Alloy and Grey Iron Castings
High Temperature Alloys
         
 
HIGH TEMPERATURE ALLOYS
by Jayne Industries Inc.
Refractory Anchors and Hardware
Feb/99

JAYNE INDUSTRIES PERSPECTIVE:
As a supplier of alloy refractory anchors and hardware, Jayne Industries buys and processes high temp alloys to make finished parts. Jayne Industries represents the viewpoint of an enterprise which manufactures and services high temp alloy products, and receives real-world feedback about high temp alloy performance.
Jayne Industries does not design nor specify alloy grades, and has no particular allegiance to any supplier of alloys.

GOALS OF THIS PRESENTATION:
To promote a clearer understanding of the current state of commercially available high temp alloys which apply to refractory hardware.
To illustrate the characteristics of both traditional heat resisting stainless steel alloys, and the higher performance, true ‘high temp alloys’.

WHAT ARE HIGH TEMPERATURE ALLOYS?

Designed to maintain strength above room temperature.
Generally fulfill requirements for 500°F to 2300°F environments.
Alloying elements added to conventional stainless steels to improve properties at elevated temperatures.
Originally driven by Aerospace developments.

DEFINITION:
Broadly speaking, high temperature alloys are metals designed to maintain strength above room temperature, and which generally operate between temperatures of 500°F and 2200°F.

HISTORY AND EVOLUTION:
In the early 1920’s, adding chrome to steel produced the first true high temperature materials, for resistance heating elements. Later, alloying with nickel was found to stabilize austenite, and promote protective chromia at lower chrome contents, giving the foundation for most of today’s high temperature alloys. Aerospace and gas turbine developments initially motivated the quest for improving the Fe-Cr-Ni alloys. This quest has since been accelerated by industry demands for continuous processing, reduced downtime, and the improved process efficiencies gained at increased temperatures. Today’s techniques used to improve high temp alloys include further alloying with molybdenum, cobalt, tungsten, aluminum, silicon, or rare earth elements (e.g. tantalum, cerium), and advanced melting techniques such as VIM-vacuum induced melting, VAR-vacuum arc remelting, and ESR-electroslag remelting.

MATERIAL PROPERTIES

  • Thermal Expansion
  • Thermal Conductivity
  • Creep Strength
  • Rupture Strength
  • Thermal Fatigue Strength
  • Thermal Shock Strength
  • Erosion and Wear Resistance
  • Corrosion Resistance

MATERIAL PROPERTIES AND HIGH TEMPERATURE ALLOYS
All metals expand when heated. Proper provision for expansion and contraction will reduce possibility of early mechanical failure. Thermal conductivity governs the rate at which localized heating is dissipated. Low thermal conductivity could produce distortion and burn-through in situations such as direct flame heating. Above 700°F, steel will flow continuously under applied load, rendering tensile and yield strengths inappropriate measures of material strength. Creep and stress-rupture are measures of elevated temperature strengths. Creep strength is commonly expressed as the stress to produce a 1% creep rate in 10,000 hours at a certain elevated temperature. The stress to produce rupture of a material over a certain amount of time, at a certain temperature, is called rupture strength. Thermal fatigue strength is the ability to survive cyclic temperature changes. Thermal shock resistance is the ability to survive rapid temperature change.
Erosion and wear resistance are important factors in abrasive or moisture-laden environments.
Corrosion and oxidation resistance are of primary importance, since high temperature materials must not deteriorate quickly at high temperatures.

TYPES OF CORROSION

  • Pitting
  • Galvanic
  • Crevice
  • General Corrosion
  • Intergranular
  • Stress-Corrosion Cracking

The ability of stainless steel to resist corrosion rests primarily in the ability of chrome to combine with oxygen to form a passive, protective film over the material. At high temperatures, this passive film may fail to protect the material by the following types or modes of corrosion:

  • Pitting is a form of localized breakdown in the passive film, which is generally caused by the displacement of oxygen in the passive film by one of the halogen elements (e.g. chlorine, fluorine).
  • Galvanic corrosion involves the transfer of metal between dissimilar materials, when electrically connected in an electrolytic solution.
  • Crevice corrosion is another form of localized break in the passive film, caused by the buildup of contaminants (e.g. chlorides) in the absence of film-regenerating oxygen, which may occur in the closed sections between adjacent metal parts.
  • General corrosion, intergranular corrosion, and stress-corrosion cracking are modes of corrosion explained in the following slides.

STAINLESS, HEAT-RESISTING, AND HIGH TEMPERATURE ALLOY

STAINLESS AND
HEAT-RESISTING
HIGH TEMPERATURE
304 253MATM
316 RA330TM
321 ALLOY 601
347 RA333TM
309 230TM
310 556TM

There are over 50 commercially available grades of heat-resisting and high temperature alloys. The alloys listed represent refractory hardware materials most commonly experienced by Jayne Industries, and those materials projected to have increasing usage in the near future. Of the alloys not discussed, many are suited to narrowly defined applications (particular corrodants), or are prohibitively expensive for furnace applications (e.g high cobalt or molybdenum alloys for severe corrosion or ultra-high temperatures). The alloys discussed are often available in many forms, including plate, sheet, bar, wire and tube.

