Device for evacuation of a ventilated lubricated chamber of a turbomachine
A ventilated chamber ( 19 ), subject to an irruption of air at a pressure higher than that in a surrounding chamber ( 20 ) through labyrinth seals separating them and evacuation of excess air through an evacuation duct ( 30 ), comprises a motor-driven compressor ( 32 ) in the evacuation duct to facilitate suction and evacuation, even when the engine speed does not allow a large overpressure in the chamber ( 20 ).
1. A device for evacuation of a ventilated lubricated chamber of a turbomachine, said device comprising a ventilation duct connecting the ventilated lubricated chamber to an ambient environment around the turbomachine, comprising a motor-driven compressor, creating a negative pressure differential in the ventilation duct and suction from the ventilated lubricated chamber, wherein the ventilation duct is a central tube coaxial with a rotation axis of a turbomachine rotor and rigidly fixed to said turbomachine rotor, wherein the motor-driven compressor is at least partly received in said central tube.
2. The device for evacuation of the ventilated lubricated chamber according to claim 1 , wherein the motor-driven compressor is installed in one end close to the ambient environment of said central tube, and is connected to said one end through a rotating seal, and is coaxial with said rotation axis.
3. The device for evacuation of the ventilated lubricated chamber according to claim 2 , wherein the central tube is included in a low pressure shaft belonging to the rotor of the turbomachine.
4. The device for evacuation of the ventilated lubricated chamber according to claim 3 , wherein the motor-driven compressor is housed in a hollow of a tail cone forming part of a stator of the turbomachine, and to which it is connected by a support.
5. The device for evacuation of the ventilated lubricated chamber according to claim 4 , wherein the motor-driven compressor comprises a circular collar clamped to the support.
6. The device for evacuation of the ventilated lubricated chamber according to claim 1 , wherein the motor-driven compressor comprises at least one compressor stage and an electric motor controlled by an electric cable leading to a control device external to the turbomachine.
7. The device for evacuation of the ventilated lubricated chamber according to claim 1 , wherein the motor-driven compressor comprises at least one compression stage with axial flow.
8. A turbomachine, comprising a ventilated lubricated chamber, and a device for evacuation of the ventilated lubricated chamber according to claim 1 .
9. The turbomachine according to claim 8 , further comprising an air take-off point leading to a pressurised chamber surrounding the ventilated lubricated chamber, said take-off point being located upstream from turbomachine compressors, upstream from an inlet fan, said air take-off point drawing air being at ambient pressure.