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ATI 3-2.5
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Journal Articles
Publisher: Journals Gateway
Alloy Digest (2020) 69 (5): Ti-166.
Published: 01 May 2020
... 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...
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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.
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Publisher: Journals Gateway
Alloy Digest (2004) 53 (7): Ti-133.
Published: 01 July 2004
... workability thermal properties Chemical Composition, wt (Typical) Aluminum 4 Vanadium 2.5 Iron 1.5 Oxygen 0.250 Titanium bal Ruthenium can be added for better corrosion resistance. Physical Properties: Density, kg/m3 (lb/in.3 ) 4490 (0.162) Melting range, °C (°F) 1600 1650 (2912 3002) Mechanical...
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ATI 425 was originally developed for hot-rolled armor plate to provide ballistic protection comparable to Ti-6Al-4V and has been evaluated against a variety of projectile threats for use as armor. While processing the alloy for armor plate applications, it was observed that the material exhibited very good hot workability, permitting a more lenient window of processing parameters than necessary for Ti-6Al-4V. Versatility then expanded, and applications now exist in the chemical process industry (CPI) and in the aerospace industry. This datasheet provides information on composition, physical properties, and tensile properties as well as fracture toughness and fatigue. It also includes information on corrosion resistance. Filing Code: TI-133. Producer or source: ATI Wah Chang, Allegheny Technologies. Originally published March 2004, revised July 2004.
Journal Articles
Publisher: Journals Gateway
Alloy Digest (2012) 61 (1): Ti-149.
Published: 01 January 2012
...-2Sn-2Zr-4Cr-4Mo (Alpha-Beta Titanium Alloy) ATI ALLOY Ti-5Al-2Sn-2Zr-4Cr-4Mo Chemical Composition, wt (ASTM A240 limits) Aluminum 4.5 5.5 Tin 1.5 2.5 Zirconium 1.5 2.5 Molybdenum 3.5 4.5 Chromium 3.5 4.15 Oxygen 0.08 0.13 Nitrogen 0.04 max Hydrogen 0.0125 max Iron 0.3 max Titanium bal Physical...
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ATI Ti-5Al-2Sn-2Zr-4Cr-4Mo is known as Ti-17 alloy and is a beta-rich material for large aerospace components. This datasheet provides information on composition, physical properties, hardness, and tensile properties. It also includes information on corrosion resistance as well as forming, heat treating, and joining. Filing Code: Ti-149. Producer or source: ATI Allvac.
Journal Articles
Publisher: Journals Gateway
Alloy Digest (2013) 62 (6): Ti-150.
Published: 01 June 2013
.... It was developed by General Electric for fan and compressor discs. ATI 17 Ti-5Al-2Sn-2Zr-4Cr-4Mo (Beta Rich Titanium Alloy) ATI 17 Ti-5Al- 2Sn-2Zr-4Cr-4Mo Chemical Composition, wt Aluminum 4.5 5.5 Tin 1.5 2.5 Chromium 3.5 4.5 Molybdenum 3.5 4.5 Zirconium 1.5 2.5 Iron 0.3 max Oxygen 0.08 0.13 Nitrogen 0.04 max...
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ATI 17 Ti-5Al-2Sn-2Zr-4Cr-4Mo is also known as Ti-17. It was developed by General Electric for fan and compressor discs. This datasheet provides information on composition, physical properties, hardness, and tensile properties. It also includes information on corrosion resistance as well as forming, heat treating, and joining. Filing Code: Ti-150. Producer or source: Allvac, An Allegheny Technologies Company.
Journal Articles
Publisher: Journals Gateway
Alloy Digest (2020) 69 (2): Ni-756.
Published: 01 February 2020
... ATI 10242 is an age-hardenable nickel-molybdenum-chromium alloy that derives its strength from a long-range ordering reaction during aging. This ordering reaction not only provides the alloy’s strength, but also imparts excellent thermal stability. This datasheet provides information...
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ATI 10242 is an age-hardenable nickel-molybdenum-chromium alloy that derives its strength from a long-range ordering reaction during aging. This ordering reaction not only provides the alloy’s strength, but also imparts excellent thermal stability. This datasheet provides information on composition, physical properties, and hardness. It also includes information on high temperature performance as well as forming, machining, and joining. Filing Code: Ni-756. Producer or source: ATI.
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Publisher: Journals Gateway
Alloy Digest (2021) 70 (2): SS-1331.
Published: 01 February 2021
.... A filler metal of matching composition or a higher alloy weld metal is generally specified. One common choice for this grade is AWS ERNiCrMo-3 (com- monly known as alloy 625 filler metal). This alloy can also be vacuum-brazed. Comparable Grades Fig. 1 Typical short-term elevated temperature tensile ATI ATI...
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ATI 20-25+Nb is an austenitic stainless steel intended primarily for elevated-temperature service. This alloy fills a performance gap between conventional heat-resistant stainless steels and nickel-base superalloys, providing high performance with an economical composition. 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 forming, heat treating, machining, and joining. Filing Code: SS-1331. Producer or source: ATI.
