US20060018772A1 - Rotary vacuum pump, structure and method for the balancing thereof - Google Patents
Rotary vacuum pump, structure and method for the balancing thereof Download PDFInfo
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- US20060018772A1 US20060018772A1 US11/184,280 US18428005A US2006018772A1 US 20060018772 A1 US20060018772 A1 US 20060018772A1 US 18428005 A US18428005 A US 18428005A US 2006018772 A1 US2006018772 A1 US 2006018772A1
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- rotor
- pump
- rotating
- rotating shaft
- rotor assembly
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Classifications
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- 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
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D17/00—Radial-flow pumps, e.g. centrifugal pumps; Helico-centrifugal pumps
- F04D17/08—Centrifugal pumps
- F04D17/16—Centrifugal pumps for displacing without appreciable compression
- F04D17/168—Pumps specially adapted to produce a vacuum
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- 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
- F04D27/001—Testing thereof; Determination or simulation of flow characteristics; Stall or surge detection, e.g. condition monitoring
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- 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
Definitions
- the present invention concerns a rotary vacuum pump and a structure and a method for balancing thereof.
- the present invention concerns a rotary vacuum pump of the kind equipped with mechanical bearings.
- the present invention concerns a turbomolecular rotary vacuum pump of the kind disclosed for instance in U.S. Pat. No. 6,158,986 or U.S. Pat. No. 5,688,106.
- rotary pumps and especially turbomolecular rotary pumps, are machines equipped with a rotating portion, including a rotating shaft to which a set of parallel rotor discs are secured, and co-operating with a stationary portion, generally a set of stator discs, in order to obtain gas pumping from an inlet port to an outlet port of the pump.
- a turbomolecular pump can generate a vacuum of the order of 10 ⁇ 7 mbar (10 ⁇ 5 pa) with a shaft rotation speed in a range 2 ⁇ 10 4 to 9 ⁇ 10 4 rpm.
- a vacuum pump is thus a machine with a mass that is rotated at extremely high speed.
- a rotating mass generally includes a rotating shaft, the rotor of the electric motor driving said shaft into rotation, the set of rotor discs and the inner rings of the rolling bearings rotatably supporting the pump shaft.
- vibrations are sources of disturbances altering the operation of the measuring instrument and therefore they cannot be tolerated.
- balancing of a rotating mass can be obtained by means of further additional rotating masses, coupled to the main mass so that the center of gravity of the overall mass is brought again on the rotation axis (static balancing) and the rotation axis coincides with a main axis of inertia (dynamic balancing).
- static balancing static balancing
- dynamic balancing dynamic balancing
- the pump rotor is dynamically balanced through an iterative process in which measuring steps of the vibrations transmitted by the pump to an external structure alternate with adjusting steps of the position of one or more additional masses placed on the rotor, until the optimum conditions are attained.
- the main problems related to the rotor balancing step are, on one hand, the definition of the mathematical model used in order to relate the vibrations measured during the balancing step to the rotor unbalance and, consequently, to the arrangement of the correcting masses, and, on the other hand, the choice of the kind of vibration sensors and the arrangement thereof.
- the sensors generally used during the rotor balancing step are accelerometers, that is sensors capable of transforming the acceleration of a moving body to which they are secured into an electric signal, the intensity of which is just a function of the acceleration the sensor is being submitted to.
- the dynamic balancing of a vacuum pump rotor is performed by placing the pump, without stator discs, inside a bell-shaped casing onto which at least two accelerometers, for instance piezoelectric accelerometers, are located. Once the rotor is rotated at high speed, the accelerometers located onto the stationary bell allow measuring the vibrations induced unbalances, if any, of the rotating masses.
- the iterative balancing process may need several pump stopping and starting phases in order to apply the correcting masses, and this results in a considerable increase of the time required to reach the optimum conditions and hence in a considerable slowing down of the production.
- the vibration measurement is not affected by the presence of other pump components, which allows for a considerable simplification of the mathematical model relating the measured displacements to the rotor unbalance inducing them.
- the provision of displacement sensors permanently located inside the pump allows for measuring the rotating mass unbalance also during steady state operation of the same pump, that is when the pump has been completed with the stator part, assembled and delivered to the customer.
