Оценка структуры поверхности профиля пера лопаток газотурбинных двигателей

Носов, Н.В.; Абрамов, А.Д.; Косулин, С.И.

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Full metadata record

DC Field	Value	Language
dc.contributor.author	Носов, Н.В.
dc.contributor.author	Абрамов, А.Д.
dc.contributor.author	Косулин, С.И.
dc.date	2016
dc.date.accessioned	2025-08-22T12:21:35Z	-
dc.date.available	2025-08-22T12:21:35Z	-
dc.date.issued	2016
dc.identifier.identifier	Dspace\SGAU\20161118\59951
dc.identifier.citation	Материалы докладов междунар. науч.-техн. конф. 22-24 июня 2016 г. Ч. 1, с. 128-129
dc.identifier.isbn	978-5-7883-1084-8
dc.identifier.uri	http://repo.ssau.ru/jspui/handle/123456789/14633	-
dc.description	УДК 621.923.46
dc.description.abstract	Research structure GTE blades surface has been carried out after finishing. Has been analyzed the profile of blades aerofoil and fillet radius between aerofoil and root. Electro-optics method determines the parameters of the autocorrelation function of the surface. It has been found that the amplitude of the autocorrelation component of the aerofoil is reached 21-22 relative unit or counted b2 formulas Ra=0,22 microns, and the fillet radius is 24 rel. u or Ra=0,24 microns.
dc.language	rus
dc.publisher	Самарский университет
dc.title	Оценка структуры поверхности профиля пера лопаток газотурбинных двигателей
dc.title.alternative	Research of surface structure of GTE blades
dc.type	Article
local.identifier.olduri	http://repo.ssau.ru/handle/Mezhdunarodnaya-nauchnotehnicheskaya-konferenciya-Problemy-i-perspektivy-razvitiya-dvigatelestroeniya/Ocenka-struktury-poverhnosti-profilya-pera-lopatok-gazoturbinnyh-dvigatelei-59951
local.identifier.olduri	http://repo.ssau.ru/handle/Mezhdunarodnaya-nauchnotehnicheskaya-konferenciya-Problemy-i-perspektivy-razvitiya-dvigatelestroeniya/Ocenka-struktury-poverhnosti-profilya-pera-lopatok-gazoturbinnyh-dvigatelei-59951
Appears in Collections:	Проблемы и перспективы развития двигателестроения

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File	Description	Size	Format
128-129.pdf	Основная статья	176.31 kB	Adobe PDF	View/Open

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