Turbine engine provided with a lubrication unit
A turbine engine includes two rotary shafts and a lubrication unit. The lubrication unit has at least one pump which a casing inside of which a rotor is mounted and driven by one of the rotary shafts. The pump casing is rotated by the other rotary shaft such that the actuation of the pump depends on the difference between rotational speeds of the shafts. The shafts are a drive shaft and a fan shaft, respectively, wherein the fan shaft is driven by the drive shaft by means of a reduction gear which is lubricated by the lubrication unit. The reduction gear is annular and the pump passes axially therethrough.
1. A turbine engine including two rotary shafts and a lubrication unit comprising at least one pump which comprises a casing inside of which a rotor is mounted and driven by one of said rotary shafts, the pump casing being rotated by the other of said rotary shafts such that the actuation of the pump depends on the difference between rotational speeds of the rotary shafts, wherein the rotary shafts are a drive shaft and a fan shaft, respectively, the fan shaft being driven by the drive shaft by an annular reduction gear which is lubricated by the lubrication unit, the pump axially passing through the reduction gear and the fan shaft, and wherein the casing of the pump is coupled by splines to the fan shaft and the rotor of the pump is coupled by splines or knucklebones to the drive shaft.
2. The turbine engine according to claim 1 , wherein the rotary shafts are coaxial and the casing of the pump is mounted coaxially with the shafts.
3. The turbine engine according to claim 1 , wherein the rotor of the pump is driven by the drive shaft by a ring gear with internal or external toothing.
4. The turbine engine according to claim 1 , wherein the pump has blades or a gerotor.
5. The turbine engine according to claim 4 , the rotor of the pump comprises a pump shaft which supports:
at least one internal gerotor pinion engaging with an internally toothed ring gear which is movable in rotation in the casing of the pump, or
at least one rotor with blades engaging with the casing of the pump.
6. The turbine engine according to claim 5 , wherein the axis of rotation of the pump shaft is fixed within a reference system of the casing of the pump.
7. The turbine engine according to claim 1 , wherein the pump has an elongated shape.
8. A torque transmission system for a turbine engine, including two rotary shafts coupled together by a reduction gear having an epicyclic gear train, the system further comprising a lubrication unit comprising at least one pump which comprises a casing inside of which a rotor is mounted and driven by one of said rotary shafts, the pump casing being rotated by the other of said rotary shafts such that the actuation of the pump depends on the difference between rotational speeds of the rotary shafts, wherein the rotary shafts are a drive shaft and a fan shaft, respectively, the fan shaft being driven by the drive shaft by an annular reduction gear which is lubricated by the lubrication unit, the pump axially passing through the reduction gear and the fan shaft, and wherein the casing of the pump is coupled to the fan shaft, and the rotor of the pump is coupled to the drive shaft.