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Alloy Digest (1982) 31 (10): Cu-446.
Published: 01 October 1982
... Copper Alloy No. C84200 is a free-cutting copper-zinc-tin-lead alloy. It is characterized by good casting properties, moderate strength and ductility, good machinability and good resistance to corrosion. Formerly used named (not recommended) are 101, Leaded Semi-Red Brass and 80-5-2.5-12.5...
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Copper Alloy No. C84200 is a free-cutting copper-zinc-tin-lead alloy. It is characterized by good casting properties, moderate strength and ductility, good machinability and good resistance to corrosion. Formerly used named (not recommended) are 101, Leaded Semi-Red Brass and 80-5-2.5-12.5. Typical applications are pipe fittings, bushings, locknuts and unions. This datasheet provides information on composition, physical properties, hardness, elasticity, and tensile properties. It also includes information on corrosion resistance as well as casting, heat treating, machining, and joining. Filing Code: Cu-446. Producer or source: Copper alloy foundries. See also Alloy Digest Cu-450, December 1982.
Journal Articles
Publisher: Journals Gateway
Alloy Digest (2003) 52 (2): Ni-601.
Published: 01 February 2003
... Chromium 19.5 22.5 Iron 22.0 max Molybdenum 2.5 3.5 Copper 1.5 3.0 Titanium 1.9 2.3 Aluminum 0.1 0.5 Carbon 0.03 max Physical Properties: Density, kg/m3 (lb/in.3 ) 8030 (0.29) Melting range, °C (°F) 1301 1370 (2375 2500) See also Figures 1 3. Mechanical Properties: Tensile strength, solution treated 1170...
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Nickelvac 925 is an alloy similar to alloy 825 (N08825), but with the age-hardening constituents of titanium and aluminum to achieve high strength while maintaining excellent corrosion resistance. This datasheet provides information on composition, physical properties, hardness, and tensile properties as well as fracture toughness. It also includes information on corrosion resistance as well as forming, heat treating, machining, and joining. Filing Code: Ni-601. Producer or source: Allvac Metals Company.
Journal Articles
Publisher: Journals Gateway
Alloy Digest (2004) 53 (11): Ti-135.
Published: 01 November 2004
... International® 2004 2004 ASM International ALLVAC Ti-17 chemical composition corrosion-resistant alloys hardness high-temperature alloys joinability physical properties tensile properties Chemical Composition, wt Aluminum 4.6 5.5 Tin 1.5 2.5 Chromium 3.5 4.5 Molybdenum 3.5 4.5 Zirconium 1.5 2.5...
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Allvac Ti-17 is a high-strength deep-hardening alloy. The alloy is alpha-beta, but beta-rich, and can be worked in both the beta and alpha-beta region. The alloy is commonly referred to as grade 17 in specifications. This datasheet provides information on composition, physical properties, hardness, and tensile properties. It also includes information on high temperature performance and corrosion resistance as well as joining. Filing Code: TI-135. Producer or source: Allvac, An Allegheny Technologies Company.
Journal Articles
Publisher: Journals Gateway
Alloy Digest (1984) 33 (8): Cu-481.
Published: 01 August 1984
... 1980, Engineering Publications, Inc. AtI rights reserved. MN: 002-614X Published b] Alloy Digest, Inc. 27 Canfield Street Orange. New Jersey 07050 (201) 761-1090 MUELLER Alloy 6732 (High-Leaded Bearing Alloy) MUELLER Alloy 6732 is a free-machining high-leaded copper-base alloy that is especially well...
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MUELLER Alloy 6732 is a free-machining high-leaded copper-base alloy that is especially well suited for screw machine work. It can be used with hard or soft mating members. It can be joined readily by soft or silver soldering. It possesses excellent bearing properties, high mechanical properties and good resistance to corrosion. Its uses include bushings gears, bearings and pump parts. 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, machining, and joining. Filing Code: Cu-481. Producer or source: Mueller Brass Company.
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Publisher: Journals Gateway
Alloy Digest (2007) 56 (3): Ni-647.
Published: 01 March 2007
.... The triple melting produces a stronger alloy with consistent properties in strength, stability, and forgeability. Allvac is a registered trademark and Allvac Plus is a trademark of ATI Properties, Inc. Fig. 2 Linear coefficient of thermal expansionFig. 1 Thermal conductivity Mechanical Properties: See Fig. 3...
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Allvac 718Plus alloy is a variant of alloy 718 (Alloy Digest Ni-90, April 1964) made by adding new elements and adjusting others. The triple melting produces a stronger alloy with consistent properties in strength, stability, and forgeability. 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, machining, and joining. Filing Code: Ni-647. Producer or source: Allvac, an Allegheny Technologies Company.
Journal Articles
Publisher: Journals Gateway
Alloy Digest (1984) 33 (9): TS-428.
