Propeller blade pivot
View Patent ↗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 ).
1. A pivot for a blade of a propeller, the pivot comprising:
a proximal portion suitable for being retained in a radial orifice in a propeller hub while being capable of turning in the orifice about a longitudinal axis of the pivot; and
a distal portion including at least one arm extending laterally relative to said longitudinal axis and supporting a flyweight at an end of said at least one arm furthest from said longitudinal axis;
wherein at least said proximal portion is made of metal, at least said at least one arm is made of organic matrix composite material, and a receptacle for retaining a blade root is formed in a metal extension of the proximal portion of the pivot that passes through the distal portion of the pivot and presents a longitudinal section that diverges towards a distal end of the pivot to retain along the longitudinal axis, by interlocking shapes, the distal portion of the pivot.
2. The pivot according to claim 1 , wherein said proximal and distal portions are bonded together by adhesive.
3. The pivot according to claim 1 , wherein said proximal and distal portions are bonded together by a bolted connection.
4. The pivot according to claim 1 , wherein said receptacle is in the form of a dovetail slot extending in a direction that is substantially perpendicular to said at least one arm.
5. The pivot according to claim 1 , wherein said distal portion comprises two opposite arms extending laterally relative to said longitudinal axis and each supporting a respective flyweight.