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

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:
DRNTU::Engineering::Aeronautical engineering::Materials of construction
DRNTU::Engineering::Aeronautical engineering
Online Access:http://hdl.handle.net/10356/13467
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Institution: Nanyang Technological University
Language: English
id sg-ntu-dr.10356-13467
record_format dspace
spelling sg-ntu-dr.10356-134672023-03-11T17:25:32Z An autonomous ultrasonic fastener holes inspection system of an aircraft lower wing skin Lim, Chee Wei. Wong, Brian Stephen School of Mechanical and Production Engineering DRNTU::Engineering::Aeronautical engineering::Materials of construction DRNTU::Engineering::Aeronautical engineering 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. Master of Engineering (MPE) 2008-10-20T08:19:35Z 2008-10-20T08:19:35Z 1999 1999 Thesis http://hdl.handle.net/10356/13467 en 156 p. application/pdf
institution Nanyang Technological University
building NTU Library
continent Asia
country Singapore
Singapore
content_provider NTU Library
collection DR-NTU
language English
topic DRNTU::Engineering::Aeronautical engineering::Materials of construction
DRNTU::Engineering::Aeronautical engineering
spellingShingle DRNTU::Engineering::Aeronautical engineering::Materials of construction
DRNTU::Engineering::Aeronautical engineering
Lim, Chee Wei.
An autonomous ultrasonic fastener holes inspection system of an aircraft lower wing skin
description 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.
author2 Wong, Brian Stephen
author_facet Wong, Brian Stephen
Lim, Chee Wei.
format Theses and Dissertations
author Lim, Chee Wei.
author_sort Lim, Chee Wei.
title An autonomous ultrasonic fastener holes inspection system of an aircraft lower wing skin
title_short An autonomous ultrasonic fastener holes inspection system of an aircraft lower wing skin
title_full An autonomous ultrasonic fastener holes inspection system of an aircraft lower wing skin
title_fullStr An autonomous ultrasonic fastener holes inspection system of an aircraft lower wing skin
title_full_unstemmed An autonomous ultrasonic fastener holes inspection system of an aircraft lower wing skin
title_sort autonomous ultrasonic fastener holes inspection system of an aircraft lower wing skin
publishDate 2008
url http://hdl.handle.net/10356/13467
_version_ 1761781940438958080

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