Type
Analysis
Element
|
Min
|
Max
|
Carbon
|
--
|
0.05
|
Manganese
|
--
|
0.10
|
Silicon
|
--
|
0.10
|
Chromium
|
12.25
|
13.25
|
Nickel
|
7.50
|
8.50
|
Nitrogen
|
--
|
0.01
|
Sulfur
|
--
|
0.008
|
Phosphorus
|
--
|
0.01
|
Aluminum
|
0.90
|
1.35
|
Molybdenum
|
2.00
|
2.50
|
Description
PH 13-8 Mo* stainless is a
martensitic precipitation/age-hardening stainless steel capable of
high strength and hardness along with good levels of resistance to
both general corrosion and stress-corrosion cracking. In addition,
the alloy exhibits good ductility and toughness in large sections in
both the longitudinal and transverse directions. The excellent
properties of PH 13-8 Mo stainless are obtained through close control
of chemical composition and microstructure plus specialized melting
which reduces impurities and minimizes segregation. Compared to other
ferrous-based materials, this alloy offers a high level of useful
mechanical properties under severe environmental conditions. 13-8
Mo stainless has good fabrication characteristics and can be
age-hardened by a single low temperature treatment. Cold work prior
to aging increases the aging, especially for lower aging
tempratures. 13-8 Mo stainless has been used for valve parts,
fittings, cold-headed and machined fasteners, shafts, landing gear
parts, pins, lockwashers, aircraft components, nuclear reactor
components and petrochemical applications requiring resistance to
stress-corrosion cracking. Generally, this alloy should be considered
where high strength, toughness, corrosion resistance, and resistance
to stress-corrosion cracking are required in a steel showing minimal
directionality in properties. *PH 13-8 Mo stainless
is a registered trademark of Armco Inc.
Corrosion Resistance
In condition H 950, PH 13-8 Mo
stainless has rusting resistance similar to that of Type 304
Stainless in 5 weight percent salt fog. In strongly oxidizing and
reducing acids and in atmospheric exposures, the general-corrosion
resistance of PH 13-8 Mo stainless approaches that of Type 304. As
with other precipitation hardening stainless steels, the alloy's
level of general-corrosion reistance is greatest in the fully
hardened condition and decreased slightly as the aging temperature is
increased. Numerous tests representing a marine environment have
shown the alloy, in both the wrought and welded conditions, to have a
high level of resistance to stress-corrosion cracking. For best
resistance to stress-corrosion cracking, a minimum aging temperature
of 1000°F (538°C) is suggested. For optimum corrosion
resistance, surfaces must be free of scale and foreign particles and
finished parts should be passivated. Typical
Stress-Corrosion-Cracking Resistance in an Atmospheric Marine
Environment 0.062" (1.57 mm) thick strip
Aged
Condition
|
Applied
Stress*
|
Days
to Failure** 80-ft lot (Kure Beach)
|
ksi
|
MPa
|
H 950***
|
204
184 153
|
1406
1269 1055
|
1 sample failed after 353
days; 1-1077 days; 1 NF** 1 sample failed after 51 days; 2
NF 1 sample failed after 1077 days, 2 NF
|
H 1000***
|
199 179 149
|
1372 1234 1027
|
3 NF 3 NF 3 NF
|
H 1050***
|
172 155 149
|
1186 1069 1027
|
3 NF 3 NF 3 NF
|
Solution treated, welded, aged
at 1000°F for 4 hrs
|
195 176 146
|
1344 1213 1007
|
3 samples failed after 43 days 3
samples failed after 43 daysr 1 sample failed after 43 days;
1-100 days
|
Solution treated, welded solution
treated and aged at 1000°F for 4 hrs
|
195 176 146
|
1344 1213 1077
|
3 NF 3 NF 3 NF
|
*Applied stress were 100, 90 and 75
percent fo the 0.2 percent yield strength, using smooth bent beam
specimens tested in the longitudinal directiong. **NF indicates No
Failure in 1405 day's exposure. ***Heat treatment includes
solution treatment at 1700°F, 15 minutes.
