TIMETAL 367

Alloy Digest ◽  
2001 ◽  
Vol 50 (12) ◽  
Keyword(s):  
Physical Properties ◽  
Tensile Properties ◽  
Heat Treating ◽  
Alloying Element ◽  
Surgical Implants ◽  
Beta Alloy ◽  
Medium Strength ◽  
Alpha Beta

Abstract TIMETAL 367 is a Ti-6Al-7Nb medium-strength alpha-beta alloy for surgical implants. The alloy is analogous to TIMETAL 367 6-4 (revised as Ti-6Al-4V, Alloy Digest Ti-66, September 1992), but with niobium as the more biocompatible alloying element. This datasheet provides information on composition, physical properties, elasticity, and tensile properties as well as fatigue. It also includes information on heat treating. Filing Code: TI-123. Producer or source: Timet.

TIMETAL 550

Alloy Digest ◽  
1998 ◽  
Vol 47 (7) ◽  
Keyword(s):  
Fracture Toughness ◽  
High Temperature ◽  
Physical Properties ◽  
Tensile Properties ◽  
Heat Treating ◽  
Temperature Performance ◽  
Beta Alloy ◽  
Medium Strength ◽  
Alpha Beta

Abstract TIMETAL 550 is a medium strength forgeable alpha beta alloy for applications in the aerospace and automotive industries. This datasheet provides information on composition, physical properties, and tensile properties as well as fracture toughness, creep, and fatigue. It also includes information on high temperature performance as well as heat treating and joining. Filing Code: TI-112. Producer or source: Titanium Metals Corporation (Timet).

ATI 3-2.5

Alloy Digest ◽  
2020 ◽  
Vol 69 (5) ◽  
Keyword(s):  
Corrosion Resistance ◽  
Physical Properties ◽  
Tensile Properties ◽  
Cold Working ◽  
Heat Treating ◽  
Beta Alloy ◽  
Alpha Beta ◽  
Cold Worked

Abstract ATI 3-2.5 is a Titanium-3Aluminum-2.5Vanadium alloy that has higher strength than unalloyed titanium and is much more amenable to cold working than Ti-6Al-4V. This near-alpha, alpha-beta alloy is generally used in the annealed or cold-worked and stress-relieved conditions. This datasheet provides information on composition, physical properties, elasticity, and tensile properties. It also includes information on corrosion resistance as well as forming, heat treating, machining, and joining. Filing Code: Ti-166. Producer or source: ATI.

TIMETAL 622

Alloy Digest ◽  
1993 ◽  
Vol 42 (1) ◽  
Keyword(s):  
Fracture Toughness ◽  
Fracture Mechanics ◽  
Physical Properties ◽  
Tensile Properties ◽  
Heat Treating ◽  
Beta Alloy ◽  
Alpha Beta

Abstract TIMETAL 622 is useful for damages tolerant designs in airframes and engines. It offers fracture mechanics properties comparable to Ti-6A1-4V Beta Annealed, but with higher strength. Metallurgically, it is an ELI alpha-beta alloy. This datasheet provides information on composition, physical properties, and tensile properties as well as fracture toughness. It also includes information on forming and heat treating. Filing Code: TI-103. Producer or source: Titanium Metals Corporation (Timet).

BRUSH CASTING ALLOY 21C

Alloy Digest ◽  
1992 ◽  
Vol 41 (8) ◽  
Keyword(s):  
Physical Properties ◽  
Tensile Properties ◽  
Copper Alloy ◽  
High Strength ◽  
Heat Treating ◽  
Casting Alloy ◽  
Alloying Element ◽  
Beryllium Copper

Abstract BRUSH CASTING ALLOY 21C is a beryllium copper alloy of high strength with cobalt as the second alloying element (1.0 to 2.0% Co). Use is in age-hardened temper. This datasheet provides information on composition, physical properties, hardness, and tensile properties. It also includes information on casting, heat treating, and machining. Filing Code: Cu-575. Producer or source: Brush Wellman Inc..

COPPER ALLOY No. C61000

Alloy Digest ◽  
1983 ◽  
Vol 32 (5) ◽  
Keyword(s):  
Corrosion Resistance ◽  
Physical Properties ◽  
Tensile Properties ◽  
Copper Alloy ◽  
Heat Treating ◽  
Aluminum Bronze ◽  
Good Resistance ◽  
Medium Strength ◽  
Cold Worked ◽  
Strength Medium

Abstract Copper Alloy No. C61000 is an aluminum bronze containing nominally 92% copper and 8% aluminum. It is characterized by medium strength, medium ductility and a good capacity for being hot formed or cold worked. It has good resistance to corrosion. Its many uses include shafts, pump parts and bolts. This datasheet provides information on composition, physical properties, hardness, elasticity, and tensile properties. It also includes information on corrosion resistance as well as forming, heat treating, and machining. Filing Code: Cu-458. Producer or source: Copper and copper alloy mills.

