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TIMETAL 62S
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Journal Articles
Alloy Digest (1992) 41 (12): Ti-102.
Published: 01 December 1992
... TIMETAL 62S, because iron is used for the beta stabilizer in lieu of more expensive elements, has a lower formulation cost than most titanium alloys, yet the properties and processing characteristics of Ti-6A1-2Fe-0. 1Si are equivalent to or better than those of the workhorses of the titanium...
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TIMETAL 62S, because iron is used for the beta stabilizer in lieu of more expensive elements, has a lower formulation cost than most titanium alloys, yet the properties and processing characteristics of Ti-6A1-2Fe-0. 1Si are equivalent to or better than those of the workhorses of the titanium industry, including Ti-6A1-4V. The combination of reasonable cost and excellent mechanical properties make TIMETAL 62S a practical substitute for other engineering materials in numerous industrial applications that require low weight and high corrosion resistance. This datasheet provides information on composition, physical properties, elasticity, and tensile properties as well as fracture toughness and fatigue. It also includes information on heat treating. Filing Code: Ti-102. Producer or source: Timet.
Journal Articles
Alloy Digest (2007) 56 (10): Ti-142.
Published: 01 October 2007
... Timetal 685 is a titanium alloy with 6 Al, 5 Zr, 0.5 Mo, and 0.25 Si. It is a near-alpha alloy with high strength and creep resistance. Applications are in the aerospace industry. This datasheet provides information on composition, physical properties, elasticity, tensile properties, and shear...
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Timetal 685 is a titanium alloy with 6 Al, 5 Zr, 0.5 Mo, and 0.25 Si. It is a near-alpha alloy with high strength and creep resistance. Applications are in the aerospace industry. 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 forming, heat treating, and joining. Filing Code: TI-142. Producer or source: Timet.
Journal Articles
Alloy Digest (2001) 50 (8): Ti-118.
Published: 01 August 2001
... 38.5 650 1202 425 62 575 83 16 43 Disc forgings DOI: 10.31399/asm.ad.ti0118 Fig. 1 Fatigue properties of forgings Producer: TIMET 1999 Broadway Denver, CO 80202 (303) 296-5600 Technical Support: Henderson, NV (702) 566-1400 ISSN: 002-614X Ti-118B Table 3 Creep Properties Creep test, typical Post-creep...
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TIMETAL 829 is a Ti-5.5Al-3.5Sn-3Zr-1Nb-0.25Mo-0.3Si near-alpha titanium alloy that is weldable and has high strength and is a creep resistant high temperature alloy. The major application is as gas turbine engine components. This datasheet provides information on composition, physical properties, elasticity, and tensile properties as well as fracture toughness, creep, and fatigue. It also includes information on forming and heat treating. Filing Code: TI-118. Producer or source: Timet.
Journal Articles
Alloy Digest (1990) 39 (1): P-15.
Published: 01 January 1990
.../TAcIIXH41 FoIlllttlation TACTIX 123 - 100 - 100 TACTIX 138 100 - 100 - Hardcna 16 17 24 25 Viscosity, cps @ 43oC (110°F) 200 160 500 400 Pot life. min. @ 43oC (110°F) 24 42 150 240 cure schedule lh/8ooc+2h/l77oc 1h/s0 c+2h/177 c lh/l2O C+2h/177 c 1h/120oC+2h/177 =C Table 4 -PROPERTIES OF UNREINFORCED RESIN...
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TAXTIX 123 and TACTIX 138 resins cured with TACTIX H31 and TAXTIX H41 hardeners are specifically designed to maximum performance properties most critical to advanced composites. This datasheet provides information on composition, physical properties, tensile properties, and compressive strength. Filing Code: P-15. Producer or source: The Dow Chemical Company, Dow Plastics.
Journal Articles
Alloy Digest (2008) 57 (4): Al-412.
Published: 01 April 2008
...: This alloy has an optimized processing schedule; 7040 T7451 plates display a reduced level of residual stress, leading to minimum machining distortion. Fig. 2 Fatigue crack growth rate. Center-cracked tension (CCT) test specimen according to ASTM E647. Typical curves Corrosion Resistance: Stress-corrosion...
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Alcan 7040 alloy is an Al-Mg-Zn-Cu-Zr plate alloy, developed to improve strength-toughness over incumbent alloys 7010 and 7050. 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 as well as forming, heat treating, and machining. Filing Code: AL-412. Producer or source: Alcan Inc.
Journal Articles
Alloy Digest (1974) 23 (2): Ni-201.
Published: 01 February 1974
.... Critical erain erowth could be the resultant effect. S&e Unitemp 7 lg wori hardens rapidly, intermediate annealing wiU normally be required on a more frequent schedule than experienced with the 300 series stainless types. 51 43 34 25 19 16 15 10 26 42 25 42 17 41 17 40 17 40 15 35 10 25 8 20 Heat Treatment...
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UNITEMP 718 is a nickel-base austenitic precipitation-hardenable alloy for extended service at temperatures up to 1200 F. For short periods the alloy performs well to about 1300 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 low and high temperature performance, and corrosion resistance as well as forming, heat treating, machining, joining, and surface treatment. Filing Code: Ni-201. Producer or source: Cyclops Corporation.