Elevated Temperature Use
PH 13-8 Mo stainless has displayed
excellent resistance to oxidation up to approximately 1100°F.
Long-term exposure to temperatures between about 600-900°F
(288-482°C) can result in reduced toughness in precipitation
hardenable stainless steels. The reduction in toughness can be
minimized in some cases by using higher aging temperatures. Short
exposures to elevated temperatures can be considered, provided the
maximum temperature is at least 50°F (28°C) less than the
aging temperature.
Physical Properties
Specific Gravity:
(Condition H 1000)............................... 7.76
Density:
(Condition H 1000)
...................... 0.280 lb/cu in (7760 kg/cu m)
Electrical Resistivity Condition
A
Test Temperature
|
ohms
c/mf
|
microhm-mm
|
°F
|
°C
|
212
|
100
|
613
|
1020
|
Magnetic Permeability Conditon
H 950
Field
Strength H (Oersteds)
|
Permeability
|
10.5 54.7 110.5 164.5 217.0 264.0
|
52 127 85 65 53 46
|
Mean Coefficient of Thermal
Expansion
H
950
|
10(-6)/°F
|
10(-6)/K
|
H
1050
|
10(-6)/°F
|
10(-6)/K
|
70-200°F
(21-93°C) 70-400°F (21-204°C) 70-600°F
(21-316°C) 70-800°F (21-427°C) 70-900°F
(21-482°C)
|
5.9 6.0 6.2 6.3 6.6
|
10.6 10.8 11.2 11.3 11.9
|
70-200°F
(21-93°C) 70-400°F (21-204°C) 70-600°F
(21-316°C) 70-800°F (21-427°C) 70-900°F
(21-482°C)
|
5.7 5.9 6.2 6.4 6.6
|
10.3 10.6 11.2 11.5 11.9
|
H
1000
|
10(-6)/°F
|
10(-6)/K
|
H
1100
|
10(-6)/°F
|
10(-6)/K
|
70-200°F
(21-93°C) 70-400°F (21-204°C) 70-600°F
(21-316°C) 70-800°F (21-427°C) 70-900°F
(21-482°C)
|
5.7 6.0 6.2 6.3 6.6
|
10.3 10.8 11.2 11.3 11.9
|
70-200°F
(21-93°C) 70-400°F (21-204°C) 70-600°F
(21-316°C) 70-800°F (21-427°C) 70-900°F
(21-482°C)
|
6.0 6.2 6.4 6.6 6.8
|
10.8 11.2 11.5 11.9 12.2
|
Thermal Conductivity Condition
A
Test Temperature
|
Btu-in/ft²-h-°F
|
W/m-K
|
°F
|
°C
|
212
|
100
|
97.2
|
14.0
|
Heat Treatment
PH 13-8 Mo stainless is hardened by
heating solution-treated material, Condition A, to a temperature of
950°F to 1150°F for 4 hours, then air cooling. The various
heat treatments are as follows (note all times are "at
temperature"): Condition A(Solution treated
or Annealed) Heat at 1700°F +/-15°F (time dependent on
section size), cool to below 60°F so that the material is
completely transformed to martensite. Normally, 1 hour hold at
temperature is suggested. Section under 36 sq. inches can be quenched
in a suitable liquid quenchant; larger sections should be air cooled. Condition RH 950 (Precipitation
or Age Hardened) Cold treat solution treated material to -100°F
for 2 hours minimum. Air warm to room temperature. This must be done
within 24 hours after solution treatment. Heat cold-treated material
to 950°F +/-10°F for 4 hrs. Air cool. Condition H 950, H 1000, H 1050, H
1100, H 1150 (Precipitation or Age Hardened) Heat
solution-treated material at specified temperature +/-10°F for 4
hrs. Air cool. Condition H 1159M(Precipitation
or Age Hardened) Heat solution-treated material at 1400°F
+/-10°F for 2 hrs. Air cool; then treat at 1150°F +/-10°F
for 4 hrs. Air cool. Heat Treating After Overaging PH
13-8 Mo stainless in the H 1150 and H 1150M overaged conditions will
not respond to further aging treatments. Therefore, if the alloy is
obtained in either condition (for forging, optimum cold heading and
machining) it must be solution treated at 1700°F, after these
operations and before subsequent aging. It should be kept in mind
that the hardness for the H 1150 condition falls within the hardness
range for the solution-treated condition; therefore, hardness cannot
be used to distinguish between the H 1150 and solution-treated
conditions. Size Change Upon Aging Upon
aging a predictable size change will occur for PH 13-8 Mo stainless.
