Rotor structure and methodology for assembly or disassembly of such rotor structure

Patent metadata

Field	Value
Publication number	US-12435727-B2
Application number	US-202218840953-A
Country	US
Kind code	B2
Filing date	Apr 15, 2022
Priority date	Apr 15, 2022
Publication date	Oct 7, 2025
Grant date	Oct 7, 2025

Abstract

Turbomachine and method for assembling/disassembling a rotor structure of the turbomachine are disclosed. A plurality of impeller bodies is supported on a tie bolt. Threadingly connecting a first coupling nut with the tie bolt to axially press the impeller bodies to define a compression section. The first coupling nut is arranged to apply a first coupling force within the compression section to hold the compression section attached during rotating operation of the turbomachine. Threadingly connecting a second coupling nut with the tie bolt to axially press a rotor shaft portion onto the compression section. The second coupling nut is arranged to apply a second coupling force to the rotor shaft portion to hold the rotor shaft portion affixed onto the compression section during a non-rotating condition of the turbomachine. The foregoing multi-nut coupling arrangement in a cost-effective and reliable manner provides user-friendly flexibility for assembly/disassembly of the rotor structure while maintaining a mechanically robust rotor structure.

First claim

What is claimed is:

1. A method for assembling and disassembling a rotor structure in a turbomachine, the method comprising:
supporting a plurality of impeller bodies on a tie bolt;
threadingly connecting a first coupling nut with the tie bolt to axially press the plurality of impeller bodies to define a compression section of the turbomachine, wherein the threadingly connecting of the first coupling nut is arranged to apply a first coupling force within the compression section to hold the compression section of the turbomachine attached during rotating operation of the turbomachine;
positioning a rotor shaft portion adjacent the compression section;
threadingly connecting a second coupling nut with the tie bolt to axially press the rotor shaft portion onto the compression section, wherein the threadingly connecting of the second coupling nut on the tie rod is arranged to apply a second coupling force to the rotor shaft portion to hold the rotor shaft portion affixed onto the compression section during a non-rotating condition of the turbomachine;
after threadingly connecting the second coupling nut on the tie bolt, assembling at least one component of the turbomachine about the rotor shaft portion, wherein the assembling is carried out without unloading the first coupling force within the compression section; and
disposing an O-ring in a circumferentially-extending groove in a rotor shaft end, the O-ring positioned to circumferentially abut against a head of the second coupling nut.

2. The method of claim 1 , threadably connecting a third coupling nut with the tie rod to axially press the rotor shaft end onto the rotor shaft portion, wherein the threadingly connecting of the third coupling nut on the tie rod is arranged to apply a third coupling force on the rotor shaft end to hold the rotor shaft end and the rotor shaft portion affixed to the compressor section during the rotating operation of the turbomachine, after the assembling of the at least one component of the turbomachine.

3. The method of claim 2 , further comprising threadingly disconnecting the third coupling nut to axially separate the rotor shaft end from the rotor shaft portion.

4. The method of claim 3 , further comprising carrying out disassembly from the rotor shaft portion of the least one component of the turbomachine without unloading the first coupling force within the compression section.

5. The method of claim 1 , wherein the first coupling force is larger than the second coupling force.

6. The method of claim 5 , wherein the O-ring frictionally engages the second coupling nut to hold the second coupling nut in place.

7. The method of claim 1 , wherein the turbomachine is a centrifugal compressor.

8. The method of claim 5 ,
wherein the at least one component of the turbomachine being assembled about the rotor shaft portion comprises at least one of a seal arrangement and a bearing arrangement.

