Titanium 6Al4V Titanium Alloys Mechanical Chemical Physical Properties Titanium Grades 1 2 3 4 5 7 9 11 12 19 Beta C Titanium 6Al4V Titanium Alloys Mechanical Chemical Physical Properties Titanium Grades 1 2 3 4 5 7 9 11 12 19 Beta C

Titanium 6Al4V Titanium Alloys Mechanical Chemical Physical Properties Titanium Grades 1 2 3 4 5 7 9 11 12 19 Beta C Titanium 6Al4V Grades Titanium Alloys Mechanical Chemical Physical Properties Ti 6-2-4-2 Titanium Grades 1 2 3 4 5 7 9 11 12 19 Beta C Ti 15-3-3-3 Titanium 6Al4V IMI 685 Titanium Alloys Mechanical Chemical Physical Properties IMI 829 Titanium Grades 1 2 3 4 5 7 9 11 12 19 Beta C CP Grade 1 CP Grade 12 CP Grade 2 CP Grade 3 CP Grade 4 CP Grade 7 / 11 / 16 Grade 5 / ELI / 23 Grade 9 / 18 Grade 19 / 20 titanioum , titan, titane, titanio, tianium, titaium, titanim, titaniom, titanium, titanum, titnium, ttanium, t1tan1um, titanium, titamium, titanimu, titanuim, titainum, titnaium, tiatnium, ttianium, ittanium, titaniu, titanim, titanum, titaium, titnium, tianium, ttanium, itanium, titaniom

- about Ti - Introduction Ind. Specification Medical Specification Applications Characteristics Classification Markets Corrosion Engineering Fabrication   - Ti Grades - Introduction Ti 6-2-4-2 Ti 15-3-3-3 Ti 13Nb-13Zr IMI 685 IMI 829 SMA CP Grade 1 CP Grade 12 CP Grade 2 CP Grade 3 CP Grade 4 CP Grade 7 / 11 / 16 6Al4V Grade 5 / 23 6Al7Nb Alloy Grade 9 / 18 Alloy Grade 19 / 20   - Ti Products - Introduction Fine Wire - Cable Foil Sheet / Plate Titanium Targets Tube Oilfield Tubes

» Titanium IMI 685

Titanex supplies this HIGH-TEMPERATURE, HIGH-STRENGTH CREEP RESISTANT ALLOY as a wire with max. 12 mm diameter. Ti-6Al-5Zr-0.5Mo-0.25Si is a near alpha alloy, combines excellent tensile strength with high temperature (968°F / 520°C) creep resistance. It is a weldable alloy that has good forging characteristics - forging temperatures above the beta transus can be used. The alloy may be joined by the processes normally used in the fabrication of titanium, including argon-arc, electron beam and friction welding. Material should be fully heat treated prior to welding, and also given a suitable post-weld treatment (exam-ple 4-8hrs at 1022°F / 550°C). The weld zone of material treated in this way will have similar structure and properties to the parent metal. IMI 685 alloy was specifically developed for the aero-engine industry.

Composition Physical Data Mechanical Data Fabrication Information

» Composition

C	< 0.08 %
N2	< 0.03 %
O2	< 0.2 %
H2	< 0.01 %
Al	5.7 - 6.3 %
Zr	4.5-6 %
Mo	0.25-0.75 %
Si	0.015-0.35 %
Ti =	Rem

» Physical Data

	Minimum	Typical
Density g/cm3 (lb/cu.in)		4.45(0.161)
Thermal Conductivity W/mK	2.4
*Mean Thermal Exp. Coeff. 0-100°C/°C		9.7-10.1 x 10 -6
Beta Transus °C+/-15°C(°F)		1020 (1868)

» Mechanical Data

	Minimum	Typical
Tensile Strength MPa(ksi)		1030 (149)
0.2% Proof Stress MPa(ksi)		900 (131)
Elongation over 2 Inches %		10
Reduction in Area %		20
Elastic Modulus GPa(Msi)		125 (18.1)
@ 520 °C	Minimum	Typical
Tensile Strength MPa(ksi)		670 (97)
0.2% Proof Stress MPa(ksi)		525 (76)
Elongation over 2 Inches %		12
Reduction in Area %		36

» HEAT TREATMENT

Treatment Temperature [°F (°C)] Time Hours Cooling Method

Solution Heat Treatment

1922°F (1050°C) / 30 minutes / Oil Quench*

Aging Heat Treatment

1022°F (550°C) /24 hours / Air Cool

Titanium Tantalum Molybdenum Niobium Zirconium Tungsten
Tel CH: +41 444 6353 82 Tel DE: +49 7424 9699616
REACH, RoHS compliant - Conflict Free Materials © 1994-2024 Titanex GmbH Switzerland
 

Titanium 6Al4V

Titanium Alloys Mechanical Chemical Physical Properties

Titanium Grades 1 2 3 4 5 7 9 11 12 19 Beta C

Titanium 6Al4V