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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Main Authors | , , , |
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Format | Patent |
Language | English French German |
Published |
31.05.2023
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Subjects | |
Online Access | Get full text |
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