Ti-5Al-4FeCr

Alloy Digest ◽  
1969 ◽  
Vol 18 (6) ◽  
Keyword(s):  
Heat Treatment ◽  
Fracture Toughness ◽  
Corrosion Resistance ◽  
Titanium Alloy ◽  
High Temperature ◽  
Heat Treating ◽  
Age Hardening ◽  
Temperature Performance ◽  
Alpha Beta ◽  
Hardening Heat Treatment

Abstract Ti-5A1-4FeCr is an alpha-beta type titanium alloy recommended for airframe components. It responds to an age-hardening heat treatment. This datasheet provides information on composition, physical properties, hardness, elasticity, and tensile properties as well as fracture toughness. It also includes information on high temperature performance and corrosion resistance as well as forming, heat treating, machining, and joining. Filing Code: Ti-58. Producer or source: Titanium alloy mills.

ARMCO 17-10P

Alloy Digest ◽  
1958 ◽  
Vol 7 (2) ◽  
Keyword(s):  
Heat Treatment ◽  
Fracture Toughness ◽  
Stainless Steel ◽  
Corrosion Resistance ◽  
High Temperature ◽  
High Strength ◽  
Heat Treating ◽  
Age Hardening ◽  
Temperature Performance ◽  
Hardening Heat Treatment

Abstract ARMCO 17-10P is an austenitic stainless steel that responds favorably to an age-hardening heat treatment. It is recommended for use in applications requiring high strength with low magnetic permeability. This datasheet provides information on composition, physical properties, hardness, elasticity, and tensile properties as well as fracture toughness and fatigue. It also includes information on high temperature performance and corrosion resistance as well as casting, forming, heat treating, machining, joining, and surface treatment. Filing Code: SS-69. Producer or source: Armco Inc., Eastern Steel Division.

COOPER PH-55B

Alloy Digest ◽  
1961 ◽  
Vol 10 (5) ◽  
Keyword(s):  
Heat Treatment ◽  
Fracture Toughness ◽  
Corrosion Resistance ◽  
High Temperature ◽  
High Strength ◽  
Heat Treating ◽  
Age Hardening ◽  
High Ductility ◽  
Temperature Performance ◽  
Hardening Heat Treatment

Abstract COOPER PH-55B is a high-strength high-ductility alloy recommended for corrosion resistance of parts subjected to a combination of stress and shock. It responds to an age-hardening heat treatment. This datasheet provides information on composition, hardness, and tensile properties as well as fracture toughness. It also includes information on high temperature performance and corrosion resistance as well as heat treating, machining, joining, and surface treatment. Filing Code: SS-117. Producer or source: Cooper Alloy Corporation.

ARMCO 17-14 Cu-Mo

Alloy Digest ◽  
1958 ◽  
Vol 7 (1) ◽  
Keyword(s):  
Heat Treatment ◽  
Fracture Toughness ◽  
Stainless Steel ◽  
Corrosion Resistance ◽  
High Temperature ◽  
Austenitic Stainless Steel ◽  
Heat Treating ◽  
Age Hardening ◽  
Temperature Performance ◽  
Hardening Heat Treatment

Abstract ARMCO 17-14 Cu-Mo is an austenitic stainless steel which responds favorably to an age-hardening heat treatment. It is recommended for highly stressed stainless steel parts requiring long service at temperatures up to 1500 F. This datasheet provides information on composition, physical properties, hardness, elasticity, and tensile properties as well as fracture toughness and creep. It also includes information on high temperature performance and corrosion resistance as well as forming, heat treating, machining, joining, and surface treatment. Filing Code: SS-68. Producer or source: Armco Inc., Eastern Steel Division.

ALLVAC 718

Alloy Digest ◽  
1964 ◽  
Vol 13 (4) ◽  
Keyword(s):  
Heat Treatment ◽  
Corrosion Resistance ◽  
High Temperature ◽  
Iron Alloy ◽  
High Strength ◽  
Heat Treating ◽  
Age Hardening ◽  
Nickel Chromium ◽  
Temperature Performance ◽  
Hardening Heat Treatment

Abstract Allvac 718 is a nickel-chromium-iron alloy that responds to an age-hardening heat treatment. It is recommended for parts requiring high strength and oxidation resistance up to about 1300 F and particularly for such parts that require welding. This datasheet provides information on composition, physical properties, hardness, elasticity, and tensile properties. It also includes information on high temperature performance and corrosion resistance as well as forming, heat treating, machining, joining, and surface treatment. Filing Code: Ni-90. Producer or source: Allvac Inc..

