Multi-stage centrifugal compressor

Abstract

A multi-stage centrifugal compressor comprising a shaft (2) having a plurality of blades (3), the shaft (2) being mounted to a housing (4) by bearings (7), at least one bearing (7) comprising a bearing damper element (10) consisting of a ring (11) arranged between the shaft (2) and the bearing (7), the ring (11) comprising a slot (12) passing through the thickness of the ring (11) in the axial direction (X-X') and spaced apart from the radial inner and outer surfaces (13a, 13b) of the ring (11), the slot (12) at least partially overlapping, and (A) the slots (12) are filled with a liquid and the axial annular surfaces (16) of the rings (11) are closed by protective caps (17), or (B) at least one of the axial annular surfaces (16) comprises a viscoelastic material (20) or a hysteresis damping material (20) sandwiched between two concentric disks (21), the disks (21) being attached to the rings (11), or (C) the slots (12) are filled with a viscoelastic material.

Description

[Technical field]

[0001] The present invention relates to a multi-stage centrifugal compressor. [Background technology]

[0002] In such compressors it is known that a number of blades forming the different stages of the compressor are mounted on a shaft which is supported in bearings in the housing.

[0003] Typically, roller bearings are used in these machines since the typical rotational speeds of 50 Hz or 60 Hz are not very high.

[0004] The maximum number of blades on a shaft, i.e. the maximum number of stages, and the maximum speed at which the blades can rotate are determined by the rotor dynamics. More specifically, the first critical lateral speed is the absolute upper limit on the rotational speed.

[0005] If the mass is too large or the shaft is too long, resonance problems will occur and the resulting vibrations may approach a natural frequency that cannot be exceeded. This problem occurs mainly with rolling bearings and less with plain or hydrodynamic bearings. The main reason for this limitation is the exceeding of the critical speed due to lack of sufficient damping.

[0006] These resulting dynamic or resonance problems therefore impose limitations on the speed and possible number of blades, i.e. stages.

[0007] The maximum number of stages in known multi-stage centrifugal compressors is limited to certain variables depending on the power variant.

[0008] To solve the resonance problem, thin film dampers or so-called "squeeze film dampers" are already known.

[0009] This utilizes the damping effect of a liquid (usually oil) in a thin gap.

[0010] Such a thin film damper is known, for example, from WO 2019 / 002959.

[0011] Such known dampers have the disadvantage that an oil supply to the membrane damper is required.

[0012] That is, to realize this oil supply, it is necessary to provide an oil circuit, an oil reservoir, and an oil pump.

[0013] Since known multi-stage centrifugal compressors with roller bearings in most cases do not have oil pumps or the like and, after all, the bearings are generally lubricated according to the principle of grease lubrication or "splash oil lubrication", the use of such dampers means additional costs and a bulkier and more complex machine.

[0014] Therefore, such dampers are not used in known multi-stage centrifugal compressors, which as a result are limited in terms of speed and number of stages. [Prior art documents] [Patent documents]

[0015] [Patent Document 1] International Publication No. 2019 / 002959 Summary of the Invention [Problem to be solved by the invention]

[0016] The present invention aims to provide a solution to at least one of the above and other disadvantages. [Means for solving the problem]

[0017] To this end, the invention provides a multi-stage centrifugal compressor comprising a shaft having a plurality of blades thereon, the shaft being mounted in a housing by bearings, at least one of the bearings comprising a bearing damper element consisting of a ring arranged between the shaft or the housing and the bearing, the ring comprising a slot passing axially through the thickness of the ring and spaced apart from the radial inner and outer surfaces of the ring, the slots at least partially overlapping, (A) The slot is filled with liquid and the axial annular face of the ring is closed by a protective cap; Or, (B) at least one of both axial annular surfaces of the ring comprises a viscoelastic or hysteretic damping material sandwiched between two concentric disks, the disks being attached to the ring; or (C) The slot is filled with a viscoelastic material. Characterized in that

[0018] This slot configuration forms a radial spring mechanism. The spring constant of this mechanism determines the critical speed region, which is selected somewhere in the rotational speed range of the machine. To exceed the critical speed while still limiting dynamic amplification, i.e. vibration, damping is added to this elastic element by one of options (A), (B) or (C) above.

[0019] By "overlapping" it is meant that a line originating from the midpoint or center of the ring and passing through the ring will intersect each of the slots.

[0020] By "slot" it is meant slots, slits, cuts, etc., and it is important that these slots extend axially through the entire thickness of the ring.

