WO2013083000A1 - 一种磁悬浮分子泵动平衡方法(5) - Google Patents
一种磁悬浮分子泵动平衡方法(5) Download PDFInfo
- Publication number
- WO2013083000A1 WO2013083000A1 PCT/CN2012/085077 CN2012085077W WO2013083000A1 WO 2013083000 A1 WO2013083000 A1 WO 2013083000A1 CN 2012085077 W CN2012085077 W CN 2012085077W WO 2013083000 A1 WO2013083000 A1 WO 2013083000A1
- Authority
- WO
- WIPO (PCT)
- Prior art keywords
- rotor
- speed
- radial
- vibration
- molecular pump
- Prior art date
- Legal status (The legal status 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 status listed.)
- Ceased
Links
Classifications
-
- H—ELECTRICITY
- H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
- H02K—DYNAMO-ELECTRIC MACHINES
- H02K15/00—Processes or apparatus specially adapted for manufacturing, assembling, maintaining or repairing of dynamo-electric machines
- H02K15/16—Centring rotors within the stators
- H02K15/165—Balancing the rotors
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D27/00—Control, e.g. regulation, of pumps, pumping installations or pumping systems specially adapted for elastic fluids
- F04D27/02—Surge control
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D19/00—Axial-flow pumps
- F04D19/02—Multi-stage pumps
- F04D19/04—Multi-stage pumps specially adapted to the production of a high vacuum, e.g. molecular pumps
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D19/00—Axial-flow pumps
- F04D19/02—Multi-stage pumps
- F04D19/04—Multi-stage pumps specially adapted to the production of a high vacuum, e.g. molecular pumps
- F04D19/042—Turbomolecular vacuum pumps
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D29/00—Details, component parts, or accessories
- F04D29/05—Shafts or bearings, or assemblies thereof, specially adapted for elastic fluid pumps
- F04D29/056—Bearings
- F04D29/058—Bearings magnetic; electromagnetic
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D29/00—Details, component parts, or accessories
- F04D29/66—Combating cavitation, whirls, noise, vibration or the like; Balancing
- F04D29/661—Combating cavitation, whirls, noise, vibration or the like; Balancing especially adapted for elastic fluid pumps
- F04D29/662—Balancing of rotors
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
- F16C32/00—Bearings not otherwise provided for
- F16C32/04—Bearings not otherwise provided for using magnetic or electric supporting means
- F16C32/0406—Magnetic bearings
- F16C32/044—Active magnetic bearings
- F16C32/0442—Active magnetic bearings with devices affected by abnormal, undesired or non-standard conditions such as shock-load, power outage, start-up or touchdown
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01M—TESTING STATIC OR DYNAMIC BALANCE OF MACHINES OR STRUCTURES; TESTING OF STRUCTURES OR APPARATUS, NOT OTHERWISE PROVIDED FOR
- G01M1/00—Testing static or dynamic balance of machines or structures
- G01M1/14—Determining imbalance
- G01M1/16—Determining imbalance by oscillating or rotating the body to be tested
- G01M1/20—Determining imbalance by oscillating or rotating the body to be tested and applying external forces compensating forces due to imbalance
-
- H—ELECTRICITY
- H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
- H02K—DYNAMO-ELECTRIC MACHINES
- H02K7/00—Arrangements for handling mechanical energy structurally associated with dynamo-electric machines, e.g. structural association with mechanical driving motors or auxiliary dynamo-electric machines
- H02K7/08—Structural association with bearings
- H02K7/09—Structural association with bearings with magnetic bearings
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
- F16C2231/00—Running-in; Initial operation
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
- F16C2360/00—Engines or pumps
- F16C2360/44—Centrifugal pumps
- F16C2360/45—Turbo-molecular pumps
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
- F16C32/00—Bearings not otherwise provided for
- F16C32/04—Bearings not otherwise provided for using magnetic or electric supporting means
- F16C32/0406—Magnetic bearings
- F16C32/044—Active magnetic bearings
- F16C32/0444—Details of devices to control the actuation of the electromagnets
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T29/00—Metal working
- Y10T29/49—Method of mechanical manufacture
- Y10T29/49002—Electrical device making
- Y10T29/49004—Electrical device making including measuring or testing of device or component part
Definitions
- the present invention relates to the field of vacuum acquisition equipment, and more particularly to a magnetic suspension molecular pump balancing method. Background technique
- the molecular pump is a vacuum pump that uses a high-speed rotating rotor to transmit momentum to gas molecules to obtain a directional velocity, so that the gas is compressed and driven to the exhaust port, and then pumped away by the foreline pump.
- the magnetic suspension molecular pump is a molecular pump that uses a magnetic bearing (also called an active magnetic suspension bearing) as a molecular pump rotor. It uses a magnetic bearing to stably suspend the rotor in the air, so that there is no mechanical between the rotor and the stator during high-speed operation. Contact, with no mechanical wear, low energy consumption, high allowable speed, low noise, long life, no lubrication, etc.
- the internal structure of the magnetic levitation molecular pump is as shown in Fig. 1.
- the rotor of the magnetic levitation molecular pump includes a rotor shaft 7 and an impeller 1 fixedly coupled to the rotor shaft 7.
- the impeller 1 is fixedly mounted on an upper portion of the rotor shaft 7; the rotor shaft 7 is sleeved with a first radial magnetic bearing 6, a motor 8 and a second radial magnetic bearing 9 and the like.
- the devices together form the rotor shafting of the magnetic suspension molecular pump.