- FIG. 1 is a diagrammatic view of the displacement sensor
- FIG. 2 is a diagram of the electronic circuitry of the displacement sensor
- FIG. 3 a is a cross-sectional view of a first embodiment of a vacuum pump according to the present invention.
- FIG. 3 b is a cross-sectional view of a second embodiment of a vacuum pump according to the present invention.
- a first turbomolecular rotary pump 101 is schematically shown.
- Pump 101 comprises a stationary portion and a rotating portion.
- the stationary portion comprises a basement 103 on which the rotating portion is mounted.
- the latter comprises a rotating shaft 105 supported by rolling bearings 107 , for instance ball bearings.
- Rotor 109 of electric motor 111 (the stator of which has not been shown for sake of simplicity) used to rotate shaft 105
- pump rotor 113 equipped with smooth or finned discs 115 , are mounted on the rotating shaft 105 .
- the pump rotor 113 has a bell-shaped cavity 117 housing rotating shaft 105 of the pump and electric motor 111 , in order to make the pump axially more compact.
- Such an arrangement is generally used for big turbomolecular pumps (rotor diameter of about 250 mm).
- FIG. 3 a the pump is shown during the balancing phase and hence rotor 113 is not located inside the pump housing, which is equipped with stator discs, but inside a vacuum-tight stationary bell 119 specifically intended for the balancing of said rotor 113 .
- Vacuum in the bell is achieved by means of an ancillary pumping system, not shown.
- a plurality of displacement sensors (four in the disclosed embodiment) 121 A- 121 D are directly mounted in basement 103 of pump 101 , close to rotor 113 and to rotating shaft 105 thereof.
- Each sensor faces the shaft 105 or the rotor 113 so that changes, if any, in the distance between the rotor and the sensor during rotation of the rotor can be detected.
- a first pair of sensors 121 A, 121 B face rotating shaft 105 and are turned towards it, whereas a second pair of sensors 121 C, 121 D face internal wall 113 a of rotor 113 and are turned towards such wall.
- eddy current displacement sensors are advantageously employed.
- FIG. 1 there is schematically shown a generic displacement sensor 51 comprising a coil 53 , which is wound on a core 55 and in which a high frequency AC current generating a main magnetic field flows.
- the variation of distance “a” between coil 53 and an electrically conducting body R, for instance the pump rotor or the shaft thereof, causes a corresponding variation of the magnetic field induced and consequently of impedance Z measured in the coil of sensor 51 .
- a voltage signal D the value of which depends on impedance Z and hence on the distance of the metal body from the sensor, can be obtained at the output from sensor 51 .
- the circuit shown in FIG. 2 comprises a high frequency oscillator 65 , an impedance 67 in series and a demodulator 63 .
- Impedance 67 must be sufficiently high to obtain a high sensitivity.
- Demodulation of voltage signal u outgoing from the sensor allows obtaining a voltage signal D that is a function of distance “a”.
- Eddy current displacement sensors are capable of measuring distance variations of the order of 1 nm and are perfectly suitable for use in balancing turbomolecular pump rotors.
- a variation of the distance of internal wall 113 a of rotor 113 from facing sensors 121 C, 121 D, caused by an unbalance in rotor 113 will cause a measurable impedance variation in the sensors.
- cylindrical threaded bores 123 are provided in rotor 113 and are arranged with their axes lying in a plane orthogonal to the rotation axis of the rotor and tangentially relative to the same rotor. Additional masses consisting of threaded dowels can be located and displaced in said bores.
- balancing methods comprise the insertion of masses consisting of threaded dowels to be screwed into bores with axes radially arranged relative to the rotor.
- a third pair of displacement sensors 121 E, 121 F is provided, which sensors are arranged close to external wall 113 b of rotor 113 , between a pair of said rotor discs, and are turned towards the wall.
- the sensors 121 E, 121 F are cantilevered on a vertical support 120 adjacent to a wall of outer bell 119 .
- FIG. 3 b a second embodiment of the invention is partially depicted.
- a turbomolecular pump 201 differs from that previously disclosed with reference to FIG. 3 a in that rotor 213 has no bell-shaped cavity receiving rotating shaft 205 and electric motor 211 .
- Shaft 205 is instead supported by a pair of rolling bearings 207 , for instance ball bearings, and is driven by an electric motor 211 , the bearings and the motor are located in a pump region that is axially separated from the pumping region where rotor 213 is located.
