Shaft for a turbomachine
A turbomachine including a turbine rotor, a compressor rotor, and a shaft, and at least one balance weight assembly connected to the shaft. The shaft drivingly connects the turbine rotor with the compressor rotor to rotate the compressor rotor about a rotational axis when the turbine rotor rotates about the rotational axis. The at least one balance weight assembly including a first chamber, at least one additional chamber, and a balance weight movable between the first chamber and the at least one additional chamber.
1. A method of balancing a shaft of a turbomachine that is bowed, the method comprising:
determining a direction of bow of the shaft;
monitoring at least one of a time after shutdown of the turbomachine or a temperature indictive of the bow of the shaft;
determining a magnitude of the bow of the shaft based on the at least one of the time after shutdown or the temperature; and
moving a balance weight connected to the shaft from a first position to a second position to move the center of gravity of the shaft in a direction opposite to the direction of bow based on the magnitude of bow of the shaft.
2. The method of claim 1 , wherein the balance weight is part of a balance weight assembly including a first chamber and at least one additional chamber, and
wherein moving the balance weight from the first position to the second position includes moving the balance weight from the first chamber to the at least one additional chamber.
3. The method of claim 1 , wherein the turbomachine includes:
a turbine rotor rotatable about a rotational axis; and
a compressor rotor rotatable about the rotational axis to compress air flowing past the compressor rotor, the shaft drivingly connecting the turbine rotor with the compressor rotor to rotate the compressor rotor about the rotational axis when the turbine rotor rotates about the rotational axis.
4. The method of claim 1 , further comprising determining an amount of bow correction needed to facilitate start-up of the turbomachine based on the direction of bow and the magnitude, wherein the balance weight is moved based on the amount of bow correction needed.
5. The method of claim 1 , wherein the balance weight is a flowable mass.
6. A method of balancing a shaft of a turbomachine that is bowed, the method comprising:
determining a direction of bow of the shaft; and
moving a balance weight connected to the shaft from a first position to a second position to move the center of gravity of the shaft in a direction opposite to the direction of bow, the balance weight being a flowable mass,
wherein the balance weight is part of a balance weight assembly including a first chamber and at least one additional chamber, the first chamber and the at least one additional chamber being fluidly connected to each other by a flow passage, the flowable mass being movable between the first chamber and the at least one additional chamber by flowing through the flow passage, and
wherein moving the balance weight from the first position to the second position includes moving the balance weight from the first chamber to the at least one additional chamber.
7. The method of claim 6 , wherein the flowable mass is at least one of (i) a powder comprising a plurality of particles, (ii) a liquid, or (iii) a semi-solid viscous mass.
8. The method of claim 6 , wherein moving the balance weight between the first chamber and the at least one additional chamber includes operating a valve positioned in the flow passage.
9. The method of claim 6 , wherein the first chamber is an inner chamber and the at least one additional chamber is an outer chamber.
10. The method of claim 9 , wherein the inner chamber, the outer chamber, and the flow passage are arranged in an hourglass shape.
11. The method of claim 6 , wherein the balance weight assembly is an annular housing connected to the shaft, the annular housing being divided into a plurality of chambers in a circumferential direction of the shaft, the plurality of chambers including the first chamber and the at least one additional chamber.
12. The method of claim 11 , wherein adjacent chambers of the plurality of chambers are separated from each other by a baffle.
13. The method of claim 12 , wherein the baffle is a plate having a plurality of orifices fluidly connecting adjacent chambers of the plurality of chambers.
14. A method of balancing a shaft of a turbomachine that is bowed, the method comprising:
determining a direction of bow of the shaft;
monitoring at least one of a time after shutdown of the turbomachine or a temperature indictive of the bow of the shaft;
determining a magnitude of the bow of the shaft based on the at least one of the time after shutdown or the temperature; and
moving a plurality of balance weights connected to the shaft from a first position to a second position to move the center of gravity of the shaft in a direction opposite to the direction of bow based on the magnitude of bow of the shaft.
15. The method of claim 14 , wherein the plurality of the balance weights is arrayed circumferentially around the shaft.
16. The method of claim 14 , wherein each balance weight of the plurality of the balance weights is part of one balance weight assembly of a plurality of balance weight assemblies, each balance weight assembly including a first chamber and a second chamber, and
wherein moving the balance weight from the first position to the second position includes moving the balance weight from the first chamber to the second chamber.
17. The method of claim 16 , wherein the plurality of balance weight assemblies is arrayed circumferentially around the shaft, and
wherein the first chamber of each balance weight assembly is an inner chamber and the second chamber of each balance weight assembly is an outer chamber.
18. The method of claim 17 , wherein the outer chamber is positioned radially outward of the inner chamber.
19. The method of claim 16 , wherein the balance weight is a flowable mass, and the first chamber and a second chamber are fluidly connected to each other by a flow passage, and
wherein moving the balance weight between the first chamber and the second chamber includes operating a valve positioned in the flow passage.
20. The method of claim 2 , wherein the at least one additional chamber is a second chamber, the second chamber being located radially outward of the first chamber.