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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Abstract | 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 inside the outer casing, has a flared open top end for axial insertion of the root and in which the root of the blade can be axially affixed by a locking member; and at least one radial retention prong in a radial space reserved between the wall of the cup and the root. |
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AbstractList | 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 inside the outer casing, has a flared open top end for axial insertion of the root and in which the root of the blade can be axially affixed by a locking member; and at least one radial retention prong in a radial space reserved between the wall of the cup and the root. |
Author | COTTET, Clément JOUDON, Vincent COURTIER, Vivien Mickaël PAPIN, Thierry Georges Paul |
Author_xml | – fullname: JOUDON, Vincent – fullname: COURTIER, Vivien Mickaël – fullname: COTTET, Clément – fullname: PAPIN, Thierry Georges Paul |
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DocumentTitleAlternate | ANORDNUNG MIT EINER SCHAUFEL UND EINEM SCHAUFELSPITZENEINSTELLSYSTEM ENSEMBLE COMPORTANT UNE AUBE ET UN SYSTEME DE CALAGE ANGULAIRE DE L'AUBE |
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Notes | Application Number: EP20210754811 |
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PublicationYear | 2023 |
RelatedCompanies | SAFRAN AIRCRAFT ENGINES |
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Snippet | 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... |
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SubjectTerms | AEROPLANES AIRCRAFT AVIATION BLASTING COSMONAUTICS HEATING HELICOPTERS LIGHTING MECHANICAL ENGINEERING NON-POSITIVE DISPLACEMENT PUMPS PERFORMING OPERATIONS POSITIVE DISPLACEMENT MACHINES FOR LIQUIDS PUMPS FOR LIQUIDS OR ELASTIC FLUIDS TRANSPORTING WEAPONS |
Title | ASSEMBLY COMPRISING A BLADE AND A BLADE PITCH SETTING SYSTEM |
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