Drone Propeller Blade Material Optimization Using Modern Computational Method
The result's identifiers
Result code in IS VaVaI
<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F00216275%3A25510%2F21%3A39917372" target="_blank" >RIV/00216275:25510/21:39917372 - isvavai.cz</a>
Result on the web
<a href="https://www.tf.llu.lv/conference/proceedings2021/Papers/TF199.pdf" target="_blank" >https://www.tf.llu.lv/conference/proceedings2021/Papers/TF199.pdf</a>
DOI - Digital Object Identifier
<a href="http://dx.doi.org/10.22616/ERDev.2021.20.TF199" target="_blank" >10.22616/ERDev.2021.20.TF199</a>
Alternative languages
Result language
angličtina
Original language name
Drone Propeller Blade Material Optimization Using Modern Computational Method
Original language description
The paper deals with the optimization of the material of the propeller blade Drone DJI Mavic Pro using a modern computational method in order to find a suitable material for 3D printing. For computational simulation, ANSYS Discovery Live 2019 was used as a modern computational method. SolidWorks 2020 was used to create a 3D model of the propeller blade. ABS, PLA, PETG were selected as suitable materials for the drone propeller blade, which will be produced by 3D printing. One of them was thought that would best meet all requirements. Computational models were made for this purpose. Deformation-stress states were calculated and calculations as “a wind tunnel” were done. It was a simulation of the take-off of a drone as a solution of rotation of one blade in a wind tunnel with defined different temperatures and rotational speeds. The results of these simulations are evaluated. The highest stress values in the blade area were for the ABS material and the lowest for the PLA material. In the area of the propeller legs, which simulate attachment to the drone, the ABS material showed the highest stress values and the PETG material showed the lowest stress values. The largest deformation in the part of the leaf sheets was recorded by the ABS material and the lowest by PLA. The flight and flight conditions simulations were simulated at different temperatures of -2 and + 25 ºC and flight times of 1 and 10 s for each material. Based on the computational results, the PETG material was selected for 3D printing of the drone propeller blade.
Czech name
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Czech description
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Classification
Type
D - Article in proceedings
CEP classification
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OECD FORD branch
20301 - Mechanical engineering
Result continuities
Project
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Continuities
S - Specificky vyzkum na vysokych skolach<br>I - Institucionalni podpora na dlouhodoby koncepcni rozvoj vyzkumne organizace
Others
Publication year
2021
Confidentiality
S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů
Data specific for result type
Article name in the collection
Engineering for Rural Development
ISBN
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ISSN
1691-3043
e-ISSN
1691-5976
Number of pages
6
Pages from-to
878-883
Publisher name
Latvia University of Afgriculture
Place of publication
Jelgava
Event location
Jeglava
Event date
May 26, 2021
Type of event by nationality
EUR - Evropská akce
UT code for WoS article
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