  • 253MA is a trademark of Avesta Sheffield.
  • RA330 and RA333 are trademarks of Rolled Alloys.
  • 230 and 556 are trademarks of Haynes International.
304 (L)
316 (L)
321
CHROME 18-20

16-18

17-19
NICKEL 8-10 10-14 9-12
SILICON 1.0 MAX 1.0 MAX 1.0 MAX
MANGANESE 2.0 MAX 2.0 MAX 2.0 MAX
CARBON .08 (.03) MAX .08 (.03) MAX .08 (.03) MAX
OTHERS MOLY = 2-3 Ti = .40
CREEP STRENGTH
(1%, 1000°, 10,000 HRS)
17,300 PSI 24,500 PSI 18,000 PSI
THERMAL EXPAN.
(MEAN FOR 32° -212°F)
(IN/IN°F x 10-6)
9.6 8.9 9.3
CHARACTERISTIC PROPERTIES
  • 1600°F INTER
  • 1700°F CONTIN.
  • INTERGRANULAR CORROSION AT 800°-1575°F FOR 304
  • GOOD CORR. RES.
  • EXCELLENT WELDABILITY AND FORMABILITY
  • 1600°F INTER
  • 1700°F CONTIN.
  • INTERGRANULAR CORROSION AT 800°-1575°F FOR 304
  • BETTER CORR. RES. THAN 304
  • HIGHER STRENGTH AT HIGH TEMP'S
  • 1600°F INTER
  • 1700°F CONTIN.
  • Ti STABILIZES CHROME FOR 800°-1575°F RANGE
  • GOOD CORR. RES.
347
309 (S)
310 (S)
CHROME 17-19

22-24

24-26
NICKEL 9-13 12-15 19-22
SILICON 1.0 MAX 1.0 MAX 1.5 MAX
MANGANESE 2.0 MAX 2.0 MAX 2.0 MAX
CARBON .08 MAX .20 (.08) MAX .25 (.08)
OTHERS Cb + Ta = .80 MIN
CREEP STRENGTH
(1%, 1000°, 10,000 HRS)
19,300 PSI 15,900 PSI 18,000 PSI
THERMAL EXPAN.
(MEAN FOR 32° -212°F)
(IN/IN°F x 10-6 )
9.3 8.3 9.0

CHARACTERISTIC PROPERTIES

  • 1600°F INTER
  • 1700°F CONTIN.
  • BETTER THAN 321 FOR 800°-1575°F RANGE (Cb+Ta)
  • GOOD CORR. RES. AND STRENGTH
  • 1850°F INTER
  • 1950°F CONTIN.
  • INTERGRANULAR CORROSION AT 800°-1575°F RANGE
  • EXCELLENT FOR HOT SULPHUR COMPOUNDS
  • 'S' MORE COMMON
  • 01900°F INTER
  • 2100°F CONTIN.
  • INTERGRANULAR CORROSION AT 800°-1575°F RANGE
  • DESIGNED FOR HIGH TEMP THERM CYCLING
  • 'S' MORE COMMON.
253MA
RA330
ALLOY 601
CHROME 21 TYP

18-20

21-25
NICKEL 11 TYP 34-37 58-63
SILICON 1.7 TYP 1.0-1.5 .5 MAX
MANGANESE .60 TYP 2.0 MAX 1.0 MAX
CARBON .09 TYP ..08 MAX .10 MA
OTHERS CERIUM = 0.4 TYP
NITRO = 0.17 TYP
ALUMINUM = 1.0-1.7
CREEP STRENGTH
(1%, 1600°F, 10,000 HRS)
1,450 PSI 2,100 PSI 1,300 PSI
THERMAL EXPAN.
(MEAN FOR 32° -1600°F)
(IN/IN°F x 10-6)
10.6 9.8 9.5

CHARACTERISTIC PROPERTIES

  • 1800°F OXI. RESIST.
  • EXCEPTIONAL OXI. RESISTANCE (THIN, DUCTILE ADHESIVE SCALE)
  • RESISTS SULPHUR ATTACK (LOW Ni) IN OXIDIZING ENVIRONMENT
  • 2200°F OXI. AND CARB. RESIST.
  • HIGH STRENGTH, CARB., AND THERMAL SHOCK RESISTANCE
  • FINE GRAIN SIZE 7-8
  • NO SIGMA FORMATION (Ni)
  • 2200°F OXI. RESIST.
  • 1800°F CARB. RESIST.
  • OUTSTANDING OXIDATION RESISTANCE
  • GOOD SULFIDATION RESISTANCE
RA333
230
556
CHROME 25 TYP

22 TYP

22 TYP
NICKEL 45 TYP 57 TYP 20 TYP
SILICON 1.0 TYP .40 TYP .40 TYP
MANGANESE 1.5 TYP .50 TYP 1.0 TYP
CARBON .08 MAX .10 TYP .10 TYP
OTHERS

MOLY = 3 TYP
COBALT = 3 TYP
TUNGSTEN = 3 TYP

MOLY = 2 TYP
COBALT = 5 MAX
TUNGSTEN = 14 TYP
MOLY = 3 TYP
COBALT = 18 TYP
TUNGSTEN =2.5 TYP
CREEP STRENGTH
(1%, 1600°F, 10,000 HRS)
2,700 PSI 4,400 PSI 4,100 PSI
THERMAL EXPAN.
(MEAN FOR 32° -1600°F)
(IN/IN°F x 10-6)
9.4 8.6 9.4

CHARACTERISTIC PROPERTIES

  • 2200°F OXI. RESIST.
  • VERY HIGH STRENGTH
  • EXCEPTIONAL THERM SHOCK + FATIGUE RESIST. (FINE GRAIN 7-8)
  • AQUEOUS-WHITE HEAT CORR.
  • 2100°F OXI. RESIST.
  • EXCEPTIONAL STRENGTH
  • LOW THERMAL EXPANSION
  • RESISTANCE TO GRAIN COARSENING AT HIGH TEMP'S
  • 2000°F OXI. RESIST.
  • EXCEPTIONAL STRENGTH
  • RESISTS SULFIDIZING, CARBURIZING, OZIDIZING, AND CHLORINE-BEARING ENVIRONMENTS

RELATIVE ALLOY COSTS

 
 
       


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550 Seaman St., Stoney Creek, ONT. L8E 3X7




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