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Impact of Manufacturing Tolerances on Stress in a Turbine Blade Fir-Tree Root Cover

Impact of Manufacturing Tolerances on Stress in a Turbine Blade Fir-Tree Root

Fatigue of Aircraft Structures
Volume 2020 (2020): Issue 12 (December 2020)
By:  and    
Open Access
|Jul 2021
Authors

Authors

Grzegorz Moneta

grzegorz.moneta@ilot.lukasiewicz.gov.pl

Łukasiewicz Research Network ‒ Institute of Aviation, Warsaw, Poland

Jerzy Jachimowicz

Military University of Technology, Warsaw
DOI: https://doi.org/10.2478/fas-2020-0009 | Journal eISSN: 2300-7591 | Journal ISSN: 2081-7738
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Language: English
Page range: 92 - 101
Published on: Jul 23, 2021
Published by: ŁUKASIEWICZ RESEARCH NETWORK – INSTITUTE OF AVIATION
In partnership with: Paradigm Publishing Services
Keywords:
fir-tree root,
turbine,
lock,
blade,
disk,
manufacturing tolerances,
Monte-Carlo simulations,
Six Sigma,
Low Cycle Fatigue,
Design of Experiment
Related subjects:
Engineering,
Introductions and overviews,
Engineering, other

© 2021 Grzegorz Moneta, Jerzy Jachimowicz, published by ŁUKASIEWICZ RESEARCH NETWORK – INSTITUTE OF AVIATION
This work is licensed under the Creative Commons Attribution-NonCommercial-NoDerivatives 3.0 License.

Volume 2020 (2020): Issue 12 (December 2020)
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