Increasing amounts of contraction occur as aging temperature is
increased.
Age-Hardening Treatment
|
Contraction in/in
(m/m)
|
H 950 H 1000 H
1050 H 1100
|
0.0004 to
0.0006 0.0004 to 0.0006 0.0005 to 0.0008 0.0008 to
0.0012
|
Cleaning Descaling
following forging and annealing can be accomplished by acid cleaning
or grit blasting. The acid treatment consists of 2 minutes in 50% be
volume muriatic acid at 180°F, followed by 4 minutes in a mixture
of 15% by volume nitric acid, plus 3% by volume hydrofluoric acid at
room temperature. Water rinse and desmut in 20% by volume nitric acid
at room temperature. Repeat cleaning procedure as necessary but
decrease the time by 50% (i.e., 1 and 2 minutes, respectively). The
heat tint from aging can be removed by polishing, vapor blasting or
pickling 4 to 6 minutes in a mixture of 15% by volume nitric acid,
plus 3% by volume hydrofluoric acid, followed by a water rinse.
Repeat the acid cleaning procedure if necessary, but decrease the
time by 2 to 3 minutes. Desmut in 20% by volume nitric acid at room
temperature. After acid cleaning, bake 1 to 3 hours at 300/350°F
to remove hydrogen.
Workability
Hot Working PH 13-8 Mo
stainless can be readily forged, hot headed and upset. Material which
is hot-worked must be solution treated prior to hardening if the
material is to respond properly to hardening.
Forging Heat uniformly to
2150/2200°F and hold 1 hr at temperature before forging. Do not
forge below 1750°F. To obtain optimum grain size and mechanical
properties, forging should be cooled in air to 60°F before
further processing. Forging must be solution treated prior to
hardening.
Cold Working PH 13-8 Mo
stainless can be fabricated by cold working to an extent which is
limited by the high initial yield strength.
Cutting Bars and forging
billets should be cold cut by sawing. Abrasive wheel cutting can
cause small surface cracks, particularly when cutting annealed stock,
and should be avoided.
Machining PH 13-8 Mo
stainless can be machined in both the solution treated and various
age-hardened conditions. In Condition A the alloy gives good tool
life and surface finish when machined at speeds 20 to 30% lower then
those used for Custom 630 (17Cr-4Ni) or 20 to 30% lower than used for
Stainless Type 302 and 304. The machinability as age-hardened will
improve as the hardening temperature is increased. Conditon H
1150M provides optimum machinability. Having procures Conditon H
1150M for best machinability, higher mechanical properties can be
developed only by solution treating and heat treating at standard
hardening temperatures.
Following are typical feeds and speeds for solution-treated Carpenter PH 13-8 Mo:
High-
Speed Tool
|
Turning- Cut-Off And Forming
|
Cut-Off Tool Width
|
1/16"
|
SFPM IPR
|
60 .001
|
1/8"
|
SFPM IPR
|
60 .0015
|
1/4"
|
SFPM IPR
|
60 .002
|
1/2"
|
SFPM IPR
|
60 .0015
|
Form Tool Width
|
1"
|
SFPM IPR
|
60 .001
|
1-1/2"
|
SFPM IPR
|
60 .0007
|
Drilling
|
Drill Dia.
