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Description
This executive summary covers the process and results of developing a method to measure packing loads on an evacuation slide system packboard. Since evacuation slides are packed very tightly to fit on the aircraft, the packing process requires large amount of stress on the packboard that holds the slide components.

This executive summary covers the process and results of developing a method to measure packing loads on an evacuation slide system packboard. Since evacuation slides are packed very tightly to fit on the aircraft, the packing process requires large amount of stress on the packboard that holds the slide components. Methods such as load cells, strain gauges, and pressure sensitive films were found to be too inaccurate. An electronic pressure mapping device was found to be the only feasible and accurate method in measuring loads on the packboard.
ContributorsHeitzman, Nicholas James (Author) / Liao, Yabin (Thesis director) / Rajagopalan, Jagannathan (Committee member) / Pope, Tony (Committee member) / Barrett, The Honors College (Contributor) / Mechanical and Aerospace Engineering Program (Contributor)
Created2013-05
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Description
This paper investigates Surface Mechanical Attrition Treatment (SMAT) and the influence of treatment temperature and initial sample surface finish on the corrosion resistance of 7075-T651 aluminum alloy. Ambient SMAT was performed on AA7075 samples polished to 80-grit initial surface roughness. Potentiodynamic polarization and electrochemical impedance spectroscopy (EIS) tests were used

This paper investigates Surface Mechanical Attrition Treatment (SMAT) and the influence of treatment temperature and initial sample surface finish on the corrosion resistance of 7075-T651 aluminum alloy. Ambient SMAT was performed on AA7075 samples polished to 80-grit initial surface roughness. Potentiodynamic polarization and electrochemical impedance spectroscopy (EIS) tests were used to characterize the corrosion behavior of samples before and after SMAT. Electrochemical tests indicated an improved corrosion resistance after application of SMAT process. The observed improvements in corrosion properties are potentially due to microstructural changes in the material surface induced by SMAT which encouraged the formation of a passive oxide layer. Further testing and research are required to understand the corrosion related effects of cryogenic SMAT and initial-surface finish as the COVID-19 pandemic inhibited experimentation plans.
ContributorsDeorio, Jordan Anthony (Author) / Solanki, Kiran (Thesis director) / Rajagopalan, Jagannathan (Committee member) / Mechanical and Aerospace Engineering Program (Contributor) / Barrett, The Honors College (Contributor)
Created2020-05