製品特性:...
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.
ブランド名 | ジンチュン |
起源 | 中国 |
商品名 | GH3536 powder |
申し込み | Combustion chamber components of aircraft engines and other high-temperature components. |
形状 | パウダー |
カラー | Metal gray |
サイズ | 15~53μm |
スタンダード | GB/T 19001-2016/ISO9001: 2015 |
純度 | Ni: Bal. Cr: 20.5-23.0%, Mo:8.0-10.0%, Co:0.5-2.5%,Fe: 17.0-20.0% |
素材 | Ni, Cr, Mo, Co, Fe |
梱包 | 真空包装 |
化学組成 (wt.%) | |||||||||
エレメント | C | Cr | ニー | Co | モ | アル | ティ | フェ | B |
スタンダード | 0.05~0.15 | 20.5~23.0 | バル | 0.5~2.5 | 8.0~10.0 | ≤0.50 | ≤0.15 | 17.0~20.0 | ≤0.010 |
typical | 0.08 | 21.94 | バル | 1.42 | 8.97 | 0.14 | 0.012 | 18.98 | 0.002 |
エレメント | ムン | P | S | 銅 | W | Si | O | N | |
スタンダード | ≤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 粒度分布 | 流量 秒(50gの場合) | 見掛け密度(g/cm3) | タップ密度(g/cm3) | ||
D10 | D50 | D90 | ||||
スタンダード | 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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