Inconel 625 Alloy 625 Nickel 625 Nickel-Base Alloy Sheet Factory Price

Min.Order: 500
Product origin: Liaocheng, Shandong, China
Infringement complaint: complaintComplaint
US$ 55

Description

Product name:Inconel 625 Alloy 625 Nickel 625 nickel-base alloy sheet factory price
Brief introduction of Inconel 625

Inconel Alloy 625 (UNS designation N06625) is a nickel-based superalloy that possesses high strength properties and resistance to elevated temperatures. It also demonstrates remarkable protection against corrosion and oxidation. Its ability to withstand high stress and a wide range of temperatures, both in and out of water, as well as being able to resist corrosion while being exposed to highly acidic environments makes it a fitting choice for nuclear and marine applications.
chemical properties of Inconel 625 include:

 CrMoCoNb+TaAlTiCFeMnSiPSNi
Min208--3.15----------------Balance
Max231014.15.4.4.15.5.5.015.015Balance

Mechanical Properties

Physical Properties

Physical Property°CMetric Units°FBritish Units
Density228.44 g/cubic cm720.305 lb/cubic in.
Electrical
Resistivity
23
100
200
300
400
500
600
1.26 microhm-m
1.27
1.28
1.29
1.30
1.31
1.32
74
212
392
572
752
932
1112
49.6 microhm-in.
50.0
50.4
50.8
51.2
51.6
52.0
Mean Coefficient
of Thermal
Expansion
20-204
20-316
20-427
20-538
20-649
20-760
20-871
20-982
13.1 x 10(-6)m/m-°C
13.5
13.9
14.4
15.1
15.7
16.6
17.3
68-400
68-600
68-800
68-1000
68-1200
68-1400
68-1600
68-1800
7.3 microinches/in.-°F
7.5
7.7
8.0
8.4
8.7
9.2
9.6
Thermal
Conductivity
23
100
200
300
400
500
600
9.8 W/M-°C
11.4
13.4
15.5
17.6
19.6
21.3
74
212
392
572
752
932
1112
68 Btu-in./ft².-hr.-°F
79
93
108
122
136
148
Specific
Heat
0
100
200
300
400
500
600
429 J/kg-°C
446
463
480
496
513
560
32
212
392
572
752
932
1112
0.102 Btu/lb-°F
0.107
0.111
0.115
0.118
0.123
0.134

Average Dynamic Modulus of Elasticity *
FormConditionTest Temp.,
F(C)
Average Dynamic Modulus of
Elasticity, psi x 10(6) (MPa)
Plate,
3/8 in. (9.5 mm)
thick
Annealed at
1925°F (1052°C),
rapid cooled
Room
200 (93)
400 (204)
600 (316)
800 (427)
1000 (538)
1200 (649)
1400 (760)
1600 (871)
1800 (982)
30.2 (208,000)
29.2 (201,000)
28.8 (199,000)
27.7 (191,000)
26.7 (184,000)
25.6 (176,000)
24.3 (168,000)
22.8 (157,000)
21.2 (146,000)
18.7 (129,000)

* Average of five tests at each temperature.
 

Mechanical Properties

Average Impact Strength, Plate *
Aging Temperature,
F (C)
Aging Time, hrs.Average Charpy V-Notch
Impact Strength,
ft. lbs.J
Annealed**--81110
1200 (649)1000
4000
8000
16000
11
8
5
4
15
11
7
5
1400 (760)1000
4000
8000
16000
5
4
5
4
7
5
7
5
1600 (871)1000
4000
8000
16000
12
11
15
14
16
15
20
19

*Average of four tests on 1/2-in. (12.7mm) plate from a single heat.
**1875F (1024C), rapid cooled.

