Type
Analysis
Element
|
Min
|
Max
|
Carbon
|
--
|
0.03
|
Nickel
|
58 MIN.
|
Chromium
|
20.0
|
23.0
|
Iron
|
--
|
5.00
|
Silicon
|
--
|
0.15
|
Manganese
|
--
|
0.50
|
Sulfur
|
--
|
0.015
|
Phosphorus
|
--
|
0.015
|
Molybdenum
|
8.00
|
10.0
|
Titanium
|
--
|
0.40
|
Cobalt
|
--
|
1.00
|
Columbium + Tantalum
|
3.15
|
4.15
|
Aluminum
|
--
|
0.40
|
Nitrogen
|
--
|
0.02
|
Description
Alloy 625LCF is a nonmagnetic , corrosion
- and oxidation-resistant, nickel-based alloy. It was developed as a
bellows quality version of Alloy 625 and also offers superior fatigue resistance.
Its outstanding strength and toughness in the temperature range cryogenic to 2000°F
(1093°C) are derived primarily from the solid solution effects of
the refractory metals, columbium and molybdenum, in a nickel-chromium
matrix. The alloy has excellent fatigue strength and stress-corrosion
cracking resistance to chloride ions. Some typical applications for
alloy 625LCF have included heat shields, furnace hardware, gas turbine
engine ducting, combustion liners and spray bars, chemical plant
hardware, and special seawater applications.
Corrosion
Resistance
Alloy 625 has withstood many
corrosive environments. In alkaline, salt water, fresh water, neutral
salts, and in the air, almost no attack occurs. The nickel and
chromium provide resistance to oxidizing environments. Nickel and
molybdenum provide for resistance to nonoxidizing atmospheres.
Pitting and crevice corrosion are prevented by molybdenum. Niobium
stabilizes the alloy against sensitization during welding. Chloride
stress-corrosion cracking resistance is excellent. The alloy resists
scaling and oxidation at high temperatures.
Pickling
Sodium hydride baths are necessary to
descale this alloy. After the sodium hydride treatment, the material
should be immersed in a sulfuric acid bath 165°F (74°C) for
approximately 3 minutes. A 25-minute immersion in a
nitric-hydrofluoric bath 145°F (63°C) is then necessary.
Rinse. Sulfuric solution: 16% by weight, H2SO4.
Nitric solution: 8% HNO3 by weight and 3% HF by
weight. Acid etching for macro-inspection-expose material
electrolytically to a 3-to-1 HCl to HNO3
solution, saturated with CuCl2 at a current
density of 0.645 amp/in² (25.4 A/m)
Physical Properties
Physical
Property
|
°C
|
Metric
Units
|
°F
|
British
Units
|
Density
|
22
|
8.44 g/cubic cm
|
72
|
0.305 lb/cubic in.
|
Electrical
Resistivity
|
20 100 200 300 400 500 600 700
|
1.29
microhm-m 1.32 1.34 1.35 1.36 1.37 1.38 1.38
|
70 200 400 600 800 1000 1200
|
50.7
microhm-in. 51.9 50.4 52.7 53.1 53.5 54.3 54.3
|
Mean
Coefficient of Thermal Expansion
|
100 200 300 400 500 600 700
|
12.8 x
10(-6)m/m-°C 13.1 13.3 13.7 13.9 14.4 14.9
|
200 400 600 800 1000 1200
|
7.1
microinches/in.-°F 7.3 7.4 7.6 7.8 8.2
|
Thermal Conductivity
|
-150 -100 -50 20 100 200 300 400 500 600 700
|
7.4
W/M-°C 7.9 8.7 9.7 11.0 12.4 13.8 15.3 16.9 18.3 19.8
|
-250 -200 -100 0 70 200 400 600 800 1000 1200
|
50
Btu-in./ft².-hr.-°F 52 58 64 68 75 87 98 109 121 132
|
Specific Heat
|
20 100 200 300 400 500 600 700
|
410
J/kg-°C 429 454 479 502 528 553 578
|
0 70 200 400 600 800 1000 1200
|
0.096
Btu/lb-°F 0.098 0.102 0.109 0.115 0.122 0.128 0.135
|
Average
Dynamic Modulus of Elasticity *
TEMPERATURE F
|
Young's Modulus ksi x 10^3
|
Shear Modulus ksi x 10^3
|
Poisson's Ratio mu
|
70 200 400 600 800 1000 1200
|
30.1 29.6 28.7 27.8 26.9 25.9 24.7
|
11.8 11.6 11.1 10.8 10.4 9.9 9.4
|
0.28 0.28 0.29 0.29 0.29 0.31 0.31
|
Average
Hardness and Tensile Data, Room Temperature
Condition
|
Form
|
Ultimate 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 0.014-0.100" thick
|
132.0 (910)
|
67.9 (468)
|
47
|
B94
|
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 hrs
|
100 hrs
|
1000 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. **Extrapolated
Workability
Hot
Working Hot working may done at 2100°F (1149°C)
maximum furnace temperature. Care should be exercised to avoid
frictional heat build-up which can result in overheating, exceeding
2100°F (1149°C). Alloy 625 becomes very stiff at temperatures
below 1850°F (1010°C). Work pieces that fall below this
temperature should be reheated. Uniform reductions are recommended to
avoid the formation of a duplex grain structure. Approximately 15/20%
reduction is recommended for finishing.
Cold
Forming Alloy 625 can be cold formed by standards methods.
When the material becomes too stiff from cold working, ductility can
be restored by process anneal.
Machineability Low cutting speeds, rigid tools and work piece, heavy equipment, ample coolant and positive feeds are
general recommendations.
High-Speed
Cutting Tools for Lathe Turning Operations
Angle
|
Roughing
|
Finishing
|
Back rake Positive
side rake End clearance End cutting edge Side cutting
edge
|
0°
6° 6° --
|
8° 14-18° 8° 25° Up
to 45°
|
Cutting
Speeds for High-Speed Steels
Operation
|
Speed
|
Feed
|
sfpm
|
m/s
|
ipr
|
mm/rev
|
Turning Drilling
(.500"/12.70mm) Tapping Milling Reaming
|
12-20 10-12 5-10 10-20 8-10
|
0.06/.010 0.05/0.06 0.03/0.05 0.05/0.10 0.04/0.05
|
0.010 0.006/0.010 -- -- --
|
0.25 0.15/0.25 -- -- --
|
Carbide tools
should have smaller angles than high-speed tools and operating speeds
can be higher. A sulfur-based cutting fluid is recommended. Thoroughly
clean work piece after machining to prevent surface contamination
during subsequent heat treating. Chlorine additives would be an
alternative.
Weldability Welding
can be accomplished by the gas-shielded processes using a tungsten
electrode or a consumable electrode. Postweld heat treatment of the
weld are not necessary to maintain corrosion resistance. Heavy
restrained sections can be welded and the weld's mechanical
properties follow the same trends as base metal properties. Standard
practices such as clean surfaces, good joint alignment, U-joints for
thicker sections, etc., should be followed.
|