- Such arrangement is generally used for small and medium size turbomolecular pumps (rotor diameter smaller than about 160 mm).
- a pair of displacement sensors 221 A, 221 B is provided in basement 203 of pump 201 , opposite rotating shaft 205 and at opposite sides of rotor 209 of electric motor 211 .
- said displacement sensors are preferably eddy current sensors.
- a second pair of sensors 221 C, 221 D is provided close to internal wall 213 a of rotor 213
- a third pair of sensors 221 E, 221 F is provided close to external wall 213 b of rotor 213 .
- bell 219 is advantageously equipped with a central cylindrical projection 219 a penetrating into central bore 213 c of rotor 213 .
- a removable vertical support 220 is provided adjacent to one of the walls of external bell 219 for the cantilevering of the third pair of displacement sensors 221 E, 221 F.
- pump 201 also has multiple threaded bores 223 with axes lying in planes orthogonal to the rotation axis of rotor 213 to allow locating and displacing additional masses.
- threaded dowels located in radial bores instead of tangentially oriented bores can be used.
- turbomolecular pump attains the intended aims, since using displacement sensors directly mounted inside the pump, close to the rotor or the rotating shaft thereof, allows using simpler and more precise mathematical models to determine the rotor unbalance. Consequently, the balancing phase might be carried out in quicker manner and with better results.
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- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Non-Positive Displacement Air Blowers (AREA)
- Compressors, Vaccum Pumps And Other Relevant Systems (AREA)
Abstract
A rotary vacuum pump (101; 201) comprising displacement sensors (121A-121F; 221A-221F), variously coupled to the pump basement (103; 203) and arranged close to the pump rotor (113; 213) and/or to the rotating shaft (105; 205) thereof, the sensors being turned towards it (them) and being perpendicular thereto, in order to detect non-homogeneous distributions, if any, of masses of said rotor (113; 213) with respect to its rotation axis. The invention also relates to a structure for and a method of balancing a rotary pump.
Description
- The present invention concerns a rotary vacuum pump and a structure and a method for balancing thereof.
- In the field of rotary vacuum pumps, it is known that either mechanical bearings, such as ball or roller bearings, or magnetic bearings can be used for supporting the rotating pump shaft.
- The present invention concerns a rotary vacuum pump of the kind equipped with mechanical bearings.
- More particularly, the present invention concerns a turbomolecular rotary vacuum pump of the kind disclosed for instance in U.S. Pat. No. 6,158,986 or U.S. Pat. No. 5,688,106.
- As known, rotary pumps, and especially turbomolecular rotary pumps, are machines equipped with a rotating portion, including a rotating shaft to which a set of parallel rotor discs are secured, and co-operating with a stationary portion, generally a set of stator discs, in order to obtain gas pumping from an inlet port to an outlet port of the pump.
- Depending on the kind of pump, higher or lower vacuum degrees can be obtained. For instance, a turbomolecular pump can generate a vacuum of the order of 10−7 mbar (10−5 pa) with a shaft rotation speed in a range 2×104 to 9×104 rpm.
- A vacuum pump is thus a machine with a mass that is rotated at extremely high speed. In a vacuum pump, such a rotating mass generally includes a rotating shaft, the rotor of the electric motor driving said shaft into rotation, the set of rotor discs and the inner rings of the rolling bearings rotatably supporting the pump shaft.
- When the rotating mass is not arranged with its center of gravity or the rotation axis and thus is not balanced, forces of interior are generated within the pump and are transmitted through the housing to the outside of the pump. Such forces of interior cause unwanted stresses and vibrations, which are sources of noise and lead to an early wear of the rolling bearings.
- Moreover, in some specific applications, for instance where the pump is connected to a precision measuring instrument, such as in mass spectrometry, vibrations are sources of disturbances altering the operation of the measuring instrument and therefore they cannot be tolerated.
- One of the problems encountered in designing a rotary vacuum pump equipped with mechanical bearings is thus how to reduce the vibrations produced by the pump due to unbalance of the rotating masses.
