Publications
Detailed Information
무인기용 소형 가스터빈 엔진을 위한 고감속 기어박스 개발 : Development of a High-Speed Reduction Gearbox for a Small Gas Turbine Engine of an Unmanned Aerial Vehicle
DC Field | Value | Language |
---|---|---|
dc.contributor.author | Huh, Jae Sung | - |
dc.contributor.author | Lee, Kang Hee | - |
dc.contributor.author | Park, Young Jun | - |
dc.contributor.author | Kim, Myeong Kuk | - |
dc.contributor.author | Kim, Jae Hwan | - |
dc.date.accessioned | 2023-04-19T00:30:57Z | - |
dc.date.available | 2023-04-19T00:30:57Z | - |
dc.date.created | 2021-03-29 | - |
dc.date.issued | 2021-02 | - |
dc.identifier.citation | 대한기계학회논문집 A, Vol.45 No.2, pp.167-173 | - |
dc.identifier.issn | 1226-4873 | - |
dc.identifier.uri | https://hdl.handle.net/10371/190274 | - |
dc.description.abstract | A gearbox for the transmission of an aircraft propulsion system has complex requirements, such as a gear rating of AGMA 12 or higher, application of aviation bearings, stability of the lubrication system at various aircraft attitudes and environments, compact and lightweight design, and maintenance of a high-grade quality system. These characteristics distinguish it from general gearboxes for automobiles, construction machinery, and agricultural machinery. Research and development on aircraft gearboxes became popular domestically to a limited extent after 2010 because of difficulties associated with the design and fabrication technologies as well as limited demand. In this article, we describe the development of a gearbox with a high reduction ratio that is connected to the output of a turboshaft engine of an unmanned aerial vehicle and transmits power with over 95% efficiency while decelerating to 1:10. The requirements for gearbox development are first derived for design/analysis/manufacturing, and a test rig is developed to evaluate its performance and endurance; finally, the test results are described. | - |
dc.language | 한국어 | - |
dc.publisher | 대한기계학회 | - |
dc.title | 무인기용 소형 가스터빈 엔진을 위한 고감속 기어박스 개발 | - |
dc.title.alternative | Development of a High-Speed Reduction Gearbox for a Small Gas Turbine Engine of an Unmanned Aerial Vehicle | - |
dc.type | Article | - |
dc.identifier.doi | 10.3795/KSME-A.2021.45.2.167 | - |
dc.citation.journaltitle | 대한기계학회논문집 A | - |
dc.identifier.wosid | 000623663100009 | - |
dc.identifier.scopusid | 2-s2.0-85102399195 | - |
dc.citation.endpage | 173 | - |
dc.citation.number | 2 | - |
dc.citation.startpage | 167 | - |
dc.citation.volume | 45 | - |
dc.identifier.kciid | ART002681940 | - |
dc.description.isOpenAccess | N | - |
dc.contributor.affiliatedAuthor | Park, Young Jun | - |
dc.type.docType | Article | - |
dc.description.journalClass | 1 | - |
dc.subject.keywordAuthor | Unmanned Aerial Vehicle | - |
dc.subject.keywordAuthor | Turboshaft Engine | - |
dc.subject.keywordAuthor | Gearbox | - |
dc.subject.keywordAuthor | Efficiency | - |
dc.subject.keywordAuthor | Accelerated Life Test | - |
- Appears in Collections:
- Files in This Item:
- There are no files associated with this item.
Item View & Download Count
Items in S-Space are protected by copyright, with all rights reserved, unless otherwise indicated.