Optimization of SUAV’s propeller in a hover

Small unmanned aerial vehicles (SUAVs) have found a widespread application in past decades. However, as the criticality of the missions for which they can be used increases, the demand for improvement of their efficiency increases as well. The paper focuses on a propeller driven SUAVs of a multiroto...

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Main Authors: Hnidka Jakub, Rozehnal Dalibor, Maňas Karel
Format: Article
Language:English
Published: EDP Sciences 2020-01-01
Series:MATEC Web of Conferences
Online Access:https://www.matec-conferences.org/articles/matecconf/pdf/2020/09/matecconf_dyn-wind20_00045.pdf
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author Hnidka Jakub
Rozehnal Dalibor
Maňas Karel
author_facet Hnidka Jakub
Rozehnal Dalibor
Maňas Karel
author_sort Hnidka Jakub
collection DOAJ
description Small unmanned aerial vehicles (SUAVs) have found a widespread application in past decades. However, as the criticality of the missions for which they can be used increases, the demand for improvement of their efficiency increases as well. The paper focuses on a propeller driven SUAVs of a multirotor type, equipped with an electric motor, battery and propeller. The paper presents a simplified method of calculation of the SUAV maximal endurance, if the characteristics of all components of the propulsion system are known. To improve the overall efficiency of the propulsion system of an SUAV, the correct combination of all propulsion system components is critical. However, the largest impact on the maximal endurance is, arguably, caused by the propeller. The paper proposes a simple method of optimizing the propeller characteristics for hover and compares the proposed propeller design with conventional and commercially available propellers.
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spelling doaj.art-099b7d9a676e4201bf8fc7331bdd6c2b2022-12-21T22:37:55ZengEDP SciencesMATEC Web of Conferences2261-236X2020-01-013130004510.1051/matecconf/202031300045matecconf_dyn-wind20_00045Optimization of SUAV’s propeller in a hoverHnidka Jakub0Rozehnal Dalibor1Maňas Karel2University of Defence in BrnoUniversity of Defence in BrnoUniversity of Defence in BrnoSmall unmanned aerial vehicles (SUAVs) have found a widespread application in past decades. However, as the criticality of the missions for which they can be used increases, the demand for improvement of their efficiency increases as well. The paper focuses on a propeller driven SUAVs of a multirotor type, equipped with an electric motor, battery and propeller. The paper presents a simplified method of calculation of the SUAV maximal endurance, if the characteristics of all components of the propulsion system are known. To improve the overall efficiency of the propulsion system of an SUAV, the correct combination of all propulsion system components is critical. However, the largest impact on the maximal endurance is, arguably, caused by the propeller. The paper proposes a simple method of optimizing the propeller characteristics for hover and compares the proposed propeller design with conventional and commercially available propellers.https://www.matec-conferences.org/articles/matecconf/pdf/2020/09/matecconf_dyn-wind20_00045.pdf
spellingShingle Hnidka Jakub
Rozehnal Dalibor
Maňas Karel
Optimization of SUAV’s propeller in a hover
MATEC Web of Conferences
title Optimization of SUAV’s propeller in a hover
title_full Optimization of SUAV’s propeller in a hover
title_fullStr Optimization of SUAV’s propeller in a hover
title_full_unstemmed Optimization of SUAV’s propeller in a hover
title_short Optimization of SUAV’s propeller in a hover
title_sort optimization of suav s propeller in a hover
url https://www.matec-conferences.org/articles/matecconf/pdf/2020/09/matecconf_dyn-wind20_00045.pdf
work_keys_str_mv AT hnidkajakub optimizationofsuavspropellerinahover
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AT manaskarel optimizationofsuavspropellerinahover