- Generally, it is known that balancing of a rotating mass can be obtained by means of further additional rotating masses, coupled to the main mass so that the center of gravity of the overall mass is brought again on the rotation axis (static balancing) and the rotation axis coincides with a main axis of inertia (dynamic balancing). A dynamically balanced rotor does not transmit stresses to the supports and it is therefore an optimum solution.
- In the field of rotary vacuum pumps, and in particular of turbomolecular ones, the pump rotor is dynamically balanced through an iterative process in which measuring steps of the vibrations transmitted by the pump to an external structure alternate with adjusting steps of the position of one or more additional masses placed on the rotor, until the optimum conditions are attained.
- The main problems related to the rotor balancing step are, on one hand, the definition of the mathematical model used in order to relate the vibrations measured during the balancing step to the rotor unbalance and, consequently, to the arrangement of the correcting masses, and, on the other hand, the choice of the kind of vibration sensors and the arrangement thereof.
- In the field of rotary vacuum pumps, the sensors generally used during the rotor balancing step are accelerometers, that is sensors capable of transforming the acceleration of a moving body to which they are secured into an electric signal, the intensity of which is just a function of the acceleration the sensor is being submitted to.
- According to the prior art, the dynamic balancing of a vacuum pump rotor is performed by placing the pump, without stator discs, inside a bell-shaped casing onto which at least two accelerometers, for instance piezoelectric accelerometers, are located. Once the rotor is rotated at high speed, the accelerometers located onto the stationary bell allow measuring the vibrations induced unbalances, if any, of the rotating masses.
- Yet such a solution has some drawbacks, of which the main is that the point where vibrations are measured, i.e. the area where the accelerometer is located, is relatively far from the source of said vibrations, i.e. the rotor.
- The provision of a set of masses placed between the rotor and the accelerometer, and comprising members that in part are very rigid and in part are resilient and damping, makes it complex to define a reliable mathematical model relating the vibrations to their cause, i.e. the unbalance of the rotor and the other moving masses.
- Consequently, the iterative balancing process may need several pump stopping and starting phases in order to apply the correcting masses, and this results in a considerable increase of the time required to reach the optimum conditions and hence in a considerable slowing down of the production.
- It is the main object of the present invention to solve the problem of how effectively and quickly to balance the rotating masses of a rotary vacuum pump, more particularly a pump, equipped with mechanical bearings such as a turbomolecular vacuum pump.
- The above and other objects are achieved by means of a vacuum pump and a balancing method as claimed in the appended claims.
- Due to the positioning of displacement sensors close to the rotating masses of the pump, it is possible to obtain a more direct measurement of the rotor vibrations and hence to make the proper balancing thereof simpler and quicker.
- According to the invention, the vibration measurement is not affected by the presence of other pump components, which allows for a considerable simplification of the mathematical model relating the measured displacements to the rotor unbalance inducing them.
- Advantageously, the provision of displacement sensors permanently located inside the pump allows for measuring the rotating mass unbalance also during steady state operation of the same pump, that is when the pump has been completed with the stator part, assembled and delivered to the customer.
- Two embodiments of the invention, given by way of non-limiting example, will be described hereinbelow with reference to the accompanying drawings, in which:
-
FIG. 1 is a diagrammatic view of the displacement sensor; -
FIG. 2 is a diagram of the electronic circuitry of the displacement sensor; -
FIG. 3 a is a cross-sectional view of a first embodiment of a vacuum pump according to the present invention; -
FIG. 3 b is a cross-sectional view of a second embodiment of a vacuum pump according to the present invention. - Referring to
FIG. 3 a, a firstturbomolecular rotary pump 101 is schematically shown. -
Pump 101 comprises a stationary portion and a rotating portion. The stationary portion comprises abasement 103 on which the rotating portion is mounted. The latter comprises a rotatingshaft 105 supported byrolling bearings 107, for instance ball bearings.Rotor 109 of electric motor 111 (the stator of which has not been shown for sake of simplicity) used to rotateshaft 105, andpump rotor 113, equipped with smooth orfinned discs 115, are mounted on the rotatingshaft 105. - As clearly shown in
FIG. 3 a, according to the construction design ofpump 101, thepump rotor 113 has a bell-shaped cavity 117housing rotating shaft 105 of the pump andelectric motor 111, in order to make the pump axially more compact. Such an arrangement is generally used for big turbomolecular pumps (rotor diameter of about 250 mm). - In
FIG. 3 a the pump is shown during the balancing phase and hencerotor 113 is not located inside the pump housing, which is equipped with stator discs, but inside a vacuum-tightstationary bell 119 specifically intended for the balancing of saidrotor 113. Vacuum in the bell is achieved by means of an ancillary pumping system, not shown. - According to the present invention, a plurality of displacement sensors (four in the disclosed embodiment) 121A-121D are directly mounted in
basement 103 ofpump 101, close torotor 113 and to rotatingshaft 105 thereof. Each sensor faces theshaft 105 or therotor 113 so that changes, if any, in the distance between the rotor and the sensor during rotation of the rotor can be detected. - More particularly, in the case depicted in
FIG. 3 a, a first pair ofsensors shaft 105 and are turned towards it, whereas a second pair ofsensors internal wall 113 a ofrotor 113 and are turned towards such wall. - According to present invention, eddy current displacement sensors are advantageously employed.
