• 专利附录
  • 专利说明
  • 权利要求
  • 类似技术
  • 同族专利
  • 引用文献
  • 法律状态
  • 优先权
    • 专利摘要:
    The present invention is directed to a multi-stage compressor (1) comprising at least a first compressor stage (2) comprising a first compressor element (5) driven via a first gear transmission (9) and a second compressor stage comprising a second compressor element (10) driven a separate second gear transmission (14), wherein (3) via the aforementioned first and second gear transmissions (9, 14) comprise a drive gear and a driven gear configured as a multiplier, each of the aforementioned driven gears being connected to a shaft of a rotor of said first compressor element (5) and second compressor element (10), respectively, wherein the first motor (8) and the second motor (13) are adapted to separately drive the first compressor stage (2) and the second compressor stage (3) in which the gear ratio between the driven gear and the drive gear of each of the aforementioned first gear transmission (9) and second gear transmission (14) is between two and six.
    公开号:BE1026205B1
    申请号:E2018/5769
    申请日:2018-11-02
    公开日:2019-11-12
    发明作者:Bontridder Thomas Willem I De
    申请人:Atlas Copco Airpower Naamloze Vennootschap；
    IPC主号:
    专利说明:

    Multi-stage compressor and method for setting the speed of the motors.
    The present invention relates to a multi-stage compressor comprising an inlet and a compressed gas outlet, wherein at least a first compressor stage comprises a first compressor element which is driven by a first motor via a first gear transmission and a second compressor stage comprises a second compressor element which is driven by a second engine via a separate second gear transmission, wherein each of the aforementioned first and second gear transmissions comprises a drive gear connected to the first motor and the second motor, respectively, and a driven gear configured as a multiplier, each of the aforementioned driven gear wheels being connected to a shaft of a rotor of the aforementioned first compressor element and second compressor element, respectively, wherein the first motor and the second motor are adapted to drive the first compressor element and the second compressor element separately.
    The use of multi-stage compressors is widespread in the industry, such known devices generally having at least two compressor stages with compressor elements driven either by the same motor or by separate motors.
    If the compressor elements are driven by the same motor, even though they may be reliable, the flexibility of these compressors in controlling the speed of the two compressor stages is limited.
    BE2018 / 5769
    An example of a two-stage compressor in which each stage comprises a motor driven via an inverter can be found in WO 2017 / 169,595 A.
    In yet another example, WO 01/31202, a multi-stage compressor is provided in which the compressor elements of the compressor stages are driven separately on the basis of the pressure measured at the outlet of the multi-stage compressor.
    Usually a relatively large motor is integrated in these known compressors, which is driven at low speeds, which makes them inefficient in terms of production costs and operating costs since the full power of the motor is not used.
    Taking into account the aforementioned disadvantages, it is an object of the present invention to provide a multi-stage compressor that allows a higher flexibility in controlling the speed of the different compressor stages as a function of their respective parameters.
    Another object of the present invention is to provide a multi-stage compressor that is efficient both in terms of production costs and in terms of operating costs.
    Yet another object of the present invention is to provide a solution to use the motors that drive the compressor elements of different compressor stages at high power.
    The present invention provides a solution to at least one of the above-mentioned and / or other problems caused by one
    BE2018 / 5769 multi-stage compressor comprising an inlet and a compressed gas outlet, wherein at least a first compressor stage comprises a first compressor element driven by a first motor via a first gear transmission and a second compressor stage comprises a second compressor element driven by a second motor via a separate second gear transmission, wherein each of the aforementioned first and second gear transmissions comprises a drive gear connected to the first motor and the second motor, respectively, and a driven gear configured as a multiplier, each of the aforementioned driven gear wheels being connected to a shaft of a rotor of the said first compressor element and second compressor element respectively, wherein the first motor and the second motor are adapted to separately drive the first compressor element and the second compressor element in which the gear ratio between the driven gear and the drive gear of each of the aforementioned first gear transmission and second gear transmission is between two and six.
    By assuming such a gear ratio between the driven gear and the drive gear of each of the aforementioned first and second gear transmissions, the multistage compressor according to the present invention can integrate smaller motors that are driven at a higher speed and at the same time still meet the demand of the user, which increases the efficiency of the multi-stage compressor, compared to existing compressors.
    BE2018 / 5769
    Consequently, since the motors are smaller, not only the operational efficiency of the multi-stage compressor is increased, but also the production costs are lowered.
    Moreover, the energy footprint of a multi-stage compressor according to the present invention also becomes smaller.
    Furthermore, the use of smaller motors reduces the dimensions and weight of the multi-stage compressor.
    This makes the multi-stage compressor easier to handle, not only during production but also during transport.
    By using such a layout, the rotational speed of the rotors of the respective compressor elements is higher than the respective rotational speed of the motors, whereby the efficiency of the multistage compressor increases.
    In fact, through this classification, the rotors of the first compressor element and of the second compressor element achieve the same speeds with a small motor as they would have achieved with a large motor. This translates into a reduction in the overall production costs and in the complexity of the system, since for a smaller engine conventional materials, conventional connecting means and conventional controls would have to be used.
    The present invention is further directed to a method for controlling the speed of the motors of a multi-stage compressor, wherein the method comprises the following steps:
    providing a first compressor stage comprising a first compressor element and this first compressor element
    BE2018 / 5769 drives by means of a first motor via a first gear transmission;
    providing a second compressor stage comprising a second compressor element and driving said second compressor element separately from the first compressor element by means of a second motor via a separate second gear transmission;
    connecting a drive gear of each of the first gear transmission and second gear transmission to the first motor and second motor, respectively;
    connecting a driven gear of each of the first gear transmission and second gear transmission to a shaft of a rotor of said first compressor element and second compressor element, respectively
    The method further comprising the step of adjusting the gear ratio between the drive gear and the driven gear of each of said first gear transmission and second gear transmission between two and six.