[0021] The advantage of this is that it creates a bearing damper element that does not require liquid to be pumped into the slots and therefore does not require an associated liquid circuit, liquid pump or liquid reservoir.

[0022] Therefore, the bearing damper element can be easily applied to a multi-stage centrifugal compressor.

[0023] By applying bearing damper elements, resonance problems can be avoided and the machine can be rotated faster and / or additional stages can be provided by placing additional blades on the shaft.

[0024] In option (A), there is liquid in the slot, but the protective cap keeps the liquid in the slot so that this liquid does not need to be continually replenished.

[0025] Here, it is not excluded that a liquid-filled space exists between the protective cap and the axial annular surface of the ring.

[0026] The protective cap can be designed in various ways and is preferably made from an elastomer, such as rubber.

[0027] For example, the protective cap can be a 3D printed structure with some flexibility, or it can be a thin-walled protective cap with a harmonica structure.

[0028] It will be apparent, however, that many different variations are possible.

[0029] In option (B), a viscoelastic material, for example rubber, or a hysteretic damping material, for example metal gauze, is placed in juxtaposition with the ring, such as by two concentric discs.

[0030] Also in this case, the concentric disks can be embodied in various ways, but in the simplest embodiment they are two flat planar disks which can be fixed to a ring, for example by screws or bolts.

[0031] This allows the ring to have concentric disks on one or both axial annular faces with a viscoelastic or hysteretic damping material sandwiched therebetween.

[0032] The viscoelastic material may be, for example, an O-ring, and the hysteretic damping material may be, for example, a wire metal mesh.

[0033] In this case, it is important to note that usually no liquid is needed if the damping is sufficient, but it can still be combined with the presence of liquid in small gaps to increase damping. Thus, oil damping is combined with rubber seals.

[0034] Also, in option (C) there is no liquid present.The viscoelastic material provided in the slot is preferably rubber which is attached to the slot by vulcanization.

[0035] Preferably, the slot is completely filled with the viscoelastic material.

[0036] In order to better explain the characteristics of the present invention, some preferred embodiments of a multi-stage centrifugal compressor according to the invention will now be described, by way of non-limiting examples, with reference to the accompanying drawings, in which: [Brief description of the drawings]

[0037] [Figure 1] 1 illustrates diagrammatically a multi-stage centrifugal compressor according to the invention; [Diagram 2] 1 shows a practical embodiment of the portion indicated by F2 in FIG. [Diagram 3] 3 shows a practical embodiment of the ring of the bearing damper element of FIG. 2; [Figure 4] 3 shows the bearing damper element of FIG. 2 in more detail. [Diagram 5] A modification of FIG. 4 is shown. [Figure 6] A modification of FIG. 4 is shown. DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS

[0038] In FIG. 1 a multi-stage centrifugal compressor 1 according to the invention is shown diagrammatically.

[0039] It basically comprises a shaft 2 having a number of blades 3 thereon, the shaft 2 being rotatably mounted within a housing 4 .

[0040] In this case, there are eight blades 3, but it is not excluded that there are more than eight or even more than ten blades 3.

[0041] As is known, the housing 2 has an inlet opening 5 and an outlet opening 6 .

[0042] The shaft 2 is supported on both sides by bearings 7 .

[0043] In this case, the bearing 7 is a rolling bearing 7, specifically a double row deep groove ball bearing.

[0044] One end 8 of the shaft 2 is the drive end 8, i.e. to which a drive, for example in the form of a motor, is coupled so as to be able to rotate the shaft 2. The drive is not shown in the figures.

[0045] The other end 9 of the shaft 2 is a non-drive end 8 .

[0046] According to the invention, at least one bearing 7 is equipped with a bearing damper element 10 .

[0047] In this case, although this is not essential to the invention, the bearing 7 is provided with a bearing damper element 10 only at one end 9 of the shaft 2 .

[0048] In this case, this concerns the non-drive end 9 of the shaft 2 .

[0049] This has the advantage that maintenance of the bearing damper element 10 is easier.

[0050] Of course, it is not excluded that the bearing 7 is provided with bearing damper elements 10 at both ends 8 , 9 of the shaft 2 .

[0051] FIG. 2 shows each bearing 7 with a bearing damper element 10 at the non-drive end 9 of the shaft.

[0052] According to the invention, the bearing damper element 10 consists of a ring 11 arranged between the housing 4 and the respective bearing 7. Of course, it is not excluded that the bearing damper element 10 is also arranged between the shaft 2 and the bearing 7.