9. A turbomachine comprising:
a tie bolt;
a plurality of impeller bodies stacked adjacent one another on the tie bolt;
a first coupling nut threadingly connected with the tie bolt to axially press the plurality of impeller bodies to define a compression section of the turbomachine, wherein the first coupling nut is arranged to apply a first coupling force within the compression section to hold the compression section of the turbomachine affixed during rotating operation of the turbomachine;
a rotor shaft portion adjacent the compression section;
a second coupling nut threadingly connected with the tie bolt to axially press the rotor shaft portion onto the compression section, wherein the second coupling nut is arranged to apply a second coupling force to the rotor shaft portion, wherein the second coupling force is smaller than the first coupling force to hold the rotor shaft portion affixed onto the compression section during a non-rotating condition of the turbomachine;
at least one component of the turbomachine being assembled about the rotor shaft portion during the non-rotating condition of the turbomachine without unloading the first coupling force within the compression section,
a rotor shaft end adjacent the rotor shaft portion;
a third coupling nut threadingly connected with the tie bolt to apply a third coupling force on the rotor shaft end to hold the rotor shaft end and the rotor shaft portion affixed to the compression section during rotating operation of the turbomachine; and
an O-ring disposed in a circumferentially-extending groove in the rotor shaft end, the O-ring positioned to circumferentially abut against a head of the second coupling nut, wherein the O-ring is arranged to frictionally engage the second coupling nut and hold the second coupling nut in place.

10. The turbomachine of claim 9 , further comprising a radially-extending coupling flange integrally constructed to form one-piece with the rotor shaft end.

11. The turbomachine of claim 9 , further comprising
a radially-extending coupling flange located adjacent a first axial edge of the rotor shaft end, and further comprising a thrust disc located adjacent a second axial edge of the rotor shaft end, the radially-extending coupling flange and the thrust disc integrally constructed to form one-piece with the rotor shaft end.

12. The turbomachine of claim 9 ,
wherein the at least one component of the turbomachine assembled about the rotor shaft portion comprises at least one of a seal arrangement and a bearing arrangement.

13. The turbomachine of claim 9 , further comprising a Hirth joint to axially couple the rotor shaft portion and the rotor shaft end.

14. A turbomachine comprising:
a tie bolt;
a plurality of impeller bodies stacked adjacent one another on the tie bolt;
a first coupling nut threadingly connected with the tie bolt to axially press the plurality of impeller bodies to define a compression section of the turbomachine, wherein the first coupling nut is arranged to apply a first coupling force within the compression section to hold the compression section of the turbomachine affixed during rotating operation of the turbomachine;
a rotor shaft portion adjacent the compression section;
a second coupling nut threadingly connected with the tie bolt to axially press the rotor shaft portion onto the compression section, wherein the second coupling nut is arranged to apply a second coupling force to the rotor shaft portion, wherein the second coupling force is smaller than the first coupling force to hold the rotor shaft portion affixed onto the compression section during a non-rotating condition of the turbomachine; and
a dowel pin positioned to engage the second coupling nut and hold the second coupling nut in place.

15. A turbomachine comprising:
a tie bolt;
a plurality of impeller bodies stacked adjacent one another on the tie bolt;
a first coupling nut threadingly connected with the tie bolt to axially press the plurality of impeller bodies to define a compression section of the turbomachine, wherein the first coupling nut is arranged to apply a first coupling force within the compression section to hold the compression section of the compression affixed during rotating operation of the turbomachine;
a rotor shaft portion adjacent the compression section;
a second coupling nut threadingly connected with the tie bolt to axially press the rotor shaft portion onto the compression section, wherein the second coupling nut is arranged to apply a second coupling force to the rotor shaft portion, wherein the second coupling force is smaller than the first coupling force to hold the rotor shaft portion affixed onto the compression section during a

Assignees

• Siemens Energy Global Gmbh & Co Kg

Inventors

• Miny Kevin

Classifications

• F04D29/624

  especially adapted for elastic fluid pumps · CPC title

• F04D17/10

  for compressing or evacuating · CPC title

• F01D5/066

  Connecting means for joining rotor-discs or rotor-elements together, e.g. by a central bolt, by clamps · CPC title

• F04D17/122

  the individual rotor discs being, one for each stage, on a common shaft and axially spaced, e.g. conventional centrifugal multi- stage compressors · CPC title

• F04D29/054 Primary

  Arrangements for joining or assembling shafts · CPC title