A Study on Topology Optimization of Airplane Air Brake Bracing Beam

Result code in IS VaVaI
<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F60162694%3AG43__%2F19%3A00537213" target="_blank" >RIV/60162694:G43__/19:00537213 - isvavai.cz</a>
Result on the web
<a href="http://dx.doi.org/10.1109/MILTECHS.2019.8870028" target="_blank" >http://dx.doi.org/10.1109/MILTECHS.2019.8870028</a>
DOI - Digital Object Identifier
<a href="http://dx.doi.org/10.1109/MILTECHS.2019.8870028" target="_blank" >10.1109/MILTECHS.2019.8870028</a>

Result language
angličtina
Original language name
A Study on Topology Optimization of Airplane Air Brake Bracing Beam
Original language description
The article presents a study of L-39ZA airplane air brake bracing beam using topology optimization in order to save the weight. Topology optimization using SW Ansys is performed for the same aluminum alloy material as the origin part to achieve the same ability of carrying the load expressed by braced beam stress-strain state and deformation. The weight saving achieved has the value 31%. The optimized part is possible to produce by additive manufacturing to match its complex shape.
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
2019
Confidentiality
S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů

Article name in the collection
International Conference on Military Technologies (ICMT) 2019
ISBN
978-172814593-8
ISSN
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e-ISSN
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Number of pages
4
Pages from-to
8870028
Publisher name
Institute of Electrical and Electronics Engineers Inc.
Place of publication
Brno
Event location
Brno, Czech Republic
Event date
May 30, 2019
Type of event by nationality
WRD - Celosvětová akce
UT code for WoS article
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