    The present invention is further directed to a multi-stage compressor comprising at least a first compressor element and a second compressor element and at least a first motor and a second motor for driving, each separately, one of the aforementioned first compressor element and second compressor element via a separate first gear transmission and second gear transmission, each of said first gear transmission and second gear transmission comprising a drive gear connected to a motor of said first motor and second motor, respectively, and a driven gear connected to a shaft of a rotor of one of said first
    BE2018 / 5769 compressor element or second compressor element, wherein the ratio between the number of teeth of the drive gear and the number of teeth of the driven gear of one of the aforementioned first gear transmission and second gear transmission is between two and six.
    In the context of the present invention, it should be assumed that the advantages set out above with regard to the multi-stage compressor also apply to the speed control method.
    With the insight to better demonstrate the characteristics of the invention, a few preferred configurations according to the present invention are described below as an example without any limiting character, with reference to the accompanying drawings, in which:
    figure 1 schematically illustrates a multi-stage compressor according to an embodiment of the present invention;
    figure 2 schematically illustrates an example of the first compressor stage according to an embodiment of the present invention;
    figure 3 schematically illustrates a multi-stage compressor according to an embodiment of the present invention;
    figure 4 schematically illustrates a side view of the multi-stage compressor according to figure 3;
    figure 5 schematically illustrates a rotated view of the multi-stage compressor according to figure 3;
    figure 6 schematically illustrates a multi-stage compressor according to another embodiment of the present invention; and
    BE2018 / 5769
    figure 7 schematically illustrates the method according to an embodiment of the present invention in a flow chart.
    Figure 1 illustrates a multi-stage compressor 1, in this case in the form of a two-stage compressor comprising a first compressor stage 2 and a second compressor stage 3 supplying pressurized gas to a user network 4.
    The first compressor stage 2 comprising a first compressor element 5 which has an inlet 6 and a compressed gas outlet 7.
    The first compressor element 5 is driven by a first motor 8 via a first gear transmission 9.
    Such a gear transmission 9 is generally received within a housing, the whole being generally known as a gearbox.
    Analogously, the second compressor stage 3 comprises a second compressor element 10 which has an inlet 11 and a compressed gas outlet 12. The second compressor element 10 is driven by a second motor 13 via a second gear transmission 14. An independent speed control is realized by such a layout.
    However, it cannot be excluded that the multi-stage compressor 1 according to the present invention may also comprise more than two compressor stages, such as, for example, without any limiting character: three, four or even more.
    BE2018 / 5769
    In the context of the present invention, multi-stage compressor 1 is understood to mean the complete compressor installation, including the compressor elements 5 and 10, all typical connecting lines and valves, the casing and possibly the motors 8 and 13 which drive the compressor elements 5 and 10.
    In the context of the present invention, the compressor element is to be understood to mean the compressor element box in which the compression process takes place, usually by means of one or more rotors.
    Each of the aforementioned first gear transmission 9 and second gear transmission 14 herein comprises a drive gear and a driven gear which fit into each other.
    With respect to the first compressor stage 2, the drive gear is mounted on a motor shaft of a rotor of the first motor 8, and the driven gear is mounted on one shaft of the first compressor element 5.
    Analogously, the drive gear of the second gear transmission 14 is mounted on a motor shaft of a rotor of the second motor 13 and the driven gear is mounted on one shaft of the second compressor element 10.
    During operation, the motor shaft and consequently the drive gear rotate, whereby the driven gear and, consequently, the rotor in the compressor element 5 also rotate. Since the driven gear is designed as a multiplier, the speed of the driven gear is
    BE2018 / 5769 during operation, higher than that of the drive gear. Consequently, the rotors in the first compressor element 5 and in the second compressor element 10 will reach higher speeds than the rotor of their respective motors.
    Each of the aforementioned first compressor element 5 and second compressor element 10 generally comprises two rotors: a male rotor and a female rotor (not shown) that engage each other.
    Each rotor herein comprises a shaft, wherein preferably, but without any limiting character, the shaft of the male rotor is connected to the driven gear of the respective gear transmission.
    It cannot be excluded that the shaft of the female rotor may be connected to the driven gear instead of the shaft of the male rotor.
    The use of such a gear transmission offers the advantage of speed range flexibility. Moreover, the lower the gear ratio between the driven gear and the drive gear of the aforementioned gear transmission, the higher the speed of the first motor 8 and the second motor 13, respectively, which makes potential cost savings possible. But beyond a certain speed, additional measures are needed to deal with the technical challenges.
    Preferably, the gear ratio between the driven gear and the drive gear is between two and six, in which case the first motor 8 and the second motor 13
    BE2018 / 5769 do not require additional measures. Consequently, the engines are used at high power, which translates into lower operating costs.
    By choosing a speed ratio between two and six, the maximum and minimum speed of the rotors of the first compressor stage 2 and the second compressor stage 3, respectively, are in fact kept within a nominal range. As a result, the temperature within the housing of the compressor element of the first compressor stage 2 and of the second compressor stage 3 can also be kept within desired limits, which protects the components and potentially extends the service life of the multi-stage compressor 1.
    By assuming a speed ratio between two and six for the first motor 8 and for the second motor 13, the speed of the respective motor may be higher than in conventional devices, without the need for additional reinforcements and without extra means for the motor. or to cool the bearings. Consequently, operating and production costs are kept low.
    In conventional systems, the gear ratio between the rotor of the motor and the rotor of the compressor element is generally selected to be higher than 6, with a larger motor operating at a low speed integrated in such systems. Since the engine is not driven at its full capacity, the efficiency of the system is not optimal and the operating costs are higher.
