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Massachusetts Institute of Technology

Durability testing of an aircraft structural health monitoring system

Abstract

dc:description.abstract

Structural health monitoring (SHM) is an emerging technology leading to systems capable of continuously monitoring structures for damage. Aerospace structures have one of the highest payoffs for SHM systems because damage can lead to catastrophic and expensive failures. Prior work in SHM has focused on damage detection methods and sensor optimization, however, the topics of durability, reliability, and longevity of these systems has not been addressed. A framework for developing SHM durability test standards for aerospace vehicles is offered. Existing standards for the durability of commercial and military aircraft avionics are identified, and the relation to SHM systems is described. Using these existing standards, a test matrix and testing specifics are developed to assess the durability of SHM systems. Careful consideration is necessary in defining the 'system' under testing. Criteria are defined to establish whether a sensor/structural system has been affected by the various environments. Extensive experimental results from durability testing of a surface-mounted piezoelectric Lamb-wave SHM system are presented. Environments tested include temperature extremes, humidity, fluid susceptibility, altitude, and mechanical strain.

Degree

thesis:*
Department dc:contributor.department
Massachusetts Institute of Technology. Dept. of Aeronautics and Astronautics.
Grantor dc:publisher
Massachusetts Institute of Technology
Year dc:date.issued
2006

Author and committee

dc:creator, dc:contributor.*
Author dc:creator
  • Chambers, Jeffrey Thomas
Advisor dc:contributor.advisor
  • Brian L. Wardle.

Subjects

dc:subject × 1

Rights

dc:rights
Statement dc:rights
  • M.I.T. theses are protected by copyright. They may be viewed from this source for any purpose, but reproduction or distribution in any format is prohibited without written permission. See provided URL for inquiries about permission.
Language dc:language.iso
eng

Identifiers

dc:identifier.*
Handle dc:identifier.uri
http://hdl.handle.net/1721.1/37849
OAI identifier oai:identifier
oai:dspace.mit.edu:1721.1/37849

Chain of custody

source
Harvested from
MIT
Base URL
dspace.mit.edu/oai/request
Last updated
2026-07-22
Source record
OAI-PMH GetRecord
citation

Chambers, Jeffrey Thomas. Durability testing of an aircraft structural health monitoring system. Massachusetts Institute of Technology, 2006. http://hdl.handle.net/1721.1/37849