- Referring to
FIG. 1 , there is schematically shown ageneric displacement sensor 51 comprising acoil 53, which is wound on acore 55 and in which a high frequency AC current generating a main magnetic field flows. The variation of distance “a” betweencoil 53 and an electrically conducting body R, for instance the pump rotor or the shaft thereof, causes a corresponding variation of the magnetic field induced and consequently of impedance Z measured in the coil ofsensor 51. - By using an impedance-to-voltage converter, such as that shown in
FIG. 2 , a voltage signal D, the value of which depends on impedance Z and hence on the distance of the metal body from the sensor, can be obtained at the output fromsensor 51. - More precisely, the circuit shown in
FIG. 2 comprises ahigh frequency oscillator 65, animpedance 67 in series and ademodulator 63.Impedance 67 must be sufficiently high to obtain a high sensitivity. Demodulation of voltage signal u outgoing from the sensor allows obtaining a voltage signal D that is a function of distance “a”. - Eddy current displacement sensors are capable of measuring distance variations of the order of 1 nm and are perfectly suitable for use in balancing turbomolecular pump rotors.
- More particularly, in the described embodiment, a variation of the distance of
internal wall 113 a ofrotor 113 from facingsensors rotor 113, will cause a measurable impedance variation in the sensors. By measuring such an impedance variation, it is possible to obtain the distance variation, and hence the unbalance having generated it, and to correct such unbalance. - The process in case of a distance variation between rotating shaft. 105 and
sensors - To correct the unbalance of
rotor 113, cylindrical threadedbores 123 are provided inrotor 113 and are arranged with their axes lying in a plane orthogonal to the rotation axis of the rotor and tangentially relative to the same rotor. Additional masses consisting of threaded dowels can be located and displaced in said bores. - As an alternative, other balancing methods comprise the insertion of masses consisting of threaded dowels to be screwed into bores with axes radially arranged relative to the rotor.
- Further in accordance with the invention, and still referring to
FIG. 3 a, a third pair ofdisplacement sensors external wall 113 b ofrotor 113, between a pair of said rotor discs, and are turned towards the wall. Thesensors vertical support 120 adjacent to a wall ofouter bell 119. - It is clear that, at the end of the balancing phase,
bell 119 andsupport 120, if provided, will be removed and replaced by pump housing 121 with the stator integral thereto, so that the pump will be ready for being sent to the customer and used. Consequently, at the end of the balancing phase,displacement sensors bell 119 will be removed. On the contrary,sensors 121A-121D mounted inbasement 103 ofpump 101 will remain inside the pump even during operation thereof, and they could be advantageously used to carry out measurements on the rotor balance conditions during normal pump operation. - Turning now to
FIG. 3 b, a second embodiment of the invention is partially depicted. - A
turbomolecular pump 201 differs from that previously disclosed with reference toFIG. 3 a in thatrotor 213 has no bell-shaped cavity receivingrotating shaft 205 andelectric motor 211.Shaft 205 is instead supported by a pair of rollingbearings 207, for instance ball bearings, and is driven by anelectric motor 211, the bearings and the motor are located in a pump region that is axially separated from the pumping region whererotor 213 is located. - Such arrangement is generally used for small and medium size turbomolecular pumps (rotor diameter smaller than about 160 mm).
