Epicyclic reduction device for the rotational drive of blade sets of a reduction turbomachine
An epicyclic gear device for driving rotation of a first blade set of a turbine engine, the device: including a sunwheel centered on a longitudinal axis of the turbine engine and connected to a rotor of the engine in order to be driven in rotation; at least one planet meshing with the sunwheel; a planet carrier rotatably carrying the planet and connected to a first blade set in order to drive it in rotation; and a ring meshing with the planet; the sunwheel being connected to the rotor via a first constant velocity ball transmission joint.
1. An epicyclic gear device for driving rotation of at least a first blade set of a turbine engine, the device comprising:
a sunwheel centered on a longitudinal axis of the turbine engine and adapted to be connected to a rotor of the engine in order to be driven in rotation;
at least one planet meshing with said sunwheel;
a planet carrier rotatably carrying said at least one planet and suitable for being connected to said at least one first blade set in order to drive said at least one first blade set in rotation;
a ring meshing with said at least one planet; and
a first constant velocity ball transmission joint,
wherein the sunwheel is configured to be connected to said rotor of the engine via said first constant velocity ball transmission joint, and
wherein said first constant velocity ball transmission joint has a first end provided with a flange extending radially outwards, and a second end opposite from said first end and provided with an annular portion mounted around said sunwheel by a system of fluting.
2. The device according to claim 1 , wherein said first constant velocity ball transmission joint is a joint selected from the following: a Rzeppa joint, a Weiss joint, a plunging joint, a double-offset plunging joint.
3. The device according to claim 1 , wherein said flange of said first constant velocity ball transmission joint is suitable for being fastened to a flexible drive shaft of said rotor of the engine via a plurality of bolted connections.
4. The device according to claim 1 , wherein said ring is suitable for being connected to a second blade set via a second constant velocity ball transmission joint.
5. The device according to claim 4 , wherein said first or second blade sets belong to one or two propellers of a turboprop or to one or two fans of a turbojet.
6. The device according to claim 4 , wherein said second constant velocity ball transmission joint is selected from the following: a Rzeppa joint, a Weiss joint, a plunging joint, a double-offset plunging joint.
7. The device according to claim 4 , wherein said second constant velocity ball transmission joint has a first end provided with a first flange extending radially outwards and a second end opposite from said first end and provided with a second flange extending radially inwards.
8. The device according to claim 7 , wherein a flexible drive shaft of said second blade set is mounted inside a stiff drive shaft of said first blade set that is suitable for being fastened to said planet carrier.
9. The device according to claim 1 , wherein said sunwheel, said at least one planet, and said ring are each doubled up axially and comprising helical wheels mounted in opposition in a double helix configuration so as to cancel an induced axial thrust.
10. The device according to claim 7 , wherein said second flange of said second constant velocity ball transmission joint is suitable for being fastened to a flexible drive shaft of said second blade set via a plurality of bolted connections.