Mechanical reducer
The present invention relates to a mechanical reducer ( 6 ) for a turbomachine, in particular an aircraft, this reducer ( 6 ) including: a sun gear extending around an axis ( 61 ) of rotation, a crown which extends around the sun gear and which is configured to be fixed in rotation around said axis ( 61 ), planet gears which are meshed with the sun gear and the crown and which are held by a planet carrier ( 62 ) which is configured to be movable in rotation about said axis ( 61 ), In addition, the oil distributor ( 65 ) comprises a plurality of oil distribution modules ( 67 ) assembled together, each module ( 67 ) comprising at least one lubrication pipe ( 68 ) having an inlet intended to receive oil and an outlet ( 69 ) adapted to lead the oil into an opening ( 63 ) of the planet carrier ( 62 ), the opening ( 63 ) being intended for lubricating the reducer.
1. A mechanical reducer for a turbomachine, including:
a sun gear extending around an axis of rotation,
a crown which extends around the sun gear and which is configured to be fixed in rotation around said axis of rotation,
planet gears which are meshed with the sun gear and the crown and which are held by a planet carrier which is configured to be movable in rotation about said axis of rotation,
a lubricating oil distributor,
wherein the lubricating oil distributor comprises a plurality of separate oil distribution modules, each oil distribution module comprising a plurality of pipes, said oil distribution modules being assembled outside the planet carrier so as to form together the lubricating oil distributor, each oil distribution module comprising at least one lubrication pipe having an inlet adapted to receive oil and an outlet adapted to lead the oil into at least one opening of the planet carrier, the at least one opening being configured for lubricating the reducer.
2. The reducer according to claim 1 , wherein several pipes of a same oil distribution module have different diameters.
3. The reducer according to claim 1 , wherein several pipes of a same oil distribution module have at least two different orientations.
4. The reducer according to claim 1 , wherein the planet carrier has a plurality of evenly distributed openings.
5. The reducer according to claim 4 , wherein the planet carrier comprises a number of openings defined by n times the number of planet gears, n being an integer number.
6. The reducer according to claim 1 , wherein the outlet of each lubrication pipe comprises a sealing arrangement, the sealing arrangement comprising at least one O-ring seal configured to seal a connection of the outlet with each corresponding opening.
7. The reducer according to claim 6 , wherein the sealing arrangement comprises a combination of two O-ring seals and a radial labyrinth or a coil comprising a double O-ring seal and a hoop.
8. The reducer according to claim 1 , wherein the distributor is held between the planet carrier and a nut.
9. A method for assembling a reducer according to claim 8 , the method comprising at least the following steps:
positioning the nut on the axis of rotation;
introducing the outlets of the lubrication pipes into the corresponding openings of the planet carrier;
rotating each oil distribution module to assemble each oil distribution module to another one between the planet carrier and the nut;
tightening the nut.