Nickel and nickel alloys may be subjected to one or more of five
principal types of heat treatment, depending on chemical composition,
fabrication requirements and intended service.
These methods include:
- Annealing.A heat treatment designed to produce a
recrystallized grain structure and softening in work-hardened alloys.
Annealing usually requires temperatures between 705 and
1205oC, depending on alloy composition and degree of work hardening.
- Stress relieving. A heat treatment used to remove or reduce
stresses in work-hardened non-age-hardenable alloys without producing
a recrystalized grain structure. Stress-relieving temperatures for
nickel and nickel alloys from 425 to 870oC, depending on
alloy composition and degree of work hardening.
- Stress equalizing. A low-temperature heat treatment used
to balance stresses in cold worked material without an appreciable
decrease in the mechanical strength produced by cold working.
- Solution treating. A high-temperature heat treatment
designed to put age-hardening constituents and carbides into solid
solution. Normally applied to age-hardenable materials before the
aging treatment.
- Age hardening (precipitation hardening). A treatment
performed at intermediate temperatures (425 to 870oC)
on certain alloys in order to develop maximum strength by precipitation of
a dispersed phase throughout the matrix.
Annealing
As applied to nickel and nickel alloys, annealing consists of heating
the metal at a predetermined temperature for a definite time and
then slowly or rapidly cooling it, to produce a change in
mechanical properties - usually a complete softening as a
result of recrystalization.
Nickel and nickel alloys that have been hardened by cold working
operations, such as rolling, deep drawing, spinning or severe bending,
require softening before cold working can be continued. The thermal
treatment that will produce this condition is known as annealing,
or soft annealing.
The differences in chemical composition among nickel and nickel
alloys necessitate modifications in annealing temperatures as well
as in furnace atmospheres. The precipitation-hardening alloys
must be cooled rapidly after annealing if maximum softness is desired.
Three soft-annealing methods in general commercial use - open,
closed and salt bath annealing - are described bellow (Table 2.).
Open annealing is used most often. The material to be annealed
is heated at the selected temperature and protected from oxidation
by the products of combustion in a fuel-heated furnace, or by
a reducing gas introduced into an electric furnace. Temperature
control is critical because the annealing period is short.
Closed (box) annealing requires more time than open annealing
because of the lower temperatures used. Temperature control is less
critical than in open annealing. In most instances, the weight of
the container exceeds that of the work; consequently, the amount
of fuel required, heating time and costs are greater than in open
annealing.
Table 1. Nickel and nickel alloys
|
Material
|
Composition
|
|
Ni
|
Fe
|
Cu
|
Cr
|
Mo
|
Nickel 200
|
99.5
|
0.15
|
0.05
|
-
|
-
|
Nickel 201
|
99.5
|
0.15
|
0.05
|
-
|
-
|
Monel 400
|
66.0
|
1.35
|
31.5
|
-
|
-
|
Monel R-405
|
66.0
|
1.35
|
31.5
|
-
|
-
|
Monel K-500
|
65.0
|
1.00
|
29.5
|
-
|
-
|
Inconel 600
|
76.0
|
7.20
|
0.10
|
15.8
|
-
|
Inconel 601
|
60.5
|
14.1
|
-
|
23.0
|
-
|
Inconel 617
|
54.0
|
-
|
-
|
22.0
|
9.0
|
Inconel 625
|
61.0
|
2.5
|
-
|
21.5
|
9.0
|
Inconel 718
|
52.5
|
18.0
|
0.10
|
19.0
|
3.0
|
Inconel X-750
|
73.0
|
6.75
|
0.05
|
15.0
|
-
|
Hastelloy B
|
64.0
|
5.0
|
-
|
-
|
28.0
|
Hastelloy C
|
56.0
|
5.5
|
-
|
15.5
|
16.0
|
Hastelloy X
|
48.0
|
18.5
|
-
|
22.0
|
9.0
|
|
Table 2. Soft-annealing methods for nickel and nickel alloys
|
Material
|
Open annealingoC
|
Closed annealingoC
|
Stress relievingoC
|
Nickel 200
|
815 to 925
|
705 to 760
|
480 to 705
|
Nickel 201
|
760 to 870
|
705 to 760
|
480 to 705
|
Monel 400
|
870 to 980
|
760 to 815
|
540 to 565
|
Monel R-405
|
870 to 980
|
760 to 815
|
-
|
Monel K-500
|
870 to 1040
|
Not applicable
|
-
|
Inconel 600
|
925 to 1040
|
925 to 980
|
760 to 870
|
Inconel 601
|
1095 to 1175
|
1095 to 1175
|
-
|
Inconel 617
|
1120 to 1175
|
1120 to 1175
|
-
|
Inconel 625
|
980 to 1150
|
980 to 1150
|
-
|
Inconel 718
|
955 to 980
|
Not applicable
|
-
|
Inconel X-750
|
1095 to 1150
|
Not applicable
|
-
|
Hastelloy B
|
1095 to 1185
|
-
|
1095 to 1185
|
Hastelloy C
|
1215
|
-
|
1215
|
Hastelloy X
|
1175
|
1175
|
-
|
|
Salt bath annealing is used for special work with small parts.
Inorganic salts, such as chlorides and carbonates of sodium, potassium
and barium, which are relatively stable at temperatures considerably
above their respective melting points, are fused in large metallic or
refractory containers at temperatures up to about 700oC. At higher
temperatures, heat-resisting Fe-Ni-Cr alloy pots or refractory
containers should be used. Excessive fuming of the bath is an
indication of its maximum usable temperature.
