1.4562

Data sheet material 1.4562 / Alloy 31

X1NiCrMoCu32-28-7

Iron-nickel-chromium-molybdenum alloy

Brief description

The material 1.4562 or Alloy 31 is an iron-nickel-chromium-molybdenum alloy with added copper and nitrogen. This material acts as a link between high-alloy austenitic stainless steels and nickel alloys and is characterised by excellent resistance to a wide range of corrosive media. In certain areas of application, this material represents a genuine alternative to nickel alloys.

Standards and nomenclature

EN
DIN X1NiCrMoCu32-28-7
AISI Alloy 31
US N08031
EN
DIN X1NiCrMoCu32-28-7
AISI Alloy 31
US N08031

Chemical composition

Ni (nickel) 30,0 32,0
Cr (chromium) 26,0 28,0
Fe (iron) Rest Rest
C (carbon) - 0,015
Mn (manganese) - 2,0
Si (silicon) - 0,3
Cu (copper) 1,0 1,4
P (phosphorus) - 0,02
S (sulphur) - 0,01
Mo (molybdenum) 6,0 7,0
N (nitrogen) 0,15 0,25

-
-

min.

max.

Ni
(nickel)

30,0

32,0

Cr
(chrome)

26,0

28,0

Fe
(iron)

Rest

Rest

C
(carbon)

-

0,015

Mn
(Manganese)

-

2,0

Si
(Silicon)

-

0,3

-
-

min.

max.

Cu
(copper)

1,0

1,4

P
(phosphorus)

-

0,02

S
(sulphur)

-

0,01

Mo
(Molybdenum)

6,0

7,0

N
(Nitrogen)

0,15

0,25

-
-

-

-

General properties

Corrosion resistance
Mechanical properties good
Weldability good

Corrosion resistance

The material 1.4562 is characterised by excellent corrosion resistance in oxidising and reducing atmospheres and has a high resistance to corrosion and erosion corrosion in phosphorus-containing environments. Furthermore, Alloy 31 has excellent resistance in pure and contaminated sulphuric acid up to temperatures of approx. 80°C. Its PREN value of ≥ 48 ensures resistance to seawater and high resistance to pitting corrosion.

Mechanical properties
at 20°C

Yield point
Rp0,2
N / mm²

≥ 280

Tensile strength
Rm
N / mm²

650

Elongation
A5,65

≥ 40%

Modulus of elasticity
kN / mm²

198

Weldability

The material 1.4562 should be welded in the solution-annealed condition using conventional welding processes. These include TIG, MIG/MAG and plasma welding. The workpiece should be welded in a stress-free, metallically bright and dirt-free condition. Annealing colours should be removed immediately after welding, i.e. while still warm, using a stainless steel brush.

Machinability

Alloy 31 should be annealed during machining. The material tends to work harden more than low-alloy austenites. Therefore, a low cutting speed and a low feed rate should be selected. The tool should be in constant engagement. A sufficient cutting depth should be selected so that the previously created work-hardened zone can be undercut. To ensure a stable cutting process, heat dissipation should be optimised by using large quantities of suitable, water-based cooling lubricants.

Cold forming

Cold forming should be carried out in the solution-annealed condition. The material 1.4562 has a significantly higher work hardening rate than most austenitic stainless steels. Intermediate annealing should be carried out for severe cold forming. If the degree of deformation exceeds 15%, a final solution annealing should be carried out.

Thermal treatment

Solution annealing
Hot forming 1200 - 1050°C
Cooling down quickly with water or air
Solution annealing
Hot forming 1200 - 1050°C
Cooling down quickly with water or air

Physical properties

Density
at 20°C
kg/dm³

8,05

Electrical
Resistance with
20°C
(ohm) mm²/m

1,04

Melting range

1330 - 1370°C

Thermal conductivity
at 20°C
W/m K

11,7

Markets & Applications

Mining industry
Chemistry
Oil and Gas
Offshore
Flue gas desulphurisation
Environmental technology

Frequently asked questions

Important note

TEAM EDELSTAHL operates purely as a trading company without technical staff. Consequently, we are not authorised to provide material consulting services.

The above values and information on the properties and/or usability of the material are purely informative. This information is based on the experience of the manufacturer and TEAM EDELSTAHL. All information is without guarantee. Misprints, errors and changes excepted.