- Similarly to what is described above, according to the present invention a pair of
displacement sensors basement 203 ofpump 201, opposite rotatingshaft 205 and at opposite sides ofrotor 209 ofelectric motor 211. - Also in that second embodiment, said displacement sensors are preferably eddy current sensors.
- Like in the previous embodiment,
further displacement sensors face rotor 213. - More particularly, in the embodiment shown, a second pair of
sensors internal wall 213 a ofrotor 213, whereas a third pair ofsensors external wall 213 b ofrotor 213. These sensors are turned towards the rotor so that any variation in the distance between the rotor and the sensor during rotation of the same rotor can be detected. - In order to properly locate the second pair of
sensors cylindrical projection 219 a penetrating intocentral bore 213 c ofrotor 213. - A removable
vertical support 220 is provided adjacent to one of the walls of external bell 219 for the cantilevering of the third pair ofdisplacement sensors - Similar to previous embodiment, pump 201 also has multiple threaded
bores 223 with axes lying in planes orthogonal to the rotation axis ofrotor 213 to allow locating and displacing additional masses. - Also in this case, threaded dowels located in radial bores instead of tangentially oriented bores can be used.
- When, at the end of the balancing phase, bell 219 and
support 220, if present, will be removed,displacement sensors sensors basement 203 ofpump 201 will remain inside said pump even during operation thereof, and they could be advantageously used to carry out field measurements. - It is clear that the turbomolecular pump according to the invention attains the intended aims, since using displacement sensors directly mounted inside the pump, close to the rotor or the rotating shaft thereof, allows using simpler and more precise mathematical models to determine the rotor unbalance. Consequently, the balancing phase might be carried out in quicker manner and with better results.
- It is also clear that the above description has been given only by way of non-limiting example and that several modifications are possible without departing from the scope of the invention.
Claims (20)
1. A rotary vacuum pump (101; 201) comprising a stationary portion (103; 203) and a portion rotating relative to said stationary portion, the rotating portion comprising a rotating shaft (105; 205) equipped with a rotor assembly (113; 213), driven by an electric motor (111; 211) and supported by at least one rolling mechanical bearing (107; 207) relative to said stationary portion, the rotary pump comprising:
at least two displacement sensors (121A-121D; 221A-221B) positioned between said stationary portion and said rotating portion for generating an electrical signal varying with a distance variation between said stationary portion and said rotating portion during the rotation of said shaft and said rotor assembly.
2. The rotary vacuum pump as claimed in claim 1 , wherein the pump (101) further comprises:
a basement (103) with the rotating shaft (105) supported by a pair of rolling bearings (107) and mounted theron;
a rotor (109) of the electric motor (111), which is mounted on the rotating shaft (105) for rotating said shaft (105) and the rotor assembly (113); and
the rotor assembly(113) comprises a bell-shaped cavity (117) housing the rotating shaft (105) and the electric motor (111).
3. The rotary vacuum pump as claimed in claim 2 , wherein said pump comprises at least one pair of displacement sensors (121A-121D) mounted in the basement (103) of the pump (101), close to the rotor (113) and/or to the rotating shaft (105) thereof, each sensor facing said shaft (105) or said rotor (113) so that the possible variations in the distance between the rotor and the sensor during rotation of the rotor is measured.
4. The rotary vacuum pump as claimed in claim 3 , further comprising a first pair of sensors (121A, 121B) facing the rotating shaft (105) and turned towards it, and a second pair of sensors (121C, 121D) facing the internal wall (113 a) of the rotor assembly (113) and turned towards the wall.
5. The rotary vacuum pump as claimed in claim 1 , wherein said rotor assembly (113) comprises at least one threaded cylindrical bore (123) having an axis lying in a plane orthogonal to a rotation axis of the rotor (113) and tangentially relative to said rotor, wherein additional masses of the bore consisting of threaded dowels can be located and displaced for reducing the unbalance of the rotating portion.
6. The rotary vacuum pump as claimed in claim 1 , wherein said rotor assembly (113) comprises at least one threaded cylindrical bore (123) having an axis lying in a plane orthogonal to a rotation axis of the rotor (113) and radially relative to said rotor, wherein additional masses of the bore consisting of threaded dowels can be located and displaced for reducing the unbalance of the rotating portion.
