GAS TURBINE TRAIN WITH STARTER MOTOR

Abstract

A power plant and method for operating a power plant having a gas turbine and a generator which are arranged on a section, a shaft which connects the gas turbine to the generator in order to transmit a force, and a clutch which is arranged in the shaft between the gas turbine and the generator such that the shaft includes at least two sub-shafts, a first sub-shaft between the generator and the clutch and a second sub-shaft, which is referred to as a gas turbine intermediate shaft, between the gas turbine and the clutch. An electric motor is arranged in the section between the clutch and the gas turbine in order to accelerate the gas turbine.

Claims

1.-10. (canceled)

11. A power plant comprising: a gas turbine and a generator which are arranged in a train, a shaft which connects the gas turbine to the generator for power transmission, a clutch which is arranged in the shaft between gas turbine and generator so that the shaft comprises at least two shaft sections, with a first shaft section between generator and clutch and a second shaft section, referred to as the gas turbine intermediate shaft, between gas turbine and clutch, and an electric motor for accelerating the gas turbine which is arranged in the train between clutch and gas turbine and always co-rotates at the rotational speed of the gas turbine.

12. The power plant as claimed in claim 11, wherein the motor is an asynchronous motor.

13. The power plant as claimed in claim 11, further comprising: a rotor body, wherein provision is made in the gas turbine intermediate shaft for the rotor body and the rotor body has slots in which are arranged copper bars which at their face ends are connected to the rotor body via short-circuit rings so that the gas turbine intermediate shaft is designed at least partially as a squirrel-cage solid rotor.

14. The power plant as claimed in claim 13, wherein a rotating-field stator encloses the gas turbine intermediate shaft in the region of the rotor body and is of a multi-piece construction for better installation and removal.

15. The power plant as claimed in claim 11, wherein the gas turbine intermediate shaft and the motor are interconnected via flanges.

16. The power plant as claimed in claim 11, further comprising: an intake duct for air which is to be compressed in a compressor of the gas turbine, wherein the motor is arranged in the intake duct.

17. The power plant as claimed in claim 11, further comprising: an intake duct for air which is to be compressed in a compressor of the gas turbine, wherein the motor is arranged outside the intake duct.

18. The power plant as claimed in claim 11, further comprising: a converter which is connected to the generator, wherein the converter switches over to the motor when required.

19. A method for operating a power plant during grid stabilization operation, the power plant comprising, arranged in a train, a gas turbine, a generator, a shaft which connects the gas turbine to the generator for power transmission, and also a clutch which is arranged in the shaft between gas turbine and generator, the method comprising: in a first phase, the generator is synchronized with a supply grid and is required as a rotating phase changer for grid stabilization while the gas turbine is kept in turning operation or is stationary, and in a second phase, the generator remains synchronized with the supply grid and the gas turbine is started via a motor which is arranged in the train of the power plant.

20. The method as claimed in claim 19, wherein in the case of a rotational speed of the gas turbine between firing rotational speed and synchronization rotational speed the motor is switched off and co-rotates in idling mode at the rotational speed of the gas turbine.

Description

BRIEF DESCRIPTION OF THE DRAWINGS

[0028] The invention is explained in more detail by way of example with reference to the drawings. In the drawings, schematically and not to scale:

[0029] FIG. 1 shows the train of a power plant, especially a gas turbine plant with a starter motor, integrated into the intermediate shaft, for the gas turbine,

[0030] FIG. 2 shows a starter motor split open along the longitudinal axis and

[0031] FIG. 3 shows a starter motor in cross section.

DETAILED DESCRIPTION OF INVENTION

[0032] FIG. 1 shows, schematically and by way of example, a power plant 1 with a gas turbine 2 and a generator 3, arranged in a train 18. The gas turbine 2 is connected to the generator 3 for power transmission via a shaft 4 in which is arranged a clutch 5. As a result, the shaft comprises two shaft sections 6 and 7, with a first shaft section 6 between generator 3 and clutch 5 and a second shaft section 7, referred to as the gas turbine intermediate shaft 7, between gas turbine 2 and clutch 5. According to the invention, an electric motor 8 for accelerating the gas turbine 2 is arranged in the train 18. The electric starter motor 8 is positioned directly in the train 18 between gas turbine 2 and the clutch 5, which is advantageously constructed as a self-shifting and synchronizing clutch.

[0033] FIG. 1 shows an exemplary embodiment in which the motor 8 is arranged in the intake duct 15 for air which is to be compressed in a compressor 16 of the gas turbine 2. Alternatively, the motor 8 can also be arranged outside the intake duct 15 but still in the train 18. This, however, is not shown.

[0034] FIG. 1 also shows that a converter 17, which is connected to a generator 3, can expediently also be switched over to the motor 8.

[0035] FIG. 2 shows details relating to the motor 8 in longitudinal section. In the exemplary embodiment of FIG. 2, provision is made in the gas turbine intermediate shaft 7 for a rotor body 9. The rotor body 9 has slots 10 in which are arranged copper bars 11 which serve as rotor cage bars. These are connected at their face ends 12 to the rotor body 9 via short-circuit rings 13 so that the gas turbine intermediate shaft 7 is designed at least partially as a squirrel-cage solid rotor.

[0036] FIG. 2 also shows a rotating-field stator 14 with a stator overhang winding 20 and also a rotating-field laminated core 21 which encloses the gas turbine intermediate shaft 7 in the region of the rotor body 9.

[0037] In the simplest case, the rotating-field stator 14 is constructed in one piece. The gas turbine intermediate shaft 7 and the motor 8 are then expediently interconnected via flanges. FIG. 2 shows a shrunk-on coupling 19 for this.

[0038] In an alternative embodiment, which is not shown, the rotating-field stator 14 is of a multipiece or separable construction for better installation and removal.

[0039] FIG. 3 shows the motor 8 from FIG. 2 in cross section with rotating-field stator 14, stator slot 23 and intermediate shaft 7 with rotor body 9 and copper bars 11 (=rotor bars).