The material to be annealed is placed in molten salts and absorbs
heat rapidly. After being annealed, the work metal is quenched in
water to free it from particles of the salt mixture. The annealed
material will not be bright and may be flash pickled to achieve a
bright surface.
Bright Annealing. The temperatures required for soft annealing
of nickel and nickel alloys are sufficiently high to cause slight
surface oxidation unless the materials are heated in vacuum or in
a furnace provided with a reducing atmosphere. Nickel 200, Monel 400
and similar alloys will remain bright and free from discoloration
when heated and cooled in a reducing atmosphere. However, nickel
alloys containing chromium, titanium and aluminum will form a thin
oxide film. Even if oxidation is not important, the furnace
atmosphere must be suitably sulfur-free and not strongly oxidizing.
The protective atmosphere most commonly used in heating nickel and
nickel alloys is that provided by controlling the ratio between
the fuel and air supplied to burners firing directly into the furnace.
A desirable reducing condition may be obtained by using a slight
excess of fuel so that the products of combustion contain at
least 2% carbon monoxide plus hydrogen (preferably 4%) with no
more than 0.05% uncombined oxygen.
Another method of maintaining desired conditions of furnace atmosphere
is to introduce a prepared atmosphere into the heating and cooling
chambers. This can be added to the products of combustion in a
direct-fired furnace; however, introduction of prepared
atmospheres is more commonly practiced with indirectly heated
equipment.
Prepared atmospheres suitable for use with nickel and nickel alloys
include: dried hydrogen, dried nitrogen, dissociated ammonia, and
cracked or partially reacted natural gas.
Dead-Soft Annealing. When the nickel alloys are annealed at
higher temperatures and for longer periods, a condition commonly
described as "dead-soft" is obtained, and hardness numbers will
result that are 10 to 20% lower than those of the "soft" condition.
This cannot be accomplished without increasing the grain size of
the metal. Therefore, this treatment should be used only for those
few applications in which grain size is of little importance.
Torch Annealing. Some large equipment is hardened locally
by fabricating operations. If the available annealing furnace is
too small to hold the work piece, the hardened sections can be
annealed with the flames of oil or acetylene torches adjusted so
as to be highly reducing.
The work should be warmed gently at first, with sweeping motions
of the torch, and should not be brought to the annealing temperature
until sufficient preheating has been done to prevent cracking as
a result of sudden release of stress. (Note: Torch annealing is
a poor method for general use, because it provides irregular and
insufficient annealing and produces heavily oxidized surfaces.)
Among the more important process-control factors in annealing nickel
and nickel alloys are selection of suitably sulfur-free for heating,
control of furnace temperature, effects of prior cold work and of
cooling rates, control of grain size, control of protective
atmospheres, and protection from contamination by foreign material.
Age hardening
Age-hardening practices for several nickel alloys are summarized in
the Table 3. In general nickel alloys are soft when quenched from
temperatures ranging from 790 to 1220oC, however, they may be
hardened by holding at 480 to 870oC or above and then furnace or
air-cooling. Quenching is not a prerequisite to aging; the alloys
can be hardened from the hot worked and cold worked conditions,
as well as from the soft condition.
Table 3. Age-hardening practices for nickel and nickel alloys |
Alloy
|
Solution treated
|
|
Temperature
|
Cooling method
|
Age hardening
|
Monel K-500
|
980 oC
|
WQ
|
Heat to 595oC, hold 16h; furnace cool to 540oC, hold 6h; furnace cool to 480oC, hold 8h; air-cool
|
Inconel 718
|
980 oC
|
AC
|
Heat to 720oC, hold 8h; furnace cool to 620oC, hold until furnace time for entire age-hardening cycle equals 18h; air cool
|
Inconel X-750
|
1150 oC
|
AC
|
Heat to 845oC, hold 24h; air cool; reheat to 705oC, hold 20h; air cool
|
|
980 oC
|
AC
|
Heat to 730oC, hold 8h; furnace cool to 620oC, hold until furnace time for entire age-hardening cycle equals 18h; air cool
|
Hastelloy X
|
1175 oC
|
AC
|
Heat to 760oC, hold 3h; air cool; reheat to 595oC, hold 3h; air cool
|
|
Hardening Techniques. Nickel alloys usually are hardened in
sealed boxes placed inside a furnace, although small horizontal or
vertical furnaces without boxes may be used also. The box or furnace
should hold the parts loosely packed, yet afford a minimum of excess
space. Electric furnaces provide the optimum temperature uniformity
of ± 6°C and the freedom from contamination required for this work.
Gas-heated furnaces, particularly those of the radiant-tube type,
can be made to give satisfactory results. It is difficult to obtain
good results from oil heating, even with the muffle furnaces.
All lubricants should be removed from the work before hardening.
Because of the long time of aging and the difficulty of excluding
air from the box or furnace, truly bright hardening cannot be
accomplished commercially. For semibright hardening, dry hydrogen
or cracked and dried ammonia should be used. When bright or
semibright hardening is not required, other atmospheres may be used,
such as nitrogen, cracked natural gas free of sulfur, cracked city gas,
cracked hydrocarbons, or a generated gas. The use of sulfur-free gases
is necessary to avoid embrittlement.
Salt baths are used occasionally for small parts. The hardened material
is never bright, and must be fresh pickled to restore the natural color.
Inorganic salts are used, such as chlorides and carbonates of sodium
or potassium, which are relatively stable at temperatures considerably
above their respective melting points. It is extremely important that
the salts be free of all traces of sulfur, so that the work does not
become embrittled.
List of Articles - Knowledge Base