Monitoring of Crack Growth in a Structure Under a Composite Patch

Michał Sałaciński; Piotr Synaszko; Michał Stefaniuk; Krzysztof Dragan

doi:10.2478/v10164-010-0043-5

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Monitoring of Crack Growth in a Structure Under a Composite Patch

Fatigue of Aircraft Structures

Volume 2011 (2011): Issue 3 (August 2011)

By: Michał Sałaciński, Piotr Synaszko, Michał Stefaniuk and Krzysztof Dragan

Open Access

|Aug 2011

Abstract

In civil as well as in military aviation, boron, carbon and aramid fiber reinforced composites are employed for the repair of metal structures. After such composite bonded repairs, the monitoring of the repaired structure along with the composite patch and its bond is necessary.

The paper describes the possibilities of utilizing NDT methods for periodical check-ups and examinations. Also, a novel approach to continuous monitoring of the repaired structure is presented.

References

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Articles in this issue

DOI: https://doi.org/10.2478/v10164-010-0043-5 | Journal eISSN: 2300-7591 | Journal ISSN: 2081-7738

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Language: English

Page range: 103 - 111

Published on: Aug 25, 2011

Published by: ŁUKASIEWICZ RESEARCH NETWORK – INSTITUTE OF AVIATION

In partnership with: Paradigm Publishing Services

Publication frequency: 1 issue per year

Related subjects:

Engineering,

Introductions and overviews,

Engineering, other

© 2011 Michał Sałaciński, Piotr Synaszko, Michał Stefaniuk, Krzysztof Dragan, published by ŁUKASIEWICZ RESEARCH NETWORK – INSTITUTE OF AVIATION
This work is licensed under the Creative Commons License.

Volume 2011 (2011): Issue 3 (August 2011)