    Newer systems would choose a gear ratio of less than 2 to increase efficiency, but on to
    BE2018 / 5769 at such high speeds, additional reinforcements of the rotor of the first motor 8 and of the second motor 13 would be needed.
    In addition, a larger engine would require special connecting elements and materials that should withstand high vibrations and high temperatures that occur when the engine is driven at full power.
    Moreover, high speeds of the first motor 8 and / or of the second motor 13 require high switching frequencies of the frequency converter, which entails greater challenges in the field of control.
    In addition, at such high speeds, special materials for engine production, special means for controlling the magnets in it and special means for cooling should be used.
    In a preferred embodiment of the present invention, but without any limiting character, the aforementioned first and second compressor elements 5 and 10 can be selected as a screw or tooth compressor element, either oil-free or oil-injected.
    In another preferred embodiment of the present invention, each of the aforementioned first motor 8 and second motor 13 includes a frequency converter (not shown) to change the speed of the motor 8 and 13, respectively.
    BE2018 / 5769
    In a preferred embodiment according to the present invention, the speed for the first motor 8 and the second motor 13 can be changed via each of the frequency converters independently of each other.
    By choosing such a layout of the multi-stage compressor 1, not only the flexibility of the system is increased but also the multi-stage compressor 1 can be adjusted according to the specific system conditions.
    Consequently, the independent speed control allows the performance of the multi-stage compressor 1 to be improved on the basis of environmental and operating conditions.
    In a preferred embodiment of the present invention, but without any limiting character, the first compressor stage 2 and the second compressor stage 3 are serially connected. For example, the compressed gas outlet 7 of the first compressor stage 2 is in fluid communication with the inlet 11 of the second compressor element 10, and the compressed gas outlet 12 of the second compressor stage 3 is in fluid communication with the user network 4 (Figure 1).
    However, it cannot be excluded that the first compressor stage 2 is connected in parallel with the second compressor stage 3. In such a case, the inlet of the two compressor stages would branch off from a common inlet and the two compressed gas outlets would be connected to a common outlet that the user network achieved.
    BE2018 / 5769
    In a preferred embodiment according to the present invention, the multi-stage compressor 1 comprises a cooling unit 15 for cooling a compressed gas flowing from the first compressor element 5 or the second compressor element 10.
    Such a cooling unit 15 is herein positioned either between the first compressor stage 2 and the second compressor stage 10 or between the second compressor stage 10 and the user network 4.
    The cooling unit 15 is preferably positioned on the fluid line between the first compressor stage 2 and the second compressor stage 10.
    Typically, the cooling unit 15 comprises two sections: a first section of channels through which the press gas flows and a second section along which a coolant flows, the temperature of the coolant generally being much lower than that of the press gas. Consequently, the pressurized gas flowing out of the first compressor stage 3 is cooled by passing through the cooling unit 15 before it is passed through the inlet of the second compressor element 10 where it is further compressed.
    The coolant in the cooling unit 15 is hereby selected from the group comprising: air, water, oil or any other coolant.
    In another embodiment of the present invention, but without any limiting character, the refrigerant may further comprise an additive such as, for example, glycol.
    BE2018 / 5769
    In an embodiment according to the present invention, the multi-stage compressor 1 further comprises a controller 16 connected to the first motor 8 via a first communication link 17 and to the second motor 13 via a second communication link 18.
    Preferably, but without any limiting character, the controller 16 is connected via the first communication link 17 to a frequency converter adapted to increase or decrease the speed of the first motor 8.
    In a similar manner, the controller 16 is connected via the second communication link 18 to a frequency converter adapted to increase or decrease the speed of the second motor 13.
    The controller 16 determines the speed of the first motor 8 and the second motor 13 and generates an electrical signal to each of the frequency converters.
    In a preferred embodiment according to the present invention, the multi-stage compressor 1 here generally comprises a series of sensors such as for example: a first pressure sensor 23 and / or a first temperature sensor 25 positioned at the compressed gas outlet 7 of the first compressor element 5 and a second pressure sensor 24 and / or a second temperature sensor 26 positioned at the compressed gas outlet 12 of the second compressor element 10.
    By measuring the pressure and / or temperature at the compressed gas outlet 7 of the first compressor stage 2 and at the compressed gas outlet 12 of the second compressor stage 3 and taking this into account
    BE2018 / 5769 with the requirements of the compressed gas at the level of the user network 4, the speed of the first motor 8 and of the second motor 13 can be determined so that an optimum operating condition of the multistage compressor 1 is maintained.
    In another embodiment according to the present invention, the controller 16 is adapted to receive measurement data from the pressure sensor (s) 23 and / or 24, and / or temperature sensor (s) 10 and / or 26, via a third communication link 19 and a fourth communication link 27.
    In the design of the multi-stage compressor 1, the operating pattern of the compressor 1 is determined by taking into account the parameters of the various compressor elements, their geometric dimensions and the ideal behavior during the gas compression process. A graphical representation or a matrix is thus realized whereby the relationship between the speed of the engine and the pressure at the compressed gas outlet can be found.
    Such a graph or matrix can be used to determine the speed of the first motor 8 and the second motor 13 based on the respective pressure and / or temperature measurements and the requirements for the user network.
    In another embodiment according to the present invention, the controller 16 may further use a graph of the mass flow over pressure of the first compressor element 5 and 30 of the second compressor element 10 to determine the equilibrium state of the multi-stage compressor 1 and the speed of the
    BE2018 / 5769 first motor 8 and second motor 13 so that the equilibrium state is maintained.
    In such a state, the efficiency of the cooling unit 15 is optimum. Moreover, the pressure ratio between the second compressor element 10 and the first compressor element 5 is kept within nominal parameters, which means that the situation in which the pressure difference between the stages would be very high is avoided. Consequently, the temperature of each of the compressor elements 5 and 10 must not rise to very high levels, which would potentially have an effect on the operation of the respective compressor stages 2 and 3.
