The Effect of Heat Treatment on the Mechanical Properties of the Alloy Ti-8Al-1Mo-1V. PDF Download

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The Effect of Heat Treatment on the Mechanical Properties of the Alloy Ti-8Al-1Mo-1V.

The Effect of Heat Treatment on the Mechanical Properties of the Alloy Ti-8Al-1Mo-1V. PDF Author: Paul J. Fopiano
Publisher:
ISBN:
Category :
Languages : en
Pages : 17

Book Description
REPT., Fopiano, Paul J. ;Hickey, Charles F., Jr;AMMRC-TR-73-17DA-1-T-062105-A-328(*titanium alloys, mechanical properties), (*heat treatment, titanium alloys), tensile properties, notch toughness, aging(materials), hardness, microstructure, phase studies, modulus of elasticity, aluminum alloys, molybdenum alloys, vanadium alloystitanium alloy 8al 1mo 1vThe effect of heat treatment on the mechanical properties of the alloy Ti-8Al-1Mo-1V (8-1-1) was investigated for solution temperatures from 1400 to 1900F. Significant increases in strength can be obtained by selected solution and aging heat treatments. A critical temperature range for this alloy is observed to be 1550 to 1700F where a yield strength minimum and ductility and toughness maximums were found. X-ray and replica electron microscopic studies were also conducted. A detailed discussion of the results and observations is contained in this report. (Author).

The Effect of Heat Treatment on the Mechanical Properties of the Alloy Ti-8Al-1Mo-1V.

The Effect of Heat Treatment on the Mechanical Properties of the Alloy Ti-8Al-1Mo-1V. PDF Author: Paul J. Fopiano
Publisher:
ISBN:
Category :
Languages : en
Pages : 17

Book Description
REPT., Fopiano, Paul J. ;Hickey, Charles F., Jr;AMMRC-TR-73-17DA-1-T-062105-A-328(*titanium alloys, mechanical properties), (*heat treatment, titanium alloys), tensile properties, notch toughness, aging(materials), hardness, microstructure, phase studies, modulus of elasticity, aluminum alloys, molybdenum alloys, vanadium alloystitanium alloy 8al 1mo 1vThe effect of heat treatment on the mechanical properties of the alloy Ti-8Al-1Mo-1V (8-1-1) was investigated for solution temperatures from 1400 to 1900F. Significant increases in strength can be obtained by selected solution and aging heat treatments. A critical temperature range for this alloy is observed to be 1550 to 1700F where a yield strength minimum and ductility and toughness maximums were found. X-ray and replica electron microscopic studies were also conducted. A detailed discussion of the results and observations is contained in this report. (Author).

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Designed to support the need of engineering, management, and other professionals for information on titanium by providing an overview of the major topics, this book provides a concise summary of the most useful information required to understand titanium and its alloys. The author provides a review of the significant features of the metallurgy and application of titanium and its alloys. All technical aspects of the use of titanium are covered, with sufficient metals property data for most users. Because of its unique density, corrosion resistance, and relative strength advantages over competing materials such as aluminum, steels, and superalloys, titanium has found a niche in many industries. Much of this use has occurred through military research, and subsequent applications in aircraft, of gas turbine engines, although more recent use features replacement joints, golf clubs, and bicycles.Contents include: A primer on titanium and its alloys, Introduction to selection of titanium alloys, Understanding titanium's metallurgy and mill products, Forging and forming, Castings, Powder metallurgy, Heat treating, Joining technology and practice, Machining, Cleaning and finishing, Structure/processing/property relationships, Corrosion resistance, Advanced alloys and future directions, Appendices: Summary table of titanium alloys, Titanium alloy datasheets, Cross-reference to titanium alloys, Listing of selected specification and standardization organizations, Selected manufacturers, suppliers, services, Corrosion data, Machining data.

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