Assembly of Aircraft Engine Fans Subject to Icing

This article considers the possibility of using assembly algorithms for aircraft engine fans that maintain the specified balance of the fan design even when icing occurs.

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Bibliographic Details
Published inRussian engineering research Vol. 45; no. 3; pp. 308 - 311
Main Authors Beloborodov, S. M., Modorskiy, V. Ya
Format Journal Article
LanguageEnglish
Published Moscow Pleiades Publishing 01.03.2025
Springer Nature B.V
Subjects
Aircraft engines
Aircraft icing
Algorithms
Engineering
Engineering Design
assembly
balancing
fan
imbalance
icing
aircraft engines
Online AccessGet full text
ISSN1068-798X
1934-8088
DOI10.3103/S1068798X2570025X

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Summary:This article considers the possibility of using assembly algorithms for aircraft engine fans that maintain the specified balance of the fan design even when icing occurs.
Bibliography:ObjectType-Article-1
SourceType-Scholarly Journals-1
ObjectType-Feature-2
content type line 14
ISSN:1068-798X
1934-8088
DOI:10.3103/S1068798X2570025X