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Output details

12 - Aeronautical, Mechanical, Chemical and Manufacturing Engineering

Cranfield University

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Article title

Effect of laser shock peening on residual stress and fatigue life of clad 2024 aluminium sheet containing scribe defects

Type
D - Journal article
Title of journal
Materials Science and Engineering A: Structural Materials: Properties, Microstructure and Processing
Article number
-
Volume number
548
Issue number
-
First page of article
142
ISSN of journal
0921-5093
Year of publication
2012
URL
-
Number of additional authors
5
Additional information

An international collaboration between Cranfield, the Open University, Airbus Germany and Metal Improvements (UK) into laser peening treatments to repair mechanical damage in aircraft and control growth of fatigue cracks. This is quicker and less intrusive than cutting out the damaged area and riveting a repair patch. (Domenico Furfari, domenico.furfari@airbus.com) Research results achieved the desired performance, leading to two further industry-funded projects with Airbus. Collaborations also emerged with Metal Improvements and Toshiba, suppliers of laser peen treatments. Airbus now have high Technology-Readiness level internal programmes to further develop other peening treatments to enhance performance of metallic aircraft structures (contact as above).

Interdisciplinary
-
Cross-referral requested
-
Research group
F - Structures and Machine Systems
Proposed double-weighted
No
Double-weighted statement
-
Reserve for a double-weighted output
No
Non-English
No
English abstract
-