    Consequently, not only are operating costs reduced, but compressor elements 5 and 10 are also prevented from reaching very high temperatures, very low or very high pressure levels, and the first and second motors 8 and 13 are prevented from running at speeds outside the nominal range.
    In an ideal situation, the equilibrium state is also maintained even when the speed of the first motor 8 and / or the second motor 13 is reduced.
    But in practice, tests have shown that the parameters for which the equilibrium condition is reached shift on the mass flow pressure graph, once the motors experience a speed variation, which can lead to a situation where the pressure at the compressed gas outlet 7 is very high because the first motor is driven at a very low speed.
    This situation is undesirable and the controller 16 helps to control the high pressure values at the compressed gas outlet 7 of the first
    BE2018 / 5769 compressor element 5 and at the compressed gas outlet 12 of the second compressor element 10 by individually adjusting the speed of the first motor 8 and the second motor 13.
    Typically, the first compressor element 5 determines the pressurized gas volume supplied at the user network 4, while the second compressor element 10 determines the pressure of the pressurized gas supplied to the user network 4.
    If the system reaches a situation where the speed of the rotors of the first compressor element 5 is considerably reduced due to a change in demand at the user network and the rotors of the second compressor element 10 are kept at the same speed, the pressure value at the compressed gas outlet can be 7 of the first compressor element 5 and consequently the temperature rise to very high levels.
    The controller 16 prevents this situation by setting the speed of the second motor 13 individually and by taking into account the measurements of the pressure and / or temperature at the compressed gas outlet 7 of the first compressor stage 2.
    By such a speed control, the speed range of the first compressor stage 2 and of the second compressor stage 3 is in fact extended.
    Consequently, when the first motor 8 runs at very low speeds, the pressure and temperature measured at the compressed gas outlet 7 of the first compressor element 5 become very high,
    BE2018 / 5769 where the operating limit is reached or nearly reached. When such a situation occurs, instead of stopping the multi-stage compressor 1, the speed is preferably adjusted at the level of the second compressor stage 3. Consequently, by increasing the speed of the second motor 13, the pressure at the level of the compressed gas outlet 7 of the first compressor element 5 is lowered and the multistage compressor 1 therefore remains within nominal parameters.
    In this way the first motor is allowed to run at speeds that are even lower than the minimum setting, which increases the reliability of the multi-stage compressor 1.
    The same applies if extreme pressure or temperature values are achieved at the compressed gas outlet 12 of the second compressor element 10, then those values are adjusted via an adjustment of the speed of the first motor 8.
    In known compressors, when the first compressor stage is running at low speeds, the pressure measured at the first compressor element increases and the leakage detected at the second compressor element also increases, which is detrimental to the operation of the compressor.
    However, by using a multi-stage compressor 1 according to the present invention, such a situation is avoided.
    Consequently, the first compressor element 5 and second compressor element 10 are driven separately via separate gear transmissions, so that a state of equilibrium between the
    BE2018 / 5769 pressure and the mass flow between the two stages can be maintained by controlling the pressure of the compressed gas at the compressed gas outlet 7 of the first compressor element 5.
    By maintaining the equilibrium state, the multi-stage compressor 1 will be more efficient in terms of power consumption and the compressor stages 2 and 3 will be kept within nominal operating parameters.
    Because the first compressor element 5 and the second compressor element 10 are driven separately by the first motor 8 and the second motor 13 and because the transmission ratio is between two and six, the multi-stage compressor 1 makes use of motors that are easier to control, such motors being better have dynamic control. As a result, the first motor 8 and the second motor 13 are easily kept in a stable operating condition and are controlled more precisely.
    Since the dynamic control of the motors determines the dynamics of the multistage compressor 1 as a whole, the aforementioned multistage compressor 1 can use a simpler software.
    In the context of the present invention, the first communication link 17, the second communication link 18, the third communication link 19 and the fourth communication link 27 can each be selected as a wired or wireless communication link.
    In the case of a wire-bound connection, an electrical wire is provided through which an electrical signal can be sent with at both ends of the wire
    BE2018 / 5769 connector elements to connect the controller 16 and the respective component (s).
    In the case of a wireless connection, a connection between two components comprises a transmitter and a receiver that are in communication with each other and through which an electrical signal can be sent, or each can comprise a transceiver which allows communication in both directions.
    In an embodiment according to the present invention, at least one of the first motor 8 or second motor 13 is an electric motor.
    In yet another embodiment according to the present invention without any limiting character, at least one electric motor is a VSD motor (variable speed motor).
    The challenges and the corresponding speed ranges depend on the size of the electric motor (2). To remedy that dependence, according to a preferred feature of the invention, at least one of the first motor 8 and / or second motor 13 is configured such that the product of the nominal power, in kW, and the square of the nominal speed, in rpm, is in a range between 0.0006x10E12 and 0.025x10E12.
    Typically, motor-related costs decrease as the value of the product increases between the nominal power and the square of the nominal speed. Such a situation occurs until, due to technical limitations, a limit has been reached. If such a limit should be
    BE2018 / 5769, more expensive motors and control systems must be selected.
    In another embodiment of the present invention, at least one of the first motor 8 and / or second motor 13 can be configured such that the product of the maximum power, in kW, and the square of the maximum speed, in rpm, in a range between 0 , 0006x10E12 and 0.025x10E12.
    In another embodiment of the present invention, the first compressor stage 2 and the second compressor stage 3 are received within a housing (not shown).
    In order to limit the footprint of the multistage compressor 1 and improve the gas flow, it is preferable to have at least one of the first compressor element 5 or second compressor element 10 and the first motor 8 or second motor 13 which this at least one first compressor element 5 or second compressor element 10 drives to be directed transversely to the direction 20 of the longest side of the multi-stage compressor 1, and consequently, the longest side of the housing (Figure 3).