ECLIPSALOY 517

Alloy Digest ◽  
1956 ◽  
Vol 5 (11) ◽  
Keyword(s):  
Heat Treatment ◽  
Compressive Strength ◽  
Corrosion Resistance ◽  
High Temperature ◽  
Heat Treating ◽  
Age Hardening ◽  
Casting Alloy ◽  
Good Corrosion Resistance ◽  
Temperature Performance ◽  
Hardening Heat Treatment

Abstract ECLIPSALOY 517 is a cerium-magnesium sand casting alloy having excellent creep resistance up to 500 deg. F. It is suitable for applications where pressure tightness is required and good corrosion resistance is important. It responds to an age-hardening heat treatment. This datasheet provides information on composition, physical properties, hardness, elasticity, tensile properties, and compressive strength as well as creep. It also includes information on high temperature performance and corrosion resistance as well as casting, heat treating, machining, and joining. Filing Code: Mg-29. Producer or source: Bendix Aviation Corporation.

MST 2.5Al-16V

Alloy Digest ◽  
1960 ◽  
Vol 9 (2) ◽  
Keyword(s):  
Heat Treatment ◽  
Corrosion Resistance ◽  
Shear Strength ◽  
High Temperature ◽  
Elevated Temperatures ◽  
Base Alloy ◽  
Heat Treating ◽  
Age Hardening ◽  
Temperature Performance ◽  
Hardening Heat Treatment

Abstract MST 2.5A1-16V is a titanium-base alloy having a favorable combination of strength, formability and resistance to creep at elevated temperatures. It responds to an age-hardening heat treatment. This datasheet provides information on composition, physical properties, elasticity, tensile properties, and compressive and shear strength as well as creep. It also includes information on high temperature performance and corrosion resistance as well as forming, heat treating, machining, and joining. Filing Code: Ti-24. Producer or source: Mallory-Sharon Metals Company.

ALUMINUM 2024

Alloy Digest ◽  
1973 ◽  
Vol 22 (8) ◽  
Keyword(s):  
Heat Treatment ◽  
Corrosion Resistance ◽  
Shear Strength ◽  
High Temperature ◽  
Physical Properties ◽  
High Strength ◽  
Heat Treating ◽  
Age Hardening ◽  
Temperature Performance ◽  
Hardening Heat Treatment

Abstract ALUMINUM 2024 is a high-strength wrought alloy that responds readily to an age-hardening heat treatment. It is recommended for applications requiring highly favorable strength-weight ratios. This datasheet provides information on composition, physical properties, hardness, elasticity, tensile properties, and shear strength as well as fatigue. It also includes information on low and high temperature performance, and corrosion resistance as well as forming, heat treating, and machining. Filing Code: Al-23. Producer or source: Various aluminum companies. Originally published February 1955, revised August 1973.

Ti-13V-11Cr-3Al

Alloy Digest ◽  
1960 ◽  
Vol 9 (10) ◽  
Keyword(s):  
Heat Treatment ◽  
Corrosion Resistance ◽  
High Temperature ◽  
Base Alloy ◽  
High Strength ◽  
Heat Treating ◽  
Age Hardening ◽  
Temperature Performance ◽  
Beta Titanium ◽  
Hardening Heat Treatment

Abstract Ti-13V-11Cr-3Al is a high strength, meta-stable beta titanium-base alloy recommended for service in the temperature range of -65 to plus 600 F. It responds to an age-hardening heat treatment. This datasheet provides information on composition, physical properties, elasticity, and tensile properties as well as creep. 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-27. Producer or source: Titanium Metals Corporation of America.

MAGNESIUM AZ92A

Alloy Digest ◽  
1958 ◽  
Vol 7 (6) ◽  
Keyword(s):  
Heat Treatment ◽  
Corrosion Resistance ◽  
High Temperature ◽  
Heat Treating ◽  
Age Hardening ◽  
Bearing Strength ◽  
Temperature Performance ◽  
Variable Wall Thickness ◽  
Variable Wall ◽  
Hardening Heat Treatment

Abstract MAGNESIUM AZ92A is a good structural magnesium alloy particularly suitable for castings of variable wall thickness. It responds o an age-hardening heat treatment. This datasheet provides information on composition, physical properties, hardness, elasticity, tensile properties, and compressive, shear, and bearing strength as well as creep and fatigue. It also includes information on high temperature performance and corrosion resistance as well as casting, heat treating, machining, and joining. Filing Code: Mg-38. Producer or source: Magnesium foundries.

HYLITE 45

Alloy Digest ◽  
1963 ◽  
Vol 12 (11) ◽  
Keyword(s):  
Heat Treatment ◽  
Corrosion Resistance ◽  
Titanium Alloy ◽  
High Temperature ◽  
High Strength ◽  
Heat Treating ◽  
Beta Titanium Alloy ◽  
Temperature Performance ◽  
Beta Titanium ◽  
Alpha Beta

Abstract Hylite 45 is an alpha-beta titanium alloy that responds to a heat treatment for hardening and strengthening. It is recommended for forgings, etc., where a high strength is required. This datasheet provides information on composition, physical properties, hardness, elasticity, and tensile properties as well as creep and fatigue. It also includes information on high temperature performance and corrosion resistance as well as heat treating, machining, and joining. Filing Code: Ti-37. Producer or source: Jessop-Saville Ltd, Brightside Works.

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