DD403
DD403Chemical composition:
Ni | Cr | Co | W | Mo | AI | Ti | C | Fe | Mn | Si | P | S | Cu | |
Min | Bal | 9 | 4.5 | 5 | 3.5 | 5.5 | 1.7 | ≤ | ||||||
Max | 10 | 5.5 | 6 | 4.5 | 6.2 | 2.4 | 0.01 | 0.5 | 0.2 | 0.2 | 0.01 | 0.001 | 0.1 |
DD403Physical properties:
Density | 8.2g/cm³ |
Melting point | 1328℃~1376℃ |
Magnetic properties | not |
Coefficient of linear expansion
θ/℃ | 20~300 | 20~400 | 20~500 | 20~600 | 20~700 | 20~800 | 20~900 | 20~1000 | 20~1100 | |
α/(10-6℃-1) |
[001] | 12.38 | 12.96 | 13.38 | 13.92 | 14.36 | 14.66 | 15.30 | 16.14 | 17.16 |
[011] | 12.47 | 13.02 | 13.42 | 13.72 | 14.22 | 14.72 | 15.35 | 16.19 | 17.16 | |
[111] | 12.62 | 13.19 | 13.55 | 13.82 | 13.95 | 14.82 | 15.47 | 16.37 | 17.35 |
Resilient performance
θ/℃ | 20 | 700 | 750 | 760 | 800 | 850 | 900 | 950 | 980 | 1000 | |
E/GPa |
[001] | 115 | 89 | 82 | 97.5 | 85 | 90.5 | 80 | 74.5 | 64 | 61 |
[011] | -— | 162.0 | 144.0 | —- | 100.5 | 1224 | |||||
[111] | — | — | —— | 217.0 | — | 202.5 | — | 171.0 | 178① |
DD403Mechanical properties:
Standard number | Variety | sampling | Heat treatment | Long-lasting performance | Tensile properties | |||||
θ/℃ | σ/MPa | τ/h | θ/℃ | σ/MPa | δ₅/% | ψ/% | ||||
Q/6S 366 |
Master alloy |
001Monocrystalline test sticks | standardHeat treatment | 760 | 785 | ≥70 | 760 | ≥1030 | ≥3 | ≥3 |
1000 | 195 | ≥70 | 900 | ≥835 | ≥6 | ≥6 | ||||
1040 | 165 | ≥70 | — | — |
DD403Alloy properties:
The surface of HuaNickel DD403 alloy parts needs to be infiltrated with Pt Al coating or M Cr Al Y coating to further improve the oxidation and corrosion resistance of the alloy. After long-term aging at 850°C, no σ phase precipitation was found.
DD403Uses of alloys:
DD403 alloy is suitable for making gas turbine rotor blades operating below 1040°C and guide vanes working below 1100°C. An engine blade made of this alloy has passed the test run and flight test assessment of 3 benches, and has passed the material finalization identification.
DD403Process performance:
Welding process: vacuum brazing or diffusion connection welding.
Parts Heat treatment: notBal blades should be treated at 1250°C, 4h solution treatment under argon protection or vacuum, followed by forced cooling by argon blowing, the cooling rate should be greater than 300°C/min, and then 870°C, 32h aging, argon cooling by blowing.
Relevant standards:
GB/T14992 、Q/6S 366