Приказ основних података о документу

dc.creatorTanasković, M.
dc.creatorRistanović, Milan
dc.creatorStojanović, S.
dc.creatorLazić, Dragan
dc.creatorMiloš, Marko
dc.date.accessioned2022-09-19T18:37:45Z
dc.date.available2022-09-19T18:37:45Z
dc.date.issued2018
dc.identifier.issn1757-8981
dc.identifier.urihttps://machinery.mas.bg.ac.rs/handle/123456789/2974
dc.description.abstractThis paper presents the design of an electro-mechanical actuator that is used for actuation of a medium sized helicopter. The designed actuator consists of a commercially available electro-mechanical cylinder EMC40 from Rexroth Bosch and a brushless DC motor EC45 from maxon motor. Cylinder and the motor are connected by a custom-made gearbox, which allows for their parallel axial mount. In addition to the actuator, the paper describes a test platform that can be used to emulate the forces generated by an actual helicopter. Designed test platform consists of a torsional spring and an AC motor with excentre. Frequency regulator is used to achieve the desired frequency of the force. Experimental results obtained by testing the designed actuator on the test platform are also given in the paper.en
dc.publisherInstitute of Physics Publishing
dc.rightsopenAccess
dc.rights.urihttps://creativecommons.org/licenses/by/4.0/
dc.sourceIOP Conference Series: Materials Science and Engineering
dc.titleDesign of electro-mechanical actuator for medium sized helicopter and a test platform for its testing and verificationen
dc.typeconferenceObject
dc.rights.licenseBY
dc.citation.issue1
dc.citation.other393(1): -
dc.citation.volume393
dc.identifier.doi10.1088/1757-899X/393/1/012008
dc.identifier.fulltexthttp://machinery.mas.bg.ac.rs/bitstream/id/8966/tanask.pdf
dc.identifier.scopus2-s2.0-85051871046
dc.type.versionpublishedVersion


Документи

Thumbnail

Овај документ се појављује у следећим колекцијама

Приказ основних података о документу