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M50 (AMS 6191) and M50NiL (AMS 6278) High-performance VIM-VAR Melted Bearing Steels for the Aviation Industry

机译:M50(AMS 6191)和M50nil(AMS 6278)用于航空工业的高性能Vim-var熔化轴承钢

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The history of aircraft turbine engine bearings is one of great improvements in reliability and performance. Today's aerospace engineering challenges demand materials which can operate under conditions of temperature extremes, high loads and harsh environments. Progress in steel has followed two parallel paths. One is in steel composition from low alloys to high-speed, fracture-tough, corrosion-resistant compositions. The other path is in steel quality, from electric arc furnace to vacuum and remelting methods, and forging and inspection techniques to prevent stress-raising flaws. This papers reviews some of the key parameters in the production and development of the aircraft bearing steels M50 (AMS 6191) and M50NiL (AMS 6278). The nominal chemistry of the through-hardening M50 high-speed steel type includes (by weight): 0.83% carbon, 4.20% chromium, 4.25% molybdenum and 1.0% vanadium. Careful balancing of these components combined with VIM-VAR melting procedures leads to the following material properties in operation (minimum): hardness > 61HRc, hot hardness at 300°C > 58 HRc, fracture toughness 15 - 20 Mpam{sup}(-1/2), fatigue strength ~1000MPa (3×10{sup}6 cycles). The nominal chemistry of the surface-hardening M50NiL steel type includes (by weight): 0.13% carbon, 4.10% chromium, 4.40% molybdenum, 1.15% vanadium and 3.40 nickel. M50NiL was developed from M50, and VIM-VAR melting procedures also lead to material properties in operation (minimum) of: case hardness > 61HRc, core hardness ~40-45 HRc, fracture toughness (core) > 50 MPam{sup}(-1/2), fatigue strength ~800 MPa (3×10{sup}6 cycles). Several important parameters, such as the VIM procedure and VIM melt "recipe", electrode teeming including launder tundish system, heat treatment and surface conditioning of the electrodes, VAR procedure and VAR melt recipe including the influence of ingot homogenization, must be optimized following the production process to achieve the abovementioned material properties. Results from more than 30 heats from the modern VIDP furnace at Bohler Edelstahl and more than 60 heats from the VAR are discussed. Special attention is given to the influence of the production method on the size and distribution of primary carbides in the finished product. Also, the effects of non-metallic inclusions on the finished product and methods of preventing this are included in this paper. The results of this melting practice are compared with data and details from the literature and competitor's material and results. Case study of the material in use is considered at the end of this paper.
机译:飞机涡轮发动机轴承的历史是可靠性和性能的巨大改进之一。今天的航空航天工程挑战需要在极端温度,高负荷和恶劣环境的条件下运行的材料。钢的进展跟随两个平行路径。一种是从低合金的钢结构到高速,骨折坚硬,耐腐蚀组合物。另一条路以钢材质量,从电弧炉到真空和重熔方法,以及锻造和检查技术,以防止延长应力缺陷。本文审查了一些主要参数在飞机钢材M50(AMS 6191)和M50nil(AMS 6278)的生产和开发中。通过硬化M50高速钢型的标称化学物质包括(按重量):0.83%碳,4.20%铬,4.25%钼和1.0%钒。这些组分的仔细平衡与Vim-var熔化程序相结合,导致操作中的以下材料特性(最小):硬度> 61Hrc,300℃下的热硬度58小时,断裂韧性15-20mpam {sup}( - 1 / 2),疲劳强度〜1000MPa(3×10 {SUP} 6循环)。表面硬化M50nil钢型的标称化学包括(按重量):0.13%碳,4.10%铬,4.40%钼,1.15%钒和3.40镍。 M50nil是从M50开发的,Vim-Var熔化程序还导致操作中的材料性能(最小):壳体硬度> 61Hrc,核心硬度〜40-45 HRC,断裂韧性(核心)> 50 mpam {sup}( - 1/2),疲劳强度〜800MPa(3×10 {SUP} 6个循环)。包括vim手术和vim熔体“配方”等几个重要参数,包括洗衣房系统,热处理和电极表面调理,var程序和var熔体配方,包括铸锭均匀化的影响,必须优化生产过程实现上述材料特性。讨论了来自Bohler Edelstahl的现代VIDP炉的30多个热量的结果和来自VAR的超过60个热量。特别注意生产方法对成品中原代碳化物尺寸和分布的影响。此外,本文还包括非金属夹杂物对成品和预防其方法的影响。将该熔化实践的结果与文献和竞争对手的材料和结果的数据和细节进行比较。在本文末尾考虑了对使用中材料的案例研究。

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