- unbalanced mass refers to the mass at a specific radius of the rotor, and the product of the mass and the centripetal acceleration is equal to Unbalanced centrifugal force.
- unbalanced mass is much larger than 10 mg, the unbalanced mass will cause a significant eccentric moment of the center of gravity of the rotor and the axis.
- the centrifugal inertia caused by the unbalanced mass of the rotor causes lateral mechanical vibration of the rotor (usually radial vibration), which affects the normal operation of the system.
- the magnetic suspension molecular pump rotor The normal working speed is in the high speed zone exceeding the critical speed of the rotor.
- the unbalanced mass mentioned above also causes the rotor speed to not rise directly to its working speed and cannot work normally.
- the rotor rigid critical speed refers to the corresponding rotational speed when the rotor rotational frequency is equal to the rigid resonant frequency of the rotor bearing system; and the high speed region exceeding the rigid critical rotational speed may be referred to as the ultra-rigid critical rotational speed region.
- the kind is force free control
- the basic idea is to generate a compensation signal with the same phase and same amplitude as the rotor displacement/vibration signal, which is used to cancel the same frequency signal of the rotor vibration, so that the controller can synchronously vibrate.
- the signal is not responsive; the other is open loop feed forward contro l (or force control).
- the basic idea is to extract the co-frequency vibration component of the rotor vibration signal and then control it by another feedforward.
- a corresponding control signal is generated and superimposed on the control signal of the main controller.
- a magnetic field is disclosed in Chinese Patent Publication No. CN101261496A.
- High-precision active vibration control system for suspension flywheel including displacement sensor, current sensor, magnetic bearing controller and magnetic bearing power amplifier.
- the magnetic bearing controller includes stability controller, eccentricity estimation, magnetic compensation and action switch.
- the patent is in stable control.
- the eccentricity estimation and the magnetic compensation are introduced, and the unbalanced vibration parameters of the flywheel are used to compensate the unbalanced amount and the negative displacement of the flywheel in the whole rotational speed range, thereby realizing the unbalanced vibration control of the flywheel in the entire rotational speed range, so that the flywheel is In the whole process of ascending and descending speed, the spindle can be operated with high precision.
- the Chinese patent document CN 101046692A discloses a high-precision unbalance vibration control system for a magnetic suspension reaction flywheel open-loop, including a displacement sensor and a displacement signal interface circuit. , rotation speed detecting device, magnetic bearing controller, magnetic bearing power amplification driving circuit and flywheel position identification device.
- Magnetic bearing controller includes axial magnetic bearing controller and radial magnetic bearing controller, radial magnetic bearing controller is controlled by stability And unbalanced vibration
- the controller consists of two parts, in which the unbalanced vibration controller compensates the displacement feedback of the stability controller. On the basis of the stability control, the unbalanced vibration control is introduced, and the flywheel unbalanced vibration parameters identified by the flywheel at high speed are combined with the flywheel.
- the position of the flywheel rotor obtained by the position discriminating device, the entire speed of the flywheel The high-precision unbalanced vibration control of the open-loop is carried out to realize the unbalanced vibration control of the flywheel in the whole speed range, so that the flywheel can operate with high precision during the whole process of raising and lowering.
- the above two patent documents are specific applications of the "unbalanced vibration control method". However, due to the limited adjustment control force of the "unbalanced vibration control method", the rotation can be suppressed only when the unbalanced mass of the rotating body is within a certain threshold range.
- the unbalanced vibration of the body that is, the "unbalanced vibration control method” cannot completely solve the problem of rotor vibration caused by the presence of unbalanced mass. Therefore, when the rotor has a large unbalanced mass, the "unbalanced vibration control method” cannot be used to achieve rotor vibration suppression, and the rotor speed directly exceeds the rigid critical speed to reach its normal operating speed.
- the rotor after the magnetic suspension molecular pump is assembled, the rotor must be dynamically balanced.
- the so-called "dynamic balance" means that the rotor with unbalanced mass is corrected and the unbalanced mass is corrected after measuring the magnitude and phase of the unbalanced mass.
- a dynamic balancing machine is usually used to perform dynamic balancing operation on the rotor. The operation process is as follows: First, the rotor is rotated at a low speed (ie, a speed range below the rotor critical speed), and the dynamic balancing machine is utilized at a low speed.
- the rotor is dynamically balanced, and then the rotor is subjected to weighting or de-weighing balancing processing to initially eliminate the unbalanced mass. Then the above steps are repeated several times to make the rotor speed break through the rotor rigid critical speed and enter the super-rigid critical speed zone. After the speed enters the ultra-rigid critical speed zone, the rotor is dynamically balanced by the dynamic balancing machine at high speed, and then the rotor is subjected to weighting or de-weighing balancing processing. Moreover, in order to accurately remove the unbalanced mass, the above dynamic balancing operation is usually repeated several times.
- the working speed of the magnetic suspension molecular pump rotor is in the ultra-rigid critical speed range. Our concern is the performance of the high-speed rotor. Therefore, the dynamic balance effect at low speed is limited, only when the rotor speed exceeds and leaves the rotor rigid critical speed. After a certain distance (into the ultra-rigid critical speed zone), the rotor will rotate approximately around its center of mass. At this point, the dynamic balance is more accurate and better results can be obtained. However, because the rotor with unbalanced mass can't directly increase to the super-rigid critical speed, it can't be directly balanced at high speed. Therefore, it must first be dynamically balanced at low speed to gradually increase the speed to the ultra-rigid critical speed zone.
