Alloy 725 is a nickel-chromium alloy with significant additions of molybdenum, niobium and titanium. It can be supplied in the hot worked, annealed and age-hardened condition. It is age-hardened to achieve extremely high strength, approximately twice that of Alloy 625 in the annealed condition, through the precipitation of ϒ” phase during a controlled heat treatment process. As this high strength is achieved by ageing rather than cold working, it retains excellent ductility and toughness, and this approach is useful for large or non-uniform sections that cannot be strengthened through cold working.
Alloy 725 has very similar corrosion resistance to Alloy 625, and so is utilised in a wide range of very corrosive environments. The high nickel content ensures resistance to stress corrosion cracking, combined with molybdenum to strongly resist reducing environments such as sulphuric and phosphoric acids, chromium to resist oxidising environments such as nitric acid, titanium to inhibit intergranular corrosion, and overall resistance to pitting and crevice corrosion. The overall combination of alloying elements provides excellent resistance to conditions found in sour oil and gas wells, containing carbon dioxide, chlorides and hydrogen sulphide, and is approved under NACE MR 1075 for such applications.
Specifications:
ASTM B637
UNS N07725
For enquiries about this product, call us on +44 (0)1782 610250
Suitable for use in highly corrosive sour oil and gas wells, approved under NACE MR 1075
Excellent corrosion resistance in a wide variety of corrosive environments including seawater and industrial acids
Age hardened for extremely high strength
Good ductility and toughness
Excellent resistance to stress corrosion cracking
Applications:
Downhole equipment for corrosive/sour service
Oil and gas hangers, connectors
Fasteners, especially in marine applications
Chemical process equipment
Agitators
Valve stems
Chemical Composition:
Cr
Ni
Mo
Co
Nb (+Ta)
Ti
W
Cu
C
Mn
N
Si
P
S
Fe
Al
Min
19.00
55.00
7.00
2.75
1.00
Max
22.50
59.00
9.50
4.00
1.70
0.03
0.35
0.20
0.015
0.01
Bal
0.35
Mechanical Properties:
Bars up to 3” (76mm) diameter or section
Bars greater than 10” (254mm) diameter or section
Bars greater than 10” (254mm) diameter or section
0.2% Proof Stress, min
827 N/mm2
120 ksi
827 N/mm2
120 ksi
827 N/mm2
120 ksi
Tensile strength, min
1034 N/mm2
150 ksi
1034 N/mm2
150 ksi
1034 N/mm2
150 ksi
Elongation, 5.65√S0 and 4D
20%
20%
20%
Reduction of Area
35%
35%
35%
Hardness (Rockwell C)
<43
<43
<43
Impact Strength (-60oC) Longitudinal, Typical
54J av (47J min)
40 ft.lb av (35 ft.lb min)
Impact Strength (-60oC) Transverse, Typical
50J av (43J min)
37 ft.lb av (32 ft.lb min)
43J av (37J min)
32 ft.lb av (27 ft.lb min)
Notes:
Tensile testing shall be carried out in accordance with ASTM A370 or EN10002-1
Minimum properties quoted (tested at room temperature in a longitudinal direction)
Testing performed on each melt of material per heat treatment batch
Physical Properties:
Density (Kg.m-1)
8310
Magnetic Permeability (20°C)
< 1.001
Young’s Modulus (kN/mm2)
204
Poissons Ration
0.31
Specific Heat, 20°C (J/(g.K))
0.43
Electrical Resistivity, 20°C (µΩ-m)
1.144
Thermal conductivity, 20°C (W/(m.K))
10.6
Mean coefficient of thermal expansion, 20-100°C (/K)
13 x 10-6
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