Titanium, Titanium Alloy Sheet AMS 4911 (Gr5Ti-6Al-4V

Titanium, Titanium Alloy Sheet AMS 4911 (Gr5Ti-6Al-4V Ti6Al4V, also known as grade 5, Ti-6Al-4V or Ti 6-4, is the most commonly used titanium alloy. It has a chemical composition of 6% aluminum, 4% vanadium, 0.25% (maximum) iron, 0.2% (maximum) oxygen, and the remainder titanium. It is significantly stronger than commercially pure titanium while having the same stiffness and thermal properties (excluding thermal conductivity, which is about 60% lower in Grade 5 Ti than in CP Ti). Among its many advantages, it is heat treatable. This grade is an excellent combination of strength, corrosion resistance, weld and fabric ability. This alpha-beta alloy is the workhorse alloy of the titanium industry. The alloy is fully heat treatable in section sizes up to 15mm and is used up to approximately 400°C (750°F). Over 70% of all alloy grades melted are a sub-grade of Ti6Al4V, its uses vary in many aerospace airframe and engine component uses and also major non-aerospace applications in the marine, offshore and power generation industries in particular. Generally, Ti-6Al-4V is used in applications up to 400 degrees Celsius. It has a density of roughly 4420 kg/m3, Young's modulus of 110 GPa, and tensile strength of 1000 Mpa. By comparison, annealed type 316 stainless steel has a density of 8000 kg/m3, modulus of 193 GPa, and tensile strength of only 570 Mpa. While tempered 6061 aluminum alloy has 2700 kg/m3, 69 GPa, and 310 MPa, respectively. Titanium AMS 4911 BarsMill anneal 1300-1450°F 2 hours, air cool. Re-crystallization anneal bar for better ductility and fatigue strength, 1750°F 2 hours, furnace cool. For maximum fracture toughness and stress corrosion cracking resistance (SCC), Beta anneal 1950°F 1-2 hours, water quench. Then age 1150-1300°F 2 to 4 hours, air cool. For maximum strength, solution-treated and aged (STA) condition is: For sheet, 1675-1725°F 5 to 25 minutes, water quench. Age 975°F 4 to 6 hours, air cool. For bars and forgings, 1675-1725°F 1 hour, water quench. Age 975-1025°F 3 hours, air cool. For increased fracture toughness, but lower tensile strength, precipitation treat (overage) 1150-1250°F 4 hours, air cool. Stress relief annealing is commonly 1000-1200°F 1 to 4 hours, air cool. Ti 6Al-4V is susceptible to chloride (SCC), although being among the better of the titanium alloys in this regard. For marine environments silver plated bolts are not used, as silver bonds easily with chlorine in this environment. Ti 6Al-4V is also susceptible to SCC in environments such as methyl alcohol, red fuming HNO3, and N2O4. In the case of red fuming nitric acid, the problem is limited to environments containing less than 1.5% water, or more than 6% NO2. Failure in N2O4 has occurred when oxygen and chlorides were present as impurities. Ti-6Al-4V is the alloy most commonly used in wrought and cast forms. Palladium or ruthenium can be added for increased corrosion resistance. Most properties are affected by the microstructure, which is determined by the thermo-mechanical history. It is highly resistant to general corrosion in sea water. This alloy is available in most common product forms including billet, bar, wire, plate, and sheet. Ti-6Al-4V has Excellent biocompatibility, especially when direct contact with tissue or bone is required. Ti-6Al-4V's poor shear strength makes it undesirable for bone screws or plates. It also has poor surface wear properties and tends to seize when in sliding contact with itself and other metals. Surface treatments such as nitriding and oxidizing can improve the surface wear properties.

