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GH3536 high-temperature alloy is a nickel based alloy with high iron content that has been solid solution strengthened with Cr and Mo elements high temperature alloy, which has good corrosion resistance and oxidation resistance, can be used for a long time at 900 ℃, suitable for manufacturing combustion chamber components of aircraft engines with a short-term working temperature of 1080 ℃ other high-temperature components.
Nome da marca | Jinchun |
Origem | China |
Nome do produto | GH3536 powder |
Aplicação | Combustion chamber components of aircraft engines and other high-temperature components. |
Forma | Pó |
Cor | Metal gray |
Tamanho | 15~53μm |
Padrão | GB/T 19001-2016/ISO9001: 2015 |
Pureza | Ni: Bal. Cr: 20.5-23.0%, Mo:8.0-10.0%, Co:0.5-2.5%,Fe: 17.0-20.0% |
Material | Ni, Cr, Mo, Co, Fe |
Embalagem | Embalagem a vácuo |
Composição química (wt.%) | |||||||||
Elemento | C | Cr | Ni | Co | Mo | Al | Ti | Fe | B |
Padrão | 0.05~0.15 | 20.5~23.0 | Bal. | 0.5~2.5 | 8.0~10.0 | ≤0.50 | ≤0.15 | 17.0~20.0 | ≤0.010 |
typical | 0.08 | 21.94 | Bal. | 1.42 | 8.97 | 0.14 | 0.012 | 18.98 | 0.002 |
Elemento | Mn | P | S | Cu | W | Si | O | N | |
Padrão | ≤1.0 | ≤0.025 | ≤0.015 | ≤0.50 | 0.2-1.0 | ≤1.0 | ≤0.030 | ≤0.030 | |
typical | 0.26 | 0.005 | 0.005 | 0.007 | 0.55 | 0.34 | 0.017 | 0.024 |
GH3536 | 15~53μm Distribuição do tamanho das partículas | Caudal (seg. para 50 g) | Densidade aparente (g/cm3) | Densidade da torneira (g/cm3) | ||
D10 | D50 | D90 | ||||
Padrão | 15~25 | 30~40 | 50~60 | ≤25 | ≥4.2 | ≥4.9 |
typical | 23.4μm | 36.2μm | 55.2μm | 20 | 4.24 | 5.03 |
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