scholarly journals Metal Matrix Composite Material by Direct Metal Deposition

2011 ◽  
Vol 12 ◽  
pp. 296-302 ◽  
Author(s):  
D. Novichenko ◽  
A. Marants ◽  
L. Thivillon ◽  
P.H. Bertrand ◽  
I. Smurov
Keyword(s):  
Composite Material ◽  
Metal Matrix Composite ◽  
Matrix Composite ◽  
Metal Matrix ◽  
Metal Deposition ◽  
Direct Metal Deposition ◽  
Metal Matrix Composite Material

Mechanical and Bond Behavior of an Advanced Quranic Metal-Matrix Composite Material (QMMC)

2019 ◽  
Author(s):  
S. Mousa ◽  
M. Atta ◽  
A. A. Abd-Elhady ◽  
Ahmed Abu-Sinna ◽  
O. Bafakeeh ◽  
...  
Keyword(s):  
Composite Material ◽  
Metal Matrix Composite ◽  
Matrix Composite ◽  
Metal Matrix ◽  
Molten Copper ◽  
The Finite Element Method ◽  
Holy Quran ◽  
The Matrix ◽  
The Holy Quran ◽  
Metal Matrix Composite Material

Abstract The holy Quran, from more than 1400 years, told us that Zul-karnain had made a metallic composite material between iron and copper [1,2] as follows: “Bring me sheets of iron” — until, when he had leveled [them] between the two mountain walls, he said, “Blow [with bellows],” until when he had made it [like] fire, he said, “Bring me, that I may pour over it molten copper * So Gog and Magog were unable to pass over it, nor were they able [to effect] in it any penetration.”: Translation of verses 96 and 97 in Surah Al-Kahf (18), The holy Quran [3]. According to the above story, the matrix is copper, while reinforcement is iron of this metal matrix composite. The present paper is going to investigate the Metal-Matrix Composite Material (MMC) suggested by Zul-karnain at different manufacturing conditions by using the experimental method. The effect of reinforcement temperature on the integrity of such MMC is one of the main goals of the present work. The mechanical behavior of the present QMMC is also examined in the present research as preliminary study. Furthermore, the finite element method is used to predicate the debonding force of MMC based on Virtual-Crack-Closing-Technique (VCCT).

Topological Optimization of the Strength Element of the Aircraft Compartment Made of Metal-Matrix Composite Material

2022 ◽  
pp. 53-60
Author(s):  
I.S. Magidov ◽  
K.V. Mikhailovskiy
Keyword(s):  
Composite Material ◽  
Metal Matrix Composite ◽  
Matrix Composite ◽  
Metal Matrix ◽  
Topological Optimization ◽  
Vehicle Body ◽  
Flight Vehicle ◽  
Direct Laser ◽  
Metal Matrix Composite Material ◽  
Growth Technology

At present, in order to increase the weight efficiency of parts and structures of promising aircraft and rocket-space vehicles, various types of additive technologies and topological optimization methods are being actively introduced. Their purpose is a significant reduction in time and financial costs in the manufacture and creation of fundamentally new geometric solutions. The article considers approaches to selecting the geometric parameters of the strength elements of the flight vehicle body made of a metal-matrix composite material based on VT6 titanium alloy, reinforced with a finely dispersed silicon carbide powder, which is produced by direct laser growth technology. On the basis of numerical simulation, the dependences of the metal-matrix composite material physicomechanical and thermophysical characteristics on the volume fraction of silicon carbide have been determined. It was found that the use of a metal-matrix composite material and the optimization of geometric parameters with adaptation to the direct laser growth technology allows reducing the weight of the strength element of the flight vehicle body by more than 30% (depending on the overall dimensions).

scholarly journals Carbide-reinforced metal matrix composite by direct metal deposition

2010 ◽  
Vol 5 ◽  
pp. 369-377 ◽  
Author(s):  
D. Novichenko ◽  
L. Thivillon ◽  
Ph. Bertrand ◽  
I. Smurov
Keyword(s):  
Metal Matrix Composite ◽  
Matrix Composite ◽  
Metal Matrix ◽  
Metal Deposition ◽  
Direct Metal Deposition
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