ECONOMICALLY ALLOYED TITANIUM ALLOY WITH PREDICTABLE PROPERTIES

    公开(公告)号:EP3196321A4

    公开(公告)日:2018-05-16

    申请号:EP15842559

    申请日:2015-09-02

    IPC分类号: C22C14/00

    摘要: This invention relates to non-ferrous metallurgy, namely to the development of titanium alloys, which, due to their advantageous properties, can be used not only for traditional applications, e.g. defense industry, but also for civil applications. The alloy consists of 0.1 to 3.0 Al, 0.3 to 3.0 Fe, 0.1 to 1.0 Cr, 0.05 to 1.0 Ni, 0.02 to 0.3 Si, 0.02 to 0.2 N, 0.05 to 0.5 O, 0.02 to 0.1 C, and balance Ti. A technical result is a competitive titanium alloy with the guaranteed stable predictable properties which is made using low-grade titanium sponge. The result is achieved with the help of alloying elements which consist of impurities as part of low-grade sponge and separately introduced alloy additions. This titanium-base alloy is characterized by the lower costs as compared with the existing commercial alloys, with the alloy composition selected based on the required physical, mechanical and processing properties. 1 claim, 11 tables.

    METHOD FOR MANUFACTURING DEFORMED ARTICLES FROM PSEUDO- BETA-TITANIUM ALLOYS
    2.
    发明公开
    METHOD FOR MANUFACTURING DEFORMED ARTICLES FROM PSEUDO- BETA-TITANIUM ALLOYS 有权
    的生产方法形变文章从伪BETA-钛合金

    公开(公告)号:EP2623628A4

    公开(公告)日:2016-06-29

    申请号:EP11829668

    申请日:2011-09-23

    IPC分类号: C22F1/18

    CPC分类号: C22F1/183 C22C14/00 C22F1/18

    摘要: This invention relates to nonferrous metallurgy, namely to thermomechanical processing of titanium alloys and can be used for manufacturing structural parts and assemblies of high-strength pseudo-²-titanium alloys in aerospace engineering, mainly for landing gear and airframe application. The method for thermomechanical processing of titanium alloy items consisting of, in weight percentages, 4.0 - 6.0 aluminum, 4.5 - 6.0 vanadium, 4.5 - 6.0 molybdenum, 2.0 - 3.6 chromium, 0.2 - 0.5 iron, 2.0 max. zirconium, 0.2 max. oxygen and 0.05 max. nitrogen is proposed. The method consists of multiple heating operations to a temperature that is above or below beta transus temperature (BTT), hot working with the specified strain and cooling. A technical result of this method is manufacture of near-net shape forgings with stable properties having sections with thickness 100 mm and over and length over 6 m with the guaranteed level of the following mechanical properties: 1. Ultimate tensile strength over 1200 MPa with fracture toughness, K 1C , not less than 35MPaˆšm. 2. Fracture toughness, K 1C , over 70 MPaˆšm with ultimate tensile strength not less than 1100 MPa.

    SECONDARY TITANIUM ALLOY AND METHOD FOR MANUFACTURING SAME
    4.
    发明公开
    SECONDARY TITANIUM ALLOY AND METHOD FOR MANUFACTURING SAME 审中-公开
    SEKUNDÄRETITANLEGIERUNG UND HERSTELLUNGSVERFAHRENDAFÜR

    公开(公告)号:EP2527478A4

    公开(公告)日:2017-05-24

    申请号:EP10844080

    申请日:2010-12-31

    IPC分类号: C22C14/00 C22B9/20 C22C1/02

    摘要: This invention relates to production of ±-, near ±- and ±+²-titanium alloys from secondary raw materials, which are used mainly in manufacture of sheet material, structural parts and structural armor for defense and civil sectors. This alloy is characterized by the following chemical composition, weight percentage: 0.01-6.5 Al, 0.01-5.5 V, 0.05 - 2.0 Mo, 0.01 - 1.5 Cr, 0.1 - 2.5 Fe, 0.01-0.5 Ni, 0.01-0.5 Zr, 0.01-0.25 Si, oxygen - up to 0.3, carbon - up to 0.1, nitrogen - up to 0.07 and titanium - remainder. Blend is formulated based on the required tensile strength, while content of alloying elements is calculated based on design value of aluminum and molybdenum strength equivalents. The proposed alloy and the art of its manufacture helps to solve a problem of introduction of a wide range of titanium wastes to make a finished product with the required processing and structural behavior.

    摘要翻译: 本发明涉及由二次原材料生产±,近±和±+²-钛合金,其主要用于防御和民用部门的片材,结构部件和结构装甲的制造。 该合金的特征在于以下化学组成,重量百分比:0.01-6.5 Al,0.01-5.5 V,0.05-2.0 Mo,0.01-1.5 Cr,0.1-2.5 Fe,0.01-0.5 Ni,0.01-0.5 Zr, 0.25硅,氧 - 最多0.3,碳 - 最多0.1,氮 - 最多0.07,钛 - 余量。 基于所需的拉伸强度配制混合物,而合金元素的含量则根据铝和钼强度等价物的设计值计算。 所提出的合金及其制造技术有助于解决引入各种钛废料的问题,以制成具有所需加工和结构行为的成品。