    Typically, the motor that drives a compressor element is mounted next to the aforementioned compressor element and in line with it, since the motor will directly drive a rotor of the compressor element. By the gear transmission, the rotation axis of the rotor of the compressor element is shifted from the rotation axis of the rotor of the respective motors, but is held parallel to it.
    The axis of rotation of the compressor element herein determines an axis A-A 'as illustrated in Figure 3.
    BE2018 / 5769
    Preferably, at least one of the aforementioned first compressor stage 2 and second compressor stage 3 is mounted such that the axis A-A 'which they define is positioned transversely of the direction of the longest side of the multi-stage compressor 1.
    Preferably, but without any limiting character, both the first compressor element 5 and the first motor 8 and the second compressor element 10 and the second motor 13 are transverse to the direction of the longest side of the multi-stage compressor 1 and, consequently, the longest side of the housing oriented.
    For reasons of standardization, identical electric motors are preferably used for different compressor elements. In particular, the dimensions of the motors are preferably identical.
    For reasons of electromagnetic compatibility, the frequency converters may be positioned in a first booth 20 and the controller 16 and respective control electronics in a second booth 21. The first and second booths 20 and 21 are preferably positioned side by side on an end face of the multi-stage compressor 1.
    In other words, after mounting, the first box 20 and the second box 21 define an axis B-B 'corresponding to the longest side of the housing. The axis A-A 'is preferably parallel or approximately parallel to the axis B-B'.
    In another embodiment according to the present invention, without any limiting character, the second compressor stage 3 can be mounted parallel to the first compressor stage 2.
    BE2018 / 5769
    In yet another embodiment of the present invention, for improved gas flow through the multi-stage compressor 1, the second compressor stage 3 can be rotated 180 ° with respect to the first compressor stage 2, as illustrated in Figure 6. Consequently, the first motor 8 will be mounted in parallel with the second compressor element 10 and the second motor 13 will be mounted in parallel with the first compressor element 5.
    Such a layout shortens the path of the gas that passes through the multi-stage compressor 1.
    In another embodiment according to the present invention, the first motor 8 and the second motor 13 can be air or liquid cooled.
    Preferably, for the sake of robustness, at least one of the first motor 8 and second motor 13 is liquid-cooled.
    Preferably, but without any limiting character, both the first motor 8 and the second motor 13 are liquid-cooled.
    In a preferred embodiment according to the present invention, but without any limiting character, at least one of the first motor 8 and second motor 13 is cooled with the same liquid as the first compressor element 5 or second compressor element 10 which is driven by said first motor 8 and second respectively engine 13.
    To realize efficient cooling and a compact multi-stage compressor 1 for which a minimum number of components and connecting means is required, at least
    BE2018 / 5769 one engine 8 and / or 13, and the compressor element 5 and / or 10, which are cooled with the same liquid, a cooling circuit comprising the aforementioned liquid, which cooling circuit is configured such that that engine 8 and / or 13, and the associated compressor element 5 and / or 10, are serially cooled.
    Preferably, but without any limiting character, each of the first motor 8 and second motor 13 comprises cooling channels through their motor housing, along the periphery of the aforementioned motor housing, thereby increasing the cooling efficiency.
    Analogously, the compressor housing of each of said first compressor element 5 and second compressor element 10 may comprise cooling channels along the periphery of the respective compressor housing.
    In another embodiment according to the present invention, in order to arrive at an even more compact multi-stage compressor 1, a compressed gas outlet of at least one of the aforementioned first compressor element 5 or second compressor element 10 is connected to the cooling unit 15, and positioned on top of that cooling unit 15.
    In another embodiment of the present invention, the multi-stage compressor 1 further comprises a second cooling unit 22 positioned on the fluid line between the second compressor stage 3 and the user network 4.
    In a further preferred embodiment but without any limiting character, the first compressor element 5 is positioned on top of the cooling unit 15 and the second
    BE2018 / 5769
    compressor element 10 positioned on top of the second
    cooling unit 22.
    Preferably, but without any limiting character, the connection between the first compressor element 5 and the cooling unit 15 and / or the connection between the second compressor element 10 and the second cooling unit 22 is preferably configured as support for the aforementioned first compressor element 5 and / or said second compressor element 10.
    In another embodiment of the present invention, the first motor 8 driving the first compressor element 5 is positioned together with the first compressor element 5 on top of the cooling unit 15.
    Further preferably but without any limiting character, the second motor 13 driving the second compressor element 10, and the second compressor element 10 are positioned on top of the second cooling unit 22.
    Preferably, but not necessarily, the cooling outlet of each of the aforementioned first motor 8 and second motor 13 is connected to a cooling inlet of the aforementioned cooling unit 15 and second cooling unit 22, respectively, or is a cooling inlet of each of the aforementioned first motor 8 and second motor 13 connected to a cooling outlet of the aforementioned cooling unit 15 and second cooling unit 22, respectively.
    In another embodiment of the present invention, the connection between one of the aforementioned first
    BE2018 / 5769 compressor element 5 and / or said second compressor element 10 and the cooling unit 15 designed with the aid of a connecting part 28, wherein said connecting part 28 is configured as support for this first compressor element 5 or second compressor element 10.
    In another preferred embodiment according to the present invention without any limiting character, the aforementioned at least one of the aforementioned first compressor element 5 or second compressor element 10 is connected to the first motor 8 and second motor 13, respectively, by means of a second connecting part, said second connecting part is configured as support for this first compressor element 5 or second compressor element 10. By assuming such a layout, the multi-stage compressor 1 according to the present invention is very compact. Moreover, an easy maintenance procedure can be achieved with an easy, standardized access to the various components.
