Nimonic 105
Referred Standards
1.Composition(wt%)
C
|
Cr
|
Ni
|
Fe
|
Mo
|
Cu
|
Al
|
Ti
|
≦0.17
|
14.0- 15.7
|
balance
|
≦1.0
|
4.5-5.5
|
≦0.2
|
4.5-4.9
|
0.9-1.5
|
Co
|
Zr
|
B
|
Mn
|
Si
|
S
|
Pb
|
- |
18.0-22.0
|
≦0.15
|
0.003-0.01
|
≦1.0
|
≦1.0
|
≦0.015
|
≦0.0015
|
- |
2.Physical Properties
Density
(g/cm3)
|
Melting point
(℃)
|
Specific heat capacity
(J/kg·℃)
|
Thermal conductivity
(9W/m·°C)
|
8.01
|
1290-1345
|
419
|
10.8
|
3.Mechanical Properties
Instantaneous rupture properties(bar,typical hot treatment).
Test temperature
℃
|
Tensile strength
MPa
|
Yield strength
(0.2yield point)MPa
|
Elongation
%
|
Shrinkage of area
%
|
Kinetic Young;s modulus
GPa
|
20
|
1140
|
776
|
22
|
31
|
189
|
300
|
1091
|
735
|
20
|
30
|
174
|
600
|
1038
|
720
|
25
|
38
|
154
|
900
|
496
|
400
|
30
|
47
|
129
|
1000
|
175
|
152
|
42
|
73
|
110
|
1100
|
51
|
29
|
172
|
99
|
-
|
High temperature endurance properties(bar,typical hot treatment)
Test temperature
℃
|
Test time
h
|
Burst pressure
MPa
|
Elongation
%
|
750
|
100
|
456
|
12-18
|
815
|
100
|
324
|
8-21
|
870
|
100
|
208
|
7-17
|
940
|
100
|
108
|
10-21
|
980
|
100
|
68
|
12-22
|
4.Applications
Used for high temperature gas turbine components. |