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Engineered metals
for precision industries

Data sheet - POLIDUR

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POLIDUR
X2 NiCoMo18-16.5-5

Fe reste Ni17-19 Co16-17 Mo4.5-5.5

Chemical composition

Ni17-19

FeBAL

Co16-17

Mo4.5-5.5

Alloy name
RLSA no.971
EN standard
DIN standard
UNS no.*

*Unified Numbering System (USA)

Characteristics and main uses

High elastic limit alloy, very resistant, allowing the production of spring parts. A very high quality polished surface can be obtained with this alloy compared to YAG 250RL and RODUR. This is thanks to the absence of titanium in the chemical composition.

  • Superior formability and extremely high mechanical properties after aging, thanks to intensive precipitation with moderate temperature hardening heat treatment. This treatment can be done after shaping because it causes very little dimensional change.
  • No weakening at low temperature.
  • Excellent resistance to fatigue.
  • Structural stability after aging.
  • Low thermoelastic coefficient.
  • Excellent weldability. The post-weld hardening treatment significantly reduces the differences in properties between welded and non-welded areas, thereby eliminating weak spots.
  • No TiN => better properties for polishing

Main uses

PHYTIME® is specially designed for all applications requiring high resistance to fatigue, such as those used in the automotive industry:

  • Belt for automatic gearbox
  • Cable connectors to motors
  • Springs
  • Automotive, injection
  • Watchmaking

Physical properties Units
Density (20°C) 8,14 Kg/dm³
Melting point 1430-1460 °C
Longitudinal elasticity modulus GPa
Thermal conductivity W/m·K
Electrical conductivity m/Ω·mm²
Electrical resistivity 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 deformation2
Electrodepositing
Diamond cutting
Nitriding3
Mechanical polishing4
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

Durcissement par vieillissement de la martensite

Heat treatment condition

  • The standard hardening treatment is 3 hours at 480°C. This treatment causes the precipitation of intermetallic compounds. This precipitation treatment can be combined with work-hardening.
  • Although treatment in air does not impair the material’s properties, it does spoil its appearance, with the metal taking on a blue hue. For this reason, we recommend treating under deep vacuum in the order of 10-5 Torr or under inert atmosphere such as argon.
  • Certain atmospheres regarded as inert due to the absence of colouration are in reality chemically active and thus may cause the material to become extremely brittle. This is particularly true in the case of hydrogen and cracked ammonia.
  • Influence of service temperature.
  •  Following tempering, the tensile and yield strengths of this alloy decreases slower with temperature than those of traditional “piano wire” type spring steels or 18-8 stainless steels his is due to dislocation locking by the precipitates formed during the temper hardening treatment. Variations in the modulus of elasticity (Young’s modulus) as a function of temperature

Alloy mechanical properties

POLIDUR
Possible hardness range 310 - 500 HV
Possible Rm range 700 - 1950 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 - 335
ROB05 RLSA 360

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

Contact us

Do not hesitate to contact us for a quote, any questions or advice. We will get back to you as soon as possible. 

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