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공기시동모터의 터빈방식 로터 노즐수에 따른 유동 메커니즘분석에 관한 연구

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dc.contributor.author박성배-
dc.contributor.author김남용-
dc.contributor.author진의군-
dc.contributor.author李氷-
dc.contributor.author류성기-
dc.date.accessioned2023-06-05T06:41:44Z-
dc.date.available2023-06-05T06:41:44Z-
dc.date.issued2023-05-
dc.identifier.issn1598-6721-
dc.identifier.issn2288-0771-
dc.identifier.urihttps://scholarworks.gnu.ac.kr/handle/sw.gnu/59586-
dc.description.abstractThis study was conducted to increase the output torque of the turbine rotors of ship air-start motors. Theturbine-type output of the air start motor was analyzed based on the pneumatic pressure and partial admissionnozzle characteristics. The most efficient maximum output torque was analyzed and designed by changing thenumber of turbine nozzles and increasing the number of rotations. Computational fluid dynamics analysis wasconducted and test results were analyzed to obtain the appropriate number of rotations according to thepartial admission nozzle.-
dc.format.extent6-
dc.language한국어-
dc.language.isoKOR-
dc.publisher한국기계가공학회-
dc.title공기시동모터의 터빈방식 로터 노즐수에 따른 유동 메커니즘분석에 관한 연구-
dc.title.alternativeAnalysis of the Flow Mechanism according to the Number of Nozzles for the Turbine Rotor in the Air-Starting Motor-
dc.typeArticle-
dc.publisher.location대한민국-
dc.identifier.doi10.14775/ksmpe.2023.22.05.031-
dc.identifier.bibliographicCitation한국기계가공학회지, v.22, no.5, pp 31 - 36-
dc.citation.title한국기계가공학회지-
dc.citation.volume22-
dc.citation.number5-
dc.citation.startPage31-
dc.citation.endPage36-
dc.identifier.kciidART002960869-
dc.description.isOpenAccessN-
dc.description.journalRegisteredClasskci-
dc.subject.keywordAuthorPartial Admission Nozzle(부분 분사이론)-
dc.subject.keywordAuthorAir Motor( )-
dc.subject.keywordAuthorNozzle( )-
dc.subject.keywordAuthor공압 모터 노즐 Turbine Type Rotor(터빈 방식 로터)-
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공학계열 > 기계항공우주공학부 > Journal Articles

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대학원 (기계항공우주공학부)
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