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M.E.G. Systems Corporation - Using computer generated programs we calculate the existing or new application to insure maximum life of the heating element material.

Fabricated alloys used in manufacturing are KANTHAL A-1, KANTHAL APM, KANTHAL D, KANTHAL AF, NIKROTHAL 80/20, NIKROTHAL 60, and NIKROTHAL 40.

Please review design factors in selecting the best alloy for your application. Call us to review the application and we can make recommendations based on 30 years of experience.

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Element Design Factors

Factors affecting the design of an element include desired operating life, required operating temperature, and required degree and type of corrosion resistance. They are discussed in this section. Also discussed is the effect of operating practices on element resistivity.
Operating Life.............................

The element life is dependent on the alloy used, element temperature, element design, ambient at- mosphere, heating cycle, type of element support, etc.
When heated, resistance-heating alloys form an oxide layer on their surface, which prevents further oxidation of the material. To accomplish this function the oxide layer must be dense and resist the diffusion of gases as well as metal ions. It must also be thin and adhere to the metal under temperature fluctuations. By carefully balancing the alloying elements, alloys with longer life, higher maximum operating temperature and improved high-temperature mechanical strength will result.
The protective oxide layer on KANTHAL alloys formed at temperatures above 1000º C 1830º F consists mainly of alumina. The color is light gray, while at lower temperatures (under 1000º C, 1830º F) the oxide color becomes darker. The alumina layer has excellent electrical insulating properties and good chemical resistance to most compounds.
Even if the adherence of the oxide is good, some spalling (flaking-off) cannot be avoided. Damages to the oxide layer are repaired by the spontaneous formation of new oxide.
The oxide formed on NIKROTHAL alloys consists mainly of chromium oxide. The color is dark and the electrical insulating properties inferior to those of alumina.
The oxide layer on NIKROTHAL alloys spalls and evaporates more easily than the tighter oxide layer that is formed on the KANTHAL alloys.

For a round wire, the ratio of volume to surface area is proportional to the diameter. Practically, this means that as wire diameter is increased, more alloying element is available per surface unit to form a new oxide. Thus, at a given temperature, thicker wires have longer lifetimes than thinner wires. According to the same way of reasoning for strip elements, increased thickness gives a longer life.
To estimate the relative quality of a resistance alloy, a test method must be chosen which takes into account both oxidation rate and spalling. The method used at Kanthal is the Bash-test (ASTM B-76 and B-78). A 0.7 mm 0.0276 in wire is electrically heated to a standardized temperature and cycled on and off every two minutes. The time to failure is recorded.
Results of such tests are given in Table III, for KANTHAL and NIKROTHAL alloys. In the table, the durability of KANTHAL A-1 wire at 1200º C 2190º F is set at 100%, and the durability of the other alloys is related to that figure.
Numerous practical applications also show a much longer life of KANTHAL elements.
TABLE III
Relative Durability Values, KANTHAL and NIKROTHAL

Alloys (ASTM-test wire 0.7 mm 0.03 in)


1100ºC


2010ºF

1200ºC


2190ºF

1300ºC

2370ºF

1400ºC

2550ºF

KANTHAL A-1

KANTHAL AF

KANTHAL D

NIKROTHAL 80 Plus

NIKROTHAL 60 Plus

NIKROTHAL 40 Plus

 340

465

250

120

95

40

100%

120%

75%

25%

25%

15%

30

30

25

---

---

---

 (1)

(1) At this temperature only A-1 and AF can work. A-1 has 10% better durability than AF.
Maximum Permissible Temperature

The maximum permissible temperature of a heating alloy depends on both the wire size (diameter) and the atmosphere.


Wire Size



The effect of wire size on element life was previously explained. Hence, the maximum temperatures given are only valid for heavy gauges of wires and strips. As a rule, elements that operate at the maximum recommended temperatures should have a wire diameter not less than 3 mm 0.12 in or a strip thickness of at least 2 mm 0.08 in.
Table IV gives maximum wire temperatures as a function of wire diameter when operating in air.

