Oil distribution device for a rotating planet carrier of a mechanical reduction gear of a turbomachine

1. An oil distribution device for a rotating planet carrier of a mechanical reduction gear of a turbomachine, the oil distribution device being integral with a tubular member for supporting a bearing of the rotating planet carrier, said oil distribution device comprising:

an oil inlet and a row of oil outlets opening onto an external surface configured to be surrounded at least in part by the tubular member; and

at least two internal cavities connected in series by at least one calibrated orifice,

wherein a receiving cavity of the at least two internal cavities is connected to said oil inlet, and internal calibrated channels for conveying oil extend from said at least two internal cavities to orifices of said external surface to form said row of oil outlets.

2. The oil distribution device according to claim 1 , wherein the oil distribution device is configured to be attached and fixed in said tubular member.

3. The oil distribution device according to claim 1 , wherein the at least two internal cavities are arranged along a line (Z) which passes through a center of the oil distribution device.

4. The oil distribution device according to claim 3 , wherein said receiving cavity is disposed at a periphery of the oil distribution device and is configured to be closest to an axis (X) of rotation of the planet carrier when the oil distribution device is mounted on the planet carrier.

5. The oil distribution device according to claim 1 , further comprising an internal bore in which are inserted and fixed, pellets which each comprise one of the said at least one calibrated orifice, the pellets delimiting between them said at least two internal cavities.

6. The oil distribution device according to claim 5 , in which said internal bore is stepped and comprises a plurality of sections of different diameters.

7. The device according to claim 6 , wherein the plurality of sections of different diameters is arranged from a smallest diameter section to a largest diameter section opening out at the periphery of the oil distribution device.

8. The oil distribution device according to claim 1 , further comprising:

a circular base having a machined face; and

an annular cover attached to said circular base, on a side of the machined face, the machined face being machined to define said at least two internal cavities and said internal calibrated channels between the circular base and the annular cover.

9. A rotating planet carrier for a mechanical reduction gear of a turbomachine, comprising an annular row of tubular members configured for supporting bearings which are parallel to each other and to an axis (X) of rotation of the rotating planet carrier, cylindrical tracks and surfaces configured for guiding rolling elements and at least one cage of the rolling elements being defined at a periphery of each of the tubular members, and at least one oil distribution device according to claim 1 being integral coaxially with each of these the tubular members.

10. The planet carrier according to claim 9 , wherein each of the tubular members comprises a tubular support comprising an external cylindrical surface configured for mounting an inner ring, and on which tubular member are formed oil circulation grooves which are in fluid communication with said oil outlets of the oil distribution device and oil ducts formed in the inner ring, wherein said grooves are rectilinear and parallel to each other and to an axis of revolution (Y) of the cylindrical surface.

11. An aircraft turbomachine, comprising the rotating planet carrier according to claim 9 .

12. An aircraft turbomachine, comprising an oil distribution device according to claim 1 .