- the technical problem to be solved by the present invention is that the dynamic balance method of the magnetic suspension molecular pump in the prior art has complicated steps and low efficiency, thereby providing a dynamic balancing operation of the rotor of the magnetic suspension molecular pump directly at a high speed. High efficiency, no need to use dynamic balancing machine, low cost magnetic suspension molecular pump balancing method.
- the technical solution adopted by the present invention is as follows: The above technical solution of the present invention has the following advantages over the prior art:
- the magnetic suspension molecular pump dynamic balance method provided by the invention, after starting the magnetic suspension molecular pump motor, the opening force free unbalance vibration control module, wherein the force free unbalance vibration control module uses a force free imbalance control algorithm, which can basically eliminate The same frequency component in the current is controlled to suppress the co-frequency vibration of the rotor, so that the rotor rotates around the center of mass, and the force free unbalance control can ensure that the excitation current of the coil output is small, and the requirement for the power amplifier is relatively low.
- the force free unbalanced vibration control module can suppress the co-frequency vibration of the rotor so that the rotor speed can quickly exceed its rigid critical speed, and the rotor of the magnetic suspension molecular pump is dynamically balanced at a higher speed.
- the operation steps can perform dynamic balancing operation quickly and efficiently, which greatly improves the efficiency of dynamic balance and has a good balance effect.
- the dynamic balance method of the magnetic suspension molecular pump provided by the invention does not need to additionally use the dynamic balance instrument, and is measured by the first radial sensor and the second radial sensor which are provided by the invention, and the equipment is reduced, thereby reducing the cost. Increased the value of the product.
- the magnetic suspension molecular pump dynamic balance method provided by the invention can complete the calculation of the required balance quality and balance mass loading phase of the rotor by using the dynamic balance module built in the controller, and the dynamic balancing machine is no longer needed, thereby saving cost.
- the two balance surfaces are disposed at a position away from the center of the rotor and close to both ends, so that when a compensation vector is added, a large torque can be generated to improve the balance efficiency.
- the magnetic suspension molecular pump dynamic balance method provided by the present invention, wherein the preset non-rated speed vibration threshold is 40 ⁇ m, which can meet the vibration requirement of the rotor radial amplitude at a non-rated speed, so that the rotor can speed up relatively smoothly until The rated speed is reached.
- the preset rated speed vibration threshold is Q.
- the preset unbalanced mass is 10mg.
- FIG. 2 is a schematic diagram of a force free unbalance vibration control algorithm in the present invention
- FIG. 3 is a flow chart of the dynamic balancing method of the present invention.
- FIG. 4 is a flow chart of the dynamic balance using the influence coefficient method in the present invention.
- the reference numerals in the figure are indicated as: 1-impeller, 2-magnetic suspension molecular pump controller, 3-pump body, 4- first radial protection bearing, 5-first radial sensor, 6-first radial magnetic bearing , 7-rotor shaft, 8-motor, 9-second radial magnetic bearing, 10-second radial sensor, 11-second radial protection bearing, 12-axial protection bearing, 13-first axial magnetic Bearing, 14-thrust disk, 15-second axial magnetic bearing, 16-axial sensor, 17-terminal, 18-displacement detection device, 19-speed detection device. detailed description
- FIG. 1 it is a schematic structural view of a magnetic suspension molecular pump according to the present invention.
- the magnetic suspension molecular pump is vertically disposed, and the magnetic suspension molecular pump includes a pump body 3 and is disposed in the pump body 3 .
- the rotor shaft system includes a rotor, a first radial magnetic bearing 6, a second radial magnetic bearing 9, a first axial magnetic shaft 7
- the rotor includes a rotor A shaft 7, an impeller 1 fixed to the rotor shaft 7, and a fitting member for fixing the impeller 1, such as a screw, a nut, or the like.
- the axis of the rotor shaft is disposed in a vertical direction, and the impeller 1 is fixedly disposed at an upper portion of the rotor shaft 7.
- the lower portion of the rotor shaft 7 is provided with the first axial magnetic bearing 13 , the second axial magnetic bearing 15 , the thrust disk 14 and the axial protection bearing 12 and for detecting the axial displacement signal of the rotor Axial sensor 16.
- the rotor shaft 7 is sleeved with a first radial protection bearing 4, a first radial sensor 5, a first radial magnetic bearing 6, a motor 8, a second radial magnetic bearing 9, and a second diameter.
- a device such as a sensor 10 and a second radial protection bearing 11 is provided.
- the first radial protection bearing 4 and the second radial protection bearing 11 are coaxial and have the same radial dimension.
- the first radial magnetic bearing 6 includes a first radial magnetic bearing stator and a first radial magnetic bearing rotor, the first radial magnetic bearing stator being fixedly coupled to the pump body 3, the first radial direction A magnetic bearing rotor is fixedly coupled to the rotor shaft 7; the first radial sensor 5 is for detecting a radial displacement signal of the rotor at the first radial sensor 5.
- the second radial magnetic bearing 9 includes a second radial magnetic bearing stator and a second radial magnetic bearing rotor, the second radial magnetic bearing stator is fixedly coupled to the pump body 3, the second radial direction A magnetic bearing rotor is fixedly coupled to the rotor shaft 7; the second radial sensor 10 is for detecting a radial displacement signal of the rotor at the second radial sensor 10.
- the rotor shaft 7 is supported by the first radial magnetic bearing 6, the second radial magnetic bearing 9, the first axial magnetic bearing 13 and the second axial magnetic bearing 15.