Average Hardness and Tensile Data, Room Temperature
ConditionFormUltimate
Tensile
Strength,
ksi (MPa)
Yield
Strength
at 0.2%
offset,ksi (MPa)
Elongation
in 2"
percent
Hardness,
Rockwell
Annealed at
1925°F (1052°C),
rapid cooled
Sheet
0.014-0.063"
thick
132.0 (910)67.9 (468)47B94
Annealed at
1925°F (1052°C),
rapid cooled
Sheet,*
0.0.78-0.155"
thick
131.5 (907)67.4 (465)45B97
Annealed at
1925°F (1052°C),
rapid cooled
Plate,***
1/4"
1/2"
3/4"
1.00"
1-1/2"
1-3/4"

132.0 (910)
130.0 (896)
132.3 (912)
127.2 (877)
127.3 (878)
128.0 (883)

65.5 (452)
67.0 (462)
80.0 (552)
75.3 (519)
73.7 (508)
66.0 (455)

46
44
44
42
43
44

B94
B98
B98
B97
B97
C20

*Based on average of 146 tests
**Based on average of 67 tests.
***Based on average of 4 or less tests.

Aged Hardness, Room Temperature*
FormAging Temperature,
F (C)
Aging Tme, hrs.Hardness,
Rockwell A
Plate,
1/2 in. (12.7 mm)
thick
Annealed**--58
1200 (649)1000
4000
8000
68
68
68
1400 (760)1000
4000
8000
65
66
65
1600 (871)1000
4000
8000
60
60
60

*Single tests from a single heat.
**1875F (1024C), rapid cooled.

Average Tensile Data, Room Temperature*
FormAging Temperature,
F (C)
Aging Tme, hrs.Ultimate
Tensile
Strength,
Ksi (MPa)
Yield
Strength
at 0.2%
offset,
Ksi (MPa)
Elongation
in 2 in.,
(50.8 mm),
percent
Plate,
1/2 in. (12.7 mm)
thick
Annealed**--127.7 (880)66.2 (456)46
1200 (649)1000
4000
8000
16000
165.0 (1138)
163.6 (1128)
164.2 (1132)
165.4 (1140)
122.3 (843)
117.9 (813)
117.8 (812)
118.5 (817)
28
24
18
12
1400 (760)1000
4000
8000
16000
142.9 (985)
145.5 (1003)
142.6 (983)
140.4 (968)
95.5 (658)
104.1 (718)
97.4 (672)
96.1 (663)
17
12
13
12
1600 (871)1000
4000
8000
16000
130.0 (896)
130.0 (896)
127.0 (876)
128.4 (885)
68.3 (471)
66.4 (458)
63.7 (439)
63.4 (437)
30
29
26
32

*Average of three tests from a single heat.
**1875F (1024C), rapid cooled.

Average Tensile Data, Sheet*
Test
Temperature,
°F(°C)
Ultimate
Tensile
Strength,
ksi (MPa)
Yield
Strength
at 0.2%
offset,ksi (MPa)
Elongation
in 2"
percent
Room
200
400
600
800
1000
1200
1400
1600
1800
2000
138.8 (957)
133.3 (919)
129.4 (892)
125.6 (866)
122.2 (843)
119.9 (827)
119.6 (825)
88.4 (609)
52.1 (359)
25.0 (172)
13.3 (92)
72.0 (496)
67.3 (464)
62.2 (429)
59.5 (410)
59.2 (408)
58.8 (405)
57.0 (393)
55.3 (381)
34.9 (241)
10.8 (75)
6.1 (42)
38
41
44
45
45
46
47
70
69
108
89

*Annealed at 1925°F (1052°C), rapid cooled.
Average Rupture Data, Sheet*
Test Temperature,
°F(°C)
Average Rupture Strength, ksi (MPa)
for Time Indicated
10 hrs100 hrs1000 hrs
1200 (649)
1400 (760)
1600 (871)
82 (565)
36 (248)
12 (83)
71 (490)
27 (186)
6.7 (46)
60 (414)
20 (138)**
3.7 (26)**

*Annealed at 1925°F (1052°C), rapid cooled.
 

Select AMS Number:

AMS NumberAlloyTypeUNSCross Ref. SpecMisc./Shape
AMS 5715Inconel 601NickelN06601-Bar
AMS 5715Inconel 601NickelN06601-Forging
AMS 5715Inconel 601NickelN06601-Ring
AMS 5870Inconel 601NickelN06601-Plate
AMS 5870Inconel 601NickelN06601-Sheet
AMS 5870Inconel 601NickelN06601-Strip


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