TABLE IV
Maximum Permissible Temperature as a Function of Wire Size

Diameter, mm in:

1.0-3.0ºC

0.039-0.118ºF

>3.0ºC

>0.118ºF

KANTHAL A-1
KANTHAL AF
KANTHAL D
ALKROTHAL
NIKROTHAL 80 Plus
NIKROTHAL 60 Plus
NIKROTHAL 40 Plus
NIKROTHAL 20 Plus

1225-1350

2240-2460

1225-1350

2240-2460

1100-1200

2010-2190

1000-1050

1830-1920

1075-1150

1970-2100

1000-1075

1830-1970

1000-1050

1830-1920

975-1025

1790-1880

1400

2550

1400

2550

1300

2370

1100

2010

1200

2190

1150

2100

1100

2010

1050

1920

Furnace Atmospheres

As stated earlier, the life of a resistance-heating element depends on the continuous presence of a dense oxide layer completely coating the element surface. Corrosion results from interference with the formation or replenishment of the oxide layer by the presence of specific compounds in the atmosphere. The greater the interference, the shorter the element life. The effect of the corrosive compounds is often temperature dependent.
Table V lists maximum permissible element temperatures for various furnace atmospheres. The values are intended for guidance only, since they may be affected by changes in gas composition and dew- point, or the presence of impurities. However, the figures given should not be exceeded, since the heating material will tend to deteriorate rapidly at higher temperatures than those indicated.
Air. The possibility of using resistance alloys in air at high temperatures depends entirely on the protective oxide formed at the surface of the material. However, impurities in the atmosphere may disturb the oxide formation. Often fumes, gases, dust, etc. coming from the batch or the furnace insulation contaminate the atmosphere. Unless such furnaces are well ventilated, the gases may escape along the terminals, which may become excessively corroded and fail prematurely.
The tendency for the oxide to spall is greater for NIKROTHAL alloys than for KANTHAL alloys under normal operating conditions. This must be kept in mind when heating goods with sensitive surfaces, for example, white porcelain. Furthermore, ceramic element supports may become contaminated to such an extent that creep-currents may cause premature element failure.

Controlled atmospheres. In carbonaceous atmospheres of both endothermic and exothermic types, the alumina layer on the surface of KANTHAL alloys provides effective protection against the active components of these gas mixtures. Pre-oxidation in air at 1050º C 1920º F for seven to ten hours considerably lengthens the life of KANTHAL elements in such "protective" atmospheres.

In order to secure the longest possible life, the elements should be re-oxidized at intervals, depending on the operating conditionsCarbon deposits may damage the elements. In exothermic and endothermic atmospheres, the oxide layer on NIKROTHAL 80 Plus is not protective.
Instead a selective Cr-oxidation along the grain boundaries occurs ("green rot"). The tendency to "green rot" formation is strongest at low oxygen potential in the element temperature range 800 - 950º C 1470 - 1740º F. In such cases a KANTHAL alloy is recommended.
Hydrogen and nitrogen atmospheres. Pure hydrogen is not harmful to KANTHAL or NIKROTHAL alloys. However, service life will be shortened if the gas mixture contains uncracked ammonia.
Very dry nitrogen, deficient in oxygen, causes the formation of
aluminum nitride, thus limiting the permissible temperature (KANTHAL A-1 1050º C 1920º F, KANTHAL AF 1100º C 2012º F). On the other hand, the strong affinity for oxygen tends to inhibit nitride formation in a furnace atmosphere of technical pure nitrogen, which often contains some oxygen.
KANTHAL AF is relatively stable in a pure nitrogen atmosphere at temperatures up to 1250º C 2280º F, provided that controlled pre-oxidation is performed at the service temperature.
Vacuum. The oxide formed on NIKROTHAL alloys is decomposed at temperatures exceeding 1000º C 1830º F when subjected to a high vacuum, and the components in the alloy may vaporize to an extent depending on pressure and temperature.

The protective oxide on KANTHAL alloys is more stable, and pre-oxidized elements can be operated at lower pressures and higher temperatures. At 5 · 10-5 torr and 1100' C 2010º F the element life is very good. If the element temperature is 1150'C 2100 F the element should be re-oxidized after 250 service hours. At 1250º C 2200ºF re-oxidize after 100 hours (1050º C 1920º F at 5 hours).

Table V.
Maximum Permissible Temperatures in various Atmospheres

KANTHAL A-1

KANTHAL AF

KANTHAL D

NIKROTHAL

80 Plus

NIKROTHAL

60 plus

NIKROTHAL

40 plus

 