- the control system of the magnetic levitation molecular pump comprises a displacement detecting device 18, a rotational speed detecting device 19 and a magnetic levitation molecular pump controller 2; the displacement detecting device 18 is configured to receive a displacement signal, the signal input end thereof and the first radial sensor 5.
- the second radial sensor 10 and the signal output end of the axial sensor 16 are connected, and the signal output end of the displacement detecting device 18 is connected to the signal input end of the magnetic levitation molecular pump controller 2;
- the rotation speed detecting device 19 is configured to detect a rotor speed signal, and a signal input end thereof is connected to the rotation speed detecting sensor through a connection terminal 17 of the magnetic levitation molecular pump, and a signal output end of the rotation speed detecting device 19 and the magnetic levitation molecular pump controller 2 The signal input is connected.
- the magnetic suspension molecular pump controller 1 has various control algorithm modules built therein, and the magnetic suspension molecular pump The controller 2 can call an appropriate control algorithm to perform an analysis operation according to the displacement signal obtained by the displacement detecting device 18, and finally drive the corresponding magnetic bearing (the first radial magnetic bearing 6, the second radial magnetic bearing) 9.
- One or more of the first axial magnetic bearing 13 and the second axial magnetic bearing 15 output electromagnetic force to exert control on the motion of the rotor.
- the magnetic levitation molecular pump controller 1 can also monitor the rotation of the rotor in real time according to the rotational speed signal obtained by the rotational speed detecting device 19, and adjust the rotational speed of the rotor as needed.
- the magnetic suspension molecular pump controller 1 also has a built-in force free unbalance vibration control module and a dynamic balance module.
- the force free unbalance vibration control module uses a force free imbalance control algorithm, which substantially eliminates the same frequency component in the control current, suppresses the co-frequency vibration of the rotor, and surrounds the rotor around the mass center. Rotate, as shown in Figure 2.
- the method can ensure that the excitation current of the coil output is small, and is suitable for the case where the requirement of the power amplifier is relatively low.
- the dynamic balance module is configured to calculate a balance phase of the rotor and a load phase of the balance mass.
- the dynamic balance module uses the influence coefficient method used for the balance of the rigid rotor to obtain the imbalance of the rotor. quality.
- the magnetic suspension molecular pump needs to be dynamically balanced to remove the unbalanced mass of the rotor.
- the rigid critical speed and the rated rotational speed of the rotor are known.
- the dynamic balancing method includes:
- the force free unbalance vibration control module adopts force free unbalance vibration Control algorithm.
- the displacement detecting device 18 passes The first radial sensor 5 and the second radial sensor 10 acquire a radial amplitude of the rotor.
- the unbalanced vibration control module can suppress the co-frequency vibration of the rotor, and the rotor speed exceeds its rigid critical speed, and step 2 is sequentially performed. If the maximum radial amplitude of the rotor exceeds 1 /2 of the protection gap, the traditional dynamic balancing method is adopted, firstly, the low-speed dynamic balance is performed to ensure that the radial vibration of the rotor does not exceed the protection gap during the rotor speed exceeding the rigid critical speed. /2 ; then the rotor speed exceeds its rigid critical turn After the speed, perform step 2 in sequence.
- the predetermined non-rated speed vibration threshold is in the range of [20 ⁇ m, 40 ⁇ m]. In the embodiment, the preset non-rated speed vibration threshold is 40 ⁇ m.
- the rotational speed detecting means 19 is controlled by the magnetic levitation molecular pump controller 2 to detect the rotational speed of the rotor at this time.
- the rotational speed detecting means 19 collects the rotational speed of the rotor by the rotational speed detecting sensor. Determine if the speed is less than the rated speed of the rotor. If it is less, execute step 3 in sequence. Otherwise, perform step 5.
- the rotor is pre-arranged with two balance surfaces, respectively disposed at an upper portion and a lower portion near the center of the rotor and near the ends of the rotor.
- the magnetic suspension molecular pump controller (2) is according to the time.
- the radial amplitude and rotational speed of the rotor, the dynamic balance module is called, and the initial imbalance vector V measured by the first radial sensor and the second radial sensor at this time is recorded. ;
- M 2 is the initial unbalanced mass corresponding to the two unbalanced surfaces, and the influence coefficient matrix T is calculated according to the influence coefficient method, that is,
- V! T [M!+ni! ⁇ 2 ] ⁇
- step 3e reducing the rotor speed to 0, and performing a weighting or de-weighting dynamic balancing operation on the two unbalanced surfaces according to the respective initial unbalanced masses calculated in step 3d);
- step 3f restarting the magnetic levitation molecular pump again, detecting whether the vibration amount of the rotor is less than a preset non-rated rotational speed vibration amplitude when the rotor rotational speed is reached, and if the vibration amplitude is less than the preset non-rated rotational speed vibration amplitude, After the dynamic balance is completed, proceed to the next step. Otherwise, repeat steps 3a) -3f) until the rotor speed is reached, the detected vibration amount of the rotor is less than the preset non-rated speed vibration amplitude, and then step 4 is performed in sequence.
- the rotor speed is the dynamic speed balancing operation of the rated speed, so that the rotor rotational speed is increased from zero to the process, and the radial vibration amplitude of the rotor is less than the preset non-rated The rotational speed vibration threshold; and when the rotor rotational speed is set, the radial vibration amplitude of the rotor is less than the preset rated rotational speed vibration threshold and the unbalanced mass of the rotor residual is less than the preset unbalanced quality, and thus the entire dynamic balance process is completed.
