WO2010124350A1 - Device for taking up an axial force exercised on a shaft of a machine and centrifugal compressor provided with such device - Google Patents

Device for taking up an axial force exercised on a shaft of a machine and centrifugal compressor provided with such device Download PDF

Info

Publication number
WO2010124350A1
WO2010124350A1 PCT/BE2010/000035 BE2010000035W WO2010124350A1 WO 2010124350 A1 WO2010124350 A1 WO 2010124350A1 BE 2010000035 W BE2010000035 W BE 2010000035W WO 2010124350 A1 WO2010124350 A1 WO 2010124350A1
Authority
WO
WIPO (PCT)
Prior art keywords
bearing
shaft
aforesaid
axial force
axial
Prior art date
Application number
PCT/BE2010/000035
Other languages
French (fr)
Inventor
Erik Paul Fabry
Original Assignee
Atlas Copco Airpower
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Atlas Copco Airpower filed Critical Atlas Copco Airpower
Publication of WO2010124350A1 publication Critical patent/WO2010124350A1/en

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16CSHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C32/00Bearings not otherwise provided for
    • F16C32/04Bearings not otherwise provided for using magnetic or electric supporting means
    • F16C32/0406Magnetic bearings
    • F16C32/044Active magnetic bearings
    • F16C32/0474Active magnetic bearings for rotary movement
    • F16C32/0489Active magnetic bearings for rotary movement with active support of five degrees of freedom, e.g. two radial magnetic bearings combined with an axial bearing
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00Details, component parts, or accessories
    • F04D29/05Shafts or bearings, or assemblies thereof, specially adapted for elastic fluid pumps
    • F04D29/051Axial thrust balancing
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00Details, component parts, or accessories
    • F04D29/05Shafts or bearings, or assemblies thereof, specially adapted for elastic fluid pumps
    • F04D29/056Bearings
    • F04D29/058Bearings magnetic; electromagnetic
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16CSHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C39/00Relieving load on bearings
    • F16C39/06Relieving load on bearings using magnetic means
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16CSHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C2360/00Engines or pumps
    • F16C2360/42Pumps with cylinders or pistons

