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Product Information
Name 17-4PH Steel
Stocklist & Inventory Available: Blade Steel
Material Specification: ASTM,AISI,UNS,AMS,Werkstoffe,Miscellaneous
Equivalent Grade: A564,AISI 630,UNS S17400,AMS 5622 / 5643,1.4542,X5CrNiCuNb16-4,10705GU-GV,TLV 9239 01
Condition of delivery: Hot forging/hot rolling + annealing/normalizing + tempering/quenching + tempering
Surface condition Scaled (hot working finished)/ground/rough machining/fine machining
Product Shape available: Round,Flat,Square,Hexagon,Plate,Sheet,Other
Description
Chemical Composition
Mechanical Properties
More

GENERAL CHARACTERISTICS OF PH GRADES 17-4PH

17-4 PH steel is a martensitic precipitation age hardening stainless steel that combines high strength and hardness with excellent corrosion resistance. It may be age hardened by a single-step low- temperature treatment.

17-4 PH Inventory Size Ranges

 

Plates / Sheets

Steel Bar

Coil / Stri

     

0.08-200mm(T)*W*L

Φ8-1200mm*L

0.03-16.0xLmm

     

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APPLICATIONS

This grade of steel is used for a variety of applications including oil field valve parts, chemical process equipment, forged aircraft fittings, fasteners and pump shafts, gears, nuclear reactor parts and jet engine parts.

FORGING

Forging of this grade should be carried out between 2150/2200ºF (1180/1200ºC) and 1850ºF (1010ºC.) For optimum grain size and mechanical properties, forgings should be air cooled to below 90ºF (32ºC) prior to further processing. Forgings must be solution treated prior to hardening.

HEAT TREATMENT

Type 17-4 PH alloy is hardened by heating solution-treated material, condition A, to between 900/ºF (480ºC) and 1150ºF (620ºC) for one to four hours, depending upon the temperature, then air cooling.

SOLUTION TREATMENT

Heat at 1900ºF (1040ºC) for 30 minutes and cool to below 90ºF (32ºC) to allow complete
transformation to martensite. Sections less than 3” may be quenched in a suitable liquid while those sections over 3” should be rapidly air cooled. Parts should not be used in the solution – treated condition due to possible problems with stress corrosion cracking.

AGE HARDENING

For condition H900 heat solution-treated material at 900ºF (480ºC) for 1 hour and air cool. For conditions H925, H1025, H1075, H1100, H1150: heat solution-treated material at appropriate temperature ± 15ºF (± 8ºC) for 4 hours and air cool.

MACHINABILITY

17-4 PH grade is readily machinable in both the solution-treated and various age-hardened conditions. In the solution-treated condition it machines in a similar way to stainless 304. The machinability improves as the hardening temperature increases.

WELDABILITY

17-4 PH grade can be satisfactorily welded by the shielded fusion and resistance welding processes.
Oxyacetylene welding is not recommended since carbon pick up may occur in the weld. If a filler metal is required a 17-4PH type welding rod should be used to provide welds with base-metal properties. If high strength is not required an austenitic stainless filler metal is satisfactory.
Welding in the solution-treated condition is normally satisfactory, but if high welding stresses are a possibility it may be best to weld in the overaged (H1150) condition.
If welded in the solution-treated condition, 17-4PH alloy may be aged to the desired strength level after welding, but the optimum strength-ductility-corrosion resistance combination is obtained by solution treating the welded part before aging. Welding in the overaged conditioned must be followed by solution treating then aging.

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17-4PH Chemical Composition

      

Composition

(wt %)

C

Carbon

0.07 max.

Mn

Manganese

1.00 max.

P

Phosphorus

0.040 max.

S

Sulfur

0.030 max.

Si

Silicon

1.00 max.

Cr

Chromium

15.00 -17.50

Ni

Nickel

3.00 - 5.00

Cu

Copper

3.00 - 5.00

Nb

Ta

Columbium plus Tantalum                     

0.15 - 0.45

*ASTM A693 requirements call for Niobium plus Tantalum = 0.15 - 0.45.

Please contact us for more details. The technical data provided is for information only and not for design purposes.

17-4PH Standard Heat Treatments

As supplied from the mill in Condition A, PCSSC-LTD 17-4 PH Stainless Steel can be heat treated at a variety of temperatures to develop a wide range of properties. Eight standard heat treatments have been developed. The following chart outlines the times and temperatures required.
This alloy exhibits useful mechanical properties in Condition A. Tests conducted at an exposed marine atmosphere on a 80 ft. (24.4 m) lot, 82 ft. (25 m) from the waterline, show excellent stress corrosion
resistance. Condition A material has been used successfully in numerous applications. The hardness and tensile properties fall within the range of those for Conditions H 1100 and H 1150.
However, in critical applications, the alloy is used in the precipitation- hardened condition, rather than Condition A. Heat treating to the hardened condition, especially at the higher end of the temperature range, stress relieves the structure and may provide more reliable resistance to stress corrosion cracking than in Condition A.

TABLE 1 - STANDARD HEAT TREATMENTS

Condition A Solution Treated at 1900 °F ± 25 °F (1038 °C ± 14 °C) or Air cool below 90 °F (32 °C).

