High-temperature alloys are a class of metal materials that exhibit excellent performance in high-temperature environments. They are widely used in aerospace, petrochemical, energy, and other high-temperature industrial fields. Traditional metal materials often experience creep, oxidation, erosion, and corrosion issues under high-temperature conditions, while high-temperature alloys can maintain good mechanical properties, oxidation resistance, and corrosion resistance under these extreme conditions.
Here are several common high-temperature alloy grades:
A286: A286 high-temperature alloy is an iron-based alloy that possesses excellent high-temperature strength and oxidation resistance. It can be used for long periods at temperatures around 700°C and exhibits good creep and fracture toughness. A286 is commonly used in the manufacturing of bolts, springs, and other structural components operating at high temperatures.
Nimonic 80A: Nimonic 80A is a nickel-based high-temperature alloy that offers excellent high-temperature strength and creep resistance. It can be used for long periods at temperatures around 815°C and exhibits good oxidation and corrosion resistance. Nimonic 80A is commonly used in the manufacturing of turbine blades, combustion chamber components, and heat exchangers operating at high temperatures.
Nimonic 90: Nimonic 90 is a nickel-based high-temperature alloy that provides high strength and good oxidation resistance. It can be used for long periods at temperatures around 950°C and exhibits good corrosion resistance. Nimonic 90 is commonly used in the manufacturing of nozzles, combustion chamber components, and turbine components operating at high temperatures.
GH1140: GH1140 is an iron-based high-temperature alloy that offers good high-temperature strength and oxidation resistance. It can be used for long periods at temperatures around 1000°C and exhibits good corrosion resistance. GH1140 is commonly used in the manufacturing of bolts, springs, and other structural components operating at high temperatures.
GH3625: GH3625 is a nickel-based high-temperature alloy that provides excellent high-temperature strength and oxidation resistance. It can be used for long periods at temperatures around 1050°C and exhibits good corrosion resistance. GH3625 is commonly used in the manufacturing of combustion chamber components, turbine blades, and heat treatment equipment operating at high temperatures.
These high-temperature alloy grades play important roles in their respective application fields and provide reliable material solutions for industries and aerospace sectors operating in high-temperature environments.
Item
|
A-286
|
Nimonic80A
|
Nimonic 90
|
GH1140
|
GH3625
|
GH3536
|
GH4169
|
C
|
≤0.08
|
≤0.1
|
≤0.13
|
0.06-0.12
|
≤0.1
|
0.05-0.15
|
≤0.08
|
Mn
|
≤2
|
≤1
|
≤1
|
≤0.7
|
3.14-4.15
|
--
|
≤0.35
|
Fe
|
rest
|
≤3
|
≤1.5
|
rest
|
≤0.5
|
--
|
rest
|
P
|
≤0.04
|
≤0.02
|
--
|
≤0.025
|
--
|
--
|
--
|
S
|
≤0.03
|
≤0.015
|
≤0.015
|
≤0.015
|
--
|
--
|
≤0.01
|
Si
|
≤1
|
≤1
|
≤1
|
≤0.8
|
--
|
--
|
≤0.35
|
Cu
|
--
|
--
|
≤0.2
|
--
|
--
|
--
|
≤0.3
|
Ni
|
24-27
|
rest
|
--
|
35-40
|
rest
|
rest
|
50-55
|
Co
|
--
|
≤2
|
15-21
|
--
|
≤1.00
|
0.5-2.5
|
≤1.00
|
Al
|
≤0.35
|
1-1.8
|
1-2
|
0.2-0.6
|
≤0.4
|
≤0.5
|
0.2-0.8
|
Ti
|
1.9-2.35
|
1.8-2.7
|
2-3
|
0.7-1.2
|
≤0.4
|
≤0.15
|
0.7-1.15
|
Cr
|
13.5-16
|
18-21
|
18-21
|
20-23
|
20-23
|
20.5-23
|
17-21
|
Nb
|
--
|
--
|
--
|
--
|
--
|
--
|
4.75-5.5
|
Mo
|
1-1.5
|
--
|
--
|
2-2.5
|
8-10
|
8-10
|
2.8-3.3
|
B
|
0.001-0.1
|
≤0.008
|
≤0.02
|
--
|
--
|
--
|
--
|
V
|
0.1-0.5
|
--
|
--
|
--
|
--
|
--
|
--
|
W
|
--
|
--
|
--
|
1.4-1.8
|
--
|
0.2-1
|
--
|
Zr
|
--
|
≤0.15
|
≤0.15
|
--
|
--
|
--
|
--
|
Pb
|
--
|
--
|
≤0.002
|
--
|
--
|
--
|
--
|
Ce
|
--
|
--
|
--
|
≤0.05
|
--
|
--
|
--
|