Definitions

  • Device for taking up an axial force exercised on a shaft of a machine and centrifugal compressor provided with such device .
  • the present invention concerns a device for absorbing an axial force exerted on a machine shaft supported on radial bearings, such as the shaft of a compressor, a motor, a turbine or the like.
  • the invention concerns a device for absorbing an axial force exerted on a machine shaft .
  • the shaft is supported on radial bearings by means of two radial bearings provided at a certain distance from one another to ensure a good stability for the shaft and any rotor possibly provided upon the latter.
  • the shaft is axially loaded with a force whose magnitude varies in time and which may also change direction.
  • a large speed of rotation of the shaft causes a large centrifugal force on the shaft and the radial bearings in case " of the slightest imbalance, making it necessary to balance the shaft before the machine is put into use. Even when the shaft is balanced, some imbalance still remains to a certain extent, as a result of which the shaft is excited by the centrifugal force while rotating.
  • the centrifugal force will excite the shaft with a frequency which, as is known, coincides with the first characteristic frequency of the shaft, resulting in resonance of the shaft.
  • the first characteristic frequency of this shaft concerns a bending frequency, whereby the length of the shaft is the most decisive factor.
  • the first characteristic frequency of the shaft strongly decreases as the length of the shaft increases.
  • Heavy loaded machines which are conventionally supported on axial bearings in the above-described manner have the major disadvantage that the first characteristic frequency of the shaft of such a machine, and consequently the critical rotational speed of the shaft, tend to be relatively low, as a result of which the useful rotational speed of the machine is restricted. If the machine is a compressor, this will result in an output of the compressor concerned having a low energy density.
  • the gas bearing is controlled by the measurement of force in a hydrodynamic tilting pad bearing, such that the forces in the hydrodynamic bearing are restricted by compensation in the gas bearing.
  • control hereby provides in a closed loop system with feedback in order to reduce the force to zero.
  • additional measures are thereby necessary, such as a low-pass filter, in order to guarantee a stable working under all circumstances.
  • the present invention aims to remedy one or several of the above-mentioned and/or other disadvantages by providing a device for absorbing an axial force exerted on a machine shaft, which shaft is provided with one or several rotors, and whereby this device comprises at least two axial bearings to support the aforesaid shaft, namely a first bearing and a second bearing, whereby the aforesaid first bearing is a primary bearing of the active magnet type which absorbs the major part of the aforesaid axial force and which is designed such that, for the mounting thereof, no mounting space on the shaft's length needs to be provided, whereby the aforesaid first bearing is controlled by means of a control unit and whereby the control unit is at least connected to a pressure sensor and comprises an algorithm to control the aforesaid first bearing on the basis of a measuring signal from the aforesaid pressure sensor.
  • the aforesaid first bearing is preferably not controlled on the basis of an axial position measurement of the machine's shaft.
  • An advantage hereby is that it is easier to control the first bearing than to control a conventional axial active bearing.
  • the shaft must not be extended to place the bearing, or to rephrase it, the first bearing is designed such that it has no influence whatsoever on the shaft length that is required for the working of the machine.
  • the aforesaid first bearing hereby works in one direction and absorbs more than 75% of the total axial force in that particular direction, preferably at least 85% of the total axial force, and even more preferably at least 95% of the total axial force.
  • the shaft can be made shorter than the shaft of an identical machine, supported in the conventional manner on axial bearings.
  • the most heavily loaded and consequently the most sizeable bearing is provided in the device in such a manner that this bearing has no influence whatsoever on the length of the shaft that is required for the working of the machine, as a result of which the length of the shaft can be restricted to an absolute minimum.
  • the aforesaid first bearing will not occupy any axial mounting space on the shaft while the device according to the invention is in use.
  • the reduced length of the shaft in the case of the invention offers several advantages.
  • the first characteristic frequency and the critical rotational speed of said shaft increase, as a result of which the maximally permitted rotational speed of the machine will be higher than in the case of a machine with conventional bearings.
  • Another advantage is that the shaft has less mass, which allows savings on material and transport costs.
  • the first bearing acts directly on a far end of the shaft or on a rotor which has been provided on the shaft or which is a part of it. What precedes implies that, for the good functioning of the first bearing, the shaft or rotor must not be provided with additional elements that are traditionally used, such as a thrust disc, shoulder or the like.
  • the pressure sensor may be provided nearby the impeller, and the magnetic bearing is controlled by the measuring signal from the pressure sensor.
  • Another advantage is that no consumption of compressed air occurs .
  • the second axial bearing is also of the active magnetic type, whereby the first bearing is controlled as a function of a machine variable, for example, in the case of a compressor, the outlet pressure.
  • a machine variable for example, in the case of a compressor, the outlet pressure.
  • the aforesaid machine variable that is used to this end is preferably a variable that varies little in time.
  • Another advantage is that a control on the basis of a simple open loop control system with a gain factor may be provided.
  • the present invention also concerns a centrifugal compressor provided with a shaft with one or several rotors and with a device for absorbing an axial force that is exerted on the aforesaid shaft, which device comprises at least two axial bearings supporting the aforesaid shaft, a first bearing and a second bearing respectively, whereby the aforesaid first bearing is a primary bearing of the active magnetic type which absorbs the major part of the aforesaid axial force and which is made such that it does not affect the required length of the shaft, or, in other words, no mounting space must be provided on the shaft length for this first bearing, whereby the aforesaid first bearing is controlled by means of a control unit and whereby the control unit is at least connected to a pressure sensor and comprises an algorithm to control the aforesaid first bearing on the basis of a measuring signal from the aforesaid pressure sensor.
  • figure 1 schematically shows a section of a centrifugal compressor provided with a conventional device for absorbing an axial force
  • figure 2 shows a variant of figure 1
