An autonomous ultrasonic fastener holes inspection system of an aircraft lower wing skin

An aircraft structure is subjected to stress and fatigue during flying. Fasteners like rivets and bolts bear a large part of the stress and thus require frequent inspection for cracks around the fastener's holes. These cracks are unique in that it radial from the fastener's hole which made...

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Bibliographic Details
Main Author: Lim, Chee Wei.
Other Authors: Wong, Brian Stephen
Format: Theses and Dissertations
Language:English
Published: 2008
Subjects:
Online Access:http://hdl.handle.net/10356/13467
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Institution: Nanyang Technological University
Language: English
Description
Summary:An aircraft structure is subjected to stress and fatigue during flying. Fasteners like rivets and bolts bear a large part of the stress and thus require frequent inspection for cracks around the fastener's holes. These cracks are unique in that it radial from the fastener's hole which made radiography nearly impossible in picking it up.