MS 4928, AMS 4911, AMS 2631, AMS 4901, AMS 4907, AMS 4919

MS 4928, AMS 4911, AMS 2631, AMS 4901, AMS 4907, AMS 4919

AMS 4911 Titanium Plate Annealed Gr5 Ti-6Al-4v

AMS 4911 Titanium Plate Annealed Gr5 Ti-6Al-4v phone-icon 800-521-0332 email-icononlinesales@rolledalloys.comchat-icon Chat Now! 6AL-4V PRODUCT INFORMATION 6Al-4V Data Sheet Request A Quote JUMP TO 6Al-4V Chemistry 6Al-4V Features 6Al-4V Applications 6Al-4V Physical Properties 6Al-4V Mechanical Properties MARKETS Medical Aerospace Oil and Gas 6Al-4V Ti 6Al-4V is the most widely used of all the alpha-beta titanium alloys. It is typically used in the annealed condition, at service temperatures through 750°F. However it may be heat treated for high strength in sections under 4" thick. Hardenability is limited and sections over one inch may not develop full properties. Ti 6Al-4V is welded with matching or with ELI filler wire. Mill anneal 1300-1450°F 2 hours, air cool. Recrystallization anneal bar for better ductility and fatigue strength, 1750°F 2 hours, furnace cool. For maximum fracture toughness and SCC resistance, Beta anneal 1950°F 1-2 hours, water quench. Then age 1150-1300°F 2 to 4 hours, air cool. For maximum strength, solution-treated and aged (STA) condition is: For sheet, 1675-1725°F 5 to 25 minutes, water quench. Age 975°F 4 to 6 hours, air cool. For bars and forgings, 1675-1725°F 1 hour, water quench. Age 975-1025°F 3 hours, air cool. For increased fracture toughness, but lower tensile strength, precipitation treat (overage) 1150-1250°F 4 hours, air cool. Stress relief annealing is commonly 1000-1200°F 1 to 4 hours, air cool. Ti 6Al-4V is resistant to general corrosion but may be quickly attacked by environments that cause breakdown of the protective oxide. These include hydrofluoric (HF), hydrochloric (HCl), sulfuric and phosphoric acids. Inhibitors may help for the last four but not for HF. Ti 6Al-4V resists attack by pure hydrocarbons, and most chlorinated and fluorinated hydrocarbons (provided water has not caused formation of small amounts of HCl and HF). Ti 6Al-4V is susceptible to chloride stress corrosion cracking (SCC), although being among the better of the titanium alloys in this regard. For marine environments silver plated bolts are not used, as silver bonds easily with chlorine in this environment. Ti 6Al-4V is also susceptible to SCC in environments such as methyl alcohol, red fuming HNO3, and N2O4. In the case of red fuming nitric acid, the problem is limited to environments containing less than 1.5% water, or more than 6% NO2. Failure in N2O4 has occurred when oxygen and chlorides were present as impurities.

TI 6-4 Titanium Alloy (Ti-6Al-4V; ASTM Grade 5) Sheet

TI 6-4 Titanium Alloy (Ti-6Al-4V; ASTM Grade 5) Sheet 6Al-4V Ti 6Al-4V is the most widely used of all the alpha-beta titanium alloys. It is typically used in the annealed condition, at service temperatures through 750°F. However it may be heat treated for high strength in sections under 4" thick. Hardenability is limited and sections over one inch may not develop full properties. Ti 6Al-4V is welded with matching or with ELI filler wire. Mill anneal 1300-1450°F 2 hours, air cool. Recrystallization anneal bar for better ductility and fatigue strength, 1750°F 2 hours, furnace cool. For maximum fracture toughness and SCC resistance, Beta anneal 1950°F 1-2 hours, water quench. Then age 1150-1300°F 2 to 4 hours, air cool. For maximum strength, solution-treated and aged (STA) condition is: For sheet, 1675-1725°F 5 to 25 minutes, water quench. Age 975°F 4 to 6 hours, air cool. For bars and forgings, 1675-1725°F 1 hour, water quench. Age 975-1025°F 3 hours, air cool. For increased fracture toughness, but lower tensile strength, precipitation treat (overage) 1150-1250°F 4 hours, air cool. Stress relief annealing is commonly 1000-1200°F 1 to 4 hours, air cool. Ti 6Al-4V is resistant to general corrosion but may be quickly attacked by environments that cause breakdown of the protective oxide. These include hydrofluoric (HF), hydrochloric (HCl), sulfuric and phosphoric acids. Inhibitors may help for the last four but not for HF. Ti 6Al-4V resists attack by pure hydrocarbons, and most chlorinated and fluorinated hydrocarbons (provided water has not caused formation of small amounts of HCl and HF). Ti 6Al-4V is susceptible to chloride stress corrosion cracking (SCC), although being among the better of the titanium alloys in this regard. For marine environments silver plated bolts are not used, as silver bonds easily with chlorine in this environment. Ti 6Al-4V is also susceptible to SCC in environments such as methyl alcohol, red fuming HNO3, and N2O4. In the case of red fuming nitric acid, the problem is limited to environments containing less than 1.5% water, or more than 6% NO2. Failure in N2O4 has occurred when oxygen and chlorides were present as impurities.