  • figure 3 schematically shows a section as that in figure 1, but for a centrifugal compressor provided with a device according to the invention
  • figure 4 shows a variant of figure 3.
  • the figures represent the shaft 1 of a machine which is in this case made as a centrifugal compressor, whereby said shaft 1 is provided with a rotor 2 in the shape of an impeller on one far end.
  • the shaft 1 and rotor 2 are mounted in a rotating manner in a housing 3 of the compressor.
  • the shaft 1 is provided with two radial bearings 4.
  • the shaft 1 is driven by an electromotor, as represented in figure 1, whereby said electromotor is made as a high-speed permanent-magnet motor in the present example.
  • the shaft 1 in figure 1 is radially supported by two radial bearings 4, whereas the axial forces, introduced during working of the machine, are absorbed by two axial bearings ⁇ .
  • the axial as well as the radial bearings 6, 4 respectively, are in this case active magnetic bearings.
  • the aforesaid axial bearings 6 act on a shoulder 7 of the shaft 1, namely on the radially directed side flanges of a shaft part having a larger diameter than the rest of the shaft 1.
  • the two axial bearings 6 are represented in a configuration whereby these bearings 6 act on an axial thrust disc 8 which is fixed to the shaft 1 or which is part of it, and whereby these bearings 6 also make it necessary for the shaft 1 to have a certain length.
  • Figure 3 shows a device according to the invention, whereby two bearings are applied, namely a first bearing 9 which serves as a primary axial bearing and which is provided on a free end of the shaft 1, and a second bearing 10 in the shape of a secondary axial bearing which is in this case made as a double-acting bearing extending on either side of an axial thrust disc 8 on the shaft 1.
  • a first bearing 9 which serves as a primary axial bearing and which is provided on a free end of the shaft 1
  • a second bearing 10 in the shape of a secondary axial bearing which is in this case made as a double-acting bearing extending on either side of an axial thrust disc 8 on the shaft 1.
  • the bearings 9 and 10 which are represented in the figures are in this case of the active magnet type. According to the invention, it is not strictly necessary that the second bearing is of the active magnet type.
  • the shaft 1 is driven by the motor 5, whereby the rotor 2 at the far end of the shaft 1 rotates in the housing 3.
  • the sucked-in air is compressed in the known manner, after which the compressed air is discharged to a downstream application.
  • bearings of the active magnetic type are preferably used.
  • the working of an active magnetic bearing is known, and it uses amongst others an electromagnet, amplifiers and sensors to support the shaft 1 in a contactless way.
  • the shaft/rotor system 1, 2 is loaded with an axial force in the direction of arrow A.
  • This axial force mainly consists of a nominal, almost static component, caused by the pressure distribution on the rotor 2.
  • the first axial bearing 9 is dimensioned such that it can absorb this nominal, almost static axial force. Consequently, this first bearing 9 must be made relatively large and heavy.
  • the axial bearings 6 act on an axial thrust disc 8, on a shoulder 7 or on other elements which are provided on the shaft 1. It is clear that in such cases, the shaft 1 must be made sufficiently long so as to provide sufficient room for the axial bearings 6.
  • the first, primary bearing 9 is made such that it does not affect the required length of the shaft 1, as is illustrated for example by figure 3 in which the first bearing 9 acts directly on the free end of the shaft 1.
  • the first bearing 9 can be placed in the extension of the shaft 1, at its free end, such that no mounting space must be provided on the shaft length for said bearing 9, and consequently the shaft 1 must not be extended so as to position the bearing 9.
  • the placement of the bearing 9 according to the invention has no effect whatsoever on the shaft length that is required for the operation of the machine.
  • the second bearing 10 is realised in the known manner, whereby this bearing 10 uses at least one shoulder 7, axial thrust disc 8 or the like, provided on the shaft 1, whereby the aforesaid shoulder, thrust disc or the like is an intrinsic part of said second bearing 10.
  • the second bearing 10 consists of two active magnetic bearings which each act on an axial thrust disc 8 provided along the perimeter of the shaft 1.
  • the second bearing 10 use is made of a single thrust disc 8 on which the two active magnetic bearings of the second bearing 10 act on either side.
  • the size of this bearing can be restricted, as a result of which the effect on the length of the shaft 1 is restricted.
  • the length of the shaft 1 can be restricted compared to the embodiment described in figures 1 and 2.
  • the critical rotational speed of the shaft 1 increases, which makes it possible to make the shaft 1 rotate at higher rotational speeds with the same impeller 2 design and with the same materials being applied, and consequently to deliver higher pressures and more power.
  • Figure 4 shows a variant according to the invention whereby the first bearing 9 acts directly on the back side of the impeller 2.
  • the back side of the impeller 2 is the flat side of the rotor, which is the side without any blades.
  • the second bearing 10 in this case consists of two axial bearings which are each positioned at a shoulder 7 provided on the shaft 1.
  • this second bearing 10 can be made small, thus limiting the impact on the length of the shaft 1.
  • the first bearing 9 is controlled as a function of a machine variable whereby use is made of a control unit 11 comprising an algorithm to control the bearing 9 on the basis of a measuring signal from a pressure sensor 12.
  • the aforesaid pressure sensor 13 measures a variable that varies little in time.
  • An example of a relevant variable which varies little in time that can be used to this end is the prevailing pressure in the compressor, in particular the outlet pressure of the compressor. Indeed, this pressure forms the major contribution to the total axial force.
  • the aforesaid pressure sensor 12 is provided to that end on the flat side of the impeller, which is free of blades.
  • the second bearing 10 is preferably controlled by a control unit 13 which is connected to a position sensor 14 to determine the axial position of the shaft 1.
  • first bearing 9 may act on the back side of the impeller 2 while the second bearing 10 makes use of an axial thrust disc 8 provided along the perimeter of a shaft 1.
  • Another possible embodiment within the scope of the invention makes use of a first bearing 9 which acts on a shaft end of the shaft 1 with a second bearing 10 which acts via two shoulders 7 on the shaft 1.
  • the device according to the invention is always applied in a centrifugal compressor, in particular in a turbo compressor, but a device according to the invention can also be applied in other machines which are provided with a shaft which is subject to axial forces, such as for example a turbine, a motor or the like.
  • a device according to the invention for absorbing an axial force exerted on a machine shaft and a centrifugal compressor provided with such a device can be made in all sorts of shapes and dimensions while still remaining within the scope of the invention.

