Energy consumption comparison of static pitch propeller and variable pitch propeller using maximum thrust equation approach in small scale electric unmanned aerial vehicle

Variable pitch propeller is being implemented in a small-scale electric Unmanned Aerial Vehicles (UAV)21 to improve efficiency of energy consumption, especially in a cruise flight condition of UAVs. The pitch value of the variable pitch propeller is determined with an equation that depends on two ma...

Full description

Saved in:
Bibliographic Details
Main Authors: Stevenson, R., Chandra, C., Christon, J., Wiryanto, W., Virginio, R., Adiprawita, W.
Format: Conference Proceeding
Language:English
Citations: Items that cite this one
Online Access:Get full text
Tags: Add Tag
No Tags, Be the first to tag this record!
cited_by cdi_FETCH-LOGICAL-c265t-5106b98213fbb75dcc4be0ba5b1e4155cac1b5abb1ec4b346136d635cbb8faf03
cites
container_end_page
container_issue 1
container_start_page
container_title
container_volume 2226
creator Stevenson, R.
Chandra, C.
Christon, J.
Wiryanto, W.
Virginio, R.
Adiprawita, W.
description Variable pitch propeller is being implemented in a small-scale electric Unmanned Aerial Vehicles (UAV)21 to improve efficiency of energy consumption, especially in a cruise flight condition of UAVs. The pitch value of the variable pitch propeller is determined with an equation that depends on two main variables which is the UAV’s airspeed and RPM of the UAV’s motor. In this paper, the energy consumption of a variable pitch propulsion system during a UAV’s cruising condition is being compared with the energy consumption of a cruising condition of a UAV using a fixed pitch propeller. As a result, the variable pitch propeller propulsion system is proven to be more efficient than a fixed pitch propeller propulsion system.
doi_str_mv 10.1063/5.0002285
format conference_proceeding
fullrecord <record><control><sourceid>scitation</sourceid><recordid>TN_cdi_scitation_primary_10_1063_5_0002285</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>acp</sourcerecordid><originalsourceid>FETCH-LOGICAL-c265t-5106b98213fbb75dcc4be0ba5b1e4155cac1b5abb1ec4b346136d635cbb8faf03</originalsourceid><addsrcrecordid>eNp9kE1LAzEQhoMoWD8O_oOcha3JZrPbHqXUDyh4UfC2TLLZNpJkY5It9jf5J4214EHwNDPMM-87vAhdUTKlpGY3fEoIKcsZP0ITyjktmprWx2hCyLwqyoq9nqKzGN8yM2-a2QR9Lp0K6x2Wg4uj9UkPLvfWQ9Axt0OPY4KkJfY6yQ32YfDKGBUwuA5vMwXCqD_LMWq3xhY-tB0tTpswxoTV-wh7ffCZhHygHY4WjMFRQlZRRskUstfoLDinOgwqGxi8VRstjbpAJz2YqC4P9Ry93C2fFw_F6un-cXG7KmRZ81TwHISYz0rKeiEa3klZCUUEcEFVlTORIKngIPKYN6yqKau7mnEpxKyHnrBzdP2jG6VO-5dbH7SFsGspab9jbnl7iPk_eDuEX7D1Xc--AIvwhNU</addsrcrecordid><sourcetype>Enrichment Source</sourcetype><iscdi>true</iscdi><recordtype>conference_proceeding</recordtype></control><display><type>conference_proceeding</type><title>Energy consumption comparison of static pitch propeller and variable pitch propeller using maximum thrust equation approach in small scale electric unmanned aerial vehicle</title><source>American Institute of Physics:Jisc Collections:Transitional Journals Agreement 2021-23 (Reading list)</source><creator>Stevenson, R. ; Chandra, C. ; Christon, J. ; Wiryanto, W. ; Virginio, R. ; Adiprawita, W.