首页> 外国专利> Heat Treatment to Improve Fatigue Strength of Ti-3Al-8V-6Cr-4Mo-4Zr Titanium Alloy

Heat Treatment to Improve Fatigue Strength of Ti-3Al-8V-6Cr-4Mo-4Zr Titanium Alloy

机译:热处理以提高Ti-3Al-8V-6Cr-4Mo-4Zr钛合金的疲劳强度

摘要

In the present invention, high durability (fatigue limit / tensile strength) by improving the fatigue strength of the titanium alloy of β-C type Ti-3Al-8V-6Cr-4Mo-4Zr, which is expected to be applied to high-performance driving parts due to excellent cold workability. ), A heat treatment method was obtained.;In the case of general steel, fatigue limit (fatigue strength) increases or decreases in proportion to mechanical strength such as tensile strength and hardness, but in the present Ti-3Al-8V-6Cr-4Mo-4Zr titanium alloy, The phenomenon is not applied.;Therefore, in the present invention, unlike the heat treatment conditions generally recommended by the engineering data or the manufacturer for the Ti-3Al-8V-6Cr-4Mo-4Zr titanium alloy, 700 ℃ (675 ~ 725 ℃ much lower than the transformation point 793 ℃) Solution is maintained by air cooling after 30 ~ 60 minutes in quenching, and aging treatment is carried out by aging treatment by air cooling after holding at 510 ~ 550 ℃ for 10 ~ 20 hours to maximize fatigue limit (fatigue limit / tensile strength). Improved to about 0.589.
机译:在本发明中,通过改善β-C型Ti-3Al-8V-6Cr-4Mo-4Zr的钛合金的疲劳强度,具有高耐久性(疲劳极限/拉伸强度),有望应用于高性能。出色的冷加工性,使驱动部件更安全。 ),获得了一种热处理方法。;在普通钢的情况下,疲劳极限(疲劳强度)与机械强度(例如拉伸强度和硬度)成正比增加或减少,但在目前的Ti-3Al-8V-6Cr-中因此,在本发明中,与工程数据或制造商通常推荐的Ti-3Al-8V-6Cr-4Mo-4Zr钛合金的热处理条件不同,在本发明中,不应用该现象。 700℃(比转变点793℃低675〜725℃)淬火30〜60分钟后,通过空冷保持溶液,保持在510〜550℃后,通过空冷进行时效处理,进行时效处理。 10到20小时以最大化疲劳极限(疲劳极限/拉伸强度)。改善至约0.589。

著录项

  • 公开/公告号KR970027348A

    专利类型

  • 公开/公告日1997-06-24

    原文格式PDF

  • 申请/专利权人 서상기;

    申请/专利号KR19950043693

  • 发明设计人 김창주;김형욱;박주환;이재문;

    申请日1995-11-21

  • 分类号C22F1/16;

  • 国家 KR

  • 入库时间 2022-08-22 03:17:34

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