首页 馆藏资源 舆情信息 标准服务 科研活动 关于我们
现行 ASM Ti-84
到馆提醒
收藏跟踪
购买正版
RMI 8Al-1Mo-1V - High Temperature Alloy RMI 8Al-1Mo-1V-高温合金
发布日期: 1982-02-01
查看样本合金摘要数据表(PDF)自1952年以来,合金摘要一直是世界各地使用的金属和合金材料性能数据的主要参考。以图表、图表和表格为特色,这些表格给出了有关成分或特性、物理和机械性能、热处理和可加工性的事实和数字。RMI 8A1-1Mo-1V是一种α-β钛合金,在工厂退火条件下的抗拉强度为135000 psi。它具有良好的抗拉强度和抗蠕变性能,适用于1000华氏度的环境。建议用于需要高强度且具有优异抗蠕变性能和韧性的飞机和喷气发动机零件。
View Sample Alloy Digest Data Sheet (PDF)Since 1952, Alloy Digest has been the leading reference for materials property data on metals and alloys used throughout the world. Featuring graphs, charts and tables, these sheets give facts and figures on composition or characterization, physical and mechanical properties, heat treatment, and machinability.RMI 8A1-1Mo-1V is an alpha-beta titanium alloy with a tensile strength of 135,000 psi in the mill-annealed condition. It has an excellent combination of tensile strength and creep resistance that makes it suitable for service to 1000 F. It is recommended for aircraft and jet-engine parts requiring high strength with superior creep resistance and toughness.
分类信息
关联关系
研制信息
相似标准/计划/法规