| タイトル | Low Density, High Creep Resistant Single Crystal Super Alloy for Turbine Airfoils |
| 本文（外部サイト） | http://hdl.handle.net/2060/20080009750 |
| 著者（英） | Smialek, James L.; MacKay, Rebecca A.; Gabb, Timothy P.; Nathal, Michael V. |
| 著者所属（英） | NASA Glenn Research Center |
| 発行日 | 2007-08-28 |
| 言語 | eng |
| 内容記述 | A nickel-base superalloy article for use in turbines has increased creep resistance and lower density. The superalloy article includes, as measured in % by weight, 6.0-12.0% Mo, 5.5-6.5%Al, 3.0-7.0% Ta, 0-15% Co, 2.0-6.0% Cr, 1.0-4.0% Re, 0-1.5% W, 0-1.5% Ru, 0-2.0% Ti, 0-3.0% Nb, 0-0.2% Hf, 0-0.02% Y, 0.001-0.005% B, 0.01-0.04% C, and a remainder including nickel plus impurities. |
| NASA分類 | Metals and Metallic Materials |
| 権利 | No Copyright |
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