Modal analysis of the nozzle guide vane in low pressure turbine system of aircraft engine

R. Robak; M. Szczepanik

doi:10.1088/1757-899X/1037/1/012049

Modal analysis of the nozzle guide vane in low pressure turbine system of aircraft engine

R. Robak
, M. Szczepanik

Katedra Mechaniki i Inżynierii Obliczeniowej (RMT/RMT4)

Silesian University of Technology
AvioPolska Sp. z o.o

Wyniki badań: Wkład do czasopisma › Artykuł z konferencji › recenzja

2 Cytowania z bazy Scopus

Abstrakt

The aim of the article is to present modal analysis of nozzle guide vane in low pressure turbine system of aircraft engine. Comparison of results obtained by means of finite element analysis with results of experimental one in terms of frequencies and modal forms are presented. Additionally, the article presents consistent results which will be used in further analyses and researches related to the optimization of dynamic characteristics with application of artificial intelligence.

Język oryginału	angielski
Numer artykułu	012049
Czasopismo	IOP Conference Series: Materials Science and Engineering
Tom	1037
Numer wydania	1
Identyfikatory DOI	https://doi.org/10.1088/1757-899X/1037/1/012049
Status publikacji	Opublikowano - 11 lut 2021
Wydarzenie	24th Innovative Manufacturing Engineering and Energy International Conference, IManEE 2020 - Athens, Grecja Czas trwania: 14 gru 2020 → 15 gru 2020

Obszary tematyczne ASJC Scopus

Materiałoznawstwo ogólne
Inżynieria ogólna

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10.1088/1757-899X/1037/1/012049

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title = "Modal analysis of the nozzle guide vane in low pressure turbine system of aircraft engine",

abstract = "The aim of the article is to present modal analysis of nozzle guide vane in low pressure turbine system of aircraft engine. Comparison of results obtained by means of finite element analysis with results of experimental one in terms of frequencies and modal forms are presented. Additionally, the article presents consistent results which will be used in further analyses and researches related to the optimization of dynamic characteristics with application of artificial intelligence.",

author = "R. Robak and M. Szczepanik",

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AU - Robak, R.

AU - Szczepanik, M.

N1 - Publisher Copyright: © Published under licence by IOP Publishing Ltd.

PY - 2021/2/11

Y1 - 2021/2/11

N2 - The aim of the article is to present modal analysis of nozzle guide vane in low pressure turbine system of aircraft engine. Comparison of results obtained by means of finite element analysis with results of experimental one in terms of frequencies and modal forms are presented. Additionally, the article presents consistent results which will be used in further analyses and researches related to the optimization of dynamic characteristics with application of artificial intelligence.

AB - The aim of the article is to present modal analysis of nozzle guide vane in low pressure turbine system of aircraft engine. Comparison of results obtained by means of finite element analysis with results of experimental one in terms of frequencies and modal forms are presented. Additionally, the article presents consistent results which will be used in further analyses and researches related to the optimization of dynamic characteristics with application of artificial intelligence.

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U2 - 10.1088/1757-899X/1037/1/012049

DO - 10.1088/1757-899X/1037/1/012049

M3 - Conference article

AN - SCOPUS:85101644556

SN - 1757-8981

VL - 1037

JO - IOP Conference Series: Materials Science and Engineering

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T2 - 24th Innovative Manufacturing Engineering and Energy International Conference, IManEE 2020

Y2 - 14 December 2020 through 15 December 2020

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Modal analysis of the nozzle guide vane in low pressure turbine system of aircraft engine

Abstrakt

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