Nickel-Chromium Alloys (NiCr)

06 May.,2024

 

Nickel-Chromium Alloys (NiCr)

Magnesium (Mg) Metal

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Magnesium (Mg) is a light, moderately hard, silvery-white metal that ignites easily in the air and burns with a bright light. It is strong, has good heat dissipation and dampening, and is easy to weld, forge, cast or machine. It can improve the mechanical, fabrication, and welding characteristics when used as an alloying agent since it has a low density and is the lightest structural metal (a third lighter than aluminum). It also has good electrical properties. Magnesium turnings and chips are produced by milling commercial and high-purity magnesium, keeping size under control to obtain the desired specific surface and reactivity. They are silver-white. initially, but can turn to a dark gray if stored improperly. Purity: Standard purity (99.8% Mg) Ultra-high purity (99.98% Mg)

Nickel Chrome Alloys

Nickel Chrome

(NiChrome)

Alloys

Chemical Formula

Ni/Cr Alloys

Topics Covered

Background

Oxidation Resistance

Heating Elements

Thermocouples

High Temperature Corrosion Resistant Alloys

Wear Resistant Alloys

Background

The nickel-chromium system shows that chromium is quite soluble in nickel. This is a maximum at 47% at the eutectic temperature and drops off to about 30% at room temperature. A range of commercial nickel chromium alloys is based on this solid solution. Such nickel chromium alloys have excellent resistance to high temperature oxidation and corrosion and good wear resistance.

Oxidation Resistance

The introduction of small amounts (<7%) of chromium to nickel increase the sensitivity of the nickel chromium alloy to oxidation. This is because the diffusion rate of oxygen in the scale is increased. This trend reverses after addition levels increase above 7% chromium and increases up to an addition level of approximately 30%. Above this level, there is little change.

Oxidation resistance can be attributed to the formation of a highly adherent protective scale. The adherence and coherence of the scale can be improved by the addition of small amounts of other reactive elements such as zirconium, silicon, cerium, calcium or similar. The scale thus formed is a mixture of nickel and chrome oxides (NiO and Cr2O3). These combine to form nickel chromite (NiCr2O4), which has a spinel-type structure.

Heating Elements

A marked increase in electrical resistivity is observed with increasing chromium additions. An addition level of 20% chromium is considered the optimum for electrical resistance wires suitable for heating elements. This composition combines good electrical properties with good strength and ductility, making it suitable for wire drawing. Commercial grades include Nickel Chrome NiChrome and BrightRay. Small modifications of to this composition may be made to optimise it for particular applications.

  Figure 1. Electrical resistivity as a function of chromium content for nickel-chromium alloys

The addition of the appropriate reactive alloying elements will affect the properties of the scale. The operating conditions of the alloy will largely influence the composition that should be used. Table 1 outlines the compositional differences between alloys used for intermittent and continuous usages.


Table 1. Suitable compositions for heating elements used intermittently and continuously.
Element

Intermittent

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Continuous Cr 20 20 Si 1.5 0.5 Ca 0.1 0.05 Ce 0.05 - Ni Balance Balance

Suitable compositions for heating elements used intermittently and continuously.

While the compositional changes have a negligible effect on mechanical properties, higher additions of reactive elements tend to prevent flaking of the scale during cyclic heating and cooling. This effect is less of an issue with continuously operating heating elements, so addition levels do not need to be as high.

The binary 90/10 Ni/Cr alloy is also used for heating elements, and has a maximum operating temperature of 1100°C. Other uses for this alloy are thermocouples.

Thermocouples

Thermocouples: The 90/10 nickel chromium alloy is commonly used in thermocouples, in conjunction with a 95/5 Ni/Al alloy. This combination is called chromel-alumel, and similar to heating elements has a maximum operating temperature of 1100°C. This couple becomes susceptible to drift in the region of 1000°C due to preferential oxidation after prolonged usage. The addition of silicon has been found to overcome this effect. Commercial grades include Nicrosil (containing 14% Cr and 1.5% Si) and Nisil (containing 4.5% Si and 0.1% Mg).

High Temperature Corrosion Resistant Alloys

The 80/20 nickel chromium alloy is often used for wrought and cast parts for high temperature applications, as it has better oxidation and hot corrosion resistance compared to cheaper iron-nickel-chromium alloys. This nickel chromium alloy is highly suited to applications that are subject to oxidation.

In applications where fuel ashes, and/or deposits such as alkali metal salts such as sulphates are encountered, higher chromium content alloys are more suitable. This is because fuel ashes react with the oxide scale. Ashes containing vanadium are particularly aggressive in the respect and have a fluxing effect on the scale, increasing the susceptibility of the alloy to attack by oxidation.

