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TIMETAL 550
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Journal Articles
Alloy Digest (1998) 47 (7): Ti-112.
Published: 01 July 1998
... TIMETAL 550 is a medium strength forgeable alpha beta alloy for applications in the aerospace and automotive industries. This datasheet provides information on composition, physical properties, and tensile properties as well as fracture toughness, creep, and fatigue. It also includes information...
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TIMETAL 550 is a medium strength forgeable alpha beta alloy for applications in the aerospace and automotive industries. This datasheet provides information on composition, physical properties, and tensile properties as well as fracture toughness, creep, and fatigue. It also includes information on high temperature performance as well as heat treating and joining. Filing Code: TI-112. Producer or source: Titanium Metals Corporation (Timet).
Journal Articles
Alloy Digest (2006) 55 (5): Ti-138.
Published: 01 May 2006
... Timetal 551 is an improved-strength version of Timetal 550 alloy that retains good forging characteristics. The alpha-beta alloy has a nominal composition of Ti-4Al-4Mo-4Sn-0.5 Si, and it is used in gas turbine engine parts. This datasheet provides information on composition, physical properties...
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Timetal 551 is an improved-strength version of Timetal 550 alloy that retains good forging characteristics. The alpha-beta alloy has a nominal composition of Ti-4Al-4Mo-4Sn-0.5 Si, and it is used in gas turbine engine parts. This datasheet provides information on composition, physical properties, elasticity, tensile properties, and shear strength as well as creep. It also includes information on high temperature performance as well as forming and heat treating. Filing Code: TI-138. Producer or source: Timet.
Journal Articles
Alloy Digest (1992) 41 (11): Ti-101.
Published: 01 November 1992
... up to 550 F. This datasheet provides information on composition, physical properties, and tensile properties. It also includes information on forming and heat treating. Filing Code: Ti-101. Producer or source: Titanium Metals Corporation (Timet). Producer or Source: Titanium Metals Corporation...
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TIMETAL 15-3 is a metastable beta titanium alloy that offers substantial weight reductions over other engineering materials. In the solution treated condition, it has excellent cold formability; in the aged condition, it has high strength. TIMETAL 15-3 is usually acceptable for use at temperatures up to 550 F. This datasheet provides information on composition, physical properties, and tensile properties. It also includes information on forming and heat treating. Filing Code: Ti-101. Producer or source: Titanium Metals Corporation (Timet).
Journal Articles
Alloy Digest (2010) 59 (5): Ti-147.
Published: 01 May 2010
... TIMETAL 65A is a general purpose grade of commercially pure titanium that has excellent corrosion resistance to highly oxidating to mildly reducing environments, including chlorides, and an excellent strength-to-weight ratio. This datasheet provides information on composition, physical properties...
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TIMETAL 65A is a general purpose grade of commercially pure titanium that has excellent corrosion resistance to highly oxidating to mildly reducing environments, including chlorides, and an excellent strength-to-weight ratio. This datasheet provides information on composition, physical properties, elasticity, and tensile properties as well as fatigue. It also includes information on high temperature performance as well as forming and heat treating. Filing Code: TI-147. Producer or source: Timet.
Journal Articles
Alloy Digest (2007) 56 (10): Ti-142.
Published: 01 October 2007
.... Material should be fully heat treated prior to welding and also given a suitable post weld treatment (for example 4-8 h at 550 °C, 1022 °F). The weld zone of material treated in this way will have similar structure and properties to the parent metal. General Characteristics: Timetal 685, a near-alpha alloy...
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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 (1998) 47 (10): Ti-105.
Published: 01 October 1998
... of a mctastablc-beta alloy but has been specifically designed for improved oxidation rcsistana, ckvated tcmpemure strength, creep resistance, and thermal stability. TIMETAL 21s is useful for applications from 228-593 C (550-1100 OF). The msistance of the alloy to aircraft hydraulic fluids such as Sky- drol...
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TIMETAL 21S (Ti-15%Mo-3%Nb-3%Al-0.2Si) offers the good cold formability and weldability of a beta strip alloy, but with greatly improved oxidation resistance and creep strength. Aerospace applications include engine exhaust plug and nozzle assemblies. 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 and heat treating. Filing Code: TI-105. Producer or source: Titanium Metals Corporation (Timet). Originally published March 1993, revised October 1998.
Journal Articles
Alloy Digest (2014) 63 (5): Ti-154.
Published: 01 May 2014
... mechanical properties are shown in Tables 1 5. Heat Treatment: Heat treatment Temperature, °C (°F) Solution treat and age (STA) 800 (1475) 4 h, water quench 635 (1175) 8 h, air cool Stress relieve (before finish machining) 550 (1020) 4 h, air cool General Characteristics: Timetal 17 is a high-strength deep...
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Timetal Grade 17 is a high-strength deep hardening forging alloy. This datasheet provides information on composition, physical properties, and tensile properties as well as fracture toughness and creep. It also includes information on forming and heat treating. Filing Code: Ti-154. Producer or source: Timet.
Journal Articles
Alloy Digest (2021) 70 (7): Ti-180.
Published: 01 July 2021
... strength. It is acceptable for use up to 230 °C (550 °F). 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, and joining. Filing Code: Ti-180. Producer or source...