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Physics & Mathematics (AREA)
  • Electromagnetism (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Magnetic Bearings And Hydrostatic Bearings (AREA)

Abstract

Device for absorbing an axial force exerted on a machine shaft, which shaft (1) is provided with one or several rotors (2), and whereby this device comprises at least two axial bearings to support the aforesaid shaft (1), namely a first bearing (9) and a second bearing (10), characterised in that the aforesaid first bearing (9) is a primary bearing of the active magnet type which absorbs the major part of the aforesaid axial force and which is made such that for the mounting thereof no mounting space must be provided on the shaft length, whereby the aforesaid first bearing (9) is controlled by means of a control unit (11) which is at least connected to a pressure sensor (12) and which comprises an algorithm to control the aforesaid first bearing (9) on the basis of a measuring signal from aforesaid pressure sensor (12).

Description

Device for taking up an axial force exercised on a shaft of a machine and centrifugal compressor provided with such device .
The present invention concerns a device for absorbing an axial force exerted on a machine shaft supported on radial bearings, such as the shaft of a compressor, a motor, a turbine or the like.
In particular, the invention concerns a device for absorbing an axial force exerted on a machine shaft .
While such a machine is operational, varying axial and radial forces are exerted on the shaft of the machine, which makes it necessary to provide the machine with bearings which can absorb said forces .
Traditionally, the shaft is supported on radial bearings by means of two radial bearings provided at a certain distance from one another to ensure a good stability for the shaft and any rotor possibly provided upon the latter.
The shaft is axially loaded with a force whose magnitude varies in time and which may also change direction.
Conventionally, two bearings are applied, whereby one bearing absorbs the axial force in one direction, whereas the other bearing absorbs the axial force in the opposite direction. This means that at anytime only one of both bearings is loaded, while the other one remains unloaded.
Replacement sheet (rule 26) The machine shaft is supported on axial bearings in the known manner, whereby the shaft is provided with one or several elements which are necessary for the good functioning of the axial bearing. Traditionally, the aforesaid elements have the shape of an axial thrust disc or shoulder, whereby these elements have been provided or are placed on the side wall of the shaft, and whereby these elements function as an intrinsic part of the axial bearing.
As the machine's design provides larger loads, also larger bearings will be required, which implies that the shaft in such heavier loaded machines should be made sufficiently long to offer space to such larger bearings. Indeed, the shaft must be sufficiently long to provide the necessary space and room for an axial thrust disc, shoulder or the like on the one hand, and for the fixed part of the axial bearing itself on the other hand.
What precedes shows that the required length for the shaft increases as the axial bearing is made heavier.
Higher rotational speeds of the machine's shaft result in the use of active magnetic bearings and/or air bearings being preferred or, in many cases, even necessary.
A large speed of rotation of the shaft causes a large centrifugal force on the shaft and the radial bearings in case" of the slightest imbalance, making it necessary to balance the shaft before the machine is put into use. Even when the shaft is balanced, some imbalance still remains to a certain extent, as a result of which the shaft is excited by the centrifugal force while rotating.
As soon as the shaft reaches its critical rotational speed, the centrifugal force will excite the shaft with a frequency which, as is known, coincides with the first characteristic frequency of the shaft, resulting in resonance of the shaft.
When the shaft comes into resonance, the deviation and the deformation of the shaft is only limited by the damping in the system. However, magnetic bearings and air bearings produce very little damping, which would result in irreparable damage to the machine if no additional measures were taken in case of resonance.
From what precedes it is clear that the maximal rotational speed of the machine is restricted by the critical rotational speed of the shaft. The first characteristic frequency of this shaft concerns a bending frequency, whereby the length of the shaft is the most decisive factor. The first characteristic frequency of the shaft strongly decreases as the length of the shaft increases.
Heavy loaded machines which are conventionally supported on axial bearings in the above-described manner have the major disadvantage that the first characteristic frequency of the shaft of such a machine, and consequently the critical rotational speed of the shaft, tend to be relatively low, as a result of which the useful rotational speed of the machine is restricted. If the machine is a compressor, this will result in an output of the compressor concerned having a low energy density.
From German patent DE 10 2006 049 516, the use of a static gas bearing on a free shaft end at the back of an impeller is known.
The gas bearing is controlled by the measurement of force in a hydrodynamic tilting pad bearing, such that the forces in the hydrodynamic bearing are restricted by compensation in the gas bearing.
The control hereby provides in a closed loop system with feedback in order to reduce the force to zero. As far as control engineering is concerned, additional measures are thereby necessary, such as a low-pass filter, in order to guarantee a stable working under all circumstances.
Another disadvantage is that the gas bearing must be sealed. Given the high rotational speeds and large diameter, there is a large sliding speed in said sealing, as a result of which the sealing is subject to wear and leaks may prematurely occur.
The present invention aims to remedy one or several of the above-mentioned and/or other disadvantages by providing a device for absorbing an axial force exerted on a machine shaft, which shaft is provided with one or several rotors, and whereby this device comprises at least two axial bearings to support the aforesaid shaft, namely a first bearing and a second bearing, whereby the aforesaid first bearing is a primary bearing of the active magnet type which absorbs the major part of the aforesaid axial force and which is designed such that, for the mounting thereof, no mounting space on the shaft's length needs to be provided, whereby the aforesaid first bearing is controlled by means of a control unit and whereby the control unit is at least connected to a pressure sensor and comprises an algorithm to control the aforesaid first bearing on the basis of a measuring signal from the aforesaid pressure sensor.
