Engineering method of calculation of gasdynamic foil bearings of turbocompressors

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

Izvestiya MGTU MAMI ›› 2013, Vol. 7 ›› Issue (1-1) : 126 -132.

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Izvestiya MGTU MAMI ›› 2013, Vol. 7 ›› Issue (1-1) : 126 -132. DOI: 10.17816/2074-0530-68249
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Engineering method of calculation of gasdynamic foil bearings of turbocompressors

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Abstract

In the article there is considered the engineering method of calculation of gasdynamic foil bearings. There are executed calculations according with this method and there is executed the comparison of results which were received by other authors.

Keywords

gasdynamic foil bearing / turbomachine / micro gas turbine

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V. I Merkulov, M. E. Plykin, I. V Tischenko. Engineering method of calculation of gasdynamic foil bearings of turbocompressors. Izvestiya MGTU MAMI, 2013, 7(1-1): 126-132 DOI:10.17816/2074-0530-68249

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References

[1]

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

[4]

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

[5]

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., Tischenko I.V.

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