ºC

ºF

ºC

ºF

ºC

ºF

ºC

ºF

ºC

ºF

ºC

ºF

Oxidizing:  
Air, dry

1400

2550

1400**

2500

1300

2370

1200

2190

1150

2100

1100

2010

Air, moist

1200

2190

1200

2190

1200

2190

1150

2100

1100

2010

1050

1920

   
Neutral
N2, Nitrogen*

1200/1050

2190/1920

1250/1100

2280/2010

1150/1000

2100/1830

1250

2280

1200

2190

1150

2100

Ar, Argon

1400

2500

1400

2550

1300

2370

1250

2280

1200

2190

1150

2100

Exothermic  
10 CO, 15 H2,
5 CO2, 70 N2

1150

2100

1150

2100

1100

2010

1100***

2010

1100

2010

1100

2010

   
Reducing:
Endothermic:
20 CO, 40 H2,
40 N2

1050

1920

1050

1920

1000

1830

1100***

2010

1100

2010

1100

2010

H2, Hydrogen

1400

2500

1400

2550

1300

2370

1250

2280

1200

2190

1150

2100

Cracked  
ammonia:
75 H2, 25 N2

1200

2190

1200

2190

1100

2010

1250

2280

1200

2190

1150

2100

   
Vacuum:
10-3 torr

1150

2100

1200

2190

1100

2010

1000

1830

900

1650

900

1650

 
Table V.
Maximum Permissible Temperatures in various Atmospheres

KANTHAL A-1

KANTHAL AF

KANTHAL D

NIKROTHAL

80 plus

NIKROTHAL

60 plus

NIKROTHAL

40 plus

ºC

ºF

ºC

ºF

ºC

ºF

ºC

ºF

ºC

ºF

ºC

ºF

*The higher values apply for pre-oxidized material.

**For maximum element life above 1300ºC 2370ºF we recommend KANTHAL A-1 do to better oxide properties.

***Please note risk of "green rot" formation in carburizing atmospheres. Use KANTHAL AF or NIKROTHAL 60 Plus.

Corrosion Resistance


Typical furnace atmospheres have been discussed above, and their effect on element life detailed in Table V. Other corrosive or potentially corrosive constituents can also enter the furnace atmosphere; in addition, corrosion can be caused by mounting or supporting materials or contamination.
 
Gaseous Impurities

Steam.
Steam affects the formation of the protective oxide, making it porous and non-adhering, and thus shortens element life. This effect is more pronounced on KANTHAL alloys than on NIKROTHAL alloys.
Halogens. Halogens (fluorine, chlorine, bromine and iodine), even in trace quantities, severely attack all high-temperature alloys at fairly low temperatures.
Sulphur. In sulphurous atmospheres KANTHAL iron-base alloys have considerably better durability than nickel-base alloys. KANTHAL is particularly stable in oxidizing gases containing sulphur; although reducing gases with a sulphur content diminish its service life. NIKROTHAL alloys are sensitive to sulphur. Sulphur reacts with nickel to form nickel sulphide, which has a low melting point and prevents the formation of the protective chromium oxide.
 
Salts and Oxides, Metals

Salts and oxides
. The salts of alkaline metals, boron compounds, etc. in high concentrations may interfere with oxide formation, and are therefore harmful to heating alloys.
Metals. Some molten metals, such as zinc, aluminum and copper, react with the resistance alloys.
Moreover, these metals readily combine with oxygen to produce corrosive oxides. The elements should therefore be protected from splashes.

Ceramic Support Materials


For electric furnaces, special attention must be paid to the ceramic supports that come in direct contact with the heating element. Firebricks for element support should have an alumina content of at least 45%. In high-temperature furnaces, the use of sillimanite and high-alumina firebricks is often recommended. In general, the free silica (uncombined quartz) content should be kept low, since silica may react with the surface oxide at high temperatures. Iron oxide content (Fe, O,) must be as small as possible, preferably below 1%. The content of alkali oxides (Na2, O, K, O, etc.) must be kept at very low levels (below 0.1%).
Water glass is sometimes used as a binder in cements. This compound, however, has a detrimental effect on resistance heating material and any contact must be avoided.
Leakage and creep currents occurring at high temperatures attack the points of contact between the ceramic support and the heating element, often leading to premature failure of the element. This means that support material must have as high an insulating resistance as possible at the service temperature.

Embedding Compounds


Most embedding compounds including ceramic fibers are suitable for KANTHAL and NIKROTHAL if composed of alumina, alumina-silicate, magnesia and zirconia and if the conditions under "Ceramic support material" are observed. Acceptable commercial products are generally available.
If moistened cement is used with KANTHAL alloys as in heating panels, immediate drying is necessary to prevent the possibility of corrosion caused by sulphuric impurities in the cement. Distilled water is preferred as moistening agent, since fluorinated and chlorinated tap water may cause corrosion. Similarly, degreasing solvents containing chlorine must be re- moved after cleaning the element coils.
Certain cements may attack resistance-heating materials. In a closed environment such as in embedded elements, even traces of sulphur-containing contaminants may cause severe attack on NIKROTHAL wires at elevated temperature. Boron compounds at- tack KANTHAL and NIKROTHAL alloys above 900 C 1650º F. Corrosion tests for embedding compounds should always be performed before they are specified for use.