</creator><contributor>Putro, Idris Eko ; Bahri, Sayr ; Adi, Andreas Prasetya ; Kurniawati, Frida</contributor><creatorcontrib>Stevenson, R. ; Chandra, C. ; Christon, J. ; Wiryanto, W. ; Virginio, R. ; Adiprawita, W. ; Putro, Idris Eko ; Bahri, Sayr ; Adi, Andreas Prasetya ; Kurniawati, Frida</creatorcontrib><description>Variable pitch propeller is being implemented in a small-scale electric Unmanned Aerial Vehicles (UAV)21 to improve efficiency of energy consumption, especially in a cruise flight condition of UAVs. The pitch value of the variable pitch propeller is determined with an equation that depends on two main variables which is the UAV’s airspeed and RPM of the UAV’s motor. In this paper, the energy consumption of a variable pitch propulsion system during a UAV’s cruising condition is being compared with the energy consumption of a cruising condition of a UAV using a fixed pitch propeller. As a result, the variable pitch propeller propulsion system is proven to be more efficient than a fixed pitch propeller propulsion system.</description><identifier>ISSN: 0094-243X</identifier><identifier>EISSN: 1551-7616</identifier><identifier>DOI: 10.1063/5.0002285</identifier><identifier>CODEN: APCPCS</identifier><language>eng</language><ispartof>AIP conference proceedings, 2020, Vol.2226 (1)</ispartof><rights>Author(s)</rights><lds50>peer_reviewed</lds50><woscitedreferencessubscribed>false</woscitedreferencessubscribed><citedby>FETCH-LOGICAL-c265t-5106b98213fbb75dcc4be0ba5b1e4155cac1b5abb1ec4b346136d635cbb8faf03</citedby></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><link.rule.ids>314,776,780,27903,27904</link.rule.ids></links><search><contributor>Putro, Idris Eko</contributor><contributor>Bahri, Sayr</contributor><contributor>Adi, Andreas Prasetya</contributor><contributor>Kurniawati, Frida</contributor><creatorcontrib>Stevenson, R.</creatorcontrib><creatorcontrib>Chandra, C.</creatorcontrib><creatorcontrib>Christon, J.</creatorcontrib><creatorcontrib>Wiryanto, W.</creatorcontrib><creatorcontrib>Virginio, R.</creatorcontrib><creatorcontrib>Adiprawita, W.</creatorcontrib><title>Energy consumption comparison of static pitch propeller and variable pitch propeller using maximum thrust equation approach in small scale electric unmanned aerial vehicle</title><title>AIP conference proceedings</title><description>Variable pitch propeller is being implemented in a small-scale electric Unmanned Aerial Vehicles (UAV)21 to improve efficiency of energy consumption, especially in a cruise flight condition of UAVs. The pitch value of the variable pitch propeller is determined with an equation that depends on two main variables which is the UAV’s airspeed and RPM of the UAV’s motor. In this paper, the energy consumption of a variable pitch propulsion system during a UAV’s cruising condition is being compared with the energy consumption of a cruising condition of a UAV using a fixed pitch propeller. As a result, the variable pitch propeller propulsion system is proven to be more efficient than a fixed pitch propeller propulsion system.</description><issn>0094-243X</issn><issn>1551-7616</issn><fulltext>true</fulltext><rsrctype>conference_proceeding</rsrctype><creationdate>2020</creationdate><recordtype>conference_proceeding</recordtype><sourceid/><recordid>eNp9kE1LAzEQhoMoWD8O_oOcha3JZrPbHqXUDyh4UfC2TLLZNpJkY5It9jf5J4214EHwNDPMM-87vAhdUTKlpGY3fEoIKcsZP0ITyjktmprWx2hCyLwqyoq9nqKzGN8yM2-a2QR9Lp0K6x2Wg4uj9UkPLvfWQ9Axt0OPY4KkJfY6yQ32YfDKGBUwuA5vMwXCqD_LMWq3xhY-tB0tTpswxoTV-wh7ffCZhHygHY4WjMFRQlZRRskUstfoLDinOgwqGxi8VRstjbpAJz2YqC4P9Ry93C2fFw_F6un-cXG7KmRZ81TwHISYz0rKeiEa3klZCUUEcEFVlTORIKngIPKYN6yqKau7mnEpxKyHnrBzdP2jG6VO-5dbH7SFsGspab9jbnl7iPk_eDuEX7D1Xc--AIvwhNU</recordid><startdate>20200421</startdate><enddate>20200421</enddate><creator>Stevenson, R.</creator><creator>Chandra, C.</creator><creator>Christon, J.</creator><creator>Wiryanto, W.</creator><creator>Virginio, R.</creator><creator>Adiprawita, W.</creator><scope/></search><sort><creationdate>20200421</creationdate><title>Energy consumption comparison of static pitch propeller and variable pitch propeller using maximum thrust equation approach in small scale electric unmanned aerial vehicle</title><author>Stevenson, R. ; Chandra, C. ; Christon, J. ; Wiryanto, W. ; Virginio, R. ; Adiprawita, W.