METHOD FOR MODIFYING A SINGLE SHAFT COMBINED CYCLE POWER PLANT

Abstract

A method for modifying an existing single shaft combined cycle power plant having a steam turbine part and a gas turbine part which are connected to each other rigidly by an intermediate shaft. The gas turbine part is supported by two pin-ended supports allowing a certain axial displacement of the casing by rotating about corresponding axes. The old gas turbine part is replaced by a new gas turbine part having a different structure, namely a rigid support and a flexible support. Relative thermal expansion or displacement of the intermediate shaft is compensated by a hydraulic unit comprising a double-acting piston for displacing the gas turbine rotor with respect to the gas turbine stator. The hydraulic unit is controlled based on a displacement measurement in the steam turbine.

Claims

1. A method for modifying a single shaft combined cycle power plant comprising a gas turbine part having a gas turbine stator and a gas turbine rotor supported by a thrust bearing and a loose bearing, a steam turbine part having at least one steam turbine stator and a steam turbine rotor supported by two loose bearings, and an intermediate shaft, which is rigidly connected to the gas turbine rotor and to the steam turbine rotor forming a rigid single shaft configuration, wherein the gas turbine stator is arranged on at least two pin-ended supports positioned at a cold side and on at least two pin-ended supports positioned at a hot side of the gas turbine part, and wherein several tie-rods are provided, whose first ends are connected to the gas turbine stator and whose second ends are held stationary with respect to the steam turbine stator, the method comprising: removing the gas turbine part, the pin-ended supports and the tie rods, arranging at least one measuring device at the steam turbine part designed for measuring a physical dimension representing an axial displacement of the steam turbine rotor with respect to the at least one steam turbine stator caused by a thermal expansion of the intermediate shaft, providing a new gas turbine part having a gas turbine stator, a gas turbine rotor supported by a thrust bearing and by a loose bearing, a hydraulic unit acting on the thrust bearing and a controller designed for controlling the hydraulic unit on the basis of data provided by the at least one measuring device, wherein the thrust bearing and the hydraulic unit are designed in such a manner that the axial position of the gas turbine rotor relative to the gas turbine stator can be steples sly shifted by the hydraulic unit within a predetermined range, arranging the new gas turbine part on fixed supports positioned at its cold side and flexible supports positioned at its hot side, and rigidly connecting the gas turbine rotor to the intermediate shaft.

2. Method The method according to claim 1, wherein the physical dimension is a width of an axial gap and/or a width of a radial gap between the steam turbine rotor and the steam turbine stator.

3. A method for operating a single shaft combined cycle power plant comprising a gas turbine part having a gas turbine stator and a gas turbine rotor, a steam turbine part having at least one steam turbine stator and a steam turbine rotor, and an intermediate shaft, which is rigidly connected to the gas turbine rotor and to the steam turbine rotor forming a rigid single shaft configuration, the method comprising: controlling an axial position of the gas turbine rotor relative to the gas turbine stator depending on a change of the axial position of the steam turbine rotor relative to the steam turbine stator.

4. The method according to claim 3, further comprising: monitoring a width of an axial and/or a radial gap between the steam turbine rotor and the steam turbine stator and, when a change of width is registered, steplessly moving the gas turbine rotor in an axial direction relative to the gas turbine stator in order to compensate movement of the steam turbine rotor.

5. The method according to claim 4, wherein the gas turbine rotor is hydraulically moved.

Description

BRIEF DESCRIPTION OF THE DRAWINGS

[0013] FIG. 1 is a schematically view of a part of a single shaft combined cycle power plant, whose gas turbine part needs to be replaced;

[0014] FIG. 2 is a flow chart showing steps of a method according to an embodiment of the present invention;

[0015] FIG. 3 is a schematically view of said part of the single shaft combined cycle power plant shown in FIG. 1, whose gas turbine part has been replaced within the scope of such method;

[0016] FIG. 4 is a cross sectional view of the cold side of the new gas turbine part and

[0017] FIG. 5 an enlarged view of section V in FIG. 4.

DETAILED DESCRIPTION OF INVENTION

[0018] In the following same reference numerals denote same or similar components.

[0019] FIG. 1 shows a single shaft combined cycle power plant 1 comprising a gas turbine part 2 and a steam turbine part 3.

[0020] The gas turbine part 2 has a gas turbine stator 4 and a gas turbine rotor 5 supported by a thrust bearing 6 and a loose bearing 7. The gas turbine stator 4 is arranged on two pin-ended supports 8 positioned oppositely at the cold side and on two pin-ended supports 8 positioned oppositely at the hot side of the gas turbine part 2. Accordingly, the gas turbine stator 4 can be tilted around axes 9 in direction of arrows 10 thus enabling a movement of the gas turbine stator 4 in the axial direction A. Moreover, several tie-rods 11 (only one of them is shown in FIG. 1) are provided, whose first ends are connected to the gas turbine stator 4 and whose second ends are held stationary.

