NASA NTRS · 19950008072
Advanced method and processing technology for complicated shape airframe part forming
Abstract
Slow deformation modes of forming give considerably higher residual fatigue life of the airframe part. It has experimentally proven that fatigue life of complicated shape integral airframe panels made of high strength aluminum alloys is significantly increased after creep deformation process. To implement the slow deformation mode forming methods, universal automated equipment was developed. Multichannel forming systems provide high accuracy of airframe part shape eliminating residual stresses and spring effect. Forming process multizone control technology was developed and experimentally proved that static/fatigue properties of formed airframe parts are increased.
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Miodushevsky, P. V., Rajevskaya, G. A.. 1994-09-01. Advanced method and processing technology for complicated shape airframe part forming. https://ntrs.nasa.gov/citations/19950008072
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