Compressor rotor structure

Patent metadata

Field	Value
Publication number	US-2023125483-A1
Application number	US-202017997830-A
Country	US
Kind code	A1
Filing date	May 14, 2020
Priority date	May 14, 2020
Publication date	Apr 27, 2023
Grant date	—

Abstract

Compressor rotor structure for turbomachinery, such as a compressor, is provided. Disclosed embodiments can benefit from sealing sleeves that may be arranged to inhibit passage onto respective hirth couplings of process fluid being processed by the compressor. The sealing sleeves may be affixed to adjoining structures (e.g., adjoining impeller bodies) by way of a slip fit connection to one of the adjoining structures and an interference fit connection with respect to the other adjoining structure, which is conducive to a user-friendly assembly of the sealing sleeves with the adjoining structures.

First claim

What is claimed is:

1 .- 17 . (canceled)

18 . A rotor structure for a compressor, the rotor structure comprising:
a tie bolt and two rotor shafts extending along a rotor axis, the two rotor shafts respectively affixed to the tie bolt; a plurality of impeller bodies disposed between the two rotor shafts, the plurality of impeller bodies supported by the tie bolt; a plurality of hirth couplings arranged to mechanically couple the plurality of impeller bodies to one another along the rotor axis; a respective sealing sleeve affixed onto respective radially outward surfaces of any two adjoining impeller bodies of the plurality of impeller bodies, the respective sealing sleeve arranged to span a circumferentially extending junction between the two adjoining impeller bodies to inhibit passage onto the respective hirth coupling of process fluid being processed by the compressor, wherein the sealing sleeve is affixed to a respective one of the two adjoining impeller bodies by way of an interference fit, wherein the sealing sleeve is affixed to the other one of the two adjoining impeller bodies by way of a slip fit; and a circumferentially-extending groove in a first of the radially outward surfaces, and a seal member positioned in the groove to form a seal between the first of the radially outward surfaces and the sealing sleeve.

19 . The rotor structure of claim 18 , wherein the seal member is an O-ring.

20 . The rotor structure of claim 18 , where the respective sealing sleeve is configured about the rotor axis with a cylindrical cross-section.

21 . The rotor structure of claim 18 , comprising a further sealing sleeve affixed onto respective radially outward surfaces of a respective rotor shaft of the two rotor shafts and a respective impeller body of the plurality of impeller bodies in abutting relationship with the respective rotor shaft, the abutting impeller body mechanically coupled by a further hirth coupling of the plurality of hirth couplings to the respective rotor shaft, the further sealing sleeve arranged to span a circumferentially extending junction between the abutting impeller body and the respective rotor shaft to inhibit passage onto the further hirth coupling of process fluid being processed by the compressor.

22 . The rotor structure of claim 21 , wherein the further sealing sleeve is affixed to one of the respective rotor shafts and the abutting impeller body by way of an interference fit.

23 . The rotor structure of claim 22 , wherein the further sealing sleeve is affixed to the other one of the respective rotor shafts and the abutting impeller body by way of a slip fit.

24 . The rotor structure of claim 21 , where the respective further sealing sleeve is configured about the rotor axis with a cylindrical cross-section.

25 . The rotor structure of claim 21 , further comprising a circumferentially-extending groove in a first of the radially outward surfaces, and a seal member positioned in the groove to form a seal between the first of the radially outward surfaces and the further sealing sleeve.

26 . The rotor structure of claim 25 , wherein the seal member is an O-ring.

27 . The rotor structure of claim 18 , wherein the respective sealing sleeve is arranged to span 360 degrees the circumferentially extending junction between the two adjoining impeller bodies.

28 . The rotor structure of claim 21 , wherein the respective further sealing sleeve is arranged to span 360 degrees the circumferentially extending junction between impeller body and the respective rotor shaft.

29 . The rotor structure of claim 18 , wherein the respective radially outward surfaces of the two adjoining impeller bodies are adjoining surfaces.

30 . The rotor structure of claim 21 , wherein the respective radially outward surfaces of the respective rotor shaft and the abutting impeller body are adjoining surfaces.

31 . The rotor structure of claim 18 , wherein the compressor is a centrifugal compressor.

32 . A rotor structure for a compressor, the rotor structure comprising:
a tie bolt and two rotor shafts extending along a rotor axis, the two rotor shafts respectively affixed to the tie bolt; a plurality of impeller bodies disposed between the two rotor shafts, the plurality of impeller bodies supported by the tie bolt; a plurality of hirth couplings arranged to mechanically couple the plurality of impeller bodies to one another along the rotor axis; a respective sealing sleeve affixed onto respective radially outward surfaces of any two adjoining impeller bodies of the plurality of impeller bodies, the respective sealing sleeve arranged to span a circumferentially extending junction between the two adjoining impeller bodies to inhibit passage onto the respective hirth coupling of process fluid being processed by the compressor; and a further sealing sleeve affixed onto respective radially outward surfaces of a respective rotor shaft of the two rotor shafts and a respective impeller body of the plurality of impeller bodies in abutting relationship with the respective rotor shaft, the abutting impeller body mechanically coupled by a further birth coupling of the plurality of hirth couplings to the respective rotor shaft, the further sealing sleeve arranged to span a circumferentially extending junction between the abutting impeller body and the respective rotor shaft to inhibit passage onto the further hirth coupling of process fluid being processed by the compressor.

33 . The rotor structure of claim 32 , wherein the further sealing sleeve is affixed to one of the respective rotor shafts and the abutting impeller body by way of an interference fit.

34 . The rotor structure of claim 33 , wherein the further sealing sleeve is affixed to the other one of the respective rotor shafts and the abutting impeller body by way of a slip fit.

35 . The rotor structure of claim 32 , where the respective further sealing sleeve is configured about the rotor axis with a cylindrical cross-section.

36 . The rotor structure of claim 32 , further comprising a circumferentially-extending groove in a first of the radially outward surfaces, and a seal member positioned in the groove to form a seal between the first of the radially outward surfaces and the further sealing sleeve.

37 . The rotor structure of claim 36 , wherein the seal member is an O-ring arranged to span 360 degrees the circumferentially extending junction between the impeller body and the respective rotor shaft.

Assignees

• Siemens Energy Global Gmbh & Co Kg

Inventors

• Reimann Martin
• Peer David J
• Meyer Marcus
• Huth Sebastian
• Miny Kevin

Classifications

• F04D17/122 Primary

  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

• F04D29/102

  especially adapted for elastic fluid pumps · CPC title

• F05D2260/31

  Retaining bolts or nuts · CPC title

• F04D29/286

  multi-stage rotors · CPC title

• F04D29/266

  mounting compressor rotors on shafts · CPC title