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dc.creatorKolarević, Nenad
dc.creatorKosanović, N.
dc.creatorMiloš, Marko
dc.date.accessioned2022-09-19T18:28:57Z
dc.date.available2022-09-19T18:28:57Z
dc.date.issued2018
dc.identifier.issn2214-7853
dc.identifier.urihttps://machinery.mas.bg.ac.rs/handle/123456789/2843
dc.description.abstractThe paper defines the minimum number of parameters which are sufficient for monitoring and controlling the gas generator operation in an innovative design of a tip-jet helicopter propulsion system. Firstly, the gas generator is tested separately on its test stand installation with several selected measuring and controlling parameters. Some ideas for implementing sensors for measuring certain parameters are presented in the paper. Then, a few parameters are selected as sufficient for controlling the tip-jet helicopter and experimentally verified on a helicopter hovering test as the minimum required parameters.en
dc.publisherElsevier Ltd
dc.relationTests were performed in EDePro d.o.o. facilities in Belgrade as a part of UAV tip-jet helicopter development program.
dc.rightsrestrictedAccess
dc.sourceMaterials Today: Proceedings
dc.subjectTip-jet helicopteren
dc.subjectPropulsion systemen
dc.subjectGas generatoren
dc.subjectExperimental testingen
dc.subjectAcquistion systemen
dc.titleCrucial parameters of gas generator on tip-jet helicopteren
dc.typeconferenceObject
dc.rights.licenseARR
dc.citation.epage26720
dc.citation.issue13
dc.citation.other5(13): 26715-26720
dc.citation.rankM14
dc.citation.spage26715
dc.citation.volume5
dc.identifier.doi10.1016/j.matpr.2018.08.141
dc.identifier.scopus2-s2.0-85067238501
dc.type.versionpublishedVersion


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