Titanium 6-4 UNS R56400

Titanium 6-4 UNS R56400 Ti6Al4V, also known as grade 5, Ti-6Al-4V or Ti 6-4, is the most commonly used titanium alloy. It has a chemical composition of 6% aluminum, 4% vanadium, 0.25% (maximum) iron, 0.2% (maximum) oxygen, and the remainder titanium. It is significantly stronger than commercially pure titanium while having the same stiffness and thermal properties (excluding thermal conductivity, which is about 60% lower in Grade 5 Ti than in CP Ti). Among its many advantages, it is heat treatable. This grade is an excellent combination of strength, corrosion resistance, weld and fabric ability. This alpha-beta alloy is the workhorse alloy of the titanium industry. The alloy is fully heat treatable in section sizes up to 15mm and is used up to approximately 400°C (750°F). Over 70% of all alloy grades melted are a sub-grade of Ti6Al4V, its uses vary in many aerospace airframe and engine component uses and also major non-aerospace applications in the marine, offshore and power generation industries in particular. Generally, Ti-6Al-4V is used in applications up to 400 degrees Celsius. It has a density of roughly 4420 kg/m3, Young's modulus of 110 GPa, and tensile strength of 1000 Mpa. By comparison, annealed type 316 stainless steel has a density of 8000 kg/m3, modulus of 193 GPa, and tensile strength of only 570 Mpa. While tempered 6061 aluminum alloy has 2700 kg/m3, 69 GPa, and 310 MPa, respectively. Titanium AMS 4911 BarsMill anneal 1300-1450°F 2 hours, air cool. Re-crystallization anneal bar for better ductility and fatigue strength, 1750°F 2 hours, furnace cool. For maximum fracture toughness and stress corrosion cracking resistance (SCC), Beta anneal 1950°F 1-2 hours, water quench. Then age 1150-1300°F 2 to 4 hours, air cool. For maximum strength, solution-treated and aged (STA) condition is: For sheet, 1675-1725°F 5 to 25 minutes, water quench. Age 975°F 4 to 6 hours, air cool. For bars and forgings, 1675-1725°F 1 hour, water quench. Age 975-1025°F 3 hours, air cool. For increased fracture toughness, but lower tensile strength, precipitation treat (overage) 1150-1250°F 4 hours, air cool. Stress relief annealing is commonly 1000-1200°F 1 to 4 hours, air cool. Ti 6Al-4V is susceptible to chloride (SCC), although being among the better of the titanium alloys in this regard. For marine environments silver plated bolts are not used, as silver bonds easily with chlorine in this environment. Ti 6Al-4V is also susceptible to SCC in environments such as methyl alcohol, red fuming HNO3, and N2O4. In the case of red fuming nitric acid, the problem is limited to environments containing less than 1.5% water, or more than 6% NO2. Failure in N2O4 has occurred when oxygen and chlorides were present as impurities. Ti-6Al-4V is the alloy most commonly used in wrought and cast forms. Palladium or ruthenium can be added for increased corrosion resistance. Most properties are affected by the microstructure, which is determined by the thermo-mechanical history. It is highly resistant to general corrosion in sea water. This alloy is available in most common product forms including billet, bar, wire, plate, and sheet. Ti-6Al-4V has Excellent biocompatibility, especially when direct contact with tissue or bone is required. Ti-6Al-4V's poor shear strength makes it undesirable for bone screws or plates. It also has poor surface wear properties and tends to seize when in sliding contact with itself and other metals. Surface treatments such as nitriding and oxidizing can improve the surface wear properties.