[0053] This ring 11 is shown in detail in FIG.

[0054] The ring 11 is provided with a plurality of slots 12 which extend through the thickness of the ring 11 in an axial direction XX' and are spaced apart from the radial inner and outer surfaces 13a, 13b of the ring 11.

[0055] There are preferably at least three slots 12, with at least half of the slots 12 having one or more attenuating portions 14a having a maximum width of 0.5 mm, preferably a maximum of 0.2 mm, more preferably a maximum of 1.15 mm.

[0056] The attenuating portions 14a are preferably concentric and non-overlapping.

[0057] These attenuating portions 14a preferably surround at least 80%, more preferably at least 90%, of the center or midpoint 15 of the ring.

[0058] In addition to the damping portion 14a, preferably at least one slot 12 has one or more spring portions 14b, preferably having a minimum width greater than at least 0.5 millimeters.

[0059] Spring portion 14b preferably has a width that is at least twice, and more preferably at least three times, the width of damping portion 14a.

[0060] According to the present invention, the slots 12 are at least partially overlapping.

[0061] As stated above, "slots overlap" means that a line originating from the midpoint or center of ring 11 and passing through ring 11 intersects each of slots 8.

[0062] By "at least partially" it is meant that the slots 12 overlap for at least a portion of their length, but not necessarily their entire length.

[0063] Preferably, the spring portion 14b of the slot 12 at least partially overlaps the damping portion 14a.

[0064] Also, preferably, damping portion 14a is further from the center or midpoint 15 of ring 11 than spring portion 14b.

[0065] Alternative embodiments of the ring 11 can also comprise slots 12 with only damping portions 14a or with only spring portions 14b. The embodiment with only damping portions 14a is preferably applied in option (A) above, as explained below, thereby creating a "squeeze film" effect. In the case of options (B) and (C) above, such thin damping portions 14a are of little use, since the damping is realized parallel to the slots 12. In this case, preferably an embodiment will be used in which the slots 12 only have spring portions 14b, which have mainly an elastic effect.

[0066] The narrow or thin attenuating portion 14a is preferably fabricated using a wire electrical discharge process such as "EDM" or "electrical discharge machining".

[0067] The wider spring portion 14b can be made using a water jet or milling process.

[0068] For the further implementation of the bearing damper element 10 there are several options according to the invention, which are illustrated in FIGS.

[0069] As shown in Figure 4, a first option (A) according to the invention relates to an embodiment in which the slot 12 is filled with a liquid. This liquid is viscous, for example, but not necessarily, an oil.

[0070] The axial annular face 16 of the ring 11 is closed by a protective cap 17 .

[0071] In the example shown, the protective cap 17 is made from an elastomer, for example rubber.

[0072] A protective cap 17 is secured to the axial annular surface 16 of the ring 11 by bolts or screws 18 .

[0073] Of course, other fastening methods are possible, provided they do not interfere with the elastic action and therefore with the damping.

[0074] A space 19 exists between the protective cap 17 and the axial annular surface 16 of the liquid-filled ring.

[0075] Alternatively, the protective cap 17 can be a 3D printed structure that has some flexibility.

[0076] This means that the protective cap 17 is flexible or deformable due to its construction.

[0077] 3D printing is known to enable complex structures and shapes, and can create structures with the necessary flexibility.

[0078] For example, the protective cap 17 can be a thin-walled protective cap 17 having a harmonica structure, which is flexible and deformable, as is well known.

[0079] A second option (B) according to the invention relates to an embodiment in which at least one of the two axial annular faces 16 of the ring 11 comprises a viscoelastic or hysteretic damping material 20 sandwiched between, for example, two concentric discs 21, the discs 21 being attached to the ring 11, as shown in Figures 5 and 6.

[0080] The disk 21, as well as the protective cap 17, may be secured by bolts or screws 18 or in other manner.

[0081] The disk 21 can be embodied in many different forms.

[0082] 5 and 6, the radially inner or outer surface 22 is slightly contoured to accommodate the viscoelastic or hysteresis damping material 20. In FIG.

[0083] In the case of option (B), there is no need for liquid to be present in the slot 12 .

[0084] The viscoelastic material 20 may be an O-ring 23 as shown in FIG. 5, while the hysteresis damping material 20 may be a wire screen 24 (or "wire metal mesh") as shown in FIG.