- the preset rated speed vibration threshold range is [0. 05 ⁇ , 0. ⁇ ]
- the preset unbalanced mass is [5mg, 12mg]. In this embodiment, the preset rated speed vibration threshold is 0. ⁇ , the preset unbalanced mass is 10 mg.
- the specific steps include:
- the magnetic suspension molecular pump controller (2) calls the dynamic balance module according to the radial amplitude and the rotational speed of the rotor at this time, and performs rotor dynamic balance according to the influence coefficient method, using (3a) _ (3e in step 3)
- the influence coefficient method is dynamically balanced to perform dynamic balancing of the rotor at the rotational speed to obtain the required balance mass and balance mass loading phase of the rotor, and the motor (8) is turned off to reduce the rotor speed to zero.
- step C according to the calculation of the required balance quality and balance the loading phase of the balance, the rotor is balanced processing, and then step D is performed in sequence;
- step E is performed in sequence;
- the motor (8) continues to accelerate, detecting a rotor speed increase to a radial amplitude of the rotor during the process, and if the radial amplitude of the rotor is less than a preset non-rated speed vibration threshold, performing the steps in sequence F; if the radial amplitude of the rotor is found to be greater than or equal to the preset non-rated speed vibration threshold, then the motor (8) is stopped to accelerate, repeating the step B;
- step G start the motor (8) to continue to increase speed to ⁇ 3 ⁇ 4, stop the motor (8) to accelerate, stabilize the speed at the speed, and then perform step G in sequence;
- the magnetic suspension molecular pump controller (2) calls the dynamic balance module according to the radial amplitude and the rotational speed of the rotor at this time, according to the influence coefficient
- the method performs rotor dynamic balance, obtains the balance quality required for the rotor and the loading phase of the balance mass, and closes the motor (8) to reduce the rotor speed to zero;
- step B is repeated.
- the step of obtaining the rotor stiffness critical speed and the rated speed according to the kinetic simulation calculation and experiment of the magnetic levitation molecular pump is used, and the dynamic simulation calculation and experiment adopt the prior art.
- the preset non-rated speed vibration threshold may be selected to be 20 ⁇ m, 25 ⁇ m, 30 ⁇ m, or 35 ⁇ m, etc., and the preset rated speed vibration threshold may also be selected as 0. 05 ⁇ , 0. 07 ⁇ or 0.
- the preset unbalanced mass may also be selected to be 5 mg, 8 mg or 12 mg, etc., and the object of the present invention can also be achieved. It is apparent that the above-described embodiments are merely illustrative of the examples, and are not intended to limit the embodiments. Other variations or modifications of the various forms may be made by those skilled in the art in light of the above description. There is no need and no way to exhaust all of the implementations. Obvious changes or variations resulting therefrom are still within the scope of the invention.
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Physics & Mathematics (AREA)
- Power Engineering (AREA)
- Electromagnetism (AREA)
- General Physics & Mathematics (AREA)
- Manufacturing & Machinery (AREA)
- Non-Positive Displacement Air Blowers (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Magnetic Bearings And Hydrostatic Bearings (AREA)
- Connection Of Motors, Electrical Generators, Mechanical Devices, And The Like (AREA)
Abstract
Description
Claims
Priority Applications (3)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB1411235.3A GB2511985B (en) | 2011-12-05 | 2012-11-22 | Method of rotor dynamic balancing for magnetic levitation molecular pump |