6AL-4V titanium alloy (Grade 5) Aviation Metals

Titanium 6AL-4V (AB1) 6AL-4V titanium alloy (Grade 5) is the most widely used titanium grade. Its high strength, light weight and corrosion resistance enables Ti 6-4 to be used in many applications. The most common market is aerospace. The alloy is also age hardenable by heat treatment to achieve even higher strengths. Some applications include compressor blades, discs, and rings for jet engines; airframe components; pressure vessels; rocket engine cases; helicopter rotor hubs and critical forgings requiring high strength-to-weight ratios. Properties: Non-magnetic. A two-phase alloy, containing both alpha and beta phase crystalline structures. This high strength alloy can be used at cryogenic temperatures to about 800°F (427°C). AMS 4928 requires 120,000 psi minimum yield strength at room temperature. 6AL-4V titanium can be used in the annealed condition or in the solution treated and aged condition. 6Al-4V titanium has outstanding corrosion resistance to most media including nitric acid in all concentrations to boiling point; seawater; and to alkalis in all concentrations to boiling point. Stress corrosion cracking may occur if chlorine salts are present on stressed parts subsequently subjected to high temperatures. 6Al-4V titanium has acceptable oxidation resistance up to 1000°F (538°C). Hardness: Hardness of Aerodyne stock is typically 300 BHN. The strength and hardness of the mill-annealed product may be increased by approximately 20% after an aging heat treatment. After aging at 975-1025°F (524-552°C), the typical yield strength is 150,000 psi and typical hardness is 360 BHN. Machinability: RATING: 22% of B-1112 TYPICAL STOCK REMOVAL RATE: 30 surface feet/minute COMMENTS: Tooling should consist of tungsten carbide designations C1-C4 or cobalt type high speed tools. Generally, machining characteristics are similar to those of austenitic stainless steels. 6Al-4V titanium can be machined using slow speeds, high feed rates, rigid tooling, and flooding the workpiece with non-chlorinated cutting fluid. Density: 0.160 lbs/in3, 4.47 g/cm3

AMS-4911 | Titanium Alloy, Sheet, Strip, and Plate, 6Al - 4V

AMS-4911 | Titanium Alloy, Sheet, Strip, and Plate, 6Al 4V

ti-6al-4v ams 4911 high purity titanium alloy sheet gr5

ti-6al-4v ams 4911 high purity titanium alloy sheet gr5

Titanium Alloy Grade 5 / Ti 6Al-4V - Aircraft Materials

Titanium Alloy Grade 5 / Ti 6Al-4V - Aircraft Materials Titanium Grade 5 (Ti6Al-4V) is the most commonly used alloy. Ti6Al4V is significantly stronger than other commercially pure titanium whilst still retaining the same stiffness and thermal properties (excluding thermal conductivity). Titanium Grade 5 extensively used in Aerospace, Medical, Marine and Chemical Processing.

AMS4911: Titanium Alloy, Sheet, Strip, and Plate, 6Al - 4V

AMS4911: Titanium Alloy, Sheet, Strip, and Plate, 6Al - 4V Ti6Al4V, also known as grade 5, Ti-6Al-4V or Ti 6-4, is the most commonly used titanium alloy. It has a chemical composition of 6% aluminum, 4% vanadium, 0.25% (maximum) iron, 0.2% (maximum) oxygen, and the remainder titanium. It is significantly stronger than commercially pure titanium while having the same stiffness and thermal properties (excluding thermal conductivity, which is about 60% lower in Grade 5 Ti than in CP Ti). Among its many advantages, it is heat treatable. This grade is an excellent combination of strength, corrosion resistance, weld and fabric ability. This alpha-beta alloy is the workhorse alloy of the titanium industry. The alloy is fully heat treatable in section sizes up to 15mm and is used up to approximately 400°C (750°F). Over 70% of all alloy grades melted are a sub-grade of Ti6Al4V, its uses vary in many aerospace airframe and engine component uses and also major non-aerospace applications in the marine, offshore and power generation industries in particular. Generally, Ti-6Al-4V is used in applications up to 400 degrees Celsius. It has a density of roughly 4420 kg/m3, Young's modulus of 110 GPa, and tensile strength of 1000 Mpa. By comparison, annealed type 316 stainless steel has a density of 8000 kg/m3, modulus of 193 GPa, and tensile strength of only 570 Mpa. While tempered 6061 aluminum alloy has 2700 kg/m3, 69 GPa, and 310 MPa, respectively. Titanium AMS 4911 BarsMill anneal 1300-1450°F 2 hours, air cool. Re-crystallization anneal bar for better ductility and fatigue strength, 1750°F 2 hours, furnace cool. For maximum fracture toughness and stress corrosion cracking resistance (SCC), Beta anneal 1950°F 1-2 hours, water quench. Then age 1150-1300°F 2 to 4 hours, air cool. For maximum strength, solution-treated and aged (STA) condition is: For sheet, 1675-1725°F 5 to 25 minutes, water quench. Age 975°F 4 to 6 hours, air cool. For bars and forgings, 1675-1725°F 1 hour, water quench. Age 975-1025°F 3 hours, air cool. For increased fracture toughness, but lower tensile strength, precipitation treat (overage) 1150-1250°F 4 hours, air cool. Stress relief annealing is commonly 1000-1200°F 1 to 4 hours, air cool. Ti 6Al-4V is susceptible to chloride (SCC), although being among the better of the titanium alloys in this regard. For marine environments silver plated bolts are not used, as silver bonds easily with chlorine in this environment. Ti 6Al-4V is also susceptible to SCC in environments such as methyl alcohol, red fuming HNO3, and N2O4. In the case of red fuming nitric acid, the problem is limited to environments containing less than 1.5% water, or more than 6% NO2. Failure in N2O4 has occurred when oxygen and chlorides were present as impurities. Ti-6Al-4V is the alloy most commonly used in wrought and cast forms. Palladium or ruthenium can be added for increased corrosion resistance. Most properties are affected by the microstructure, which is determined by the thermo-mechanical history. It is highly resistant to general corrosion in sea water. This alloy is available in most common product forms including billet, bar, wire, plate, and sheet. Ti-6Al-4V has Excellent biocompatibility, especially when direct contact with tissue or bone is required. Ti-6Al-4V's poor shear strength makes it undesirable for bone screws or plates. It also has poor surface wear properties and tends to seize when in sliding contact with itself and other metals. Surface treatments such as nitriding and oxidizing can improve the surface wear properties.

