The objectives of this program were to assemble a high-temperature continuous-rolling facility and to develop a process for producing typical airframe sections with 1T-bend radii. A return-flange hat and a return-flange zee were selected for development. Both shapes were to be formed from 6Al-4V and 8Al-1Mo-1V titanium alloy coil stock. Simulated production runs including part lengths up to 50 feet were planned to verify the process developed. (Author)
Development of High-Temperature Continuous-Rolling Process for Forming Minimum-Radii Titanium Sections
1969
151 pages
Report
Keine Angabe
Englisch
Manufacturing Processes & Materials Handling , Aircraft , Airframes , Titanium alloys , Structural parts , Rolling(Metallurgy) , Hot working , Configuration , Bending , Compressive properties , Material forming , Heaters , Dies , Ceramic materials , Plasticity , Weight saving , Radii , Titanium alloy 8Al 1Mo 1V , Titanium alloy 6Al 4V
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