥0.4% or ferritic heat resistant stainless steel comprising by mass % 13-18% Cr, Mn≥0.5%, Si≥1.0% and C≤0.1%.

2. The component according to claim 1 , wherein, a ratio of a total thickness of the layer material to a thickness of the core material is at most 0.4.

3. The component according to claim 1 , wherein, a ratio of a total thickness of the layer material to a thickness of the core material is at most 0.2.

4. The component according to claim 1 , wherein a ratio of a thermal conductivity of the layer material to a thermal conductivity of the core material is at most 2.

5. A method for the manufacture of the component of claim 1 , comprising: welding a core material of uncovered hardenable steel and a layer material of heat resistant stainless steel together in order to produce a metallic composite material, wherein the layer material covers outer surfaces of the core material,
heat treating the composite material at the austenization temperature for at most 5 minutes,
hot forming the heat treated composite material in a hot forming tool to have a desired shape of the component, and
cooling the hot formed component to the room temperature.

6. The method according to claim 5 , wherein welding is carried out by laser welding.

7. The method according to claim 5 , wherein welding is carried out by keyhole welding.

8. The method according to claim 5 , wherein hot forming is carried out in an atmosphere comprising at least one shielding gas.

9. The method according to claim 8 , wherein nitrogen is used as the shielding gas and a top part of the component has a nitride hardened surface with high wear resistance.

10. The method according to claim 5 , wherein the layer material for the composite material of the component is made of austenitic heat resistant stainless steel comprising by mass % 18-25% Cr, 10-19% Ni, Mn≥0.5% and Si≥0.4%.

11. The method according to claim 5 , wherein the layer material for the composite material of the component is made of ferritic heat resistant stainless steel comprising by mass % 13-18% Cr, Mn≥0.5%, Si≥1.0% and C≤0.1%.

12. The method according to claim 5 , wherein a heating rate during the hot forming process of the composite material is at least 50K/s.

13. The method according to claim 5 , wherein the composite material is removed from the hot forming tool during the cooling process when a martensitic start temperature (M s ) of the layer material is reached.

14. The method according to claim 5 , wherein a connection of the layer material to the core material is achieved by preconditioning the layer material by electrobrightening with an electrolytic solution comprising a 96% sulfuric acid and 85% orthophosphoric acid.

Assignees

• Outokumpu Oy

Inventors

• Brückner Gabriele
• Fröhlich Thomas
• Nentwig Thomas
• Skrlec Jasminko
• Lindner Stefan

Classifications

• C21D8/02

  during manufacturing of plates or strips (C21D8/12 takes precedence) · CPC title

• B32B2307/306

  Resistant to heat · CPC title

• C21D2251/02

  Clad material · CPC title

• C22C38/40

  with nickel · CPC title

• C22C38/58

  with more than 1.5% by weight of manganese · CPC title