This means that the aforesaid first bearing is preferably not controlled on the basis of an axial position measurement of the machine's shaft.
An advantage hereby is that it is easier to control the first bearing than to control a conventional axial active bearing.
In other words, according to the invention, the shaft must not be extended to place the bearing, or to rephrase it, the first bearing is designed such that it has no influence whatsoever on the shaft length that is required for the working of the machine.
The aforesaid first bearing hereby works in one direction and absorbs more than 75% of the total axial force in that particular direction, preferably at least 85% of the total axial force, and even more preferably at least 95% of the total axial force.
With a device according to the invention, the shaft can be made shorter than the shaft of an identical machine, supported in the conventional manner on axial bearings.
Indeed, according to the invention, the most heavily loaded and consequently the most sizeable bearing is provided in the device in such a manner that this bearing has no influence whatsoever on the length of the shaft that is required for the working of the machine, as a result of which the length of the shaft can be restricted to an absolute minimum. In other words, the aforesaid first bearing will not occupy any axial mounting space on the shaft while the device according to the invention is in use.
The reduced length of the shaft in the case of the invention offers several advantages. The first characteristic frequency and the critical rotational speed of said shaft increase, as a result of which the maximally permitted rotational speed of the machine will be higher than in the case of a machine with conventional bearings.
Another advantage is that the shaft has less mass, which allows savings on material and transport costs.
According to a preferred embodiment, the first bearing acts directly on a far end of the shaft or on a rotor which has been provided on the shaft or which is a part of it. What precedes implies that, for the good functioning of the first bearing, the shaft or rotor must not be provided with additional elements that are traditionally used, such as a thrust disc, shoulder or the like.
This offers the advantage that the shaft or rotor does not need any final processing to create a thrust disc, shoulder or the like in the shaft or rotor or to provide the necessary means for fixing the aforesaid elements to the shaft or rotor. As a result, the machine is less expensive to produce.
In a practical embodiment, the pressure sensor may be provided nearby the impeller, and the magnetic bearing is controlled by the measuring signal from the pressure sensor.
By replacing the gas bearing in the known devices by a magnetic bearing, a sealing to seal off the bearing is no longer necessary.
Another advantage is that no consumption of compressed air occurs .
Yet another advantage is that a pressure measurement allows to control the magnetic bearing in a simple, yet efficient manner. Indeed, the measured pressure is a major factor for the forces that are being absorbed by the magnetic bearing. The aforesaid control on the basis of pressure and the use of the magnetic bearing results in a direct compensation of the axial gas pressure forces, which leads to a stable system.
According to a preferred embodiment, the second axial bearing is also of the active magnetic type, whereby the first bearing is controlled as a function of a machine variable, for example, in the case of a compressor, the outlet pressure. The aforesaid machine variable that is used to this end is preferably a variable that varies little in time.
Another advantage is that a control on the basis of a simple open loop control system with a gain factor may be provided.
An advantage related thereto is that the primary bearing will not introduce any unstable conditions.
The present invention also concerns a centrifugal compressor provided with a shaft with one or several rotors and with a device for absorbing an axial force that is exerted on the aforesaid shaft, which device comprises at least two axial bearings supporting the aforesaid shaft, a first bearing and a second bearing respectively, whereby the aforesaid first bearing is a primary bearing of the active magnetic type which absorbs the major part of the aforesaid axial force and which is made such that it does not affect the required length of the shaft, or, in other words, no mounting space must be provided on the shaft length for this first bearing, whereby the aforesaid first bearing is controlled by means of a control unit and whereby the control unit is at least connected to a pressure sensor and comprises an algorithm to control the aforesaid first bearing on the basis of a measuring signal from the aforesaid pressure sensor.
The advantages related to a centrifugal compressor according to the invention are identical to the above- discussed advantages offered by a device according to the invention.
In order to better explain the characteristics of the invention, the following preferred embodiments of a centrifugal compressor, provided with a device according to the invention, are described by way of example only without being limitative in any way, with reference to the accompanying drawings, in which:
figure 1 schematically shows a section of a centrifugal compressor provided with a conventional device for absorbing an axial force; figure 2 shows a variant of figure 1; figure 3 schematically shows a section as that in figure 1, but for a centrifugal compressor provided with a device according to the invention; figure 4 shows a variant of figure 3.
The figures represent the shaft 1 of a machine which is in this case made as a centrifugal compressor, whereby said shaft 1 is provided with a rotor 2 in the shape of an impeller on one far end. The shaft 1 and rotor 2 are mounted in a rotating manner in a housing 3 of the compressor.
The shaft 1 is provided with two radial bearings 4. The shaft 1 is driven by an electromotor, as represented in figure 1, whereby said electromotor is made as a high-speed permanent-magnet motor in the present example.
The shaft 1 in figure 1 is radially supported by two radial bearings 4, whereas the axial forces, introduced during working of the machine, are absorbed by two axial bearings β. The axial as well as the radial bearings 6, 4 respectively, are in this case active magnetic bearings.
The aforesaid axial bearings 6 act on a shoulder 7 of the shaft 1, namely on the radially directed side flanges of a shaft part having a larger diameter than the rest of the shaft 1.
It is clear that for the axial bearings 6, a certain shaft length should be provided, in other words that mounting space should be provided on the perimeter of the shaft so as to make room for said axial bearings 6, which is disadvantageous, as explained in the introduction, to the maximally permitted rotational speed with respect to the risk of resonance phenomena occurring.
