TIMETAL ® 10-2-3
2Pages

TIMETAL® 10-2-3 HIGH-STRENGTH FORGING ALLOY TIMETAL 10-2-3 is a TIMET developed, high-strength, deep hardenable forging alloy useful for airframes and engines. Metallurgical^ it is a near beta alloy. It offers the opportunity to use near-net shape forging techniques and has excellent strength-toughness combinations. TIMETAL 10-2-3 has very high fatigue life and is well-suited for safe-life designs. Current applications for TIMETAL 10-2-3 encompass numerous aircraft structural parts, including landing gear components. CHEMICAL COMPOSITION ELEMENT WEIGHT % PHYSICAL PROPERTIES Residual Elements, each — 0.10 Residual Elements, total — 0.13 Titanium Remainder GUARANTEED MINIMUM MECHANICAL PROPERTIES SOLUTION TREATED THEN AGED 8 HRS AMS Aging Temperature Section Tensile Strength Yield Strength Elongation Reduction Toughness Specification °F (°C) Thickness in (cm) ksi (MPa) ksi (MPa) % in 2 in in Area % ksiVin (MPaVm) HEAT TREATMENT TYPICAL K1C TREND WITH STRENGTH LEVEL Solution Heat 50°-100°F (28°-56°C) below beta Treatment transus for a minimum of 30 minutes, then water quench (air cool may be used for parts less than 1 inch [2.5cm] thick) Ultimate Tensile Strength ksi (MPa) K1C ksi Vin (MPaVm) Treatment for 8 hrs, air cool Typical K1SCC Results from Forging, STA Condition K1CksiVin (MPaVm) K1SCCksiVin (MPaVm)

TYPICAL ELEVATED TEMPERATURE MECHANICAL PROPERTIES SOLUTION TREATED THEN AGED AT 950°F (510°C) FOR 8 HRS Test Ultimate Tensile Strength 0.2 % Yield Strength Elongation Reduction Tensile Modulus Temperature °F (°C) ksi (MPa) ksi (MPa) % in 2 in in Area % Msi (GPa) MINIMUM COMPRESSION, SHEAR AND BEARING STRENGTH DIE FORGINGS; ksi (MPa) SOLUTION TREATED AND AGED; L, LT, AND ST ORIENTATION Heat Treated Per: Property AMS 4984 AMS 4986 AMS 4987 Compression Yield Strength 166 (1145) 150 (1034) 134 (924) Shear Ultimate Strength 97 (669) 90...