Titanium VT1-2

  • Titanium VT1-0
  • Titanium VT1-00
  • Titanium VT1-1
  • Titanium VT1-2

    • Designation

    Name The value
    Designation GOST Cyrillic ВТ1-2
    Designation GOST Latin BT1-2
    Transliteration VT1-2
    By chemical elements ВTe1-2

    Description

    Titanium VT1−2 is used: for the manufacture of semi-finished products (sheets, strips, foils, strips, plates, bars, rods, profiles, tubes, forgings and forged blanks) by the strain, as well as ingots used in the aircraft industry for production of various parts; stamping parts billet heating up to 300−400 °C.

    Note

    Parts subjected to in-process and final annealing regime: annealing at a temperature of 550−600 °C for 10−15 minutes exposure to 1 mm thickness, and air cooling.

    Standards

    Name Code Standards
    Non-ferrous metals, including rare, and their alloys В51 GOST 19807-91, TU 1-83-39-79, TU 1-83-40-79
    Bars В55 GOST 26492-85, OST 1 90266-86

    Chemical composition

    Standard C Si Fe N Ti O H
    GOST 19807-91 ≤0.1 ≤0.15 ≤1.5 ≤0.15 Rest ≤0.3 ≤0.01
    Ti is the basis.
    According to GOST 19807-91, the total content of other impurities is ≤0.30%. The mass fraction of hydrogen is indicated for ingots. The mass fraction of chromium and manganese should not exceed 0.15% (in total). The mass fraction of copper and nickel should not be more than 0.10% (in total), including nickel not more than 0.08%.

    Mechanical properties

    Section, mm σU, MPa d5, % y, % KCU, kJ/m2 HB, MPa
    Bars hot rolled autogenie ordinary quality GOST 26492-85 (longitudinal samples)
    65-100 590-930 ≥8 ≥17 ≥245 -
    Bars hot rolled autogenie for OST 1 90266-86 (samples of the longitudinal location of cutting of the samples is 1/2R)
    ≥110 590-930 ≥8 ≥17 ≥245 179-255
    65-100 590-930 ≥10 ≥25 ≥245 179-255

    Description mechanical marks

    Name Description
    σU Limit short-term strength
    d5 Elongation after rupture
    y The relative narrowing
    KCU Toughness
    HB Brinell hardness number