In sulphur containing environments, chromium sulphide (Cr2S3, melting point 1550°C) is formed preferentially to nickel sulphide. Formation of nickel sulphide is preferred as this hinders the formation of the nickel/nickel-sulphide eutectic which has a low melting point. Eventually, local chromium supplies can be exhausted, leaving sulphur to react with nickel to form the low melting point eutectic compound, leading to liquid phase attack. Alloys that have suffered this form of attack have wart-like growths on their surface. Due to the preferential formation of chromium sulphides, it follows that higher chromium containing nickel chromium alloys are more resistant to this type of attack.

Nickel/chromium alloys containing more than 30% chromium have a two phase structure which consists of a-chromium and γ-nickel. The a-chromium phase brittle and hence the alloy decreases in ductility with increasing chromium content. Properties for some binary alloys are given in table 2. The addition of about 1.5% niobium induces improved strength and ductility, while at the same time reducing embrittlement after high temperature exposure provided impurities such as carbon, nitrogen and silicon are controlled.


Table 2. Tensile and ductility properties for some nickel chromium alloy at room temperature.
Cr Content (%)

Tensile Str (MPa)

Elong. (%) 35 480 62 50 540-680 7-24 60 800-1000 1-2

Tensile and ductility properties for some nickel chromium alloy at room temperature.

Alloys with chromium contents up to approximately 35% are suitable for hot working. Above this level, they are generally only suited to casting. Some ductility gains can be achieved by the addition of zirconium or titanium. Inconel 671, (containing 48% Cr and 0.35% Ti is such an alloy and is used in applications including duplex tubing for coal-fired superheating tubing.

Wear Resistant Alloys

Wear mechanisms are complex, but high hardness and good corrosion resistance contribute to good wear resistance. nickel chromium alloys provide an economical alternative to materials such as weld deposited cobalt-chrome alloys with additions of carbon and tungsten which are commonly used wear resistant applications. An example of a nickel chromium alloy for this type of application is 8-12% Cr, 0.3-1.0% C, 3-4% Si, 1.5-2.5% B, 1-4% Fe and the balance Ni. A coating of this material deposited by inert gas shielded arc techniques would be in the range 40-50 Rockwell C.

Property Table of Nickel Chromium Alloys

 

Material Nickel Chrome Alloys Composition:  Ni/14-46Cr + some combination of Fe Mo Cu Co Si Ti W Al + others
Property Minimum Value (S.I.) Maximum Value (S.I.) Units (S.I.) Minimum Value (Imp.) Maximum Value (Imp.) Units (Imp.) Atomic Volume (average) 0.0065 0.0072 m3/kmol 396.654 439.371 in3/kmol Density 7.75 8.65 Mg/m3 483.817 540.002 lb/ft3 Energy Content 40 200 MJ/kg 4333.55 21667.7 kcal/lb Bulk Modulus 110 205 GPa 15.9541 29.7327 106 psi Compressive Strength 170 2100 MPa 24.6564 304.579 ksi Ductility 0.005 0.7   0.005 0.7   Elastic Limit 170 2100 MPa 24.6564 304.579 ksi Endurance Limit 130 1150 MPa 18.8549 166.793 ksi Fracture Toughness 65 150 MPa.m1/2 59.153 136.507 ksi.in1/2 Hardness 1000 6000 MPa 145.038 870.227 ksi Loss Coefficient 9e-005 0.0013   9e-005 0.0013   Modulus of Rupture 170 2100 MPa 24.6564 304.579 ksi Poisson's Ratio 0.26 0.325   0.26 0.325   Shear Modulus 55 100 GPa 7.97707 14.5038 106 psi Tensile Strength 330 2300 MPa 47.8625 333.587 ksi Young's Modulus 150 245 GPa 21.7557 35.5342 106 psi Glass Temperature     K     °F Latent Heat of Fusion 275 320 kJ/kg 118.228 137.575 BTU/lb Maximum Service Temperature 1070 1473 K 1466.33 2191.73 °F Melting Point 1475 1710 K 2195.33 2618.33 °F Minimum Service Temperature 0 0 K -459.67 -459.67 °F Specific Heat 380 500 J/kg.K 0.294066 0.386929 BTU/lb.F Thermal Conductivity 8 17 W/m.K 14.9763 31.8246 BTU.ft/h.ft2.F Thermal Expansion 9 16 10-6/K 16.2 28.8 10-6/°F Breakdown Potential     MV/m     V/mil Dielectric Constant             Resistivity 84 240 10-8 ohm.m 84 240 10-8 ohm.m

 

Environmental Properties Resistance Factors 1=Poor 5=Excellent Flammability 5 Fresh Water 5 Organic Solvents 5 Oxidation at 500C 5 Sea Water 5 Strong Acid 5 Strong Alkalis 5 UV 5 Wear 5 Weak Acid 5 Weak Alkalis 5 Primary author: AZoM.com

 

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NiChrome: This group of materials on the nickel/chromium solid solution. These materials have excellent oxidation resistance, wear resistance and high temperature properties. Typical application include heating elements, thermocouples and other applications involving high temperature waer and corrosion.