In the case of figure 2, the two axial bearings 6 are represented in a configuration whereby these bearings 6 act on an axial thrust disc 8 which is fixed to the shaft 1 or which is part of it, and whereby these bearings 6 also make it necessary for the shaft 1 to have a certain length.
Figure 3, however, shows a device according to the invention, whereby two bearings are applied, namely a first bearing 9 which serves as a primary axial bearing and which is provided on a free end of the shaft 1, and a second bearing 10 in the shape of a secondary axial bearing which is in this case made as a double-acting bearing extending on either side of an axial thrust disc 8 on the shaft 1.
The bearings 9 and 10 which are represented in the figures are in this case of the active magnet type. According to the invention, it is not strictly necessary that the second bearing is of the active magnet type.
The working of a device according to the invention is simple and as follows.
The shaft 1 is driven by the motor 5, whereby the rotor 2 at the far end of the shaft 1 rotates in the housing 3. As a result, the sucked-in air is compressed in the known manner, after which the compressed air is discharged to a downstream application.
Given the high rotational speeds of the shaft 1, bearings of the active magnetic type are preferably used. The working of an active magnetic bearing is known, and it uses amongst others an electromagnet, amplifiers and sensors to support the shaft 1 in a contactless way. While the machine is working normally, the shaft/rotor system 1, 2 is loaded with an axial force in the direction of arrow A. This axial force mainly consists of a nominal, almost static component, caused by the pressure distribution on the rotor 2.
The first axial bearing 9 is dimensioned such that it can absorb this nominal, almost static axial force. Consequently, this first bearing 9 must be made relatively large and heavy.
Traditionally, as represented in figures 1 and 2, the axial bearings 6 act on an axial thrust disc 8, on a shoulder 7 or on other elements which are provided on the shaft 1. It is clear that in such cases, the shaft 1 must be made sufficiently long so as to provide sufficient room for the axial bearings 6.
According to the invention, the first, primary bearing 9 is made such that it does not affect the required length of the shaft 1, as is illustrated for example by figure 3 in which the first bearing 9 acts directly on the free end of the shaft 1.
In this way, the first bearing 9 can be placed in the extension of the shaft 1, at its free end, such that no mounting space must be provided on the shaft length for said bearing 9, and consequently the shaft 1 must not be extended so as to position the bearing 9. In other words, the placement of the bearing 9 according to the invention has no effect whatsoever on the shaft length that is required for the operation of the machine.
While the machine is operational, small force fluctuations also arise which are axially directed according to arrow A or arrow B. These small force components are absorbed by the second, secondary axial bearing 10.
The second bearing 10 is realised in the known manner, whereby this bearing 10 uses at least one shoulder 7, axial thrust disc 8 or the like, provided on the shaft 1, whereby the aforesaid shoulder, thrust disc or the like is an intrinsic part of said second bearing 10.
In this case, the second bearing 10 consists of two active magnetic bearings which each act on an axial thrust disc 8 provided along the perimeter of the shaft 1. In the given example, use is made of a single thrust disc 8 on which the two active magnetic bearings of the second bearing 10 act on either side.
As the second bearing 10 is minimally loaded, the size of this bearing can be restricted, as a result of which the effect on the length of the shaft 1 is restricted.
Consequently, with a device according to the invention, the length of the shaft 1 can be restricted compared to the embodiment described in figures 1 and 2. As a result, the critical rotational speed of the shaft 1 increases, which makes it possible to make the shaft 1 rotate at higher rotational speeds with the same impeller 2 design and with the same materials being applied, and consequently to deliver higher pressures and more power.
Figure 4 shows a variant according to the invention whereby the first bearing 9 acts directly on the back side of the impeller 2. The back side of the impeller 2 is the flat side of the rotor, which is the side without any blades. The second bearing 10 in this case consists of two axial bearings which are each positioned at a shoulder 7 provided on the shaft 1.
Given the restricted load of the second bearing 10, this second bearing 10 can be made small, thus limiting the impact on the length of the shaft 1.
According to the invention, the first bearing 9 is controlled as a function of a machine variable whereby use is made of a control unit 11 comprising an algorithm to control the bearing 9 on the basis of a measuring signal from a pressure sensor 12. Preferably, the aforesaid pressure sensor 13 measures a variable that varies little in time. An example of a relevant variable which varies little in time that can be used to this end is the prevailing pressure in the compressor, in particular the outlet pressure of the compressor. Indeed, this pressure forms the major contribution to the total axial force. In the given example, the aforesaid pressure sensor 12 is provided to that end on the flat side of the impeller, which is free of blades. The second bearing 10 is preferably controlled by a control unit 13 which is connected to a position sensor 14 to determine the axial position of the shaft 1.
Although active magnet bearings are used in the preceding embodiments, also an air bearing can be used for the second bearing.
Other embodiments than those discussed above with reference to figures 3 and 4 are possible as well, while still remaining within the scope of the invention. Thus, for example, the first bearing 9 may act on the back side of the impeller 2 while the second bearing 10 makes use of an axial thrust disc 8 provided along the perimeter of a shaft 1.
Another possible embodiment within the scope of the invention makes use of a first bearing 9 which acts on a shaft end of the shaft 1 with a second bearing 10 which acts via two shoulders 7 on the shaft 1.
In the above-described embodiments, the device according to the invention is always applied in a centrifugal compressor, in particular in a turbo compressor, but a device according to the invention can also be applied in other machines which are provided with a shaft which is subject to axial forces, such as for example a turbine, a motor or the like.
The present invention is by no means restricted to the embodiments described by way of example and represented in the accompanying drawings; on the contrary, a device according to the invention for absorbing an axial force exerted on a machine shaft and a centrifugal compressor provided with such a device can be made in all sorts of shapes and dimensions while still remaining within the scope of the invention.