    In another embodiment according to the present invention, without any limiting character, the multi-stage compressor 1 may comprise two or more compressor elements driven by the first motor 8 and / or by the second motor 13 (not shown).
    By way of example, the first compressor stage 2 may comprise the aforementioned first compressor element 5 and at least one additional compressor element (not shown) connected serially or in parallel to the first compressor element 5.
    BE2018 / 5769
    Analogously, the second compressor stage 3 may comprise the aforementioned second compressor element 10 which is serially or parallel connected to at least one additional compressor element (not shown).
    Another possibility is that the multi-stage compressor 1 comprises a connection to a first user network, which first user network receives compressed gas from a branch connection of the compressed gas outlet 7 of the first compressor stage 2, for example.
    While another user network would receive press gas from a branch connection of the press gas outlet 12 of the second compressor stage 3.
    The operation of the multi-stage compressor 1 is very simple and as follows.
    The multi-stage compressor 1 is switched on and the first motor 8 and the second motor 13 rotate the rotors of the first compressor element 5 via the first gear transmission 9 and the rotors of the second compressor element 10 via the second gear transmission 14 at a respective speed selected by the controller 16 so that the demand to the user network 4 is met.
    The compressed gas outlet 7 of the first compressor stage 2 is preferably connected to an inlet of a cooling unit 15 and a gas outlet of the cooling unit 15 is connected to an inlet 11 of the second compressor element 10.
    BE2018 / 5769
    The pressure at the compressed gas outlet 7 of the first compressor stage 2 and at the compressed gas outlet 12 of the second compressor stage 3 is measured with the aid of a first pressure sensor 23 and a second pressure sensor 24, respectively, in step 100 of FIG.
    7, and sent to the controller 16 via the third communication link 19.
    In an embodiment according to the present invention, the controller 16 is preferably able to control the speed of the first motor 8 on the basis of the pressure measured at the compressed gas outlet 12 of the second compressor stage 3 and the speed of the second motor 13 on the basis of of the pressure measured at the compressed gas outlet 7 of the first compressor stage 2.
    The controller 16 will, in step 101, compare the pressure measured at the compressed gas outlet 12 of the second compressor stage 3 from step 124 with a first reference pressure from step 102 corresponding to the required pressure at the compressed gas outlet 12 of the second compressor element 10 and, consequently, the desired pressure on the user network 4.
    If the comparison shows that the two values are different, the controller 16 determines the speed of the first motor
    8, in step 103 and generates an electrical signal via the first communication link 17 to the frequency converter of the first compressor stage 2, and controls the speed of the first motor 8 in step 104.
    On the basis of the first reference pressure 102, the controller 16 identifies in step 105 a second reference pressure, 104, at the level of the cooling unit 15, on the basis of the
    BE2018 / 5769 operating pattern of the multi-stage compressor 1, determined during design.
    It goes without saying that the controller 16 comprises a processor (not shown) capable of performing calculations and a memory unit (not shown) on which various data and calculations can be stored.
    Preferably, the operating pattern of the multi-stage compressor 1 can be stored on the memory unit before the compressor 1 leaves the factory, or can be stored thereon at any time after the compressor 1 has left the factory.
    The identified second reference pressure, step 104, is then compared to the pressure measured at the compressed gas outlet 7 of the first compressor stage 2, in step 123. If the result of the comparison shows that the two values are different, the controller 16 preferably determines the speed of the second motor 13, in step 106, and generates an electrical signal via the second communication link 18 to the frequency converter of the second compressor stage 3, and controls the speed of the first motor 13 in step 107.
    The speed control is understood to mean that the electrical signal generated by the controller 16 determines the respective frequency converter to increase or decrease the speed of the first motor 8 and second motor 13, respectively, so that the first reference pressure and / or the second reference pressure are achieved.
    BE2018 / 5769
    The second reference pressure is preferably selected by the controller 16 such that an equilibrium state between the first compressor stage 2 and the second compressor stage 3 is maintained.
    In a preferred embodiment according to the present invention without any limiting character, the controller 16 comprises a Proportionally Integrating (PI) controller for determining the required speed of the first motor 8 and / or the second motor 13.
    In another embodiment of the present invention, the controller 16 may comprise two PI controllers, each used to determine the speed of the first motor 8 and the second motor 13, respectively.
    These controllers perform the calculations in steps 103 and 106.
    In another embodiment according to the present invention, without any limiting character, the method further comprises the step of controlling the speed of the second motor 13 by multiplying the speed of the first motor 8 by a predetermined gain factor, in step 108 .
    The predetermined gain factor is herein determined as a function of the operating pattern of the multi-stage compressor 1.
    In yet another embodiment without any limiting character, the method further comprises the step of controlling the speed of the second motor 13 by multiplying the speed of the first motor 8 by a calculated gain factor calculated by the predetermined
    BE2018 / 5769 gain factor corresponding to an ideal situation to be added to a certain gain factor calculated by a PI controller based on the measurements of the multi-stage compressor 1.
    The predetermined gain is hereby calculated as a function of the speed of the first motor 8 and the desired pressure on the user network 4, taking into account the behavior of the multi-stage compressor 1 according to an ideal situation and on the basis of a theoretical calculation model of the multi-stage compressor 1.
    Whereas the determined amplification factor is calculated as a function of the speed of the first motor 8 and the desired pressure on the user network 4, taking into account the real behavior of the multi-stage compressor 1.
    By implementing such a method, the speed of the second motor 13 is determined more accurately. Consequently, an equilibrium state of the multi-stage compressor 1 is maintained during its operation.
    Depending on the design of the multi-stage compressor 1, the multi-stage compressor 1 may comprise some or even all of the technical features described herein, in any combination without departing from the scope of the invention.
