CMW 1000

Alloy Digest ◽  
2000 ◽  
Vol 49 (6) ◽  

Abstract CMW 1000, also known as NO-CHAT, is a tungsten bearing sintered alloy of high density and high strength. It is a powder metallurgy product and one of a series of alloys with densities 50% greater than lead. This datasheet provides information on composition, physical properties, hardness, elasticity, tensile properties, and compressive and bend strength as well as fracture toughness and fatigue. It also includes information on high temperature performance and corrosion resistance as well as machining and joining. Filing Code: W-2. Producer or source: CMW Inc. Originally published as Mallory 1000, November 1954, revised June 2000.

Alloy Digest ◽  
2000 ◽  
Vol 49 (7) ◽  

Abstract CMW 2000 is a tungsten-bearing sintered alloy of high density and high strength. It is a powder metallurgical product and one of a series of alloys with densities 50% greater than lead. This datasheet provides information on composition, physical properties, hardness, tensile properties, and compressive and bend strength as well as fracture toughness and fatigue. It also includes information on high temperature performance and corrosion resistance as well as machining and joining. Filing Code: W-5. Producer or source: CMW Inc. Originally published as Mallory 2000, October 1963, revised July 2000.


Alloy Digest ◽  
2000 ◽  
Vol 49 (9) ◽  

Abstract CMW 3950 is a tungsten bearing sintered alloy of high density and high strength. It is a powder metallurgical product and one of a series of alloys with densities 50% greater than lead. This datasheet provides information on composition, physical properties, hardness, elasticity, tensile properties, and compressive and bend strength as well as fracture toughness and fatigue. It also includes information on high temperature performance and corrosion resistance as well as machining and joining. Filing Code: W-11. Producer or source: CMW Inc. Originally published as Mallory 3950, March 1968, revised September 2000.


Alloy Digest ◽  
1967 ◽  
Vol 16 (4) ◽  

Abstract Magnesium ZK60A is a heat treatable extrusion and forging alloy recommended for applications where high strength with good toughness are required. This datasheet provides information on composition, physical properties, elasticity, tensile properties, and compressive, shear, bearing, and bend strength 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: Mg-62. Producer or source: The Dow Chemical Company.


Alloy Digest ◽  
1964 ◽  
Vol 13 (1) ◽  

Abstract GYROMET is a rungsten-bearing sintered alloy of high strength and density recommended for rotor applications. This datasheet provides information on composition, physical properties, hardness, elasticity, tensile properties, and compressive and bend strength 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: W-6. Producer or source: Mallory Metallurgical Company.


Alloy Digest ◽  
1990 ◽  
Vol 39 (2) ◽  

Abstract ARMCO PH 13-8Mo is designed for high-performance applications requiring high strength coupled with excellent resistance to corrosion and stress corrosion. It has excellent toughness, good transverse properties and excellent forgeability. This datasheet provides information on composition, physical properties, hardness, elasticity, and tensile properties as well as fracture toughness. It also includes information on low and high temperature performance, and corrosion resistance as well as forming, heat treating, machining, and joining. Filing Code: SS-224. Producer or source: Baltimore Specialty Steels Corporation. Originally published May 1969, revised February 1990.


Alloy Digest ◽  
2001 ◽  
Vol 50 (9) ◽  

Abstract Ti-6Al-2Sn-2Zr-2Mo-0.05Si alloy is used as heavy section forgings that require high strength, fracture toughness, and high modulus. It is used as forgings and sheet for air frames. This datasheet provides information on composition, physical properties, elasticity, tensile properties, and bend strength as well as fracture toughness and creep. It also includes information on high temperature performance as well as joining. Filing Code: TI-119. Producer or source: RMI Company.


Alloy Digest ◽  
2007 ◽  
Vol 56 (12) ◽  

Abstract Crucible 422 has a structure of tempered martensite to give the alloy high strength. It is useful in the aerospace industry for structurals with high strength/weight ratios. This datasheet provides information on composition, physical properties, elasticity, and tensile properties as well as fracture toughness. It also includes information on low and high temperature performance, and corrosion resistance as well as forming, heat treating, machining, and joining. Filing Code: SS-1004. Producer or source: Crucible Service Centers.


Alloy Digest ◽  
1956 ◽  
Vol 5 (1) ◽  

Abstract ALLOY S-590 is designed for service in the range of 1100-1400 F for applications where high strength and corrosion resistance are required. This datasheet provides information on composition, physical properties, hardness, elasticity, and tensile properties as well as fracture toughness, creep, and fatigue. 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-39. Producer or source: Allegheny Ludlum Corporation.


Alloy Digest ◽  
1958 ◽  
Vol 7 (4) ◽  

Abstract MST 821 is a weldable titanium-base alloy having a favorable combination of strength, formability and resistance to creep at elevated temperatures. This datasheet provides information on composition, physical properties, elasticity, tensile properties, and bend strength 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-15. Producer or source: Mallory-Sharon Titanium Corporation.


Alloy Digest ◽  
2002 ◽  
Vol 51 (1) ◽  

Abstract Ti 6Al-4V-0.1Ru alloy is an extra-low interstitial alloy version of Ti-6Al-4V offering improved fracture toughness in air and better corrosion resistance to crude oil with chlorides. This datasheet provides information on composition, physical properties, hardness, elasticity, tensile properties, and bend strength as well as fracture toughness. It also includes information on high temperature performance as well as joining. Filing Code: TI-125. Producer or source: RMI Titanium Company.


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