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Production of Extruded Tube Hollows for Titanium 3AI-2.5V Hydraulic Tubing
ISSN: 0148-7191, e-ISSN: 2688-3627
Published February 01, 1973 by SAE International in United States
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The warm extrusion process is described as adapted to making Ti-3A 1-2.5V tube hollows to be reduced for high-quality aircraft hydraulic tubing. The advantages of this process over conventional hot extrusion appear to be sufficient to warrant further studies aimed at improved uniformity.
Alloy segregation is noted in the forged extrusion billets which can be eliminated by heat treatment. It is presumed that this segregation is related to problems encountered in fabrication to tubing and has an effect on the variability of properties in the final tubing. An approach to the problem is suggested.
|Technical Paper||Defects in High Quality Aircraft Tubing and Inspection Methods|
|Technical Paper||Production of MAGNESIUM-Alloy Aircraft Parts|
CitationBaroch, E., McClanahan, B., and Curtis, R., "Production of Extruded Tube Hollows for Titanium 3AI-2.5V Hydraulic Tubing," SAE Technical Paper 730627, 1973, https://doi.org/10.4271/730627.
- Rice J. “Precision Metal,” “Titanium Extrusions.” February 1968 27 30
- Harruff G. W. Velden J. Vander Nelson W. G. Spurr W. Quist W. “Titanium-3A1-2.5V C W Hydraulic Tubing Development.” FAA-SS-72-60 October 1972
- Kaufmann P. D. “Final Report on Experimental Extrusion of Zr-2.5Nb Tubing.” Teledyne Wah Chang Albany May 7 1970
- Kearns J. J. “Thermal Expansion and Preferred Orientation in Zircaloy.” WAPD-TM-472, Contract AT-11-1-GEN-14 November 1965