ATI 75

Alloy Digest ◽  
2020 ◽  
Vol 69 (7) ◽  

Abstract ATI 75 (UNS N06075) is a nickel-chromium alloy with controlled additions of titanium and carbon; it derives its high temperature strength essentially from solid solution strengthening. This datasheet provides information on composition, physical properties, and tensile properties. It also includes information on high temperature performance as well as forming, heat treating, and joining. Filing Code: Ni-761. Producer or source: ATI.

Alloy Digest ◽  
2005 ◽  
Vol 54 (5) ◽  

Abstract Haynes 617 is a solid-solution nickel-chromium-cobalt-molybdenum alloy with excellent high temperature strength and oxidation resistance. It has applications at high temperature for aerospace engines. This datasheet provides information on composition, physical properties, elasticity, and tensile properties as well as creep. It also includes information on high temperature performance as well as heat treating. Filing Code: Ni-625. Producer or source: Haynes International Inc.


Alloy Digest ◽  
1977 ◽  
Vol 26 (4) ◽  

Abstract STOODY 4 is a cobalt-chromium-tungsten alloy with excellent high-temperature strength and excellent resistance to corrosion. This alloy derives its high-temperature strength from the high tungsten-to-carbon ratio which allows a large percentage of tungsten to remain in solid solution. This datasheet provides information on composition, physical properties, hardness, elasticity, tensile properties, and compressive strength. It also includes information on high temperature performance and corrosion resistance as well as heat treating, machining, and joining. Filing Code: Co-75. Producer or source: WRAP Division, Stoody Company.


Alloy Digest ◽  
1972 ◽  
Vol 21 (10) ◽  

Abstract INCONEL ALLOY 671 is a nickel-chromium alloy having excellent resistance to high-temperature corrosion. This datasheet provides information on composition, physical properties, hardness, 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: Ni-180. Producer or source: Huntington Alloy Products Division, An INCO Company.


Alloy Digest ◽  
1967 ◽  
Vol 16 (1) ◽  

Abstract Tophet-D is an iron-nickel-chromium alloy recommended for electric furnace heating elements and electrical resistors operating up to 1600 F. This datasheet provides information on composition, physical properties, hardness, and tensile properties. It also includes information on high temperature performance as well as forming, heat treating, and machining. Filing Code: Fe-30. Producer or source: Wilbur B. Driver Company.


Alloy Digest ◽  
1961 ◽  
Vol 10 (4) ◽  

Abstract Inconel 718 is an age-hardenable nickel-chromium alloy having exceptionally high tensile, yield, creep, and rupture strength at temperatures up to 1300 F. This datasheet provides information on composition, physical properties, elasticity, tensile properties, and compressive strength as well as 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: Ni-65. Producer or source: Huntington Alloy Products Division, An INCO Company.


Alloy Digest ◽  
2006 ◽  
Vol 55 (6) ◽  

Abstract HPM X-750 is a precipitation-hardenable nickel-chromium alloy that is well suited for a wide range of corrosive and oxidizing environments where strength must be maintained to elevated temperatures. The alloy composition provides a product that performs well at elevated temperatures up to 700 deg C (1300 deg F). The strength can be increased by heat treatment. This datasheet provides information on composition, physical properties, elasticity, and tensile properties. It also includes information on high temperature performance as well as forming, heat treating, and joining. Filing Code: Ni-638. Producer or source: Hamilton Precision Metals.


Alloy Digest ◽  
1966 ◽  
Vol 15 (9) ◽  

Abstract ALLEGHENY A-286 is an austenitic iron-nickel-chromium alloy designed for service up to 1300 F where high strength and corrosion resistance are required, and for service at higher temperatures where the applications are for lower stresses. It is an age-hardenable alloy. 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 low and high temperature performance, and corrosion resistance as well as forming, heat treating, machining, and joining. Filing Code: SS-4. Producer or source: Allegheny Ludlum Corporation. Originally published December 1952, revised September 1966.


Alloy Digest ◽  
1963 ◽  
Vol 12 (9) ◽  

Abstract Corronel 230 is a nickel-chromium alloy having high resistance to corrosion by hot nitric acid and excellent resistance to attack at elevated temperatures from oxidizing and reducing atmospheres high in sulfur. This datasheet provides information on composition, physical properties, elasticity, and tensile properties. It also includes information on high temperature performance and corrosion resistance as well as forming, heat treating, machining, and joining. Filing Code: Ni-86. Producer or source: Henry Wiggin & Company Ltd.


Alloy Digest ◽  
2004 ◽  
Vol 53 (1) ◽  

Abstract Inconel alloy 603XL is a nickel-chromium alloy with added elements of silicon, molybdenum, and rare earths to provide oxidation resistance and good high temperature strength. This datasheet provides information on composition, physical properties, elasticity, tensile properties, and shear strength as well as fracture toughness and creep. It also includes information on high temperature performance and corrosion resistance as well as heat treating and joining. Filing Code: Ni-619. Producer or source: Special Metals Corporation.


Alloy Digest ◽  
1997 ◽  
Vol 46 (3) ◽  

Abstract Nicrofer 2509 Si 7 is an austenitic low-carbon nickel-chromium alloy containing 7 wt.% silicon. The alloy was designed for resistance to hot concentrated sulfuric acid. 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: SS-673. Producer or source: Krupp VDM Technologies Corporation.


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