In-Flight Fatigue Crack Monitoring of an Aircraft Engine Cowling

<p>This research investigates the feasibility of implementing an in-flight fatigue crack monitoring system in an airplane to identify fatigue crack growth. An acoustic emission data acquisition system coupled with a Kohonen self organizing map neural network were used to perform the analysis.</p> <p>Fatigue cracking was responsible for ripping the top of a fuselage off an Aloha Airlines Boeing 737-200 as it carried passengers over the Pacific Ocean, killing some aboard. This tragedy is perhaps a precursor of problems to come, as our nation’s aircraft age. These planes experience fatigue as they perform their daily routine of ferrying passengers from location to location. Fatigue can initiate cracking within the aircraft’s structure and at least damage a small expendable part of the plane, or at most damage a vital part of the airplane leading to disaster as happened to the Aloha Airlines flight.</p> <p>In an attempt to curb this sort of devastation, this research involves the development of an in-flight fatigue crack monitoring system. Such a system would have the ability to identify possible crack sources before the crack would have the chance to cause significant damage. Advantages of this type of system would be first, an obvious safety cushion, and second, lower maintenance costs because routine parts replacement and inspection could be minimized.</p>

Name thesis:degree_name

Master of Science in Aerospace Engineering

Level thesis:degree_level

Thesis - Open Access

Discipline thesis:degree_discipline

Aerospace Engineering

Year

1998

Author dc:creator

• Vaughn, Samuel Gordon, III

Contributors dc:contributor

• Eric v. K. Hill
• Frank J. Radosta
• Charles W. Bishop

• fatigue
• cracks
• aircraft engine
• cowling
• Boeing 737-200
• Aerospace Engineering
• Aviation

Repository record dc:identifier

https://commons.erau.edu/db-theses/222

OAI identifier oai:identifier

oai:commons.erau.edu:db-theses-1294