TA19
Brief
Ta19 Composition and Alloy Type
- Nominal Composition: Ti-6Al-2Sn-4Zr-2Mo
- Alloy Type: Near-alpha titanium alloy
- Stabilizing Elements:
- Alpha Stabilizers: Aluminum (Al)
- Neutral Elements: Tin (Sn), Zirconium (Zr)
- Isomorphous Beta Stabilizer: Molybdenum (Mo)
- Eutectoid Beta Stabilizer: Silicon (И)
Elemental Benefits
- Molybdenum (Mo): Enhances room and high-temperature tensile strength and stability
- Aluminum (Al), Tin (Sn), Zirconium (Zr): Combined effect maintains prolonged high-temperature strength and creep resistance
- Silicon (И): Causes precipitation of silicide phase, improving high-temperature creep strength
Performance Characteristics
- High-Temperature Strength: Retains significant strength up to 540°C, superior to TA11 alloy
- Specific Strength: Better than TA14 alloy
- Creep Performance: Comparable to TA14, better than TA11 alloy
- Processing and Welding: Good machinability and weldability
Приложения
- Аэрокосмическая промышленность: Manufacturing of compressor casings in aircraft engines and airplane skins
- Maximum Long-Term Operating Temperature: 500°C
Semi-Finished Products
- Тарелки, стержни, forgings, rings, and castings
Material Grades
- TA19, ZTC6
- Equivalent Grades: Ti-6Al-2Sn-4Zr-2Mo (USA)
Technical Standards
- XJ/BS 5128—1995: Ti-6242 titanium alloy bar technical agreement
- Q/16GJX0-274—1993: Technical conditions for Ti-6242 titanium alloy ring forgings for aero engines
- GJB 2896—1997: Specifications for titanium and titanium alloy investment castings
- AMS 4975G-1994: Solution-aged Ti-6Al-2Sn-4Zr-2Mo-0.08Si titanium alloy bars, провода, and rings
Showing all 2 результаты
Стандартный размер титановой пластины и поставка OEM
Аэрокосмический титановый сплавСтандартный размер листового титана и поставка OEM
Аэрокосмический титановый сплав