7. The rotary vacuum pump as claimed in claim 1 , wherein:
the rotating shaft (205) is supported by a pair of rolling bearings (207) and is driven by the electric motor (211), the bearings and the motor are located in a pump region that is axially separated from the pumping region housing the rotor assembly (213); and
a pair of displacement sensors (221A, 221B) is positioned in a basement (203) of the pump (201), opposite to the rotating shaft (205) and at opposite sides of the rotor (209) of the electric motor (211).
8. The rotary vacuum pump as claimed in claim 1 , wherein said displacement sensors are eddy current displacement sensors, which comprise a coil (53) in which a high frequency AC current generating a variable magnetic field flows.
9. The rotary vacuum pump as claimed in claim 8 , wherein said sensors comprise an impedance-to-voltage converter (61), wherein a variation in the voltage level of an output signal of said converter (61) corresponds to an impedance variation in the coil of said sensor.
10. The rotary vacuum as claimed in claim 12 , wherein said sensors (121A-121D; 221A-221B) provide a signal representative of the displacement of the rotating portion relative to the stationary portions during the pump's operation.
11. The rotary vacuum as claimed in claim 1 , wherein said pump is a turbomolecular pump.
12. A structure for balancing a rotary vacuum pump comprising a stationary portion (103; 203) and a portion rotating relative to said stationary portion having a rotating shaft (105; 205) equipped with a rotor assembly (113; 213), driven by an electric motor (111; 211) and supported by at least one rolling mechanical bearing (107; 207) relative to said stationary portion, and a vacuum-tight bell (119; 219) in which the pump can be housed during balancing, said structure comprising:
at least two displacement sensors (121A-121D; 221A-221B), generating an electrical signal varying with the distance variation between said bell and said rotating portion during the rotation of said shaft and said rotor assembly, and being positioned between said bell and said rotating portion.
13. The structure as claimed in claim 12 , wherein:
the pump (101; 201) comprises a basement (103; 203) on which the rotating shaft (105; 205) supported by a pair of rolling bearings (107; 207) is mounted, the rotor (109; 209) of the pump electric motor (111; 211) for rotating the shaft (105; 205) and the rotor assembly (113; 213) being mounted on said rotating shaft (105; 205); and
the rotor assembly (113; 213) has a bell-shaped cavity (117) where the rotating shaft (105; 205) and the electric motor (111; 211) are housed.
14. The structure as claimed in claim 13 , wherein said pump comprises a plurality of displacement sensors (121A-121D; 221A, 221B) mounted in the basement (103; 203), in proximity to the rotor assembly (113; 213) and/or to the rotating shaft (105; 205) thereof, each sensor facing said shaft (105; 205) or said rotor (113; 213) for detecting a variation in the distance between the rotor and the sensor during rotation of the rotor.
15. The structure as claimed in claim 14 , wherein said pump comprises a first sensor pair (121A, 121B; 221A, 221B) facing the rotating shaft (105; 205) and turned towards it, and a second sensor pair (121C, 121D; 221C, 221D) facing the internal wall (113 a; 213 a) of the rotor assembly (113; 213) and turned towards internal wall.
16. The structure as claimed in claim 15 , wherein, the bell (219) is equipped with a central cylindrical projection (219 a) penetrating into the rotor assembly (213) for positioning the second sensor pair (221C, 221D).
17. The structure as claimed in claim 15 , wherein a third pair of displacement sensors (121E, 121F; 221E, 221F) is provided, said displacement sensors are arranged in proximity to the external wall (113 b; 213 b) of the rotor assembly (113; 213), between a pair of rotor discs (115; 215), and are turned towards said external wall.
18. The structure as claimed in claim 17 , wherein said sensors (121E, 121F; 221E, 221F) of said third pair of displacement sensors are cantilevered on a vertical support (120; 220) adjacent to one of the walls of the bell (119; 219).
