Design and Verification of a Jet Trainer Aircraft Primary Structure Repair Using an Adhesively Bonded Boron Composite Patch

Result code in IS VaVaI
<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F00010669%3A_____%2F13%3A%230001564" target="_blank" >RIV/00010669:_____/13:#0001564 - isvavai.cz</a>
Result on the web
<a href="http://www.vzlu.cz/cz/transfer-vysledku/clanky-ve-sbornicich-d/" target="_blank" >http://www.vzlu.cz/cz/transfer-vysledku/clanky-ve-sbornicich-d/</a>
DOI - Digital Object Identifier
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Result language
angličtina
Original language name
Design and Verification of a Jet Trainer Aircraft Primary Structure Repair Using an Adhesively Bonded Boron Composite Patch
Original language description
Different types of damages or cracks in structural parts of airframe can occur in the service of aging aircrafts. Damages are commonly repaired by patch which can be joined to the original structure by different techniques like riveting and bonding for example. The paper provides information about a repair of fatigue crack in metallic wing structure of a jet trainer aircraft using adhesively bonded boron composite patch. Design and numerical analysis of the repair is presented.
Czech name
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Czech description
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Project
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Continuities
I - Institucionalni podpora na dlouhodoby koncepcni rozvoj vyzkumne organizace

Publication year
2013
Confidentiality
S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů

Article name in the collection
3rd International Conference of Engineering Against Failure (ICEAF III)
ISBN
978-960-88104-3-3
ISSN
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e-ISSN
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Number of pages
11
Pages from-to
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Publisher name
Laboratory of Technology & Strength of Materials, University of Patras (Greece)
Place of publication
Kos (Greece)
Event location
Kos (Greece)
Event date
Jun 26, 2013
Type of event by nationality
WRD - Celosvětová akce
UT code for WoS article
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