| |
| 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 1920s, 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
todays 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. Todays 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 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

|
|