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The tests described in the article are related to the project of a high-altitude scientific rocket, which is expected to be built in the Institute of Aviation. The unguided rocket will be launched from a platform with a relatively long start beam and will be supported by slides at the start. Because of the relatively high rocket mass and nearly horizontal start needed for initial rocket tests, its slides will be under extremely high load defined as a combination of pressure and sliding velocity. In addition to the mechanical load, the slides will be also loaded thermally because of the friction in a pair: slide-guide rail (made of hard-anodized aluminium alloy). This leads to rapid wear of the slides. The aim of the tests was to establish what the friction coefficient between the slide and the guide rail is (as function of mechanical load) and how big slide-wear in a single work cycle (simulation of a single rocket launch) is. The tests were performed for few material samples: two modern plastics used in so-called “linear systems” (offered by a firm, which is one of the leaders on this market), samples made of well-known and widely used materials like cotton-phenolic textolite and well-known samples of material called Teflon (PTFE – polytetrafluoroethylene) with 15% addition of graphite. Results show that the temperature resistant plastic used in general linear systems at our condition are on the verge of wear according to our model. Textolite and Teflon with graphite addition have better characteristics of wear. They can be safely used as material of slides.
Słowa kluczowe
Wydawca
Czasopismo
Rocznik
Tom
Strony
49--56
Opis fizyczny
Bibliogr. 8 poz., rys.
Twórcy
autor
- Institute of Aviation Krakowska Avenue 110/114, 02-256 Warszawa Poland tel.: +48 228460011 ext. 345, fax: +48 228465774
autor
- Institute of Aviation Krakowska Avenue 110/114, 02-256 Warszawa Poland tel.: +48 228460011 ext. 345, fax: +48 228465774
autor
- Institute of Aviation Krakowska Avenue 110/114, 02-256 Warszawa Poland tel.: +48 228460011 ext. 345, fax: +48 228465774
autor
- Institute of Aviation Krakowska Avenue 110/114, 02-256 Warszawa Poland tel.: +48 228460011 ext. 345, fax: +48 228465774
Bibliografia
- [1] Chowdhury, M. A., Nuruzzaman, D. M., Roy, B. K., Samad, S., Sarker, R., Rezwan, A. H. M., Experimental Investigation of Friction Coefficient and Wear Rate of Composite Materials Sliding Against Smooth and Rough Mild Steel Counterfaces, Tribology in Industry, Vol. 35 , pp. 286-296, 2013.
- [2] Capanidis, D., Mechanizm tarcia i zużywania wieloskładnikowych kompozytów na osnowie polioksymetylenu, Oficyna Wydawnicza Politechniki Wrocławskiej, p. 36, Wrocław 2013.
- [3] Lawrowski, Z., Bezobsługowe łożyska ślizgowe, Problemy niekonwencjonalnych układów łożyskowych, Łódź 1995.
- [4] Quaglini, V., Dubini, P., Friction of Polymers Sliding on Smooth Surfaces, Advances in Tribology, Milano 2011.
- [5] Skorupka, Z., Grygorcewicz, P., Badania laboratoryjne hamulców ciernych w laboratorium badań podwozi lotniczych, Technika Transportu Szynowego, 2013.
- [6] http://www.plastics.pl/content/zdjecia/file/katalog_tworzywa_techniczne_107.pdf, 2016.
- [7] http://www.igus.pl/wpck/2328/iglidur_Reibwerte, 2016.
- [8] Blau, P. J., The significance and use of the friction coefficient, Tribology International 34, pp. 585-591, 2001.
Uwagi
PL
Opracowanie ze środków MNiSW w ramach umowy 812/P-DUN/2016 na działalność upowszechniającą naukę.
Typ dokumentu
Bibliografia
Identyfikator YADDA
bwmeta1.element.baztech-14fb3bf4-7a94-436f-9019-f3a791db094d