Rotorcraft blade provided with a flap that is tiltable with the help of at least one main ball joint having a first shaft that is secured to said flap
View Patent ↗The present invention relates to a rotorcraft rotor blade ( 1 ) having at least one trailing edge flap ( 5 ) that is tiltable, the flap ( 5 ) being suitable for pivoting about a virtual hinge axis (Y′) extending substantially along the span of the blade ( 1 ) and of the flap ( 5 ). The blade ( 1 ) is remarkable in that the flap ( 5 ) is provided with at least one main ball joint ( 30 ) having an inner cage ( 32 ) and an outer cage ( 33 ), and a first shaft ( 31 ) secured to the flap ( 5 ), the front portion ( 33 ′) of the outer cage ( 33 ) of the main ball joint ( 30 ) being connected to a linear actuator ( 10 ) which is arranged in the blade ( 1 ) and which enables the flap ( 5 ) to be pivoted, the first shaft ( 31 ) of the main ball joint ( 30 ) extending substantially perpendicularly to the virtual hinge axis (Y′) about which the flap ( 5 ) pivots.
1. A rotorcraft rotor blade ( 1 ) having at least one trailing edge flap ( 5 ) that is tiltable, said flap ( 5 ) being suitable for pivoting about a virtual hinge axis (Y′) extending substantially along the span of said blade ( 1 ) and of said flap ( 5 ), wherein said flap ( 5 ) is provided with at least one main ball joint ( 30 ) having an inner cage ( 32 ) and an outer cage ( 33 ), and a first shaft ( 31 ) secured to said flap ( 5 ), the front portion ( 33 ′) of said outer cage ( 33 ) of the main ball joint ( 30 ) being connected to a linear actuator ( 10 ) that is arranged in said blade ( 1 ) and that enables said flap ( 5 ) to be pivoted, said first shaft ( 31 ) of the main ball joint ( 30 ) extending substantially perpendicularly to said virtual hinge axis (Y′) about which said flap ( 5 ) pivots, wherein said flap includes a fastener ball joint ( 39 ) having an outer cage ( 37 ) and an inner cage ( 36 ), together with a second shaft ( 35 ), the front portion ( 37 ′) of the outer cage ( 37 ) of said fastener ball joint ( 39 ) being secured to a stationary point of said blade.
2. A blade according to claim 1 , wherein the axis of symmetry of said main ball joint ( 30 ) is arranged substantially at 25% of the chord of said flap ( 5 ) going from the leading edge of said flap ( 5 ).
3. A blade according to claim 1 , wherein said main ball joint ( 30 ) is selflubricating.
4. A blade according to claim 1 , wherein said front portion ( 33 ′) of the outer cage ( 33 ) of said main ball joint ( 30 ) is connected to said actuator ( 10 ) by a single connecting rod ( 46 , 46 ′).
5. A blade according to claim 1 , wherein said first and second shafts ( 31 , 35 ) coincide.
6. A blade according to claim 1 , wherein said first and second shafts ( 31 , 35 ) are offset relative to each other.
7. A blade according to claim 1 , wherein said second shaft ( 35 ) is secured to the flap ( 5 ).
8. A rotorcraft rotor blade ( 1 ) having at least one trailing edge flap ( 5 ) that is tiltable, said flap ( 5 ) being suitable for pivoting about a virtual hinge axis (Y′) extending substantially along the span of said blade ( 1 ) and of said flap ( 5 ), wherein said flap ( 5 ) is provided with at least one main ball joint ( 30 ) having an inner cage ( 32 ) and an outer cage ( 33 ), and a first shaft ( 31 ) secured to said flap ( 5 ), the front portion ( 33 ′) of said outer cage ( 33 ) of the main ball joint ( 30 ) being connected to a linear actuator ( 10 ) that is arranged in said blade ( 1 ) and that enables said flap ( 5 ) to be pivoted, said first shaft ( 31 ) of the main ball joint ( 30 ) extending substantially perpendicularly to said virtual hinge axis (Y′) about which said flap ( 5 ) pivots, wherein, for said blade ( 1 ) having two actuators ( 10 , 10 ′), said flap ( 5 ) is provided with two main ball joints ( 30 , 30 ′) with the distance between said main ball joints ( 30 , 30 ′) along the span of the flap ( 5 ) being equal to half said span of said flap.