Cold welding
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Cold or contact welding was first recognized as a general materials phenomenon in the 1940s. It was then discovered that two clean, flat surfaces of similar metal would strongly adhere if brought into contact under vacuum.
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[edit] Process
It is now known that the force of adhesion following first contact can be augmented by pressing the metals tightly together, increasing the duration of contact, raising the temperature of the workpieces, or any combination of the above. Research has shown that even for very smooth metals, only the high points of each surface, called asperities, touch the opposing piece. Perhaps as little as a few thousandths of a percent of the total surface is involved. However, these small areas of taction develop powerful molecular connections; electron microscope investigations of contact points reveal that an actual welding of the two surfaces takes place after which it is impossible to discern the former asperitic interface. If the original surfaces are sufficiently smooth the metallic forces between them eventually draw the two pieces completely together and eliminate even the macroscopic interface.
Exposure to oxygen or certain other reactive compounds produces surface layers which reduce or completely eliminate the cold welding effect. This is especially true if, say, a metal oxide has mechanical properties similar to those of the parent element (or softer), in which case surface deformations do not crack the oxide film.
[edit] Applications
Powders in powder metallurgy use cold welding to best advantage because they present large surface areas over which vacuum contact can occur. For instance, a 1 cm cube of metal comminuted into 240–100 mesh-sieved particles (60–149 μm) yields approximately 1.25×106 grains having a total surface area of 320 cm2. This powder, reassembled as a cube, would be about twice as big as before since half the volume consists of voids.
If a strong final product is desired, it is important to obtain minimum porosity (that is, high starting density) in the initial powder-formed mass. Minimum porosity results in less dimensional change upon compression of the workpiece as well as lower pressures, decreased temperatures, and less time to prepare a given part. Careful vibratory settling reduces porosity in monodiameter powders to less than 40%. A decrease in average grain size does not decrease porosity, although large increases in net grain area will enhance the contact welding effect and markedly improve the "green strength" of relatively uncompressed powder. In space applications cold welding in the forming stage may be adequate to produce usable hard parts, and molds may not even be required to hold the components for subsequent operations such as sintering.
Hard monodiameter spheres packed like cannonballs into body-centered arrays give a porosity of about 25%, significantly lower than the ultimate minimum of 35% for vibrated collections of monodiameter spheres. (The use of irregularly shaped particles produces even more porous powders.) Porosity may be reduced further by using a selected range of grain sizes, typically 3–6 carefully chosen gauges in most terrestrial applications. Theoretically, this should permit less than 4% porosity in the starting powder, but with binary or tertiary mixtures 15–20% is more the rule. In theory, powders containing a particles in a wide range of sizes can approach 0% porosity as the finest grains are introduced. However, powder mixtures do not naturally pack to the closest configuration even if free movement is induced by vibration or shaking. Gravitational differential settling of the mixture tends to segregate grains in the compress, and some degree of cold welding occurs immediately upon formation of the powder compress which generates internal frictions that strongly impede further compaction. Considerable theoretical and practical analyses already exist to assist in understanding the packing of powders.[1][2][3][4][5][6][7]
Moderate forces applied to a powder mass immediately cause grain rearrangements and superior packing. Specifically, pressures of 105 Pa (N/m2) decrease porosity by 1–4%; increasing the force to 107 Pa gains only an additional 1–2%. However, the distinct physical effects of particle deformation and mass flow become significant at still higher pressures or if heat is applied. Considerably greater force is required mechanically to close all remaining voids by plastic flow of the compressed metal.
[edit] In space
Mechanical problems in early satellites were sometimes attributed to cold welding. However, there are no documented cases of it actually occurring in orbit, except in experiments deliberately designed to provoke it (with susceptible materials, great care to avoid contamination, deliberate mechanical removal of oxide layers, etc.). While cold welding is real, an unqualified claim that "in space metals stick" should be treated as an urban legend.
[edit] References
- ^ Dexter, A. R.; and Tanner, D. W.: Packing Densities of Mixtures of Spheres with Log-Normal Size Distributions. Nature (Physical Science), vol. 238, no. 80, 10 July 1972, pp. 31-32
- ^ Criswell, David R.: The Rosiwal Principle and the Regolithic Distributions of Solar Wind Elements. Proc. 6th Lunar Sci. Conf., Pergamon Press, New York, 1975, pp. 1967-1987
- ^ Powell, M. J.: Computer-Simulated Random Packing of Spheres. Powder Technology, vol. 25, no. 1, 1980, pp.45-52
- ^ Powell, M. J.: Distribution of Near-Neighbors in Randomly Packed Hard Spheres. Powder Technology, vol. 26, no. 2, 1980, pp. 221-223
- ^ Shahinpoor, M.: Statistical Mechanical Considerations on the Random Packing of Granular Materials. Powder Technology, vol. 25, no. 2, 1980, pp. 163-176
- ^ Spencer, B. B.; and Lewis, B. E.: HP-67-97 and TI-59 Programs to Fit the Normal and Log-Normal Distribution Functions by Linear Regression. Powder Technology, vol. 27, no. 2, 1980, pp. 219-226
- ^ Visscher, W. H.; and Bolsterzi, M.: Random Packing of Equal and Unequal Spheres in Two and Three Dimensions. Nature, vol. 239, no. 5374, 27 October 1972, pp. 504-507
- Much of this article was imported from Advanced Automation for Space Missions:Appendix 4C