Damage detection in bonded repairs using piezoceramics

This paper reports on the development of a perceptive repair or smart system which will provide information on the in-service performance of the repair and the associated aerospace structure. In this respect, this paper focuses on the detection of disbond in the adhesive layer between adhered (boron...

Full description

Saved in:
Bibliographic Details
Published inSmart materials and structures Vol. 9; no. 4; pp. 466 - 475
Main Authors Chiu, W K, Galea, S C, Koss, L L, Rajic, N
Format Journal Article
LanguageEnglish
Published Bristol IOP Publishing 01.08.2000
Institute of Physics
Subjects
Online AccessGet full text
ISSN0964-1726
1361-665X
DOI10.1088/0964-1726/9/4/309

Cover

More Information
Summary:This paper reports on the development of a perceptive repair or smart system which will provide information on the in-service performance of the repair and the associated aerospace structure. In this respect, this paper focuses on the detection of disbond in the adhesive layer between adhered (boron/epoxy unidirectional composite) and the metallic parent (Al) structure. One of the criteria of this smart system is that it must be economical, reliable and, preferably, self-powered. To this end, it was proposed that piezoceramic of piezoelectric material be utilized because of their ease of application. These materials were chosen because they can be used both as a actuator and as a sensor. This paper presents a set of numerical investigations performed to highlight the viability of using this material system, and the associated signal analysis that can be employed to detect the presence or the development of disbonds in the adhesive in a bonded repair situation.
Bibliography:ObjectType-Article-2
SourceType-Scholarly Journals-1
ObjectType-Feature-1
content type line 23
ISSN:0964-1726
1361-665X
DOI:10.1088/0964-1726/9/4/309