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항공기용 2단 차동 GRA 개발

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dc.contributor.author이강희-
dc.contributor.author임대진-
dc.contributor.author이선홍-
dc.contributor.author박슬기-
dc.contributor.author최진호-
dc.date.accessioned2022-12-26T20:33:24Z-
dc.date.available2022-12-26T20:33:24Z-
dc.date.issued2016-
dc.identifier.issn1598-6721-
dc.identifier.issn2288-0771-
dc.identifier.urihttps://scholarworks.gnu.ac.kr/handle/sw.gnu/15950-
dc.description.abstractThe aircraft flight control system controls an aircraft’s direction and flying attitude, and actuators are key components of control systems. Actuators can be classified as Geared Rotary Actuator (GRA) and Ball Screw Actuator (BSA). GRA is used in mid-sized aircraft, and BSA is used in larger aircraft. A two-stage differential GRA model was suggested in this paper, and structural analysis and performance tests were performed. According to the analysis and experiment, the stiffness of the two-stage differential GRA was 17.57% higher than that of the conventional GRA, and the structural safety was improved.-
dc.format.extent7-
dc.language한국어-
dc.language.isoKOR-
dc.publisher한국기계가공학회-
dc.title항공기용 2단 차동 GRA 개발-
dc.title.alternativeDevelopment of Aircraft 2-Stage Differential GRA-
dc.typeArticle-
dc.publisher.location대한민국-
dc.identifier.doi10.14775/ksmpe.2016.15.6.115-
dc.identifier.bibliographicCitation한국기계가공학회지, v.15, no.6, pp 115 - 121-
dc.citation.title한국기계가공학회지-
dc.citation.volume15-
dc.citation.number6-
dc.citation.startPage115-
dc.citation.endPage121-
dc.identifier.kciidART002175756-
dc.description.isOpenAccessY-
dc.description.journalRegisteredClasskci-
dc.subject.keywordAuthorGRA(Geared Rotary Actuator-
dc.subject.keywordAuthor기어식 회전 작동기)-
dc.subject.keywordAuthorPlanetary Gear(유성기어)-
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