Published: 01 September 1984
... temperature should be about 2.5-3 hours per inch of greatest cross section. DOI: 10.31399/asm.ad.ts0428 Copyright © ASM International® 1996 Fig. 2-Cutting speed versus tool life for TeleCut and Al81 M-42 high-speed steels. equivalent to AISI Type M42 in wear resistance and surpasses it in toughness...
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VASCO TeleCut is a cobalt-free high-speed steel that is a cost-effective alternative to many cobalt high-speed steels because of its special combination of hot hardness, wear resistance and toughness. TeleCut is a superior high-speed steel that is ideal for a variety of cutting tools, including end mills, milling cutters, broaches and gear cutters. This datasheet provides information on composition and hardness. It also includes information on forming, heat treating, and machining. Filing Code: TS-428. Producer or source: Teledyne Vasco.
Journal Articles
Publisher: Journals Gateway
Alloy Digest (2000) 49 (11): Cb-25.
Published: 01 November 2000
... as well as forming, machining, and joining. Filing Code: CB-25. Producer or source: ATI Wah Chang, Allegheny Technologies. Producer or Source: ATI Wah Chang, Allegheny Technologies Copyright © ASM International® 2000 2000 ASM International C-103 chemical composition creep properties...
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Alloy C-103 is a niobium alloy with a high strength/density ratio for elevated temperature applications. 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 forming, machining, and joining. Filing Code: CB-25. Producer or source: ATI Wah Chang, Allegheny Technologies.
Journal Articles
Publisher: Journals Gateway
Alloy Digest (1982) 31 (7): Al-239.
Published: 01 July 1982
... strength (0.2% offset), psi (MPa) 23000 (160) Elongation (2 in. or 50 mm), % 2.5 Shear strength, psi (MPa II 28000 ( 190) Fatigue strength* (5 x 10 cycles), psi (MPa) 20000 (140) *R.R. Moore specimens. Table 3 - SHORT-TIME ELEVATED-TEMPERATURE TENSILE PROPERTIES (After heating at testing temperature...
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ALUMINUM 380.0 is a copper-silicon type of aluminum die-casting alloy. It has good castability and fairly good machinability; it is the most widely used aluminum die-casting alloy. It has satisfactory strength and ductility. Among the many applications of Aluminum 380.0 are internal combustion engine parts, pressure-tight castings, ornamental castings and machine frames. This datasheet provides information on composition, physical properties, elasticity, tensile properties, and shear strength as well as fatigue. It also includes information on high temperature performance and corrosion resistance as well as casting, heat treating, machining, joining, and surface treatment. Filing Code: Al-239. Producer or source: Various aluminum companies.
Journal Articles
Publisher: Journals Gateway
Alloy Digest (1983) 32 (11): Al-248.
Published: 01 November 1983
... - EFFECTOFTEMPERATURE ON PROPERTIES -T5TEMPER Temperature F 70 100 200 300 400 Tensile Yield Strength Elongation Brine11 Strength (0.2q Offset) (4D) Hardness psi psi 5 (500 IO) 29500 20000 5.0 70.0 29000 19800 4.7 69.5 27000 18500 3.0 67.0 21500 17000 2.5 63.0 15500 14500 2.0 56.5 Table 3 - RECOMMENDED CUTTING SPEEDS...
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ALUMINUM 852.0 contains higher concentrations of copper and nickel than either Aluminum 850.0 or Aluminum 851.0 alloy. The higher copper and nickel percentages and an addition of magnesium give Aluminum 852.0 higher strength and make it suitable for bearing applications requiring improved resistance to higher operating stresses (loads). Aluminum 852.0 is used for the production of castings by the sand and permanent-mold processes. It is normally supplied and used in the T5 temper. This datasheet provides information on composition, physical properties, hardness, elasticity, tensile properties, and compressive and shear strength as well as 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: Al-248. Producer or source: Various aluminum companies.
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Publisher: Journals Gateway
Alloy Digest (2002) 51 (12): SS-869.
Published: 01 December 2002
... 26% NaCl Austenitic type 304L (8% Ni) Failed, 850 h Austenitic type 316 (12% Ni, 2.5% Mo) Failed, 530 940 h Austenitic type 317L (13% Ni, 3.5% Mo) Failed, 1000 h Duplex AL 2003 (3% Ni, 1.7% Mo) Passed, 1000 h Duplex AL 2205 (5% Ni, 3% Mo) Passed, 1000 h Failed indicates failure by chloride stress...
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The AL 2003 alloy is a nitrogen-enhanced leaner nickel and molybdenum alloy than the duplex stainless steel AL 2205, but is similar in both phase balance and mechanical properties. Applications include areas where resistance to both general and chloride-ion stress-corrosion cracking is important. This datasheet provides information on composition, physical properties, microstructure, 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, and joining. Filing Code: SS-869. Producer or source: Allegheny Ludlum Corporation.