METHOD FOR BARRING A ROTOR OF A TURBOMACHINE AND BARRING APPARATUS FOR CONDUCTING SUCH METHOD

• US 20140199157A1
• Filed: 01/15/2014
• Published: 07/17/2014
• Est. Priority Date: 01/16/2013
• Status: Active Grant

• Current Assignee: Ansaldo Energia IP UK Limited (Ansaldo Energia SPA)
• Original Assignee: Alstom Technology Ltd. (Alstom SA)
• Inventors: HAERMS, Axel, Staehli, Felix, Rauch, Marc, Knopf, Eric
• Granted Patent: US 9,970,328 B2
• Time in Patent Office: Days
• US Class Current: 415/1
• CPC Class Codes: F01D 21/06 Shutting-down
• CPC Class Codes: F01D 25/34 Turning or inching gear
• CPC Class Codes: F01D 25/36 using electric motors
• CPC Class Codes: F05D 2260/4031 as in toothed gearing
• CPC Class Codes: F05D 2270/304 Spool rotational speed

Abstract

A method for barring a rotor of a thermally loaded turbomachine includes stopping normal operation of the turbomachine; providing a barring device for rotating the rotor about a machine axis; coupling the barring device to the rotor; letting the rotor cool down during cool down of the rotor rotating the rotor by means of the barring device. A damage of the machine due to thermally induced buckling during the barring process is avoided by consecutively determining the force or torque applied to the rotor by the barring device for rotating the rotor and/or the circumferential speed of the rotor during barring. The rotation of the rotor is controlled by means of the barring device in dependence of the determined force or torque and/or circumferential speed in order to reduce a bending or imbalance of the rotor, which is due to a nonuniform temperature distribution on the rotor during cool down.

Claims

1. A method for barring a rotor of a thermally loaded turbomachine, comprising:

stopping normal operation of said turbomachine;

providing a barring device for rotating said rotor about a machine axis;

coupling said barring device to said rotor;

letting said rotor cool down; and

during cool down of said rotor rotating said rotor by means of said barring device;

wherein

the force or torque applied to said rotor by said barring device for rotating said rotor and/or the circumferential speed of the rotor during barring are consecutively determined; and

the rotation of said rotor by means of said barring device is controlled in dependence of said determined force or torque and/or circumferential speed in order to reduce a bending or imbalance of said rotor, which is due to a nonuniform temperature distribution on said rotor during cool down.

2. The method according to claim 1, wherein the bending or imbalance of said rotor is caused by a nonuniform circumferential temperature profile outside of said rotor, and that said rotor is rotated by said barring device such that said nonuniform temperature distribution on said rotor is reduced by said nonuniform circumferential temperature profile outside of said rotor.

3. The method according to claim 2, wherein said rotor is continuously rotated by said barring device, and that the circumferential speed is varied in dependence of said determined force or torque and/or circumferential speed.

4. The method according to claim 1, wherein said rotor is rotated by said barring device in an incremental fashion.

5. The method according to claim 4, wherein said rotor is rotated by said barring device using a ratchet and pawl mechanism.

6. The method according to claim 1, wherein said barring device is driven by an electric motor, and that the current of said motor is measured to determine said force or torque applied to said rotor.

7. The method according to claim 1, wherein said barring device is driven by a hydraulic pressure, and that said hydraulic pressure is measured to determine said force or torque applied to said rotor.

8. The method according to claim 1, wherein said turbomachine is a stationary gas turbine.

9. A barring apparatus for conducting the method according to claim 1, said barring apparatus comprising a barring device with a barring drive, which can be coupled to the rotor of said turbomachine, and a control unit provided for controlling said barring device, wherein said control unit receives signals from a speed sensor and/or said barring drive of said barring device.

10. The barring apparatus according to claim 9, wherein the speed sensor provided is configured to sense the circumferential speed of said rotor.

11. The barring apparatus according to claim 9, wherein said barring drive comprises an electric motor, and that said control unit receives signals, which are related to the electric current flowing through said electric motor.

12. The barring apparatus according to claim 11, wherein said electric motor is a servo motor.

13. The barring apparatus according to claim 9, wherein said barring device comprises a barring mechanism with a pawl, which is designed to interact in a reciprocating manner with a ratchet wheel on said rotor.

14. A gas turbine comprising a barring apparatus according to claim 9.