TBC VRSTVY A ICH VPLYV NA ZVYŠOVANIE TEPELNEJ ODOLNOSTI MATERIÁLOV

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dc.contributor.authorNovakov, Mário
dc.contributor.authorČerňan, Jozef
dc.date.accessioned2020-06-19T07:39:14Z
dc.date.available2020-06-19T07:39:14Z
dc.date.issued2020
dc.description.abstractPaper is dedicated to TBC protective elements, which are used to increase heat resistance of materials used in aircraft turbine engines. In individual sections are described in detail methods of protection and increase in heat resistance using TBC materials further described in the paper. Protective elements are applied to combustion chamber and the assembly behind it – turbine and exhaust nozzle of the jet engine. Paper is dedicated to general theory of turbine engine parts, TBC layers and final experiment. Significance of these TBC layers and comparison of the same material with and without TBC layer will be aim of the experiment with thermal camera and gas burner which will simulate environment of combustion chamber.en_US
dc.identifier.doihttps://doi.org/10.26552/pas.Z.2020.2.16
dc.identifier.isbn978-80-554-1687-8
dc.identifier.urihttp://drepo.uniza.sk/handle/hdluniza/132
dc.language.isosken_US
dc.publisherŽilinská univerzita v Žilineen_US
dc.rights.urihttp://creativecommons.org/licenses/by/4.0/
dc.subjectTBCen_US
dc.subjectlayersen_US
dc.subjectcombustion chamberen_US
dc.subjectbladesen_US
dc.subjectturbineen_US
dc.subjecttemperatureen_US
dc.titleTBC VRSTVY A ICH VPLYV NA ZVYŠOVANIE TEPELNEJ ODOLNOSTI MATERIÁLOVen_US
dc.title.alternativeTBC LAYERS AND THEIR INFLUENCE ON INCREASING THE THERMAL RESISTANCE OF MATERIALSen_US
dc.typeBook of proceedingsen_US

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