    Technical characteristics are understood as a minimum: the serial connection between the compressor stages, the number of compressors included in each compressor stage and its connection, the first and second compressor elements 5 and 10 can be selected as a screw or tooth compressor element, or
    BE2018 / 5769 oil-free or oil-injected, each of the first motor 8 and second motor 13 includes a frequency converter, the use of the operating pattern, the use of a mass flow graph over pressure, at least one of the first motor 8 or second motor 13. an electric motor, at least one of the electric motors is a variable speed motor (VSD), the positioning of the compressor element and the motor on top of the respective cooling unit 15 and / or 22, the multi-stage compressor 1 comprises: the cooling unit 15, the second cooling unit 22, the controller 16, the first communication link 17, the second communication link 18, the first pressure sensor 23, the first temperature sensor 25, the second pressure sensor 24, the second temperature sensor 26, the third communication link 19, the fourth communication link 27, the connecting part 28 , etc.
    The present invention is by no means limited to the embodiments described as examples and shown in the figures, but a multi-stage compressor according to the present invention can be realized in all shapes and sizes without departing from the scope of the invention.
    权利要求:
    Claims (29)
    [1]
    Conclusions
    A multi-stage compressor (1) comprising an inlet (6) and a compressed gas outlet (12), at least a first compressor stage (2) comprising a first compressor element (5) driven by a first motor (8) via a first gear transmission (9) ) and a second compressor stage (3) comprising a second compressor element (10) driven by a second motor (13) via a separate second gear transmission (14), each of said first and second gear transmissions (9, 14) comprising a drive gear connected to the first motor (8) and the second motor (13), respectively, and a driven gear configured as a multiplier, each of the aforementioned driven gears being connected to a shaft of a rotor of said first compressor element (5) second compressor element (10), respectively, wherein the first motor (8) and the second motor (13) are adapted to separately drive the first compressor stage (2) and the second compressor stage (3) characterized in that the gear ratio between the driven gear and the driving gear of each of the aforementioned first gear transmission (9) and second gear transmission (14) is between two and six.
    [2]
    The multi-stage compressor according to claim 1, further comprising a cooling unit (15) for cooling a compressed gas exiting the first compressor element (5) or the second compressor element (10).
    [3]
    The multi-stage compressor according to claim 2, further comprising a controller (16) connected to the first motor (8) via a
    BE2018 / 5769 first communication link (17) and with the second motor (13) via a second communication link (18).
    [4]
    Multistage compressor according to claim 3, characterized in that the multistage compressor (1) comprises a first pressure sensor and / or a first temperature sensor positioned on the compressed gas outlet (7) of the first compressor element (5) and a second pressure sensor and / or a second temperature sensor positioned at the compressed gas outlet (12) of the second compressor element (10) and the controller (16) is adapted to receive measurement data from the aforementioned pressure sensor (s) and / or temperature sensor (s) via a third communication link (19).
    [5]
    Multistage compressor according to one of claims 1 to 4, characterized in that at least one of the aforementioned first motor (8) or second motor (13) is an electric motor.
    [6]
    Multi-stage compressor according to claim 5, characterized in that the at least one electric motor is a VSD motor.
    [7]
    Multi-stage compressor according to one of claims 1 to 6, characterized in that at least one of the aforementioned first motor (8) and / or second motor (13) is configured such that the product of the nominal power, in kW, and the squared of the nominal speed, in rpm, is in a range between 0.0006x10E12 and 0.025x100E12.
    [8]
    The multi-stage compressor according to any one of claims 1 to 6, wherein at least one of said motors is configured such that the product of the maximum power,
    BE2018 / 5769 kW, and the square of the maximum speed, in rpm, is in a range between 0.0006x10E12 and 0.025x10E12.
    [9]
    Multistage compressor according to one of claims 1 to 8, characterized in that at least one of the aforementioned compressor elements (5, 10) and the motor (8, 13) which drives this at least one compressor element (5, 10) transversely to the direction of the longest side of the multi-stage compressor (1).
    [10]
    Multi-stage compressor according to claim 5, characterized in that the at least two electric motors are identical or virtually identical in terms of dimensions.
    [11]
    The multi-stage compressor according to any one of claims 1 to 10, characterized in that said multi-stage compressor (1) further comprises a first box (20) which comprises one or more frequency converters, and a second box (21) comprising control electronics, the aforementioned first and second boxes (20, 21) are separated from each other.
    [12]
    The multi-stage compressor according to claim 11, characterized in that said first and second boxes (20, 21) are positioned side by side on an end face of the multi-stage compressor (1).
    [13]
    The multi-stage compressor according to one of claims 1 to 12, characterized in that at least one of the aforementioned first motor (8) and / or second motor (13) is liquid-cooled.
    BE2018 / 5769
    [14]
    Multi-stage compressor according to one of claims 1 to 13, characterized in that at least one of the aforementioned first motor (8) or second motor (13) is cooled with the same liquid axis as the first compressor element (5) or second compressor element (10) that is driven by said first motor (8) or second motor (13).
    [15]
    The multi-stage compressor according to claim 14, characterized in that the at least one motor (8, 13) and the compressor element (5, 10) which are cooled with the same liquid comprise a cooling circuit comprising said liquid, which cooling circuit is configured such that that motor (8, 13) and the associated compressor element (5, 10) are serially cooled.
    [16]
    Multi-stage compressor according to one of claims 1 to 15, characterized in that a compressed gas outlet (7, 12) of at least one of the aforementioned first compressor element (5) or second compressor element (10) is connected to a cooling unit (15), and positioned on top of that cooling unit (15).
    [17]
    The multi-stage compressor according to claim 16, characterized in that the connection between one of said first compressor element (5) and / or said second compressor element (10) and the cooling unit (15) is realized with the aid of a connecting part (28), wherein said connecting part (28) is configured as support for this first compressor element (5) or second compressor element (10).