| DE112012005062.2T DE112012005062B4 (de) | 2011-12-05 | 2012-11-22 | Ein Verfahren zur Realisierung des dynamischen Gleichgewichts der Magnetschwebe-Molekularpumpe |
| US14/362,806 US9479035B2 (en) | 2011-12-05 | 2012-11-22 | Method of dynamic balancing for magnetic levitation molecular pump |
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201110399466.X | 2011-12-05 | ||
| CN201110399466.XA CN102425561B (zh) | 2011-12-05 | 2011-12-05 | 一种磁悬浮分子泵动平衡方法 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| WO2013083000A1 true WO2013083000A1 (zh) | 2013-06-13 |
Family
ID=45959581
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| PCT/CN2012/085077 Ceased WO2013083000A1 (zh) | 2011-12-05 | 2012-11-22 | 一种磁悬浮分子泵动平衡方法(5) |
Country Status (5)
| Country | Link |
|---|---|
| US (1) | US9479035B2 (zh) |
| CN (1) | CN102425561B (zh) |
| DE (1) | DE112012005062B4 (zh) |
| GB (1) | GB2511985B (zh) |
| WO (1) | WO2013083000A1 (zh) |
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN114048594A (zh) * | 2021-10-28 | 2022-02-15 | 中国科学院理化技术研究所 | 磁悬浮压缩机叶顶间隙的在线调节方法、系统、终端 |
| CN114112193A (zh) * | 2021-09-22 | 2022-03-01 | 核工业理化工程研究院 | 一种柔性转子动平衡配重预测方法 |
| CN114577397A (zh) * | 2022-03-17 | 2022-06-03 | 湖南科技大学 | 一种高速永磁电机转子动平衡方法及系统 |
| CN114337378B (zh) * | 2021-12-29 | 2023-12-19 | 杭州电子科技大学 | 一种磁悬浮泵的控制方法及控制系统 |
| CN119023144A (zh) * | 2024-07-22 | 2024-11-26 | 东风汽车集团股份有限公司 | 动平衡检测装置及其控制方法 |
Families Citing this family (36)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102425562B (zh) | 2011-12-05 | 2014-04-30 | 北京中科科仪股份有限公司 | 一种磁悬浮分子泵动平衡方法 |
| CN102425561B (zh) * | 2011-12-05 | 2014-04-30 | 北京中科科仪股份有限公司 | 一种磁悬浮分子泵动平衡方法 |
| WO2016176597A1 (en) * | 2015-04-29 | 2016-11-03 | Active Power, Inc. | Integrated motor generator flywheel with rotating permanent magnet |
| JP6613793B2 (ja) * | 2015-10-16 | 2019-12-04 | 株式会社島津製作所 | 磁気軸受装置およびロータ回転駆動装置 |
| EP3179611B1 (en) * | 2015-12-10 | 2018-06-27 | Skf Magnetic Mechatronics | Balancing method for balancing at high speed a rotor of a rotary machine |
| CN106950062B (zh) * | 2017-04-07 | 2023-11-14 | 清华大学 | 磁悬浮轴承抗跌落性能的测试实验台 |
| US10487875B2 (en) * | 2017-08-25 | 2019-11-26 | Shimadzu Corporation | Magnetic bearing device |
| JP6937671B2 (ja) | 2017-11-22 | 2021-09-22 | エドワーズ株式会社 | 磁気軸受制御装置及び真空ポンプ |
| CN108710286B (zh) * | 2018-05-22 | 2020-05-19 | 南京航空航天大学 | 基于交叉解耦陷波器的同频振动力矩分层控制方法 |
| CN112564398A (zh) * | 2019-05-13 | 2021-03-26 | 珠海格力电器股份有限公司 | 磁悬浮轴承、电机、压缩机和空调器 |
| RU2743926C2 (ru) * | 2019-06-21 | 2021-03-01 | Публичное акционерное общество Научно-производственное объединение "Искра" | Способ балансировки ротора с магнитным подвесом |
| CN110285088B (zh) * | 2019-06-26 | 2020-09-15 | 北京航空航天大学 | 一种磁悬浮分子泵平衡质量校正方法 |
| CN110925307B (zh) * | 2019-12-05 | 2021-03-23 | 中国航发四川燃气涡轮研究院 | 一种适用于磁悬浮轴承-转子系统的辅助轴承系统 |
| CN111113265B (zh) * | 2019-12-12 | 2021-07-06 | 湖南工程学院 | 一种电主轴-刀具系统偏心距识别方法 |
| CN111271301B (zh) * | 2020-02-27 | 2021-05-18 | 宁波方太厨具有限公司 | 一种吸油烟机的离心风机的叶轮动平衡校正方法 |
| CN111307373A (zh) * | 2020-03-06 | 2020-06-19 | 运城学院 | 一种电机转子自动铣削或加胶的动平衡一体机及方法 |
| CN112014034B (zh) * | 2020-07-27 | 2021-09-24 | 清华大学 | 磁轴承转子动平衡方法及装置 |
| CN112268570B (zh) * | 2020-09-08 | 2021-11-09 | 珠海格力电器股份有限公司 | 一种传感器的相位补偿装置、方法和磁悬浮系统 |
| CN112491228B (zh) * | 2020-11-06 | 2023-01-24 | 华能澜沧江水电股份有限公司 | 基于振动波形检测引起定子低频振动的关键磁极的方法 |
| CN113765301B (zh) * | 2021-09-09 | 2022-08-16 | 鑫磊压缩机股份有限公司 | 一种提高动平衡调试准确度的磁悬浮电机及方法 |
| CN113866454A (zh) * | 2021-09-30 | 2021-12-31 | 广东美的暖通设备有限公司 | 检测方法、装置、磁悬浮电机、压缩机和可读存储介质 |
| CN114109887B (zh) * | 2021-11-25 | 2022-06-24 | 北京航空航天大学宁波创新研究院 | 一种磁悬浮分子泵的双转向变步长振动抑制方法及系统 |
| CN114520612A (zh) * | 2022-02-16 | 2022-05-20 | 微创外科医疗科技(上海)有限公司 | 转子临界转速测试系统、测试方法及可读存储介质 |
