A study of the deformation of patented steel wire

1970 ◽  
Vol 1 (2) ◽  
pp. 465-477 ◽  
Author(s):  
George Langford
Keyword(s):  
Steel Wire ◽  
Patented Steel

Relationship of internal friction to the fatigue life of patented steel wire

1984 ◽  
Vol 19 (6) ◽  
pp. 522-527 ◽  
Author(s):  
O. N. Romaniv ◽  
L. P. Laz'ko ◽  
A. S. Krys'kiv
Keyword(s):  
Fatigue Life ◽  
Internal Friction ◽  
Steel Wire ◽  
Relationship Of ◽  
Patented Steel

Fatigue of patented steel wire

1979 ◽  
Vol 15 (1) ◽  
pp. 48-50 ◽  
Author(s):  
O. N. Romaniv ◽  
I. A. Berezyuk
Keyword(s):  
Steel Wire ◽  
Patented Steel

Optimisation of brass plating condition in plating of patented steel wire

2011 ◽  
Vol 27 (1) ◽  
pp. 19-25 ◽  
Author(s):  
M Saadatmand ◽  
S Sadeghpour ◽  
J Aghazadeh Mohandesi
Keyword(s):  
Steel Wire ◽  
Brass Plating ◽  
Patented Steel

Preparation of Electron Transparent Metal-Matrix Composites

1968 ◽  
Vol 26 ◽  
pp. 334-335 ◽  
Author(s):  
M. R. Pinnel ◽  
A. Lawley
Keyword(s):  
Stainless Steel ◽  
Load Transfer ◽  
Volume Fraction ◽  
Steel Wire ◽  
Initial Step ◽  
Interfacial Region ◽  
Matrix Composites ◽  
Specific Test ◽  
The Matrix ◽  
The One

Numerous phenomenological descriptions of the mechanical behavior of composite materials have been developed. There is now an urgent need to study and interpret deformation behavior, load transfer, and strain distribution, in terms of micromechanisms at the atomic level. One approach is to characterize dislocation substructure resulting from specific test conditions by the various techniques of transmission electron microscopy. The present paper describes a technique for the preparation of electron transparent composites of aluminum-stainless steel, such that examination of the matrix-fiber (wire), or interfacial region is possible. Dislocation substructures are currently under examination following tensile, compressive, and creep loading. The technique complements and extends the one other study in this area by Hancock.The composite examined was hot-pressed (argon atmosphere) 99.99% aluminum reinforced with 15% volume fraction stainless steel wire (0.006″ dia.).Foils were prepared so that the stainless steel wires run longitudinally in the plane of the specimen i.e. the electron beam is perpendicular to the axes of the wires. The initial step involves cutting slices ∼0.040″ in thickness on a diamond slitting wheel.

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