Turning device for a turbomachine

Patent metadata

Field	Value
Publication number	US-10873252-B2
Application number	US-201615772412-A
Country	US
Kind code	B2
Filing date	Oct 27, 2016
Priority date	Oct 30, 2015
Publication date	Dec 22, 2020
Grant date	Dec 22, 2020

Abstract

A turning device for a turbomachine comprises a plurality of electromagnets connectable to an electric power source; a rotor magnetically coupled with the electromagnets, connectable to a main shaft of the turbomachine and having a rotation axis, the electromagnets are arranged facing the rotor in order to induce eddy currents on a surface of the rotor and apply a torque to the rotor, thus rotating the main shaft.

First claim

What is claimed is:

1. A turning device for a turbomachine, the turning device comprising:
a rotor connectable to a shaft of the turbomachine and having a rotation axis and two surfaces forming opposite sides of the rotor; and
at least two sets of electromagnets connectable to an electric power source, at least one of the at least two sets of electromagnets acts on one of the two surfaces of the rotor and at least another of the at least two sets of electromagnets acts on the other of the two surfaces of the rotor, and at least one of the at least two sets of electromagnets comprises at least one first electromagnet arranged to act on a peripheral zone of one of the two surfaces of the rotor relative to the rotation axis at least one second electromagnet arranged to act on a central zone of the one of the two surfaces of the rotor relative to the rotation axis and at least one third electromagnet arranged between the at least one first electromagnet and the at least one second electromagnet,
wherein the rotor is configured to be magnetically coupled to the at least two sets of electromagnets and the at least two sets of electromagnets are arranged in proximity of the rotor in order to induce eddy currents on the two surfaces of the rotor and apply a torque to the rotor to rotate the shaft of the turbomachine.

2. The turning device according to claim 1 , wherein the electromagnets are configured to apply the torque along a predefined direction of rotation of the main shaft in order to accelerate the main shaft.

3. The turning device according to claim 1 , wherein the electromagnets are configured to apply the torque opposite to a predefined direction of rotation of the main shaft in order to slow down the main shaft.

4. The turning device according to claim 1 , wherein each of the at least two sets of electromagnets is configured to be powered by a respective phase of an input electric current, the respective phases being different relative to each other.

5. The turning device according to claim 1 , wherein the rotor is shaped as a disc.

6. The turning device according to claim 1 , wherein the rotor is provided with holes to optimize both the rotor weight and cooling.

7. The turning device according to claim 1 , wherein the rotor is configured to be directly jointed to the main shaft.

8. The turning device according to claim 1 , wherein the rotor is configured to be connected to the main shaft via transmission coupling.

9. The turning device according to claim 1 , wherein the rotor is made of an electrically conductive material.

10. The turning device according to claim 1 , wherein the at least one first electromagnet, the at least one second electromagnet and the at least one third electromagnet are radially spaced evenly along a common radial direction of the rotor.

11. A turbomachine comprising:
a shaft; and
a turning device comprising:
a rotor connectable to the shaft and having a rotation axis and two surfaces forming opposite sides of the rotor; and
at least two sets of electromagnets connectable to an electric power source, at least one of the at least two sets of electromagnets acts on one of the two surfaces of the rotor and at least another of the at least two sets of electromagnets acts on the other of the two surfaces of the rotor, and at least one of the at least two sets of electromagnets comprises at least one first electromagnet arranged to act on a peripheral zone of one of the two surfaces of the rotor relative to the rotation axis, at least one second electromagnet arranged to act on a central zone of the one of the two surfaces of the rotor relative to the rotation axis and at least one third electromagnet arranged between the at least one first electromagnet and the at least one second electromagnet,
wherein the rotor is configured to be magnetically coupled to the at least two sets of electromagnets and the at least two sets of electromagnets are arranged in proximity of the rotor in order to induce eddy currents on the two surfaces of the rotor and apply a torque to the rotor to rotate the shaft.

12. The turbomachine according to claim 11 , wherein the electromagnets are configured to apply the torque along a predefined direction of rotation of the main shaft in order to accelerate the main shaft.

13. The turbomachine according to claim 11 , wherein the electromagnets are configured to apply the torque opposite to a predefined direction of rotation of the main shaft in order to slow down the main shaft.

14. The turbomachine according to claim 11 , wherein the rotor is shaped as a disc.

15. The turbomachine according to claim 11 , wherein the rotor is provided with holes to optimize both the rotor weight and cooling.

16. The turbomachine according to claim 11 , wherein the rotor is configured to be at least one of directly jointed to the main shaft or connected to the main shaft via a transmission coupling.

Assignees

• Nuovo Pignone Tecnologie Srl

Inventors

• Defranciscis Sergio
• Naldi Lorenzo
• Fioravanti Duccio
• Ortiz Neri Massimiliano

Classifications

• F01D25/36 Primary

  using electric motors · CPC title

• H02K49/046 Primary

  with an axial airgap · CPC title

• H02K49/04

  of the eddy-current hysteresis type · CPC title

• H02K7/20

  Structural association with auxiliary dynamo-electric machines, e.g. with electric starter motors or exciters · CPC title

• H02K1/182

  to stators axially facing the rotor, i.e. with axial or conical air gap · CPC title