Titanium Ti-6Al-4V (Grade 5), Annealed AMS 4928 AMS

Titanium Ti-6Al-4V (Grade 5), Annealed AMS 4928 AMS

Titanium Ti 6AL 4V - AMS 4911

Titanium Ti 6AL 4V - AMS 4911 Ti6Al4V, also known as grade 5, Ti-6Al-4V or Ti 6-4, is the most commonly used titanium alloy. It has a chemical composition of 6% aluminum, 4% vanadium, 0.25% (maximum) iron, 0.2% (maximum) oxygen, and the remainder titanium. It is significantly stronger than commercially pure titanium while having the same stiffness and thermal properties (excluding thermal conductivity, which is about 60% lower in Grade 5 Ti than in CP Ti). Among its many advantages, it is heat treatable. This grade is an excellent combination of strength, corrosion resistance, weld and fabric ability. This alpha-beta alloy is the workhorse alloy of the titanium industry. The alloy is fully heat treatable in section sizes up to 15mm and is used up to approximately 400°C (750°F). Over 70% of all alloy grades melted are a sub-grade of Ti6Al4V, its uses vary in many aerospace airframe and engine component uses and also major non-aerospace applications in the marine, offshore and power generation industries in particular. Generally, Ti-6Al-4V is used in applications up to 400 degrees Celsius. It has a density of roughly 4420 kg/m3, Young's modulus of 110 GPa, and tensile strength of 1000 Mpa. By comparison, annealed type 316 stainless steel has a density of 8000 kg/m3, modulus of 193 GPa, and tensile strength of only 570 Mpa. While tempered 6061 aluminum alloy has 2700 kg/m3, 69 GPa, and 310 MPa, respectively. Titanium AMS 4911 BarsMill anneal 1300-1450°F 2 hours, air cool. Re-crystallization anneal bar for better ductility and fatigue strength, 1750°F 2 hours, furnace cool. For maximum fracture toughness and stress corrosion cracking resistance (SCC), Beta anneal 1950°F 1-2 hours, water quench. Then age 1150-1300°F 2 to 4 hours, air cool. For maximum strength, solution-treated and aged (STA) condition is: For sheet, 1675-1725°F 5 to 25 minutes, water quench. Age 975°F 4 to 6 hours, air cool. For bars and forgings, 1675-1725°F 1 hour, water quench. Age 975-1025°F 3 hours, air cool. For increased fracture toughness, but lower tensile strength, precipitation treat (overage) 1150-1250°F 4 hours, air cool. Stress relief annealing is commonly 1000-1200°F 1 to 4 hours, air cool. Ti 6Al-4V is susceptible to chloride (SCC), although being among the better of the titanium alloys in this regard. For marine environments silver plated bolts are not used, as silver bonds easily with chlorine in this environment. Ti 6Al-4V is also susceptible to SCC in environments such as methyl alcohol, red fuming HNO3, and N2O4. In the case of red fuming nitric acid, the problem is limited to environments containing less than 1.5% water, or more than 6% NO2. Failure in N2O4 has occurred when oxygen and chlorides were present as impurities. Ti-6Al-4V is the alloy most commonly used in wrought and cast forms. Palladium or ruthenium can be added for increased corrosion resistance. Most properties are affected by the microstructure, which is determined by the thermo-mechanical history. It is highly resistant to general corrosion in sea water. This alloy is available in most common product forms including billet, bar, wire, plate, and sheet. Ti-6Al-4V has Excellent biocompatibility, especially when direct contact with tissue or bone is required. Ti-6Al-4V's poor shear strength makes it undesirable for bone screws or plates. It also has poor surface wear properties and tends to seize when in sliding contact with itself and other metals. Surface treatments such as nitriding and oxidizing can improve the surface wear properties.

