scholarly journals Fractographic Analysis of the Low Energy Fracture of an Aluminum Alloy

2009 ◽  
pp. 191-191-25 ◽  
Author(s):  
JP Tanaka ◽  
CA Pampillo ◽  
JR Low
Keyword(s):  
Aluminum Alloy ◽  
Low Energy ◽  
Fractographic Analysis

Effect of low-energy pulse laser irradiation on the properties of ultrafine-grain aluminum alloy 1421

2012 ◽  
Vol 54 (7-8) ◽  
pp. 398-401 ◽  
Author(s):  
P. Yu. Kikin ◽  
A. I. Pchelintsev ◽  
E. E. Rusin ◽  
N. V. Zemlyakova
Keyword(s):  
Aluminum Alloy ◽  
Laser Irradiation ◽  
Pulse Laser ◽  
Low Energy ◽  
Ultrafine Grain ◽  
Pulse Laser Irradiation ◽  
Energy Pulse

scholarly journals MODIFICATION OF THE ALUMINUM ALLOY BY THE RADIATION AND MECHANICAL TREATMENT

2020 ◽  
pp. 109-113
Author(s):  
S.E. Donets ◽  
V.V. Lytvynenko ◽  
V.F. Klepikov ◽  
Yu.F. Lonin ◽  
A.G. Ponomarev ◽  
...  
Keyword(s):  
Aluminum Alloy ◽  
Electron Beam ◽  
Relativistic Electron ◽  
Relativistic Electron Beam ◽  
Mechanical Treatment ◽  
Fractographic Analysis ◽  
High Current ◽  
Performance Properties ◽  
Property Modification

The paper discusses the problem of increasing the performance properties of aluminum alloy D16 for possible more efficient use in the fields of transport engineering. A property modification tool is a high current relativistic electron beam. The irradiation occurs in a vacuum. The peculiarities of the layer distribution of characteristic zones resulting from irradiation are investigated. Metallographic and fractographic analysis is carried out, and microhardness values are measured.

Characterization of SiCp/2024 aluminum alloy composites prepared by mechanical processing in a low energy ball mill

1999 ◽  
Vol 262 (1-2) ◽  
pp. 9-15 ◽  
Author(s):  
R. Angers ◽  
M.R. Krishnadev ◽  
R. Tremblay ◽  
J.-F. Corriveau ◽  
D. Dubé
Keyword(s):  
Aluminum Alloy ◽  
Ball Mill ◽  
Low Energy ◽  
Mechanical Processing ◽  
2024 Aluminum Alloy ◽  
Energy Ball

On ground test of AL6016 structure influenced from space proton irradiated by MC-50 cyclotron

2018 ◽  
Vol 32 (19) ◽  
pp. 1840072
Author(s):  
Yong Hong Kim ◽  
Dae Weon Kim ◽  
Dong Chul Shin ◽  
Tae Gyu Kim ◽  
Yong Bae Kim
Keyword(s):  
Tensile Strength ◽  
Aluminum Alloy ◽  
Elastic Modulus ◽  
Kinetic Energy ◽  
High Energy ◽  
Low Energy ◽  
The Other ◽  
Thick Wall ◽  
Ground Test ◽  
Alloy 6061

Aluminum alloy 6061 is widely used for space development since the advent of space era irradiated with protons using cyclotron. In the condition of confined 5-mm thick wall, protons of 5 MeV, the case of low energy showed larger damage in the structure of aluminum alloy than those of 25.4 MeV, the case of high energy. Protons of 5 MeV stopped and transferred all kinetic energy into the 5-mm thick wall, on the other hand, protons of 25.4 MeV were penetrating and a few energy transferred. Elastic modulus reduced, but elongation was increased, finally tensile strength obviously showed that longer duration of exposure yielded weaker strength of material.

Techniques for Transmission Electron Microscopy of Fiber-Matrix Interfaces in Aluminum Alloy-Boron Composites by Ion Erosio

1971 ◽  
Vol 29 ◽  
pp. 204-205
Author(s):  
G. G. Shaw
Keyword(s):  
Electron Microscopy ◽  
Transmission Electron Microscopy ◽  
Aluminum Alloy ◽  
Electron Beam ◽  
Pure Aluminum ◽  
Ion Milling ◽  
Transmission Electron ◽  
Fiber Matrix ◽  
Ion Erosion ◽  
Row Of Fibers

The morphology and composition of the fiber-matrix interface can best be studied by transmission electron microscopy and electron diffraction. For some composites satisfactory samples can be prepared by electropolishing. For others such as aluminum alloy-boron composites ion erosion is necessary.When one wishes to examine a specimen with the electron beam perpendicular to the fiber, preparation is as follows: A 1/8 in. disk is cut from the sample with a cylindrical tool by spark machining. Thin slices, 5 mils thick, containing one row of fibers, are then, spark-machined from the disk. After spark machining, the slice is carefully polished with diamond paste until the row of fibers is exposed on each side, as shown in Figure 1.In the case where examination is desired with the electron beam parallel to the fiber, preparation is as follows: Experimental composites are usually 50 mils or less in thickness so an auxiliary holder is necessary during ion milling and for easy transfer to the electron microscope. This holder is pure aluminum sheet, 3 mils thick.

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