    BE2018 / 5769
    [18]
    Multi-stage compressor according to claim 16 or 17, characterized in that the first motor (8) driving the first compressor element (5) is positioned together with the first compressor element (5) on top of the cooling unit (15)
    5 and / or that the second motor (13) driving the second compressor element (10) and the second compressor element (10) are positioned on top of the second cooling unit (22).
    [19]
    19. - Multi-stage compressor according to claim 18, thereby
    10 characterized in that said at least one of said first compressor element (5) or second compressor element (10) is connected to the respective first motor (8) or second motor (13) by means of a second connection part, which second connection part is configured as support of this
    First compressor element (5) or second compressor element (10).
    [20]
    20. The multi-stage compressor as claimed in claim 15, characterized in that a cooling outlet of at least one of said first engine (5) or second engine (13) which is serially
    20 is cooled with at least one of the aforementioned first compressor element (5) or second compressor element (10), is connected to a cooling inlet of a cooling unit (15, 22).
    [21]
    A multi-stage compressor according to claim 15, thereby
    Characterized in that a cooling inlet of the at least one of said first engine (8) or second engine (13) serially cooled with at least one of said first compressor element (5) or second compressor element (10) is connected to a cooling outlet of a cooling unit (15, 22).
    BE2018 / 5769
    [22]
    Multi-stage compressor according to one of the preceding claims, characterized in that the multi-stage compressor (1) is an oil-free screw compressor.
    [23]
    A multi-stage compressor comprising at least a first compressor element (5) and a second compressor element (10) and at least a first motor (8) and a second motor (13) for driving, each separately, a different one from the aforementioned first compressor element ( 5) and second compressor element (10) via a separate first gear transmission (9) and second gear transmission (14), each of said first gear transmission and second gear transmission (14) comprising a drive gear connected to one of said first motor ( 8) and second motor (13), respectively, and a driven gear connected to a shaft of a rotor of one of the aforementioned first compressor element (5) or second compressor element (10), wherein the ratio between the number of teeth of the drive gear and the number of teeth of the driven gear of one of the aforementioned first gear transmission (9) and second gear transmission (14) between two and six lines gt.
    [24]
    A method for controlling the speed of the motors of a multi-stage compressor (1), wherein the method comprises the following steps:
    - providing a first compressor stage (2) which comprises a first compressor element (5) and drives said first compressor element (5) by means of a first motor (8) via a first gear transmission (9);
    - providing a second compressor stage (3) which comprises a second compressor element (10) and said second compressor element (10) separately from the first compressor element
    BE2018 / 5769 (5) drives by means of a second motor (13) via a separate second gear transmission (14);
    - connecting a drive gear of each of the first gear transmission (9) and second gear transmission (14) to the first motor (8) and second motor (13), respectively;
    - connecting a driven gear of each of the first gear transmission (9) and second gear transmission (14) to a shaft of a rotor of said first compressor element (5) and second compressor element (10);
    characterized in that the method further comprises the step of adjusting the gear ratio between the drive gear and the driven gear of each of said first gear transmission (9) and second gear transmission (14) between two and six.
    [25]
    The method of claim 24, further comprising the step of connecting a compressed gas outlet (7) of the first compressor stage (2) to an inlet of a cooling unit (15) and a gas outlet of the cooling unit (15) to an inlet ( 11) from the second compressor stage (3) and measuring the pressure at the pressurized gas outlet (7) of the first compressor stage (2) and at the pressurized gas outlet (12) of the second compressor stage (3).
    [26]
    The method of claim 25, further comprising the step of controlling the speed of the first engine (8) based on the pressure measured at the compressed gas outlet (12) of the second compressor stage (3) and the speed of the second motor (13) based on the pressure measured at the compressed gas outlet (7) of the first compressor stage (2).
    BE2018 / 5769
    [27]
    The method of claim 26, further comprising the steps of:
    - comparing the measured pressure at the compressed gas outlet (12) of the second compressor stage (3) with a first reference pressure corresponding to the required pressure at the compressed gas outlet of the multi-stage compressor (1) and if the result of the comparison shows that the two values are different, controlling the speed of the first motor (8); and / or
    - comparing the measured pressure at the compressed gas outlet (7) of the first compressor stage (2) with a second reference pressure corresponding to a desired pressure value at the cooling unit (15) and if the result of the comparison shows that the two values are different, controlling the speed of the second motor (13).
    [28]
    The method of any one of claims 25 to 27, further comprising the step of controlling the speed of the second motor (13) by multiplying the speed of the first motor (8) by a predetermined gain.
    [29]
    The method of claim 28, further comprising the step of controlling the speed of the second motor (13) by multiplying the speed of the first motor (8) by a calculated gain factor, calculated by the predetermined gain factor corresponding to with an ideal situation to add to a certain gain factor calculated by a PI controller on the basis of the measurements of the multi-stage compressor (1).
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    同族专利:
    公开号 | 公开日
    KR20200142532A|2020-12-22|
    JP2021521370A|2021-08-26|
    BR112020020691A2|2021-01-12|
    BE1026205A1|2019-11-06|
    CN209856028U|2019-12-27|
    US20210102554A1|2021-04-08|
    EP3775557B1|2022-01-19|
    EP3775557A1|2021-02-17|
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    法律状态:
    2019-12-13| FG| Patent granted|Effective date: 20191112 |
    优先权:
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    US201862656472P| true| 2018-04-12|2018-04-12|
    US62656472|2018-04-12|
    US201862724677P| true| 2018-08-30|2018-08-30|EP19704685.7A| EP3775557B1|2018-04-12|2019-02-11|Multi-stage compressor unit and method for adjusting the rotational speed of the motors|
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