Testing of C/PPS structural element for aircraft

Result code in IS VaVaI
<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F68407700%3A21220%2F19%3A00331638" target="_blank" >RIV/68407700:21220/19:00331638 - isvavai.cz</a>
Result on the web
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DOI - Digital Object Identifier
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Result language
angličtina
Original language name
Testing of C/PPS structural element for aircraft
Original language description
Presented work deals with testing and FE evaluation of composite structural element manufactured from C/PPS 5H satin fabric [1,2] used for junction of rib with keel beam lower panel in aircraft construction. Tested composite version should replace titanium one which is used nowadays. Loading of composite special element (bracket) was simulated in FE software Abaqus and it was proved that it should withstand the load without failure. After the manufacturing of three specimens an experiment was done to confirm the FE results.
Czech name
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Czech description
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Project
<a href="/en/project/FV30033" target="_blank" >FV30033: Design and manufacturing process development of primary aircraft parts of advanced shapes of reinforced thermoplastics</a><br>
Continuities
P - Projekt vyzkumu a vyvoje financovany z verejnych zdroju (s odkazem do CEP)

Publication year
2019
Confidentiality
S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů

Article name in the collection
EAN 2019 57th conference on experimental stress analysis CONFERENCE PROCEEDINGS
ISBN
9788021457669
ISSN
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e-ISSN
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Number of pages
4
Pages from-to
361-364
Publisher name
Česká společnost pro mechaniku
Place of publication
Praha
Event location
Luhačovice
Event date
Jun 3, 2019
Type of event by nationality
WRD - Celosvětová akce
UT code for WoS article
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