</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-c265t-5106b98213fbb75dcc4be0ba5b1e4155cac1b5abb1ec4b346136d635cbb8faf03</frbrgroupid><rsrctype>conference_proceedings</rsrctype><prefilter>conference_proceedings</prefilter><language>eng</language><creationdate>2020</creationdate><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Stevenson, R.</creatorcontrib><creatorcontrib>Chandra, C.</creatorcontrib><creatorcontrib>Christon, J.</creatorcontrib><creatorcontrib>Wiryanto, W.</creatorcontrib><creatorcontrib>Virginio, R.</creatorcontrib><creatorcontrib>Adiprawita, W.</creatorcontrib></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Stevenson, R.</au><au>Chandra, C.</au><au>Christon, J.</au><au>Wiryanto, W.</au><au>Virginio, R.</au><au>Adiprawita, W.</au><au>Putro, Idris Eko</au><au>Bahri, Sayr</au><au>Adi, Andreas Prasetya</au><au>Kurniawati, Frida</au><format>book</format><genre>proceeding</genre><ristype>CONF</ristype><atitle>Energy consumption comparison of static pitch propeller and variable pitch propeller using maximum thrust equation approach in small scale electric unmanned aerial vehicle</atitle><btitle>AIP conference proceedings</btitle><date>2020-04-21</date><risdate>2020</risdate><volume>2226</volume><issue>1</issue><issn>0094-243X</issn><eissn>1551-7616</eissn><coden>APCPCS</coden><abstract>Variable pitch propeller is being implemented in a small-scale electric Unmanned Aerial Vehicles (UAV)21 to improve efficiency of energy consumption, especially in a cruise flight condition of UAVs. The pitch value of the variable pitch propeller is determined with an equation that depends on two main variables which is the UAV’s airspeed and RPM of the UAV’s motor. In this paper, the energy consumption of a variable pitch propulsion system during a UAV’s cruising condition is being compared with the energy consumption of a cruising condition of a UAV using a fixed pitch propeller. As a result, the variable pitch propeller propulsion system is proven to be more efficient than a fixed pitch propeller propulsion system.</abstract><doi>10.1063/5.0002285</doi><tpages>10</tpages></addata></record>
fulltext fulltext
identifier ISSN: 0094-243X
ispartof AIP conference proceedings, 2020, Vol.2226 (1)
issn 0094-243X
1551-7616
language eng
recordid cdi_scitation_primary_10_1063_5_0002285
source American Institute of Physics:Jisc Collections:Transitional Journals Agreement 2021-23 (Reading list)
title Energy consumption comparison of static pitch propeller and variable pitch propeller using maximum thrust equation approach in small scale electric unmanned aerial vehicle
url http://sfxeu10.hosted.exlibrisgroup.com/loughborough?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-01-27T22%3A58%3A31IST&url_ver=Z39.88-2004&url_ctx_fmt=infofi/fmt:kev:mtx:ctx&rfr_id=info:sid/primo.exlibrisgroup.com:primo3-Article-scitation&rft_val_fmt=info:ofi/fmt:kev:mtx:book&rft.genre=proceeding&rft.atitle=Energy%20consumption%20comparison%20of%20static%20pitch%20propeller%20and%20variable%20pitch%20propeller%20using%20maximum%20thrust%20equation%20approach%20in%20small%20scale%20electric%20unmanned%20aerial%20vehicle&rft.btitle=AIP%20conference%20proceedings&rft.au=Stevenson,%20R.&rft.date=2020-04-21&rft.volume=2226&rft.issue=1&rft.issn=0094-243X&rft.eissn=1551-7616&rft.coden=APCPCS&rft_id=info:doi/10.1063/5.0002285&rft_dat=%3Cscitation%3Eacp%3C/scitation%3E%3Cgrp_id%3Ecdi_FETCH-LOGICAL-c265t-5106b98213fbb75dcc4be0ba5b1e4155cac1b5abb1ec4b346136d635cbb8faf03%3C/grp_id%3E%3Coa%3E%3C/oa%3E%3Curl%3E%3C/url%3E&rft_id=info:oai/&rft_id=info:pmid/&rfr_iscdi=true