GH135
GH135 Chemical composition:
Fe | Cr | Ni | W | Mo | AI | Ti | C | B | Ce | Mn | Si | P | S | |
Min | Bal | 14 | 33 | 1.7 | 1.7 | 2 | 2.1 | |||||||
Max | 16 | 36 | 2.2 | 2.2 | 2.8 | 2.5 | 0.08 | 0.015 | 0.03 | 0.4 | 0.5 | 0.02 | 0.02 |
GH135 Physical properties:
Density | 7.92g/cm³ |
Coefficient of expansion
θ/℃ | 20~100 | 20~200 | 20~300 | 20~400 |
α/(10~5℃-I) | 15.0 | 15.2 | 15.5 | 15.7 |
θ/℃ | 20~500 | 20~600 | 20~700 | 20~800 |
α/(10-6℃-1) | 15.9 | 16.2 | 16.5 | 17.6 |
Thermal conductivity
θ/℃ | 100 | 200 | 300 | 400 | 500 |
α/[W/(m·℃) | 10.9 | 13.0 | 14.6 | 16.3 | 18.0 |
θ/℃ | 600 | 700 | 800 | 900 | |
α/[W/(m·℃)] | 19.7 | 21.8 | 23.0 | 24.3 |
Resilient performance
θ/℃ | 20 | 100 | 200 | 300 | 400 | 500 |
Ed/GPa | 200 | 196 | 189 | 183 | 176 | 169 |
G/GPa | 79.4 | 76.4 | 72.5 | 70.6 | 66.6 | 62.7 |
θ/℃ | 600 | 700 | 750 | 800 | 900 | — |
Ed/GPa | 165 | 150 | 155 | 147 | 134 | |
G/GPa | 60.8 | 58.8 | 57.8 | 56.8 |
GH135 Mechanical properties:
Standard number |
Variety |
State |
Room temperature performance | Long-lasting performance | |||||||
σb/MPa | σpo.2/MPa | δ₅/% | ψ/% | aku/kJ/m² |
HBS |
θ/℃ | σ/MPa | τ/h | |||
≥ | ≥ | ||||||||||
GB/T14997
GJB3020 |
Round cake ring blank | Standard heat treatment | 880 | 590 | 13 | 16 | 290 | 321~255 |
750 |
345 | 50 |
805 | 590 | 10 | 13 | 290 | 321~255 | 295 | 100 | ||||
GJB5301 | Rings | Standard heat treatment |
805 |
590 |
10 |
13 |
290 |
321~255 |
750 |
345 | 50 |
295 | 100 | ||||||||||
Standard number |
variety |
State |
Tensile properties at 700°C |
HBS |
Long-lasting performance | ||||||
σb/MPa | σpo.2/MPa | δ₅/% | ψ/% | θ/℃ | σ/MPa | τ/h | |||||
≥ | ≥ | ||||||||||
YB/T5245 | Rods | Standard heat treatment |
784 |
15 |
20 |
352~277 |
700 |
431 | 60 | ||
412 | 80 |
GH135 Alloy properties:
GH135 alloy can save w(Ni)41% and w(Cr) 5.5% compared with nickel-based alloys for similar purposes. After long-term aging above 800°C, the alloy has needle-like σ phase precipitation in the crystal, and Laves phase precipitation in the grain boundary.
GH135 Uses of alloys:
GH135 alloy has been used to make two types of aero engine I and II turbine discs, and two types of fighters are equipped for use in the field. China’s first 3,000-horsepower gas turbine flame cylinder made of alloy plates was installed on the “Long March 1” locomotive and passed the test of more than 300 hours of operation. The alloy can also be made of hot stamping dies working at 750°C~850°C, such as forging hammer anvils and hydraulic press anvils or insert anvils, hot stamping dies, etc.
GH135 Process performance:
Welding process:HuaNickel GH135 alloy can be connected by automatic argon arc welding, contact welding, manual argon arc welding and other methods.
Relevant standards:
GB/T 14992 、GB/T14997、GJB 3020A 、GJB 5301 、YB/T5245 、YB/T 5247