Condition

Heat To

± 15 °F (8.4 °C)

Time at Temperature, hrs.

Type of Cooling

H 900

900 °F (482 °C)

1

Air

H 925

925 °F (496 °C)

4

Air

H 1025

1025 °F (551 °C)

4

Air

H 1075

1075 °F (580 °C)

4

Air

H 1100

1100 °F (593 °C)

4

Air

H 1150

1150 °F (621 °C)

4

Air

H 1150 + 1150

1150 °F (621 °C)

 

1150 °F (621 °C)

4

followed by
4

Air

 

Air

H 1150-M 1400 °F(760 °C)

1150 °F (621 °C)
2
followed by
4
Air

Air

TABLE 2 – TYPICAL MECHANICAL PROPERTIES

Transverse Property Condition
A H 900 H 925 H 1025 H 1075 H 1150 H 1150-M
UTS, ksi. (MPa) 160 (1103) 200 (1379) 190 (1310) 170 (1172) 165 (1138) 150 (1034) 137 (945)
0.2% YS, ksi. (MPa) 115 (793) 185 (1275) 175 (1207) 165 (1138) 160 (1103) 130 (896) 111 (765)
Elongation % in 2" (50.8 mm) 5 9 9 10 11 12 17
Rockwell Hardness C 35 45 43 38 37 33 31

TABLE 3 - PROPERTIES ACCEPTABLE FOR MATERIAL SPECIFICATION*

Transverse Property Condition
A H 900 H 925 H 1025 H 1075 H 1110 H 1150
UTS, ksi. (MPa) 185 max.(1276) 190 min.(1310) 170 min.(1172) 155 min.(1069) 145 min.(1000) 140 min.(965) 135 min.(931)
0.2% YS, ksi. (MPa) 160 max.(1103) 170 min.(1172) 155 min.(1069) 145 min.(1000) 125 min.(862) 115 min.(790) 105 min.(724)
Elongation % in 2" (50.8 mm) 3 min. 5 min. 5min. 5 min. 5min. 5min. 8 min.
Rockwell Hardness C 38 max. 40 - 48 38 - 46 35 - 43 31 - 40 31 - 40 28 - 38
*Sheets and strip.

TABLE 4 - PIN BEARING PROPERTIES OF SHEET*                           

Condition

e/D†  = 1.5

e/D = 2.0

Tensile Strengths***

Bearing Yield
Strength**,
ksi. (MPa)

Bearing Strength, ksi. (MPa)

Bearing Yield Strength**,ksi. (MPa)

Bearing Strength, ksi. (MPa)

0.2% YS,

ksi. (MPa)

UTS,

ksi. (MPa)

H 925

273 (1882)

304 (2096)

308 (2124)

401 (2765)

190 (1310)

191 (1317)

H 1025

242 (1669)

270 (1862)

288 (1986)

359 (2475)

172 (1186)

172 (1186)

H 1100

233 (1606)

257 (1772)

262 (1806)

337 (2324)

160 (1103)

160 (1103)

H 1150

203 (1400)

234 (1613)

236 (1627)

313 (2158)

146 (1007)

150 (1034)

A

211 (1455)

226 (1558)

276 (1903)

296 (2041)

158 (1089)

158 (1089)

*Average of duplicate tests on one heat of 0.065 in. (1.65 mm) sheet material.
** Offset equals 2% of pin diameter.
*** Yield equals ultimate tensile strengths due to rounding.
†e/D = Distance from edge of specimen to edge of hole + hole diameter.

Please contact us for more details. The technical data provided is for information only and not for design purposes.

ELEVATED TEMPERATURE PROPERTIES

Mechanical properties of CNLHSS Steel 17-4 PH Stainless Steel Condition
H 1150 after long-time exposure at elevated temperatures are shown in Table 4. When tested at room temperature after exposure, a slight loss of toughness and gain in strength can be noted. However, H 1150 properties can be restored by heat treating at 1150 °F (621 °C) for four hours after original exposure. By taking advantage of this re-aging treatment, the service life of parts exposed at elevated temperature to 750 °F (339 °C) can be extended indefinitely.
Elevated temperature properties for short-time exposures were determined for Conditions H 900 and H 1150. Specimens were heated rapidly by resistance methods and reached exposure temperatures within two seconds. Specimens were then held at temperature for the times indicated and tested both at exposure temperature and at room temperature. 

TABLE 5 - EFFECT OF ELEVATED TEMPERATURE EXPOSURE ON MECHANICAL PROPERTIES - CONDITION H 1150

 

 

 

Exposure
Temperature,

°F (°C)

 

 

Time
hrs.