| CN114754069B (zh) * | 2022-03-15 | 2023-12-12 | 格瑞拓动力股份有限公司 | 一种径向磁悬浮轴承自适应死区控制方法及系统 |
| CN114776708B (zh) * | 2022-04-21 | 2023-03-24 | 北京航空航天大学 | 变工作点磁轴承稳定控制系统 |
| CN115541112B (zh) * | 2022-12-01 | 2023-03-21 | 南方电网调峰调频发电有限公司检修试验分公司 | 一种刚性转子的动平衡实验方法、装置、设备及介质 |
| CN115962889B (zh) * | 2022-12-08 | 2026-04-07 | 中电华创电力技术研究有限公司 | 一种汽轮发电机组动平衡方法及系统 |
| CN115788939B (zh) * | 2023-02-07 | 2023-06-30 | 山东华东风机有限公司 | 一种基于磁悬浮轴承旋转器械的防喘振控制方法及系统 |
| CN116464673B (zh) * | 2023-04-19 | 2025-09-16 | 北京航空航天大学 | 一种基于旋转电磁矢量场的磁悬浮分子泵在线动平衡方法 |
| WO2024216543A1 (en) * | 2023-04-19 | 2024-10-24 | Shanghai Qnetic Technology Co., Ltd. | A bearing system for radially constraining a rotor in a kinetic energy storage machine |
| CN116858172B (zh) * | 2023-09-05 | 2023-11-14 | 苏州中科科仪技术发展有限公司 | 一种磁悬浮分子泵的径向定子性能检测工装及检测方法 |
| CN118706652B (zh) * | 2024-08-29 | 2024-12-17 | 山东世纪安泰真空设备有限公司 | 一种用于分子泵的磁轴检测系统及方法 |
| CN119628330B (zh) * | 2024-12-24 | 2025-06-20 | 山东海纳智能装备科技股份有限公司 | 一种基于磁悬浮技术的矿用主扇风机高速永磁电机 |
| CN119628355B (zh) * | 2025-02-13 | 2025-04-15 | 海顿直线电机(常州)有限公司 | 一种电机转子动平衡调整方法 |
| CN120780947B (zh) * | 2025-09-10 | 2026-01-27 | 长江三峡集团实业发展(北京)有限公司 | 临界转速确定方法、装置、设备及存储介质 |
| CN121184387B (zh) * | 2025-11-25 | 2026-04-07 | 上海斯可络压缩机有限公司 | 空压机磁悬浮轴向轴承的混合检测及自适应控制方法 |
Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP1650441A2 (de) * | 2004-10-19 | 2006-04-26 | Pfeiffer Vacuum GmbH | Vibrationsarme Vakuumpumpe |
| CN1920511A (zh) * | 2006-08-01 | 2007-02-28 | 东北电力大学 | 离心泵振动故障融合诊断方法及振动信号采集装置 |
| CN101187589A (zh) * | 2007-12-27 | 2008-05-28 | 浙江飞旋科技有限公司 | 一种调整磁悬浮真空分子泵转子动平衡的方法 |
| CN101495760A (zh) * | 2006-07-26 | 2009-07-29 | 厄利孔莱博尔德真空技术有限责任公司 | 用于确定涡轮分子泵的状态信息的方法和涡轮分子泵 |
| CN102032208A (zh) * | 2010-12-31 | 2011-04-27 | 清华大学 | 一种磁悬浮分子泵的自适应控制系统及控制方法 |
| CN102425561A (zh) * | 2011-12-05 | 2012-04-25 | 北京中科科仪技术发展有限责任公司 | 一种磁悬浮分子泵动平衡方法 |
Family Cites Families (14)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US5214585A (en) * | 1989-06-30 | 1993-05-25 | General Electric Company | Balancing method and product |
| DE69319004T2 (de) * | 1992-03-09 | 1998-12-24 | Hitachi, Ltd., Tokio/Tokyo | Verfahren und Gerät zur Steuerung eines Magnetlagers |
| JP3319030B2 (ja) * | 1993-05-18 | 2002-08-26 | 株式会社日立製作所 | 磁気軸受の制御装置およびそれを用いた回転機械 |
| US5412583A (en) * | 1993-06-10 | 1995-05-02 | Dynamics Research Corp. | Computer implemented balancer |
| US5724271A (en) * | 1994-03-25 | 1998-03-03 | General Electric Company | Model-based method for optimized field balancing of rotating machinery |
| JPH08200367A (ja) * | 1995-01-20 | 1996-08-06 | Shimadzu Corp | 磁気軸受の制御装置 |
| DE19619997A1 (de) * | 1996-05-17 | 1997-11-20 | Karlsruhe Forschzent | Verfahren zum Bestimmen der Unwucht und zum Auswuchten eines supraleitend magnetgelagerten Rotors |
| JP2001241393A (ja) * | 1999-12-21 | 2001-09-07 | Seiko Seiki Co Ltd | 真空ポンプ |
| US6498410B1 (en) * | 2000-03-28 | 2002-12-24 | Ibiden Co., Ltd. | Motor and pressure generating apparatus incorporating the motor |
| CN100462885C (zh) * | 2007-04-20 | 2009-02-18 | 北京航空航天大学 | 一种磁悬浮反作用飞轮开环高精度不平衡振动控制系统 |
| DE102007027711A1 (de) * | 2007-06-15 | 2008-12-18 | Pfeiffer Vacuum Gmbh | Verfahren zum Betreiben einer Anordnung mit Vakuumpumpe und Anordnung mit einer Vakuumpumpe |
| CN100538564C (zh) * | 2007-11-01 | 2009-09-09 | 北京航空航天大学 | 一种磁悬浮飞轮高精度主动振动控制系统 |
| DE102009009961B4 (de) * | 2009-02-23 | 2013-10-31 | Hanning Elektro-Werke Gmbh & Co. Kg | Rotationskörper |
| CN102425562B (zh) * | 2011-12-05 | 2014-04-30 | 北京中科科仪股份有限公司 | 一种磁悬浮分子泵动平衡方法 |
-
2011
- 2011-12-05 CN CN201110399466.XA patent/CN102425561B/zh active Active
-
2012
- 2012-11-22 WO PCT/CN2012/085077 patent/WO2013083000A1/zh not_active Ceased
- 2012-11-22 DE DE112012005062.2T patent/DE112012005062B4/de active Active
