Effect of surface nanostructuring in solution treated and thermally aged condition on LCF life of AA7075

2020 ◽  
Vol 404 ◽  
pp. 126431
Author(s):  
Vaibhav Pandey ◽  
Manish Kumar Singh ◽  
Joysurya Basu ◽  
K. Chattopadhyay ◽  
N.C. Santhi Srinivas ◽  
...  
Keyword(s):  
Aged Condition ◽  
Surface Nanostructuring ◽  
Solution Treated ◽  
Effect Of Surface

RMI BETA-C

Alloy Digest ◽  
1987 ◽  
Vol 36 (8) ◽  
Keyword(s):  
Carbon Dioxide ◽  
Tensile Strength ◽  
Base Alloy ◽  
Heat Treating ◽  
Production Equipment ◽  
General Corrosion ◽  
Aged Condition ◽  
Good Resistance ◽  
Solution Treated ◽  
Low Elastic Modulus

Abstract RMI Beta C is a heat-treatable titanium-base alloy that develops a tensile strength of over 200,000 psi in the solution-treated-and-aged condition. It has good ductility and toughness, good fabricability and a low elastic modulus. It has good resistance to general corrosion and it resists hot, aggressive environments containing ferric chloride, sodium chloride, carbon dioxide and hydrogen sulfide. Its applications include coil springs, fasteners, rivets and downhole oil-production equipment. 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, joining, and surface treatment. Filing Code: Ti-87. Producer or source: RMI Company.

Effect of surface Nanostructuring on LCF behavior of aluminum alloy 2014

2015 ◽  
Vol 647 ◽  
pp. 201-211 ◽  
Author(s):  
Vaibhav Pandey ◽  
G. Sudhakar Rao ◽  
K. Chattopadhyay ◽  
N.C. Santhi Srinivas ◽  
Vakil Singh
Keyword(s):  
Aluminum Alloy ◽  
Surface Nanostructuring ◽  
Effect Of Surface

ALLVAC 38-644

Alloy Digest ◽  
2004 ◽  
Vol 53 (7) ◽  
Keyword(s):  
High Strength ◽  
Heat Treating ◽  
Aged Condition ◽  
Beta Titanium Alloy ◽  
Solution Treated Condition ◽  
Solution Treated ◽  
Treated Condition ◽  
Beta Titanium ◽  
Metastable Beta ◽  
Strength And Ductility

Abstract Allvac 38-644 is a metastable beta titanium alloy known for its ductility in the solution treated condition and its high strength and ductility in the solution treated and aged condition. This datasheet provides information on composition, physical properties, hardness, elasticity, and tensile properties. It also includes information on forming, heat treating, machining, and joining. Filing Code: TI-134. Producer or source: Allvac Metals Company.

TIMETAL 15-3

Alloy Digest ◽  
1992 ◽  
Vol 41 (11) ◽  
Keyword(s):  
Titanium Alloy ◽  
High Strength ◽  
Heat Treating ◽  
Aged Condition ◽  
Beta Titanium Alloy ◽  
Solution Treated Condition ◽  
Solution Treated ◽  
Treated Condition ◽  
Beta Titanium ◽  
Metastable Beta

Abstract 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).

Experimental Study on Tool Wear in Cutting Titanium Alloy Ti6Al4V

2011 ◽  
Vol 239-242 ◽  
pp. 2011-2014
Author(s):  
Yue Feng Yuan ◽  
Wu Yi Chen ◽  
Wen Ying Zhang
Keyword(s):  
Titanium Alloy ◽  
Tool Wear ◽  
Tool Life ◽  
Linear Regression Analysis ◽  
Cutting Speed ◽  
Cutting Parameters ◽  
Aged Condition ◽  
Cutting Depth ◽  
Solution Treated ◽  
Titanium Alloy Ti6al4v

Tool wear experiments in turning titanium alloy Ti6Al4V in the solution-treated and aged condition were carried out; the influence rules of cutting parameters such as cutting speed, feed rate and cutting depth on the tool life were obtained. Experimental formula of tool wear was regressed based on multi-variable linear regression analysis, it could predict tool life under certain conditions.

Effect of surface nanostructuring of aluminum alloy on post plasma electrolytic oxidation

2014 ◽  
Vol 317 ◽  
pp. 962-969 ◽  
Author(s):  
H.R. Masiha ◽  
H.R. Bagheri ◽  
M. Gheytani ◽  
M. Aliofkhazraei ◽  
A. Sabour Rouhaghdam ◽  
...  
Keyword(s):  
Aluminum Alloy ◽  
Plasma Electrolytic Oxidation ◽  
Surface Nanostructuring ◽  
Electrolytic Oxidation ◽  
Plasma Electrolytic ◽  
Effect Of Surface

scholarly journals Closed Die Hammer Forging of Inconel 718

2014 ◽  
Vol 2014 ◽  
pp. 1-7 ◽  
Author(s):  
S. Chenna Krishna ◽  
Satish Kumar Singh ◽  
S. V. S. Narayana Murty ◽  
Ganji Venkata Narayana ◽  
Abhay K. Jha ◽  
...  
Keyword(s):  
Mechanical Properties ◽  
Grain Size ◽  
Inconel 718 ◽  
Air Cooling ◽  
Aged Condition ◽  
Controlled Cooling ◽  
Solution Treated ◽  
Hemispherical Dome ◽  
Hammer Forging ◽  
Better Than

A method for the production of Inconel 718 (IN-718) hemispherical domes by closed die hammer forging is proposed. Different combination of operations employed for production are as follows: (i) preforging + final forging + air cooling, (ii) preforging + final forging + controlled cooling, (iii) direct forging + controlled cooling, and (iv) direct forging + air cooling. Last three combinations yielded a crack free hemispherical dome. The forged hemispherical domes were solution annealed at 980°C for 1 h and air cooled. The grain size of the domes at all locations was finer than ASTM No 4. Mechanical properties of the forged dome in solution treated and aged condition (STA) were better than feedstock used.

ALUMINUM A356.0

Alloy Digest ◽  
1985 ◽  
Vol 34 (6) ◽  
Keyword(s):  
High Strength ◽  
Heat Treating ◽  
Good Combination ◽  
Age Hardening ◽  
Casting Alloy ◽  
Aged Condition ◽  
Solution Treated ◽  
Mold Casting ◽  
Hardening Heat Treatment ◽  
Strength And Ductility

Abstract ALUMINUM A356.0 is a sand and permanent-mold casting alloy. It responds to an age-hardening heat treatment. This alloy has a relatively good combination of strength and ductility in the solution-treated and aged condition. Aluminum A356.0 is recommended for aircraft and missile components where high strength and resistance to corrosion are required. 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 corrosion resistance as well as casting, heat treating, machining, and joining. Filing Code: Al-258. Producer or source: Various aluminum companies.

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