6Al-4V Titanium Alloy, AMS 4911, Ti6Al4V, UNS R56400

6Al-4V Titanium Alloy, AMS 4911, Ti6Al4V, UNS R56400 i6Al4V, also known as grade 5, Ti-6Al-4V or Ti 6-4, is the most commonly used titanium alloy. It has a chemical composition of 6% aluminum, 4% vanadium, 0.25% (maximum) iron, 0.2% (maximum) oxygen, and the remainder titanium. It is significantly stronger than commercially pure titanium while having the same stiffness and thermal properties (excluding thermal conductivity, which is about 60% lower in Grade 5 Ti than in CP Ti). Among its many advantages, it is heat treatable. This grade is an excellent combination of strength, corrosion resistance, weld and fabric ability. This alpha-beta alloy is the workhorse alloy of the titanium industry. The alloy is fully heat treatable in section sizes up to 15mm and is used up to approximately 400°C (750°F). Over 70% of all alloy grades melted are a sub-grade of Ti6Al4V, its uses vary in many aerospace airframe and engine component uses and also major non-aerospace applications in the marine, offshore and power generation industries in particular. Generally, Ti-6Al-4V is used in applications up to 400 degrees Celsius. It has a density of roughly 4420 kg/m3, Young's modulus of 110 GPa, and tensile strength of 1000 Mpa. By comparison, annealed type 316 stainless steel has a density of 8000 kg/m3, modulus of 193 GPa, and tensile strength of only 570 Mpa. While tempered 6061 aluminum alloy has 2700 kg/m3, 69 GPa, and 310 MPa, respectively. Mill anneal 1300-1450°F 2 hours, air cool. Re-crystallization anneal bar for better ductility and fatigue strength, 1750°F 2 hours, furnace cool. For maximum fracture toughness and stress corrosion cracking resistance (SCC), Beta anneal 1950°F 1-2 hours, water quench. Then age 1150-1300°F 2 to 4 hours, air cool. For maximum strength, solution-treated and aged (STA) condition is: For sheet, 1675-1725°F 5 to 25 minutes, water quench. Age 975°F 4 to 6 hours, air cool. For bars and forgings, 1675-1725°F 1 hour, water quench. Age 975-1025°F 3 hours, air cool. For increased fracture toughness, but lower tensile strength, precipitation treat (overage) 1150-1250°F 4 hours, air cool. Stress relief annealing is commonly 1000-1200°F 1 to 4 hours, air cool. Ti 6Al-4V is susceptible to chloride (SCC), although being among the better of the titanium alloys in this regard. For marine environments silver plated bolts are not used, as silver bonds easily with chlorine in this environment. Ti 6Al-4V is also susceptible to SCC in environments such as methyl alcohol, red fuming HNO3, and N2O4. In the case of red fuming nitric acid, the problem is limited to environments containing less than 1.5% water, or more than 6% NO2. Failure in N2O4 has occurred when oxygen and chlorides were present as impurities. Ti-6Al-4V is the alloy most commonly used in wrought and cast forms. Palladium or ruthenium can be added for increased corrosion resistance. Most properties are affected by the microstructure, which is determined by the thermo-mechanical history. It is highly resistant to general corrosion in sea water. This alloy is available in most common product forms including billet, bar, wire, plate, and sheet. Ti-6Al-4V has Excellent biocompatibility, especially when direct contact with tissue or bone is required. Ti-6Al-4V's poor shear strength makes it undesirable for bone screws or plates. It also has poor surface wear properties and tends to seize when in sliding contact with itself and other metals. Surface treatments such as nitriding and oxidizing can improve the surface wear properties.

TC21 Titanium Alloy for Aviation

TC21 Titanium Alloy for Aviation

High Strength Titanium Alloy TC21

High Strength Titanium Alloy TC21