[0021] The steam turbine part 3 has two steam turbine stators 12 each being arranged on fixed supports (not shown) and a steam turbine rotor 13 supported by two loose bearings 7.

[0022] Moreover, the power plant 1 comprises an intermediate shaft 14, which is rigidly connected to the gas turbine rotor 5 and to the steam turbine rotor 13 forming a rigid single shaft configuration.

[0023] During the operation of the combined cycle power plant 1 the intermediate shaft 14 undergoes a thermal expansion, which leads to an axial displacement of the steam turbine rotor 13 within the steam turbine stators 12 as well as to an axial displacement of the gas turbine rotor 5 within the gas turbine stator 4 due to the rigid single shaft arrangement. The pin-ended supports 8 of the gas turbine part 2 in combination with the tie rods 11 at least partly compensate these axial displacements of the rotors 5, 13 relative to their stators 4, 12. The pin ended supports 8, as already stated above, allow an axial shift of the gas turbine stator 4 in a pendulum fashion. The tie rods 11, which expand similar compared to the intermediate shaft 14, initiate said axial movement. This compensation is required to keep axial clearances of both turbines in acceptable limits and to avoid damages in case of exceeding these limits.

[0024] If the gas turbine part 2 of the power plant 1 needs to be replaced by a new gas turbine part 2 in order to modify the power plant 1, the following steps are performed according to a method according to an embodiment of the present invention.

[0025] In a first step 51, the old gas turbine part 2, the pin-ended supports 8 and the tie rods 11 are removed.

[0026] Moreover, in step S2 at least one measuring device 15 is arranged at the steam turbine part 3. Said measuring 15 device is designed for measuring a physical dimension representing an axial displacement of the steam turbine rotor 13 with respect to at least one of the steam turbine stators 12. In the present case, the physical dimension is the width a of an axial gap between the steam turbine rotor 13 and the steam turbine stator 12. However, the monitoring of other physical dimensions is possible, such as the width of a radial gap between the steam turbine rotor 13 and the steam turbine stator 12. It is also possible to arrange several measuring devices 15 to monitor one or several different physical dimension(s) in order to provide redundant measuring devices 15.

[0027] In step S3 a new gas turbine part 2 is provided having a gas turbine stator 4, a gas turbine rotor 5 supported by a thrust bearing 16 and by a loose bearing 7, a hydraulic unit 17 acting on the thrust bearing 16 and a controller 18 designed for controlling the hydraulic unit 17 on the basis of data provided by the measuring devices 15. The thrust bearing 16 and the hydraulic unit 17 are designed in such a manner that the axial position of the gas turbine rotor 5 relative to the gas turbine stator 4 can be steples sly shifted by means of the hydraulic unit 17 within a predetermined range.

[0028] Thereafter, in step S4 the new gas turbine part 2 is arranged on fixed supports 19 positioned oppositely at its cold side and on flexible supports 21 positioned oppositely at its hot side, the flexible supports 21 are able to compensate thermal expansions of the stators 4. Moreover, the gas turbine rotor 5 is rigidly connected to the intermediate shaft 14. The modified power plant 1 is shown in FIG. 3.

[0029] During the operation of the combined cycle power plant 1 shown in FIG. 3, the intermediate shaft 14 undergoes a thermal expansion, which leads to an axial displacement of the steam turbine rotor 13 within the steam turbine stators 12. This displacement is registered by the measuring device 15. In order to compensate such displacement, the controller 18 controls the hydraulic unit 17 on the basis of the data received from the measuring device 15, whereupon the hydraulic unit 17 acts on the thrust bearing 16 in order to initiate an axial compensation movement of the gas turbine rotor 5 relative to the gas turbine stator 4. This compensation keeps the axial clearances of both turbines in acceptable limits and avoids damages in case of exceeding these limits.

[0030] FIGS. 4 and 5 show a possible structure of the thrust bearing 16. The thrust bearing 16 comprises an outer ring 20, which is arranged stationary at the gas turbine stator 4, wherein such movement is initiated by a plurality of circumferentially arranged double action pistons 23 manipulated by the hydraulic unit 17. Each piston 23 is provided at each of its free ends with a thrust bearing 24, which can be pressed in axial direction against the rotor shoulder 22. By moving the pistons 23 in the one or the other direction, the gas turbine rotor 5 is axially moved relative to the gas turbine stator 4.

[0031] Although the present invention has been illustrated and described in greater detail with reference to the exemplary embodiment, the invention is not limited to the examples disclosed and further variations can be inferred by a person skilled in the art, without departing from the scope of protection of the invention.