ASSEMBLY COMPRISING A BLADE AND A BLADE PITCH SETTING SYSTEM

An assembly for an aircraft turbine engine is provided. The assembly generally includes an un-ducted propeller blade of which the root has a bulbous portion; a system for setting the pitch of the blade about a pitch setting axis, the pitch setting system including a cup configured to be placed insid...

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Bibliographic Details
Main Authors JOUDON, Vincent, COURTIER, Vivien Mickaël, COTTET, Clément, PAPIN, Thierry Georges Paul
Format Patent
LanguageEnglish
French
German
Published 31.05.2023
Subjects
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