Date of Award
3-10-2010
Document Type
Thesis
Degree Name
Master of Science in Industrial Hygiene
Department
Department of Systems Engineering and Management
First Advisor
Jeremy M. Slagley, PhD
Abstract
Within the United States Air Force (USAF) Advanced Composite Material (ACM) is gaining an increasing use in military aircraft. With the number of aircraft that have increasingly large amounts of ACM materials, the probability of an incident with one of these aircraft also increases. When such an incident occurs the aircraft needs to be disassembled, removed, and later inspected as part of the accident investigation process. This disassembly process is termed “Crash Recovery Operations.” Carbon fibers have been shown to be hazardous to human health and a pilot study raised the suspicion that nanosized aerosol may be generated during the cutting of carbon fiber panels. Due to this, a bench top study was conducted to evaluate the effectiveness of several fiber controls. Additionally, an evaluation of a number of direct reading instruments and traditional gravimetric sampling techniques were evaluated to determine a sampling protocol for evaluation composite fibers. A statistically significant (F-value = < 0.0001) shift towards larger diameters in the idealized particle size distribution was shown for both wetted water and water controls when compared to a baseline of no control when cutting burnt ACM. Recommendations for future evaluation and control of composite fiber processes were made.
AFIT Designator
AFIT-GIH-ENV-10-M01
DTIC Accession Number
ADA518994
Recommended Citation
Ferreri, Matthew R., "Particulate Characterization and Control Evaluation for Carbon Fiber Composite Aircraft Crash Recovery Operations" (2010). Theses and Dissertations. 2134.
https://scholar.afit.edu/etd/2134