Engineering method of calculation of gasdynamic foil bearings of turbocompressors

V. I Merkulov , M. E Plykin , I. V Tishchenko

Izvestiya MGTU MAMI ›› 2012, Vol. 6 ›› Issue (2-1) : 279 -286.

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Izvestiya MGTU MAMI ›› 2012, Vol. 6 ›› Issue (2-1) : 279 -286. DOI: 10.17816/2074-0530-68524
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Engineering method of calculation of gasdynamic foil bearings of turbocompressors

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Abstract

In this article the engineering method of calculation of gasdynamic foil bearings is considered. Calculations according to this method were made and comparison with the experimental results, obtained by other authors, was done. Ranges of application are also considered.

Keywords

gasdynamic foil bearing / turbomachine / micro gas turbine

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V. I Merkulov, M. E Plykin, I. V Tishchenko. Engineering method of calculation of gasdynamic foil bearings of turbocompressors. Izvestiya MGTU MAMI, 2012, 6(2-1): 279-286 DOI:10.17816/2074-0530-68524

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References

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Agrawal. Foil air/gas bearing technology. An overview. ASME, 345E. New York, 1007, publication 97-GT-347

[2]

GT-2003-38606. Development of high-speed industrial turbo blowers with foil air bearing. ASME, Turbo Expo, 2003, USA

[3]

Low-friction wear-resistant coating for high-temperature foil bearings, report N.Y, 12205, USA

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Технические справки и отчеты МГТУ «МАМИ» за 2010-2011гг.

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Ермилов Ю.И. Осевые лепестковые газодинамические подшипники. Диссертация на соискание ученой степени кандидата технических наук, 2008г.

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Merkulov V.I., Plykin M.E., Tishchenko I.V.

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