ALCOA 7020 T651

Alloy Digest ◽  
2006 ◽  
Vol 55 (8) ◽  
Keyword(s):  
Corrosion Resistance ◽  
Physical Properties ◽  
Surface Treatment ◽  
Tensile Properties ◽  
High Strength ◽  
Heat Treating ◽  
Maximum Strength ◽  
Alloying Element ◽  
Engineering Applications ◽  
Aerospace Structures

Abstract Aluminum 7xxx series alloys contain zinc as the main alloying element, usually in combination with magnesium and copper. High-strength 7020 alloy is widely used in aerospace structures and is approved by the world’s leading airframe builders. For engineering applications this alloy is generally used in the T651 temper in order to provide maximum strength. This datasheet provides information on composition, physical properties, and tensile properties. It also includes information on corrosion resistance as well as forming, heat treating, machining, joining, and surface treatment. Filing Code: AL-400. Producer or source: Alcoa Mill Products Inc.

REPUBLIC RS-110A

Alloy Digest ◽  
1963 ◽  
Vol 12 (6) ◽  
Keyword(s):  
Corrosion Resistance ◽  
Titanium Alloy ◽  
Shear Strength ◽  
High Temperature ◽  
Structural Material ◽  
Physical Properties ◽  
Heat Treating ◽  
Alloying Element ◽  
Temperature Performance ◽  
Medium Strength

Abstract Republic RS-110A is a titanium alloy containing manganese as its principle alloying element. The alloy is a medium strength, highly formable sheet alloy which has been used extensively as an aircraft structural material. This datasheet provides information on composition, physical properties, hardness, elasticity, tensile properties, and shear strength. It also includes information on high temperature performance and corrosion resistance as well as forming, heat treating, machining, joining, and surface treatment. Filing Code: Ti-35. Producer or source: Republic Steel Corporation, Titanium Division.

ALLVAC 6Al-6V-2Sn

Alloy Digest ◽  
1991 ◽  
Vol 40 (8) ◽  
Keyword(s):  
Corrosion Resistance ◽  
Titanium Alloy ◽  
Physical Properties ◽  
Tensile Properties ◽  
Heat Treating ◽  
Beta Titanium Alloy ◽  
Beta Titanium ◽  
Stabilizing Effect ◽  
Alpha Beta

Abstract ALLVAC 6A1-6V-2Sn is a highly beta stabilized alpha + beta titanium alloy, a modification of the 6 A1-4V system. Added vanadium plus copper and iron produce the stabilizing effect. This datasheet provides information on composition, physical properties, elasticity, and tensile properties as well as creep. It also includes information on corrosion resistance as well as forming, heat treating, machining, and joining. Filing Code: Ti-98. Producer or source: Teledyne Allvac.

UNS G81150

Alloy Digest ◽  
1990 ◽  
Vol 39 (11) ◽  
Keyword(s):  
Physical Properties ◽  
Tensile Properties ◽  
Alloy Steel ◽  
Heat Treating ◽  
Low Carbon ◽  
Wear Resistant ◽  
Nickel Chromium ◽  
Steel Mills ◽  
Medium Strength ◽  
Strength And Toughness

Abstract UNS G 81150 is a low-carbon nickel-chromium-molybdenum carburizing steel recommended for applications where a core of medium strength and toughness combined with a wear-resistant carburized case is sufficient. It has medium hardenability and can be used without carburizing. This datasheet provides information on composition, physical properties, hardness, elasticity, and tensile properties. It also includes information on forming, heat treating, machining, and joining. Filing Code: SA-453. Producer or source: Alloy steel mills and foundries.

TIMETAL 6-2-4-6

Alloy Digest ◽  
2007 ◽  
Vol 56 (8) ◽  
Keyword(s):  
Physical Properties ◽  
Tensile Properties ◽  
Beta Alloy ◽  
Alpha Beta

Abstract Timetal 6-2-4-6 is an alpha-beta alloy with greater strength in thicker sections than Timetal 6-4. This datasheet provides information on composition, physical properties, elasticity, and tensile properties as well as creep and fatigue. It also includes information on forming. Filing Code: TI-141. Producer or source: Timet.

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