Compressor rotor structure and method for arranging said rotor structure

Patent metadata

Field	Value
Publication number	US-11959485-B2
Application number	US-202017995484-A
Country	US
Kind code	B2
Filing date	May 14, 2020
Priority date	May 14, 2020
Publication date	Apr 16, 2024
Grant date	Apr 16, 2024

Abstract

Compressor rotor structure and methodology for harmonizing compressor aerodynamics and rotordynamics are provided. Disclosed embodiments benefit from a compressor design effective for improving rotordynamics (e.g., stiffer rotor structure) without reducing a usable aerodynamics range of the compressor. This design may involve variation of the rotor structure along the rotor axis to locate respective surfaces defined by respective inlets of the one or more impellers at a varying distance relative to the rotor axis based on respective ratios selected for the configuration of the impeller bodies. This arrangement may be effective for improving rotordynamics while satisfactorily meeting the respective varying aerodynamics requirements at the various compression stages by the impeller bodies.

First claim

What is claimed is:

1. A rotor structure in a compressor, the rotor structure comprising:
a tie bolt and two rotor shafts respectively affixed to respective ends of the tie bolt;
a plurality of impeller bodies supported by the tie bolt; and
a plurality of hirth couplings to mechanically couple the plurality of impeller bodies to one another along a rotor axis,
wherein a first impeller body of the plurality of impeller bodies is arranged to provide a first stage of compression, and each subsequent impeller body provides a subsequent stage of compression,
wherein each respective impeller body defines a respective Di/D2 ratio,
wherein the Di/D2 ratio of at least one of the impeller bodies is different than the Di/D2 ratio of the remaining impeller bodies,
wherein, based on the different Di/D2 ratio, respective surfaces defined by an inlet of said at least one of the impeller bodies are located at a different distance relative to the rotor axis compared to location of respective surfaces defined by respective inlets of the remaining impeller bodies,
wherein Di is indicative of a respective inner diameter of a flow path into an inlet of a respective impeller body, and
wherein D2 is indicative of respective outer diameter of the respective impeller body.

2. The rotor structure of claim 1 , wherein a respective range of Di/D2 is from a value of 0.2 to a value of 0.65.

3. The rotor structure of claim 2 , wherein a respective range of Di/D2 is from a value of 0.25 to a value of 0.50.

4. The rotor structure of claim 1 , wherein a variation of the rotor structure along the rotor axis is based on a variation of respective Di/D2 ratios, wherein the variation of the rotor structure along the rotor axis comprises locating the respective surfaces defined by the respective inlets of the at least one of the impeller bodies at a varying distance relative to the rotor axis.

5. The rotor structure of claim 4 , wherein the locating of the respective surfaces defined by the respective inlets of the one or more impeller bodies at the varying distance relative to the rotor axis is arranged to reduce inlet Mach number in the compressions stages by the one or more impeller bodies and adjust rotor stiffness along the rotor axis.

6. The rotor structure of claim 1 , further comprising at least one spring biasing mechanism arranged to adjust radial stiffness at a respective location of the tie bolt.

7. The rotor structure of claim 6 , wherein the respective location where the at least one spring biasing mechanism is arranged is at or proximate a midspan section of the tie bolt.

8. The rotor structure of claim 6 , wherein the at least one spring biasing mechanism is selected from the group consisting of a tolerance ring, a wave spring, an O-ring, a segmented O-ring, a spring energized O-ring, a C-shaped spring, and a leaf spring.

9. The rotor structure of claim 1 , further comprising a multi-nut-retaining arrangement, wherein the multi-nut-retaining arrangement comprises at least two retaining nuts having a different diameter with respect to one another, the different diameter of the at least two retaining nuts effective for configuring a radially-outward perimeter having a multi-step configuration in a respective rotor shaft of the two rotor shafts.

10. The rotor structure of claim 9 , wherein the multi-step configuration at the radially-outward perimeter of the respective rotor shaft defines a number of axially-extending segments in the respective rotor shaft, each of the axially-extending segments having a different diameter with respect to one another.

11. A centrifugal compressor comprising the rotor structure of claim 1 .

12. A method for arranging a rotor structure of a compressor,
wherein the rotor structure comprises a tie bolt and two rotor shafts respectively affixed to respective ends of the tie bolt, and a plurality of impeller bodies supported by the tie bolt, the plurality of impeller bodies mechanically coupled to one another along a rotor axis by way of a plurality of hirth couplings,
wherein the method comprises:
arranging a first impeller body of the plurality of impeller bodies to provide a first stage of compression,
arranging each subsequent impeller body to provide a subsequent stage of compression,
wherein each respective impeller body defines a respective Di/D2 ratio,
wherein the Di/D2 ratio of at least one of the impeller bodies is different than the Di/D2 ratio for the remaining impeller bodies,
wherein, based on the different Di/D2 ratio, respective surfaces defined by an inlet of said at least one of the impeller bodies is located at a different distance relative to the rotor axis compared to location of surfaces defined by respective inlets of the remaining impeller bodies,
wherein Di is indicative of a respective inner diameter of a flow path into an inlet of a respective impeller body, and
wherein D2 is indicative of respective outer diameter of the respective impeller body.

13. The method of claim 12 , further comprising a variation of the rotor structure along the rotor axis based on a variation of respective Di/D2 ratios, wherein the variation of the rotor structure along the rotor axis comprises locating the respective surfaces defined by the respective inlets of the at least one of the impeller bodies at a varying distance relative to the rotor axis.

14. The method of claim 13 , wherein the locating of the respective surfaces defined by the respective inlets of the one or more impeller bodies is arranged to reduce inlet Mach Number in the compression stages by the one or more impeller bodies and adjust rotor stiffness along the rotor axis.

15. The method of claim 12 , wherein a respective range of Di/D2 is from a value 0.2 to a value of 0.65.

16. The method of claim 15 , wherein a respective range of Di/D2 is from a value of 0.25 to a value of 0.50.

Assignees

• Siemens Energy Global Gmbh & Co Kg

Inventors

• Kuzdzal Mark J
• Peer David J
• Meyer Marcus
• Huth Sebastian
• Sorokes James M
• Miny Kevin
• Reimann Martin
• Mensing Roman
• Pacheco Jesus
• Nove Steven

Classifications

• F04D17/12 Primary

  Multi-stage pumps · CPC title

• F04D29/053

  Shafts · CPC title

• F04D29/054

  Arrangements for joining or assembling shafts · CPC title

• F04D29/286

  multi-stage rotors · CPC title

• F04D29/624

  especially adapted for elastic fluid pumps · CPC title