[0085] In Figures 5 and 6, the concentric disks 21 with the viscoelastic or hysteresis damping material 20 are attached to only one side of the ring 11, but it is not excluded to provide the viscoelastic or hysteresis damping material 20 on both axial annular surfaces 16 of the ring 11.

[0086] A third option (C), not shown, relates to an embodiment in which the slot 12 is filled with a viscoelastic material.

[0087] The viscoelastic material, for example rubber, is attached to the slot 12 by vulcanization.

[0088] The slot 12 only has a spring portion 14b.

[0089] The advantage of such an embodiment is that there is no need to attach a protective cap 17 or a concentric disk 21 to the ring 11 .

[0090] The operation of the multi-stage centrifugal compressor 1 is very simple and is as follows.

[0091] During operation of the centrifugal compressor 1, the shaft 2 is rotated by a drive, as a result of which the blades 3 draw in air through the inlet opening 5, which is compressed in a series of stages before leaving the centrifugal compressor 1 through the outlet opening 6.

[0092] During operation, vibrations will be generated which need to be damped to avoid resonance problems.

[0093] The bearing damper element 10 will damp these vibrations.

[0094] In the situation of FIG. 4, the liquid in the slot 12 creates a thin film damper, which provides the damping.

[0095] The protective cap 17 holds the liquid in the slot 12 so that it cannot escape, and since it is made of an elastomer, it will move with the ring 11 as it deforms under the action of vibration.

[0096] In option (B), as shown in Figures 5 and 6, the viscoelastic or hysteretic damping material 20 deforms to dampen the vibrations, and the ring 11 provides some flexibility as described above.

[0097] In option (C), the thicker spring portion 14b is vulcanized and the viscoelastic material in the slot 12 has the same function as the liquid in the slot 12 in the embodiment of FIG.

[0098] Due to the damping of vibrations by the bearing damper element 10, resonance problems will be avoided. This allows the centrifugal compressor 1 to rotate at higher speeds and / or add more stages.

[0099] The invention is not limited to the embodiment described by way of example and shown in the drawings, and the multi-stage centrifugal compressor according to the invention can be realized in various forms and dimensions without departing from the scope of the invention.

Claims

1. A multi-stage centrifugal compressor comprising a shaft (2) having a plurality of blades (3) thereon, the shaft (2) being attached to a housing (4) by bearings (7), at least one of said bearings (7) comprises a bearing damper element (10) consisting of a ring (11) arranged between said shaft (2) or said housing (4) and said bearing (7), said ring (11) comprising a slot (12) passing through the thickness of said ring (11) in the axial direction (X-X') and spaced apart from the radial inner and outer surfaces (13a, 13b) of said ring (11), said slots (12) being at least partially overlapping; (A) both axial annular surfaces (16) of said ring (11) are provided with a viscoelastic material (20) comprising an O-ring or a hysteretic damping material (20) comprising a wire mesh (24) sandwiched between two concentric disks (21), said two concentric disks (21) being attached to said ring (11); and (B) the slot (12) is filled with a viscoelastic material; A multi-stage centrifugal compressor comprising:

2. 2. The multi-stage centrifugal compressor of claim 1, wherein said slots (12) are filled with liquid.

3. 2. A multi-stage centrifugal compressor according to claim 1, wherein said viscoelastic material is rubber which is installed in said slots (12) by vulcanization.

4. 4. A multi-stage centrifugal compressor according to claim 1, wherein the bearing (7) is a rolling bearing (7).

5. 5. A multi-stage centrifugal compressor according to claim 1, wherein the bearing or bearings (7) are provided only at one end (8, 9) of the shaft (2) which has the bearing damper element (10).

6. 6. A multi-stage centrifugal compressor according to claim 5, wherein the bearing damper element (10) is arranged at the non-drive end (9) of the shaft (2).

7. A multi-stage centrifugal compressor according to any one of claims 1 to 6, wherein said ring (11) comprises at least three slots (12).

8. A multi-stage centrifugal compressor according to any one of claims 1 to 7, wherein the slot (12) has a decay portion (14a) with a maximum width of 0.5 mm, preferably with a maximum width of 0.2 mm, more preferably with a maximum width of 1.15 mm.

9. 9. A multi-stage centrifugal compressor according to any one of claims 1 to 8, wherein the slot (12) has a spring portion (14b) with a minimum width of 0.5 millimeters.

10. A multi-stage centrifugal compressor according to any one of claims 1 to 9, wherein there are more than ten blades (3) on the shaft (2).

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