Claims

Claims .
1. - Device for absorbing an axial force exerted on a machine shaft, which shaft (1) is provided with one or several rotors (2), and whereby this device comprises at least two axial bearings to support the aforesaid shaft (1), namely a first bearing (9) and a second bearing (10), characterised in that the aforesaid first bearing (9) is a primary bearing of the active magnet type, which absorbs the major part of the aforesaid axial force and which is made such that for the mounting thereof no mounting space must be provided on the shaft length, whereby the aforesaid first bearing (9) is controlled by means of a control unit (11) which is at least connected to a pressure sensor (12) and which comprises an algorithm to control the aforesaid first bearing (9) on the basis of a measuring signal from aforesaid pressure sensor (12) .
2. - Device according to claim 1, characterised in that the aforesaid first bearing (9) acts directly on one far end of the shaft (1) .
3. - Device according to any one of the preceding claims, characterised in that the aforesaid first bearing (9) acts directly on a rotor (2) of the shaft (1) .
4. - Device according to any one of the preceding claims, characterised in that the second bearing (10) is of the active magnet type.
5. - Device according to any one of the preceding claims, characterised in that it is applied in a machine in the shape of a centrifugal compressor, whereby the aforesaid rotor (2) is made in the shape of an impeller, and whereby the aforesaid measuring sensor (12) is provided on the flat side of the impeller which does not have any blades.
6. - Device according to any one of the preceding claims, characterised in that the aforesaid second bearing (10) is connected to a control unit (13 or 15) which is also connected to a measuring sensor (14) and whereby this control unit (13 or 15) comprises an algorithm to control the aforesaid second bearing (10) on the basis of a measuring signal from the aforesaid measuring sensor (14) .
7. - Device according to claim 6, characterised in that the aforesaid measuring sensor (14) on the basis of which the second bearing (10) is controlled, is made as a position sensor.
8. - Device according to any one of the preceding claims, characterised in that the aforesaid first bearing (9) absorbs at least 75% of the total axial force, preferably absorbs at least 85% of the total axial force, and even more preferably absorbs at least 95% of the total axial force.
9. - Device according to claim 1, characterised in that it is applied in a machine having the shape of a turbo compressor with a rotor (2) in the shape of an impeller which is fixed directly to the shaft (1) , whereby the first bearing (9) acts directly on the flat side of this impeller which does not have any blades.
10. - Device according to any one of the preceding claims, characterised in that the aforesaid second bearing (10) is controlled by a control unit (13) which is connected to a position sensor (14) to determine the axial position of the aforesaid shaft (1) .
11. - Centrifugal compressor which is provided with a shaft (1) having one or several rotors (2) and with a device for absorbing an axial force which is exerted on the aforesaid shaft (1), which device comprises at least two axial bearings supporting the aforesaid shaft (1), namely a first bearing (9) and a second bearing (10), characterised in that the aforesaid first bearing (9) is a primary bearing of the active magnet type, which absorbs the major part of the aforesaid axial force and which is made such that for the mounting thereof no mounting space must be provided on the shaft length, whereby the aforesaid first bearing (9) is controlled by means of a control unit (11) which is at least connected to a pressure sensor (12) and comprises an algorithm to control the aforesaid first bearing (9) on the basis of a measuring signal from aforesaid pressure sensor
(12) .
PCT/BE2010/000035 2009-04-28 2010-04-27 Device for taking up an axial force exercised on a shaft of a machine and centrifugal compressor provided with such device WO2010124350A1 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
BE2009/0269 2009-04-28
BE2009/0269A BE1018544A3 (en) 2009-04-28 2009-04-28 DEVICE FOR RECORDING AN AXIAL FORCE EXERCISED ON AN AXIS OF A MACHINE AND A CENTRIFUGAL COMPRESSOR PROVIDED WITH SUCH DEVICE.

Publications (1)

Publication Number Publication Date
WO2010124350A1 true WO2010124350A1 (en) 2010-11-04

Family

ID=42026840

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/BE2010/000035 WO2010124350A1 (en) 2009-04-28 2010-04-27 Device for taking up an axial force exercised on a shaft of a machine and centrifugal compressor provided with such device

Country Status (2)

Country Link
BE (1) BE1018544A3 (en)
WO (1) WO2010124350A1 (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN105121860A (en) * 2013-05-30 2015-12-02 三菱重工业株式会社 Turbo compressor and turbo chiller using same
CN111486112A (en) * 2019-01-29 2020-08-04 青岛海尔智能技术研发有限公司 Magnetic suspension centrifugal compressor and air conditioning system

Citations (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
AT92424B (en) * 1921-03-12 1923-05-11 Ferdinand Ing Petters Electromagnetic relief from track and comb bearings.
DE835744C (en) * 1950-07-12 1952-04-03 Siemens Schuckertwerke A G Device for thrust compensation of centrifugal machines, in particular steam turbines
US5263816A (en) * 1991-09-03 1993-11-23 General Motors Corporation Turbomachine with active tip clearance control
US5543673A (en) * 1993-07-27 1996-08-06 Sundstrand Corporation High performance magnetic bearing
EP0875685A2 (en) * 1997-04-28 1998-11-04 Ntn Corporation Combined externally pressurized gas-magnetic bearing assembly and spindle device utilizing the same
US5836739A (en) * 1995-03-17 1998-11-17 Rolls-Royce Plc Gas turbine engine
US20060012258A1 (en) * 2002-07-10 2006-01-19 Turbocor, Inc. Device to relieve thrust load in a rotor-bearing system using permanent magnets
WO2007023684A1 (en) * 2005-08-22 2007-03-01 Ntn Corporation Air cycle refrigerating/cooling system and turbine unit used therefor
DE102006049516B3 (en) * 2006-10-20 2008-01-03 Atlas Copco Energas Gmbh Turbo-engine, e.g. for operating as turbo-compressor, has a rotor with radial and axial bearings in a casing with a shaft and a rotor disk fastened on the shaft
US20080012347A1 (en) * 2004-12-30 2008-01-17 Rozmus John J Wind generator system using attractive magnetic forces to reduce the load on the bearings

