{"title":"Mos2 / ws2 / finelpn复合层——活塞环低摩擦涂层的新方法","authors":"P. Kula, R. Pietrasik, S. Pawęta, J. Komorowski","doi":"10.5604/01.3001.0016.1024","DOIUrl":null,"url":null,"abstract":"In the search for alternative processes of technologically difficult and environmentally dangerous galvanic\nchromium coatings on cast iron piston rings, composite coatings of low-friction nanoparticles MoS2, WS2\nand/or rGO embedded in a hard matrix of iron nitrides have been investigated. Laboratory tribological and\noperational tests on a real aircraft engine have been carried out to select the optimal technological parameters\nand microstructures of low frictional layers. A dry friction coefficient of 0.13 has been obtained for the best\nof the processes, i.e., four times lower than for raw reference samples (0.55). According to that technological\noption, the low-friction layers were produced for a set of rings for three cylinders of a Boxer aircraft engine\nand tested comparatively in an operational test with the rings in the other three cylinders. The experimental\nengine has passed the operational test obtaining the assumed power performance, fuel consumption and\nadmission criteria of exhaust purity and oil purity.\n\n","PeriodicalId":35004,"journal":{"name":"Tribologia: Finnish Journal of Tribology","volume":"40 1","pages":""},"PeriodicalIF":0.0000,"publicationDate":"2022-11-30","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"2","resultStr":"{\"title\":\"MOS2/WS2/FINELPN COMPOSITE LAYERS – A NEW APPROACH\\nTO LOW FRICTIONAL COATINGS FOR PISTON RINGS\",\"authors\":\"P. Kula, R. Pietrasik, S. Pawęta, J. Komorowski\",\"doi\":\"10.5604/01.3001.0016.1024\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"In the search for alternative processes of technologically difficult and environmentally dangerous galvanic\\nchromium coatings on cast iron piston rings, composite coatings of low-friction nanoparticles MoS2, WS2\\nand/or rGO embedded in a hard matrix of iron nitrides have been investigated. Laboratory tribological and\\noperational tests on a real aircraft engine have been carried out to select the optimal technological parameters\\nand microstructures of low frictional layers. A dry friction coefficient of 0.13 has been obtained for the best\\nof the processes, i.e., four times lower than for raw reference samples (0.55). According to that technological\\noption, the low-friction layers were produced for a set of rings for three cylinders of a Boxer aircraft engine\\nand tested comparatively in an operational test with the rings in the other three cylinders. The experimental\\nengine has passed the operational test obtaining the assumed power performance, fuel consumption and\\nadmission criteria of exhaust purity and oil purity.\\n\\n\",\"PeriodicalId\":35004,\"journal\":{\"name\":\"Tribologia: Finnish Journal of Tribology\",\"volume\":\"40 1\",\"pages\":\"\"},\"PeriodicalIF\":0.0000,\"publicationDate\":\"2022-11-30\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"2\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"Tribologia: Finnish Journal of Tribology\",\"FirstCategoryId\":\"1085\",\"ListUrlMain\":\"https://doi.org/10.5604/01.3001.0016.1024\",\"RegionNum\":0,\"RegionCategory\":null,\"ArticlePicture\":[],\"TitleCN\":null,\"AbstractTextCN\":null,\"PMCID\":null,\"EPubDate\":\"\",\"PubModel\":\"\",\"JCR\":\"Q3\",\"JCRName\":\"Engineering\",\"Score\":null,\"Total\":0}","platform":"Semanticscholar","paperid":null,"PeriodicalName":"Tribologia: Finnish Journal of Tribology","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.5604/01.3001.0016.1024","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"Q3","JCRName":"Engineering","Score":null,"Total":0}
MOS2/WS2/FINELPN COMPOSITE LAYERS – A NEW APPROACH
TO LOW FRICTIONAL COATINGS FOR PISTON RINGS
In the search for alternative processes of technologically difficult and environmentally dangerous galvanic
chromium coatings on cast iron piston rings, composite coatings of low-friction nanoparticles MoS2, WS2
and/or rGO embedded in a hard matrix of iron nitrides have been investigated. Laboratory tribological and
operational tests on a real aircraft engine have been carried out to select the optimal technological parameters
and microstructures of low frictional layers. A dry friction coefficient of 0.13 has been obtained for the best
of the processes, i.e., four times lower than for raw reference samples (0.55). According to that technological
option, the low-friction layers were produced for a set of rings for three cylinders of a Boxer aircraft engine
and tested comparatively in an operational test with the rings in the other three cylinders. The experimental
engine has passed the operational test obtaining the assumed power performance, fuel consumption and
admission criteria of exhaust purity and oil purity.