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Engineered metals
for precision industries

Data sheet - RODUR

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RODUR
X2 NiCoMo18-9-5+Ti

Fe reste Ni17-19 Co8-10 Mo4.5-5.5 Ti0.5-0.8 C0-0.03

Chemical composition

Ni17-19

P0.01 max

FeBAL

Mn0.1 max

Si0.1 max

S0.01 max

Co8-10

Al0.05-0.15

C0.03 max

Ti0.5

Mo4.5-5.5

Alloy name
RLSA no.970
EN standard
DIN standard1.6358
UNS no.*K93120

*Unified Numbering System (USA)

Characteristics and main uses

  • Superior formability, elevated mechanical properties by precipitation hardening through heat treatment at moderate temperature (which can be carried out after forming). 
  • Hardening treatment does not cause any dimensional change.
  • No low-temperature embrittlement.
  • Excellent fatigue-resistance.
  • Structural stability after ageing.
  • A low thermoelastic coefficient.
  • Excellent weldability. Post-weld hardening treatment enables significant reduction of differences in properties between welded and non-welded zones, thus eliminating weak spots.

 

Main uses

  • Springs for clock motors.
  • Springs for rough watch movements.
  • Form springs for analogue quartz watches.
  • Springs for miscellaneous applications.
  • Weighing machines.
  • Precision ball bearings.
  • Ball bearing cages.
  • Electrical and electronic apparatuses.
  • Plastics industry.
  • Defense industry.
  • Missile and rocket fins.
  • Satellites.
  • Automatic gearbox belt.
  • Printer type-carrying band.

Physical properties Units
Density (20°C) 8,10 Kg/dm³
Melting point 1430-1460 °C
Longitudinal elasticity modulus 185-195 GPa
Thermal conductivity W/m·K
Electrical conductivity m/Ω·mm²
Electrical resistivity 0,44 µΩ·m
Linear expansion Coefficient 9,5 10⁻⁶·K⁻¹
IACS (International Annealed Copper Standard) %
Poisson's ratio 0,3
Capabilities
Corrosion resistance2
Hot deformation
Cold deformation4
Electrodepositing
Diamond cutting
Nitriding3
Mechanical polishing3
Welding without filler
Brazing3

1 poor | 2 average | 3 good | 4 very good | - no info

Heat Treatment / Hardening
Annealing temperature 830 °C
Temperature for stress relief treatment °C
Hardening temperature 420-480 °C
Hardening treatment time 3 h hour(s)

Comments on heat treatments

Aging hardening of martensite

Heat treatment condition

  • The standard final aging treatment is 3 hours at 480 ° C. This heat treatment creates the precipitation of intermetallic component. This treatment can be combined with cold rolling hardening.
  • Although the air treatment does not alter the properties of the material, it does alter its appearance, with the metal taking on a blue tint. For this reason, we recommend treating under a high vacuum of the order of 10-5 Torr or under an inert atmosphere such as argon.
  • Certain atmospheres considered inert due to the absence of coloring are in fact chemically active and can thus make the material extremely brittle. This is especially true in the case of hydrogen and cracked ammonia.
  • The influence of the operating temperature. Following tempering, the tensile strengths and elasticity of this alloy decrease more slowly with temperature than those of spring steels or 18-8 stainless steels. This is due to the blocking of the dislocations by the precipitates formed during the quench treatment. The variations in elastic modulus (Young's modulus) as a function of temperature are similar to those of other alloys.

Alloy mechanical properties

RODUR
Possible hardness range 310 - 600 HV
Possible Rm range 1000 - 2100 MPa

Non-exhaustive list of grades

Grade According to standard Hardness
(HV: Vickers)
min - max
Rm
(MPa)
min - max
Rp 0.2
(MPa)
min - max
Elongation
(%) where L0 = 100mm
min - max
L0 Grain size
(µm)
min - max
ROB00 RLSA 310 - 345 1000 - 1200
ROB01 RLSA 310 - 350 1050 - 1250
ROB05 RLSA ≥ 360 ≥ 1200
ROBM01 RLSA 540 - 630 1800 - 2100
ROBM02 RLSA 550 - 640 1900 - 2100
ROBM10 RLSA ≥ 600 ≥ 2100

Do not hesitate to ask us for your specific grades and parameters. We can make productions according to your needs.

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