- 2012-11-22 US US14/362,806 patent/US9479035B2/en active Active
- 2012-11-22 GB GB1411235.3A patent/GB2511985B/en active Active
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP1650441A2 (de) * | 2004-10-19 | 2006-04-26 | Pfeiffer Vacuum GmbH | Vibrationsarme Vakuumpumpe |
| CN101495760A (zh) * | 2006-07-26 | 2009-07-29 | 厄利孔莱博尔德真空技术有限责任公司 | 用于确定涡轮分子泵的状态信息的方法和涡轮分子泵 |
| CN1920511A (zh) * | 2006-08-01 | 2007-02-28 | 东北电力大学 | 离心泵振动故障融合诊断方法及振动信号采集装置 |
| CN101187589A (zh) * | 2007-12-27 | 2008-05-28 | 浙江飞旋科技有限公司 | 一种调整磁悬浮真空分子泵转子动平衡的方法 |
| CN102032208A (zh) * | 2010-12-31 | 2011-04-27 | 清华大学 | 一种磁悬浮分子泵的自适应控制系统及控制方法 |
| CN102425561A (zh) * | 2011-12-05 | 2012-04-25 | 北京中科科仪技术发展有限责任公司 | 一种磁悬浮分子泵动平衡方法 |
Cited By (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN114112193A (zh) * | 2021-09-22 | 2022-03-01 | 核工业理化工程研究院 | 一种柔性转子动平衡配重预测方法 |
| CN114112193B (zh) * | 2021-09-22 | 2023-10-17 | 核工业理化工程研究院 | 一种柔性转子动平衡配重预测方法 |
| CN114048594A (zh) * | 2021-10-28 | 2022-02-15 | 中国科学院理化技术研究所 | 磁悬浮压缩机叶顶间隙的在线调节方法、系统、终端 |
| CN114337378B (zh) * | 2021-12-29 | 2023-12-19 | 杭州电子科技大学 | 一种磁悬浮泵的控制方法及控制系统 |
| CN114577397A (zh) * | 2022-03-17 | 2022-06-03 | 湖南科技大学 | 一种高速永磁电机转子动平衡方法及系统 |
| CN114577397B (zh) * | 2022-03-17 | 2023-10-13 | 湖南科技大学 | 一种高速永磁电机转子动平衡方法及系统 |
| CN119023144A (zh) * | 2024-07-22 | 2024-11-26 | 东风汽车集团股份有限公司 | 动平衡检测装置及其控制方法 |
Also Published As
| Publication number | Publication date |
|---|---|
| US20140360006A1 (en) | 2014-12-11 |
| GB2511985B (en) | 2018-05-23 |
| US9479035B2 (en) | 2016-10-25 |
| DE112012005062T5 (de) | 2014-09-11 |
| GB2511985A (en) | 2014-09-17 |
| DE112012005062B4 (de) | 2016-09-01 |
| CN102425561B (zh) | 2014-04-30 |
| GB201411235D0 (en) | 2014-08-06 |
| CN102425561A (zh) | 2012-04-25 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| WO2013083000A1 (zh) | 一种磁悬浮分子泵动平衡方法(5) | |
| CN102425562B (zh) | 一种磁悬浮分子泵动平衡方法 | |
| CN113339310B (zh) | 基于磁悬浮轴向位置控制的压缩机喘振预测控制方法 | |
| CN102425560B (zh) | 一种磁悬浮分子泵动平衡方法 | |
| CN102425554B (zh) | 一种磁悬浮分子泵增益调度控制方法 | |
| CN102425553B (zh) | 磁悬浮分子泵的转子悬浮中心测定方法 | |
| CN102242722B (zh) | 一种磁悬浮分子泵及其控制方法、制造方法 | |
| CN102072251A (zh) | 磁悬浮轴承柔性转子的变偏置电流控制装置及控制方法 | |
| JP2012251486A (ja) | 磁気浮上式真空ポンプ、振れまわり推定方法、ロータバランス検査方法および磁気軸受制御ゲイン調整方法 | |
| CN102425559B (zh) | 一种磁悬浮分子泵降速过程中的平稳控制方法 | |
| CN102410238B (zh) | 一种磁悬浮分子泵升速过程中的平稳控制方法 | |
| CN102392828B (zh) | 一种磁悬浮分子泵转子章动峰振动控制方法 | |
| CN102251979B (zh) | 一种磁悬浮分子泵失稳恢复控制方法 | |
| CN118611328A (zh) | 一种双重抑制磁悬浮转子振动的装置及其工作方法 | |
| CN102410240B (zh) | 一种磁悬浮分子泵动平衡方法 | |
| CN102444607B (zh) | 一种磁悬浮分子泵动平衡方法 | |
| CN102817861B (zh) | 一种磁悬浮分子泵的变刚度控制方法 | |
| CN113719540A (zh) | 具有单向高承载力密度的非对称轴向磁轴承装置 | |
| CN102788038B (zh) | 一种磁悬浮分子泵的非线性力抑制方法 | |
| WO2024051099A1 (zh) | 悬浮离心压缩机及空调系统 | |
| JP2012163052A (ja) | 回転体及び該回転体を搭載した真空ポンプ | |
| CN202612115U (zh) | 改善变频空调器的单转子压缩机音质的控制装置 | |
| Wen et al. | Research on low frequency vibration of rotary compressor | |
| CN112727799A (zh) | 一种电机直连离心鼓风机 | |
| CN119448609A (zh) | 与泵一起使用的圆锥形电动机 |
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: 12854586 Country of ref document: EP Kind code of ref document: A1 |
|
| WWE | Wipo information: entry into national phase |
Ref document number: 14362806 Country of ref document: US Ref document number: 1120120050622 Country of ref document: DE Ref document number: 112012005062 Country of ref document: DE |
|
| ENP | Entry into the national phase |
Ref document number: 1411235 Country of ref document: GB Kind code of ref document: A Free format text: PCT FILING DATE = 20121122 |
|
| WWE | Wipo information: entry into national phase |
Ref document number: 1411235.3 Country of ref document: GB |
|
| 122 | Ep: pct application non-entry in european phase |
Ref document number: 12854586 Country of ref document: EP Kind code of ref document: A1 |