Gyroplane take-off rotor
AssigneeEla Aviacion, S.L.
InventorEmilio José LÓPEZ SÁNCHEZ
Life of this patent
Estimating the term…
Abstract
A rotor for gyroplane take-off, wherein the gyroplane comprises two blades (1), two blade holders (2), and a prelauncher device linked to the rotor via a transmission. The rotor comprises a mechanism attachable to the transmission, which comprises: a linear actuator (3); a tie rod (4), linked to the linear actuator (3); a vertical bar (5), linked to the tie rod (4); a rocker arm (6) hinged at an upper end of the vertical bar (5); two rods (7) hinged to the respective ends of the rocker arm (6) and extending downwards; and a elastic element (8) for holding the blade holders (2), and the blades (1) in flight position at a high angle of attack. The rotor allows a temporary reduction of the angle of attack of the blades (1) to shorten the take-off run.
Claims7
Gyroplane take-off rotor for shortening the take-off run of a gyroplane,
- wherein the gyroplane comprises two blades (1), two blade holders (2), for coupling the blades (1) to the rotor, and a prelauncher device linked to the rotor via a transmission;
- and
- wherein the rotor comprises a mechanism which can be coupled to the transmission with the prelauncher and is operable by said prelauncher;
- the rotor being characterized in that the mechanism comprises:
- a linear actuator (3), linked to and operable by the prelauncher;
- a tie rod (4), linked at one end to the linear actuator (3);
- a vertical bar (5), linked at one lower end to the other end of the tie rod (4);
- a rocker arm (6) hinged at an upper end of the vertical bar (5);
- two rods (7) hingedly linked to the respective ends of the rocker arm (6) and extending downwards;
- and
- a elastic element (8) for holding the blade holders (2) and the blades (1) in a flying position with a high angle of attack;
- wherein the rotor allows a temporary reduction of the angle of attack of the blades (1) to shorten the take-off stroke.
Rotor according to any one of the preceding claims wherein the vertical bar (5) passes through the rotor head.
Dependencies are inferred from the claim text.