|
1/4"
|
SFPM IPR
|
50 .004
|
3/4"
|
SFPM IPR
|
50 .008
|
Reaming
|
Under 1/2"
|
SFPM IPR
|
60 .003
|
Over 1/2"
|
SFPM IPR
|
60 .008
|
Die Threading
|
T.P.I
|
3-7½
|
SFPM
|
5-12
|
8-15
|
SFPM
|
8-15
|
Over 16
|
SFPM
|
10-20
|
Tapping
|
SFPM
|
20
|
Milling- End Peripheral
|
Depth of Cut .050"
|
SFPM IPR
|
90 .001-.004
|
Broaching
|
SFPM Chip load in./tooth
|
10 .002
|
When using carbide tools, surface speed feet/minute (sfpm) can be increased between 2 and 3 times over the high-speed suggestions. Feeds can be increased between 50 and 100%. Figures used for all metal removal operations covered are average. On certain work, the nature of the part may require adjustment of speeds and feeds. Each job has to be developed for best production results with optinum tool life. Speeds or feeds should be increased or decreased in small steps.
Welding PH 13-8 Mo
stainless can be welded using the inert-gas shielded or resistance
welding processes. When a filler metal is required, PH 13-8 welding
consumables should provide welds with properties similar to those of
the base metal. When designing the weld joint, care should be
exercised to avoid stress concentrators, such as shrap corners,
threads, and partial-penetration welds. When high weld strength is
not needed, a standard austenitic stainless filler, such as E/ER308L,
should be considered. Normally, welding in the solution annealed
condition has been satisfactory; however, where high welding stresses
are anticipated, it may be advantageous to weld in the overaged (H
1150) condition. Usually, preheating is not required to prevent
cracking. If welded in the solution treated condition. the alloy can
be directly aged to the desired strength level after welding.
However, the optimum combination of strength, ductility and corrosion
resistance is obtained by solution treating the welded part before
aging. If welded in the overage condition, the part must be solution
treated before aging.
Typical Mechanical Properties
Typical Longitudinal Room
Temperature Mechanical Properties Center or Intermediate test
location
Condition
|
0.2% Yield Strength
|
Ultimate Tensile Strength
|
% Elongation in
2"
|
% Reduction of
Area
|
Rockwell C Hardness
|
Charpy V-Notch Impact Strength
|
Modulus of
Elasticity (E)
|
ksi
|
MPa
|
ksi
|
MPa
|
ft-lb
|
J
|
ksi
|
MPa
|
RH
950 H 950 H 1000 H 1050 H 1100 H 1150 H 1150M
|
215 210 205 180 150 105 85
|
1482 1449 1413 1241 1034 724 586
|
235 225 215 190 160 145 130
|
1620 1551 1482 1310 1103 1000 896
|
12 12 13 15 18 20 22
|
45 50 55 55 60 63 70
|
48 47 45 43 35 33 32
|
20 20 30 50 60 80 120
|
27 27 41 68 81 103 163
|
-- -- 28.3
x 10³ -- -- -- --
|
-- -- 195
x 10³ -- -- -- --
|
Typical Transverse Room
Temperature Mechanical Properties Center or Intermediate test
location
Condition
|
0.2% Yield
Strength
|
Ultimate Tensile Strength
|
% Elongation in
2"
|
% Reduction of
Area
|
Rockwell
C Hardness
|
ksi
|
MPa
|
ksi
|
MPa
|
H 950 H 1000 H
1050 H 1100 H 1150 H 1150M
|
210 205 180 150 105 85
|
1448 1413 1241 1034 724 586
|
225 215 190 160 145 130
|
1551 1482 1310 1103 1000 896
|
12 13 15 18 20 22
|
40 50 55 60 63 70
|
47 45 43 35 33 32
|
Typical Room Temperature Torsional
Properties
Condition
|
Yield
Strength at 0.2% Shear Strain
|
Yield
Strength at 0.2% Normal Strain
|
Modulus
of Rupture
|
Modulus of
Rigidity (G)
|
ksi
|
MPa
|
ksi
|
MPa
|
ksi
|
MPa
|
ksi
|
MPa
|
H 950 H 1000
|
137 134
|
945 921
|
148 143
|
1020 986
|
184 172
|
1269 1186
|
11.1 x 10³ 10.9
x 10³
|
76.5 x 10³ 75.2
x 10³
|
|