Rotorcraft blade provided with a tiltable flap and a fastener tongue
View Patent ↗The present invention relates to a rotorcraft rotor blade ( 1 ) that comprises at least one tiltable trailing-edge flap ( 5 ), said flap ( 5 ) being suitable for pivoting about a virtual hinge axis (Y′) extending substantially in the span direction of said blade ( 1 ) and of said flap ( 5 ). The blade ( 1 ) is remarkable in that the flap ( 5 ) is provided with at least two fastener ball joints ( 30 ), each provided with an inner cage ( 32 ) together with an outer cage ( 33 ) and a first pin ( 31 ) that is also secured to said flap ( 5 ), the first pins ( 31 ) of the fastener ball joints ( 30 ) being perpendicular to the virtual pivot axis (Y′) of the flap ( 5 ). In addition, the blade ( 1 ) is provided at its trailing edge (BF) with a fastener tongue ( 20 ) provided with ball-receiving sockets ( 21 ), the outer cages ( 33 ) of the fastener ball joints ( 30 ) being secured to the ball-receiving sockets ( 21 ).
1. A rotorcraft rotor blade ( 1 ) having at least one tiltable trailing-edge flap ( 5 ), said flap ( 5 ) being suitable for pivoting about a virtual hinge axis (Y′) extending substantially in the span direction of said blade ( 1 ) and of said flap ( 5 ), wherein said flap ( 5 ) includes at least two fastener ball joints ( 30 ) each provided with an inner cage ( 32 ) together with an outer cage ( 33 ) and a first pin ( 31 ) secured to said flap ( 5 ), said blade being provided at its trailing edge (BF) with a fastener tongue ( 20 ) provided with ball-receiving sockets ( 21 ), said outer cages ( 33 ) of the fastener ball joints ( 30 ) being secured to said ball-receiving sockets ( 21 ), wherein said first pin ( 31 ) of each fastener ball joint ( 30 ) is perpendicular to said virtual pivot axis (Y′) of said flap ( 5 ).
2. A blade according to claim 1 , wherein said blade ( 1 ) has a suction side face ( 50 ) and a pressure side face ( 6 ), with said side faces ( 50 and 6 ) meeting at the trailing edge (BF) of said blade ( 1 ) in order to form said tongue ( 20 ).
3. A blade according to claim 1 , wherein said tongue ( 20 ) is rigid.
4. A blade according to claim 1 , wherein said flap ( 5 ) includes an opening provided with a bottom lip ( 5 ″) and a top lip ( 5 ′), said tongue ( 20 ) being arranged between said top and bottom lips ( 5 ′, 5 ″) when said flap ( 5 ) is secured to said blade ( 1 ).
5. A blade according to claim 4 , wherein said bottom and top lips ( 5 ″, 5 ′) describe an angular field β of about 20°.
6. A blade according to claim 1 , wherein the angle of inclination of said flap ( 5 ) relative to said blade ( 1 ) is controlled with the help of at least one control arm ( 46 ) secured to said flap ( 5 ), said control arm ( 46 ) being controlled by an actuator ( 10 , 10 ′) arranged in said blade ( 1 ).
7. A blade according to claim 6 , wherein said tongue ( 20 ) extends along the span direction of said flap ( 5 ), with said tongue ( 20 ) comprising at least two distinct portions ( 20 ′, 20 ″, 20 ″′) that are separated by a control arm ( 46 ).
8. A rotorcraft rotor blade ( 1 ) having at least one tiltable trailing-edge flap ( 5 ), said flap ( 5 ) being suitable for pivoting about a virtual hinge axis (Y′) extending substantially in the span direction of said blade ( 1 ) and of said flap ( 5 ), wherein said flap ( 5 ) includes at least two fastener ball joints ( 30 ) each provided with an inner cage ( 32 ) together with an outer cage ( 33 ) and a first pin ( 31 ) secured to said flap ( 5 ), said blade being provided at its trailing edge (BF) with a fastener tongue ( 20 ) provided with ball-receiving sockets ( 21 ), said outer cages ( 33 ) of the fastener ball joints ( 30 ) being secured to said ball-receiving sockets ( 21 ), wherein said blade ( 1 ) has a rib ( 7 ) in the proximity of its trailing edge (BF), with said tongue ( 20 ) being situated substantially halfway up said rib ( 7 ).
9. A rotorcraft rotor blade ( 1 ) having at least one tiltable trailing-edge flap ( 5 ), said flap ( 5 ) being suitable for pivoting about a virtual hinge axis (Y′) extending substantially in the span direction of said blade ( 1 ) and of said flap ( 5 ), wherein said flap ( 5 ) includes at least two fastener ball joints ( 30 ) each provided with an inner cage ( 32 ) together with an outer cage ( 33 ) and a first pin ( 31 ) secured to said flap ( 5 ), said blade being provided at its trailing edge (BF) with a fastener tongue ( 20 ) provided with ball-receiving sockets ( 21 ), said outer cages ( 33 ) of the fastener ball joints ( 30 ) being secured to said ball-receiving sockets ( 21 ), wherein said tongue ( 20 ) includes a flexible tape ( 22 ) at its free end (EX).