Test Temperatures

Prenotched Charpy
W/A, in.•lbs./in2.
(N/mm2)

Room Temperature

600 °F (316 °C)

750 °F (399 °C

UTS,

ksi. (MPa)

0.2% YS,

ksi. (MPa)

Elong

% in 2"

(50.8 mm)

UTS,

ksi. (MPa)

0.2% YS

ksi. (MPa)

Elong

% in 2"

(50.8 mm)

UTS,

ksi. (MPa)

0.2% YS

ksi. (MPa)

Elong

% in 2"

(50.8 mm)

75 °F

(24 °C)

-75

(-60

°F

°C)

 

600 (316)

1000

7000

7000*

151 (1041)

157 (1082)

141 (972)

142 (979)

150 (1034)

119 (820)

13

11

13

123

128

113

(848)

(882)

(779)

118

123

107

(814)

(848)

(738)

6

8

7

115

120

107

(793)

(827)

(738)

110 (758)

117 (807)

103 (710)

5

5

6

1882 (329)

1956 (342)

2168 (379)

2062

1653

2242

(361)

(289)

(392)

650 (343)

1000

7000

7000*

155 (1069)

168 (1159)

141 (972)

149 (1027)

162 (1117)

119 (820)

13

11

12

128

138

115

(882)

(952)

(793)

124

135

108

(855)

(931)

(745)

6

7

7

121

132

108

(834)

(910)

(745)

116 (800)

128 (882)

102 (703)

5

5

7

1940 (340)

1624 (284)

2264 (396)

2018

1597

2398

(353)

(279)

(420)

700 (371)

100

1000

7000

7000*

152 (1048)

162 (1117)

179 (1234)

140 (965)

144 (993)

155 (1069)

174 (1200)

117 (807)

13

11

9

13

125 (862)

134 (924)

148 (1020)

114 (786)

120

130

144

108

(827)

(896)

(993)

(745)

6

7

6

7

118

130

142

108

(814)

(896)

(979)

(745)

112 (772)

124 (855)

137 (945)

103 (710)

4

6

5

6

1874 (328)

1841 (322)

1215 (213)

2153 (377)

1973

1801

667

2260

(345)

(315)

(117)

(396)

750 (399)

100

1000

7000

7000*

154 (1062)

171 (1179)

185 (1276)

140 (965)

147 (1014)

165 (1138)

178 (1227)

117 (807)

13

11

10

13

128 (882)

140 (965)

149 (1027)

113 (779)

122

135

144

107

(841)

(931)

(993)

(738)

6

7

7

7

121

135

144

105

(834)

(931)

(993)

(724)

115 (793)

129 (889)

138 (952)

101 (696)

4

6

8

7

1807 (316)

1309 (229)

987 (173)

2308 (404)

1836

1231

420

2320

(321)

(215)

(74)

(406)

None

None

148 (1021)

134

(924)

13

121

(834)

115

(793)

5

116

(800)

111 (765)

4

2087 (365)

2124

(372)

*Re-aged at 1150 °F (621 °C) for 4 hours after exposure.

NOTE: These tests represent instant heating of the entire cross section of the test specimens. Under actual conditions, heating rates would depend on heat source, surface conditions and thermal conductivity of PCSSC-LTD 17-4 PH Stainless Steel (see Physical Properties). Times and temperatures shown in the tables apply only after parts have reached temperatures.

17-4PH Physical Properties

PHYSICAL PROPERTIES

 

Condition

A

(Magnetic)

H 900

(Magnetic)

H 1075

(Magnetic)

H 1150

(Magnetic)

Density, lbs./in3. (g/cm3)

0.28 (7.78)

0.282 (7.80)

0.283 (7.81)

0.284 (7.82)

Electrical Resistivity, µΩ•cm

98

77

Specific Heat, BTU/lbs./°F (kJ/kg/K)

32 – 212 °F (0 – 100 °C)

0.11 (0.46)

0.11 (0.46)

 

 

Thermal Conductivity,
BTU/hr./ft2./°F (W/m/K)

300 °F (149 °C)

500 °F (260 °C)

860 °F (460 °C)

900 °F (482 °C)

 

 

 

 

124 (17.9)

135 (19.5)

156 (22.5)

157 (22.6)

 

 

 

 

Mean Coefficient of Thermal Expansion,

in./in./°F (μm/m/K)

-100 – 70 °F (-73 – 21 °C)

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 x 10-6 (10.8)

6.0 x 10-6 (10.8)

6.2 x 10-6 (11.2)

6.3 x 10-6 (11.3)

 

 

5.8 x 10-6 (10.4)

6.0 x 10-6 (10.8)

6.0 x 10-6 (10.8)

6.3 x 10-6 (11.3)

6.5 x 10-6 (11.7)

 

 

6.3 x 10-6 (11.3)

6.5 x 10-6 (11.7)

6.6 x 10-6 (11.9)

6.8 x 10-6 (12.2)

 

 

6.1 x 10-6 (11.0)

6.6 x 10-6 (11.9)

6.9 x 10-6 (12.4)

7.1 x 10-6 (12.8)

7.2 x 10-6 (13.0)

7.3 x 10-6 (13.1)

Modulus of Elasticity, ksi. (MPa)

28.5 x 106 (197 x 103)

Modulus of Rigidity, in
Torsion, ksi. (MPa)

9.68 x 103 (67 x 103)

11.00 x 103 (76 x 103)

 

10.10 x 103 (70 x 103)

Poisson's Ratio (all conditions)

0.272


Please contact us for more details. The technical data provided is for information only and not for design purposes.