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CarTech Ti 15V-3Cr-3Sn-3Al (UNS R58153) is a metastable beta titanium alloy that offers substantial weight reduction in comparison with other engineering materials. If used in the solution heat treated condition, the alloy has excellent cold formability. In the aged condition, the alloy has high strength. It is acceptable for use up to 230 °C (550 °F). 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, and joining. Filing Code: Ti-180. Producer or source: Carpenter Technology Corporation.
Journal Articles
Alloy Digest (1986) 35 (10): Fe-73.
Published: 01 October 1986
... offer customer savings in heat- treating COSIS. These properties are shown in Table 2 and Figure I for the anneal schedule giben belou. Anneal Schedule: The following annealing cycle is recommended: I. Hold at 1550 F for I hour. 2. Cool IO 145O F in I hour. 3. Cool IO 1350 F in I hour. 4. Cool IO 1250...
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CMI-B Magnetic Iron is an ultra-low-carbon magnetic iron especially processed for good magnetic properties and processability. It is used for relays and other electromagnetic applications. 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: Fe-73. Producer or source: Connecticut Metals Incorporated.
Journal Articles
Alloy Digest (2008) 57 (8): Al-416.
Published: 01 August 2008
... [email protected] Fax 440-338-4634 www.asminternational.org ALCAN 7056-T7951 m m in. M P a ks i M P a ks i M P a ks i K l c M P a ks i 25 1 560 81 545 79 545 79 30 27.3 38 1.5 550 80 535 77.5 530 77 28 25.5 To ug hne s s (b) Table 1 Mechanical properties (tentative minimun) (a ) Lo ngitudina l...
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Alcan 7056 is an Al-Mg-Zn-Cu-Zr alloy developed to provide an improved static/toughness balance versus incumbent 7150 and 7449 alloys. This data sheet covers Alcan 7056 alloy in the overaged T7951 temper. The alloy possesses very high toughness with improved corrosion resistance over 7150. This datasheet provides information on composition, physical properties, and tensile properties as well as fracture toughness. It also includes information on corrosion resistance as well as forming and heat treating. Filing Code: AL-416. Producer or source: Alcan Inc.
Journal Articles
Alloy Digest (2021) 70 (5): Ti-178.
Published: 01 May 2021
... (32 °F) Oxygen 0.03 0.08 6.6 Aluminum (3.8)(b) Vanadium 0.003 0.012(c) Titanium 580 0.10 0.25 (0.140) 0.10 0.13 1.68 (1008) 6 5.5 6.50 1.00005(c) 4 3.5 4.5 Typical values for wrought Timetal 6-4, 6-4 ELI & 6-4-.1Ru. (a) ±14 °C (±25 °F). (b) For mill annealed condition. (c) At 1.59 kA/m (20 Oe) bal...
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Arcam Ti6Al4V ELI (Grade 23) is a titanium-based alloy that is used for the production of additively manufactured components using electron beam melting (EBM). This alloy offers the best all-round performance for a variety of weight reduction applications in aerospace, automotive, and marine equipment. It also has numerous applications in the medical industry. Arcam Ti6Al4V ELI is very similar to Arcam Ti6Al4V, except that Arcam Ti6Al4V ELI contains reduced levels of oxygen, nitrogen, carbon, and iron. These lower interstitials provide improved ductility and better fracture toughness. This datasheet provides information on composition, physical properties, microstructure, hardness, elasticity, and tensile properties. It also includes information on machining and joining. Filing Code: Ti-178. Producer or source: Arcam AB (a GE Additive Company).
Journal Articles
Alloy Digest (2000) 49 (6): SS-790.
Published: 01 June 2000
... a true cutting edge without excessive weakening of the cut- ting edge. Use sufficient cutting depth to ensure penetration be- low the hardened zone caused by the previous cuts. Replace or resharpen tools on a regular schedule before tools are dulled and cause surface hardening. Use adequate lubricant...
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RAM 316L is a machining-quality version of standard austenitic stainless steel type 316L. The alloy is designed to increase productivity and efficiency by allowing one to machine at higher speeds and feeds with less tool wear. 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: SS-790. Producer or source: Rolled Alloys Inc.
Journal Articles
Alloy Digest (2002) 51 (1): SS-841.
Published: 01 January 2002
... requiring miles of tubing, this can result in the need to make thousands of girth welds having an adverse impact on both cost and delivery schedule. SDSS such as alloy 2507 can form detrimental intermetallic phases that have been cited as the cause of industry-reported failures of SDSS. The need for a lower...
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Alloy 19D (UNS S32001), Nitronic 19D, is a lean duplex (ferritic-austenitic) stainless steel developed by AK Steel. Compared to conventional duplex and super-duplex stainless steels, alloy 19D has a reduced chromium content, man-ganese is substituted for most of the nickel, and molybdenum is essentially eliminated. Gibson Tube conducted a development program to produce seam-welded 19D tubing. This datasheet provides information on composition, physical properties, microstructure, hardness, elasticity, and tensile properties as well as fatigue. It also includes information on corrosion resistance. Filing Code: SS-841. Producer or source: Gibson Tube.