Propeller blade pivot

Patent metadata

Field	Value
Publication number	US-9914527-B2
Application number	US-201715454787-A
Country	US
Kind code	B2
Filing date	Mar 9, 2017
Priority date	May 17, 2013
Publication date	Mar 13, 2018
Grant date	Mar 13, 2018

Abstract

The invention relates to the field of aerial propellers, in particular the field of variable-pitch propellers, specifically for unducted fans. More specifically, the invention relates to a pivot ( 15 ) for a blade ( 14 ) of a propeller ( 3 a, 3 b ), the pivot including at least a proximal portion ( 15 a ) made of metal and suitable for being retained in a radial orifice of a propeller hub, while being capable of turning in said orifice about a longitudinal axis (Z) of the pivot ( 15 ), and a distal portion ( 15 b ) including a receptacle ( 20 ) suitable for retaining a blade root, and at least one arm ( 17 ) of organic matrix composite material extending laterally relative to said longitudinal axis (Z) and supporting a flyweight ( 16 ).

First claim

The invention claimed is:

1. A pivot for a blade of a propeller, the pivot comprising:
a proximal portion made of metal and suitable to be retained in a radial orifice in a propeller hub while being capable of turning in this orifice about a longitudinal axis of the pivot; and
a distal portion made of organic matrix composite material incorporating a metal insert forming a receptacle for retaining a blade root, the distal portion further comprising at least one arm extending laterally relative to the longitudinal axis of the pivot and supporting a flyweight;
wherein a metal extension of the proximal portion presents shoulders locking the distal portion with respect to the proximal portion in a plane perpendicular to the longitudinal axis of the pivot, and inside surfaces of the metal extension of the proximal portion and of a composite part of the distal portion align so as to form a dovetail groove receiving the metal insert of the distal portion locking the distal portion with respect to the proximal portion in the direction of the longitudinal axis of the pivot.

2. The pivot according to claim 1 , further comprising a bolted connection between the proximal and distal portions.

3. The pivot according to claim 1 , wherein the metal extension of the proximal portion of the pivot passes through the distal portion of the pivot.

4. The pivot according to claim 1 , wherein the receptacle is in the form of a slot of dovetail section extending in a direction that is substantially perpendicular to the at least one arm of the distal portion.

5. The pivot according to claim 1 , wherein the distal portion comprises two opposite arms extending laterally relative to the longitudinal axis of the pivot and each supporting a respective flyweight.

6. A propeller comprising:
a propeller blade;
a propeller hub; and
a pivot comprising:
a proximal portion made of metal and retained in a radial orifice in the propeller hub while being capable of turning in this radial orifice about a longitudinal axis of the pivot; and
a distal portion made of organic matrix composite material incorporating a metal insert forming a receptacle retaining a blade root of the propeller blade, the distal portion further comprising at least one arm extending laterally relative to the longitudinal axis of the pivot and supporting a flyweight;

wherein a metal extension of the proximal portion presents shoulders locking the distal portion with respect to the proximal portion in a plane perpendicular to the longitudinal axis of the pivot, and inside surfaces of the metal extension of the proximal portion and of a composite part of the distal portion align so as to form a dovetail groove receiving the metal insert of the distal portion locking the distal portion with respect to the proximal portion in the direction of the longitudinal axis of the pivot.

Assignees

• Snecma

Inventors

• Tajan Sebastien
• Fabre Adrien Jacques Philippe
• Jacquemard Christophe
• Laurenceau Adrien
• Boudier Romain

Classifications

• B64C11/346 Primary

  actuated by the centrifugal force or the aerodynamic drag acting on auxiliary masses or surfaces · CPC title

• F04D29/366

  Adjustment by interaction of inertion and lift · CPC title

• B64D2027/005

  Aircraft with an unducted turbofan comprising contra-rotating rotors, e.g. contra-rotating open rotors [CROR] · CPC title

• F01D7/00

  Rotors with blades adjustable in operation; Control thereof (for reversing F01D1/30) · CPC title

• B64C11/325

  comprising feathering, braking or stopping systems · CPC title