19. The structure as claimed in claim 18 , wherein said sensors are eddy current displacement sensors.
20. A method of balancing a rotary vacuum pump comprising a stationary portion (103; 203) and a rotating portion wiht a rotating shaft (105; 205) equipped with a rotor assembly (113; 213) co-operating with a stator assembly for gas pumping, said rotating shaft being driven by an electric motor (111; 211) and supported by at least one rolling mechanical bearing (107; 207) relative to said stationary portion, the method comprising the steps of:
a) providing a vacuum-tight bell (119; 219) in which the pump is housed during balancing operation;
b) coupling the pump, without the stator assembly, to the bell;
c) making vacuum in the bell;
d) driving the rotating portion into rotation;
e) measuring the displacement, at the rotation frequency, of the rotating portion relative to the stationary portion;
f) stopping the rotating portion;
g) balancing the rotating portion by means of additional masses;
h) repeating, if necessary, steps b) through g); and
i) obtaining displacement measurement by means of at least two displacement sensors (121A-121 F; 221A-221 F), capable of generating an electrical signal varying with the distance between said stationary portion or the bell and the rotating portion during the rotation of the shaft (105; 205) and said rotor assembly (113; 213).
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
EP04103445A EP1619395B1 (en) | 2004-07-20 | 2004-07-20 | Rotary vacuum pump, structure and method for the balancing thereof |
EP04103445.5 | 2004-07-20 |
Publications (1)
Publication Number | Publication Date |
---|---|
US20060018772A1 true US20060018772A1 (en) | 2006-01-26 |
Family
ID=34929350
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US11/184,280 Abandoned US20060018772A1 (en) | 2004-07-20 | 2005-07-19 | Rotary vacuum pump, structure and method for the balancing thereof |
Country Status (4)
Country | Link |
---|---|
US (1) | US20060018772A1 (en) |
EP (1) | EP1619395B1 (en) |
JP (1) | JP2006029338A (en) |
DE (1) | DE602004025916D1 (en) |
Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US20110135506A1 (en) * | 2008-05-23 | 2011-06-09 | Oberlikon Leybold Vacuum Gmbh | Multi-stage vacuum pump |
US20110286833A1 (en) * | 2010-05-21 | 2011-11-24 | Oerlikon Leybold Vacuum Gmbh | Vacuum pump |
DE102011105806A1 (en) * | 2011-05-05 | 2012-11-08 | Pfeiffer Vacuum Gmbh | Vacuum pump with rotor |
US20130121858A1 (en) * | 2011-11-15 | 2013-05-16 | Yukiteru Sekita | Vacuum pump |
US10557471B2 (en) | 2017-11-16 | 2020-02-11 | L Dean Stansbury | Turbomolecular vacuum pump for ionized matter and plasma fields |
CN114216680A (en) * | 2021-11-05 | 2022-03-22 | 上海航天控制技术研究所 | High-speed rotor kurtosis detection fault diagnosis device and method |
Families Citing this family (3)
Publication number | Priority date | Publication date | Assignee | Title |
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DE102013113400A1 (en) * | 2013-12-03 | 2015-06-03 | Pfeiffer Vacuum Gmbh | Pump and method for balancing a rotor |
GB201514001D0 (en) * | 2015-08-07 | 2015-09-23 | Edwards Ltd | Pumps |
EP3135919B1 (en) * | 2015-08-24 | 2019-02-20 | Pfeiffer Vacuum Gmbh | Vacuum pump |
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Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US20110135506A1 (en) * | 2008-05-23 | 2011-06-09 | Oberlikon Leybold Vacuum Gmbh | Multi-stage vacuum pump |
US20110286833A1 (en) * | 2010-05-21 | 2011-11-24 | Oerlikon Leybold Vacuum Gmbh | Vacuum pump |
DE102011105806A1 (en) * | 2011-05-05 | 2012-11-08 | Pfeiffer Vacuum Gmbh | Vacuum pump with rotor |
US20130121858A1 (en) * | 2011-11-15 | 2013-05-16 | Yukiteru Sekita | Vacuum pump |
US10557471B2 (en) | 2017-11-16 | 2020-02-11 | L Dean Stansbury | Turbomolecular vacuum pump for ionized matter and plasma fields |
CN114216680A (en) * | 2021-11-05 | 2022-03-22 | 上海航天控制技术研究所 | High-speed rotor kurtosis detection fault diagnosis device and method |
Also Published As
Publication number | Publication date |
---|---|
EP1619395A1 (en) | 2006-01-25 |
JP2006029338A (en) | 2006-02-02 |
EP1619395B1 (en) | 2010-03-10 |
DE602004025916D1 (en) | 2010-04-22 |
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