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE646514C (en) * 1937-06-16 Peter Leis Dr Ing Process for reducing the friction of rubbing parts
DE824231C (en) * 1949-10-01 1951-12-10 Siemens Schuckertwerke A G Arrangement for relieving the load on track bearings or support bearings in machines or apparatus with a vertical shaft
US4167295A (en) * 1977-12-08 1979-09-11 The Garrett Corporation Magnetic thrust force relief for a foil bearing turbomachine
DE10138056A1 (en) * 2001-08-03 2003-02-13 Atlas Copco Energas turbomachinery
DE102004023149A1 (en) * 2004-05-07 2005-11-24 Atlas Copco Energas Gmbh turbomachinery

Patent Citations (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
AT92424B (en) * 1921-03-12 1923-05-11 Ferdinand Ing Petters Electromagnetic relief from track and comb bearings.
DE835744C (en) * 1950-07-12 1952-04-03 Siemens Schuckertwerke A G Device for thrust compensation of centrifugal machines, in particular steam turbines
US5263816A (en) * 1991-09-03 1993-11-23 General Motors Corporation Turbomachine with active tip clearance control
US5543673A (en) * 1993-07-27 1996-08-06 Sundstrand Corporation High performance magnetic bearing
US5836739A (en) * 1995-03-17 1998-11-17 Rolls-Royce Plc Gas turbine engine
EP0875685A2 (en) * 1997-04-28 1998-11-04 Ntn Corporation Combined externally pressurized gas-magnetic bearing assembly and spindle device utilizing the same
US20060012258A1 (en) * 2002-07-10 2006-01-19 Turbocor, Inc. Device to relieve thrust load in a rotor-bearing system using permanent magnets
US20080012347A1 (en) * 2004-12-30 2008-01-17 Rozmus John J Wind generator system using attractive magnetic forces to reduce the load on the bearings
WO2007023684A1 (en) * 2005-08-22 2007-03-01 Ntn Corporation Air cycle refrigerating/cooling system and turbine unit used therefor
DE102006049516B3 (en) * 2006-10-20 2008-01-03 Atlas Copco Energas Gmbh Turbo-engine, e.g. for operating as turbo-compressor, has a rotor with radial and axial bearings in a casing with a shaft and a rotor disk fastened on the shaft

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN105121860A (en) * 2013-05-30 2015-12-02 三菱重工业株式会社 Turbo compressor and turbo chiller using same
EP2966305A4 (en) * 2013-05-30 2016-03-02 Mitsubishi Heavy Ind Ltd Turbo compressor and turbo chiller using same
CN105121860B (en) * 2013-05-30 2019-05-14 三菱重工制冷空调系统株式会社 Turbo-compressor and the turborefrigerator for using the turbo-compressor
US10858951B2 (en) 2013-05-30 2020-12-08 Mitsubishi Heavy Industries Thermal Systems, Ltd. Turbo compressor and turbo chiller using same
CN111486112A (en) * 2019-01-29 2020-08-04 青岛海尔智能技术研发有限公司 Magnetic suspension centrifugal compressor and air conditioning system

Also Published As

Publication number Publication date
BE1018544A3 (en) 2011-03-01

Similar Documents

Publication Publication Date Title
US7964982B2 (en) Axial in-line turbomachine
CN102762871B (en) Dynamic thrust for centrifugal compressor balances
EP0550801B1 (en) Turbo compressor and method of controlling the same
US6616423B2 (en) Turbo expander having automatically controlled compensation for axial thrust
EP0887557A1 (en) Free rotor stabilization
WO2013015885A1 (en) Compressor surge detection
KR102233449B1 (en) Device for counterbalancing axial load in centrifugal compressor
JPH04232397A (en) Bleeding device for conducting bleeding to high-speed rotary vacuum pump
US10107298B2 (en) Turbo machine
US6450780B1 (en) Method for generating over-pressure gas
WO2010124350A1 (en) Device for taking up an axial force exercised on a shaft of a machine and centrifugal compressor provided with such device
JP2008215107A (en) Compressor
JP6389785B2 (en) Downhole compressor
CA2674263A1 (en) Method for determination of resonant frequencies of a rotor using magnetic bearings
JP6892004B1 (en) Motor system and turbo compressor equipped with it
JP3997578B2 (en) High speed rotating equipment
JP4376021B2 (en) Fluid bearing
US20120275923A1 (en) Rotor for a turbo-machine
JPS58152951A (en) Casing support device
JPH0734236Y2 (en) Rotating machines such as turbo pumps equipped with magnetic bearings
Hawkins et al. Design and Shop Testing of a 165 kW Cryogenic Expander/Generator on Magnetic Bearings
EP1072804A2 (en) Magnetic bearing device
JPH04246299A (en) Multistage compressor
JPH0297713A (en) Rotating machine using five-axis control magnetic bearing
JP2003293987A (en) Fluid machinery and rotor installed therein

Legal Events

Date Code Title Description
121 Ep: the epo has been informed by wipo that ep was designated in this application

Ref document number: 10734890

Country of ref document: EP

Kind code of ref document: A1

DPE1 Request for preliminary examination filed after expiration of 19th month from priority date (pct application filed from 20040101)
NENP Non-entry into the national phase

Ref country code: DE

122 Ep: pct application non-entry in european phase

Ref document number: 10734890

Country of ref document: EP

Kind code of ref document: A1