EP4724706A1 - Permanent magnetic bearing insert - Google Patents

Permanent magnetic bearing insert

Info

Publication number
EP4724706A1
EP4724706A1 EP24729342.6A EP24729342A EP4724706A1 EP 4724706 A1 EP4724706 A1 EP 4724706A1 EP 24729342 A EP24729342 A EP 24729342A EP 4724706 A1 EP4724706 A1 EP 4724706A1
Authority
EP
European Patent Office
Prior art keywords
rotor
bearing
magnetic bearing
vacuum pump
sleeve
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.)
Pending
Application number
EP24729342.6A
Other languages
German (de)
French (fr)
Inventor
Emiliano LUCCHETTA
Eng Keen KHOR
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Edwards Ltd
Original Assignee
Edwards Ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Edwards Ltd filed Critical Edwards Ltd
Publication of EP4724706A1 publication Critical patent/EP4724706A1/en
Pending legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D19/00Axial-flow pumps
    • F04D19/02Multi-stage pumps
    • F04D19/04Multi-stage pumps specially adapted to the production of a high vacuum, e.g. molecular pumps
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D19/00Axial-flow pumps
    • F04D19/02Multi-stage pumps
    • F04D19/04Multi-stage pumps specially adapted to the production of a high vacuum, e.g. molecular pumps
    • F04D19/042Turbomolecular vacuum pumps
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D19/00Axial-flow pumps
    • F04D19/02Multi-stage pumps
    • F04D19/04Multi-stage pumps specially adapted to the production of a high vacuum, e.g. molecular pumps
    • F04D19/048Multi-stage pumps specially adapted to the production of a high vacuum, e.g. molecular pumps comprising magnetic bearings
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D25/00Pumping installations or systems
    • F04D25/02Units comprising pumps and their driving means
    • F04D25/06Units comprising pumps and their driving means the pump being electrically driven
    • F04D25/0606Units comprising pumps and their driving means the pump being electrically driven the electric motor being specially adapted for integration in the pump
    • F04D25/0613Units comprising pumps and their driving means the pump being electrically driven the electric motor being specially adapted for integration in the pump the electric motor being of the inside-out type, i.e. the rotor is arranged radially outside a central stator
    • F04D25/064Details of the rotor
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00Details, component parts, or accessories
    • F04D29/05Shafts or bearings, or assemblies thereof, specially adapted for elastic fluid pumps
    • F04D29/056Bearings
    • F04D29/058Bearings magnetic; electromagnetic
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16CSHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C32/00Bearings not otherwise provided for
    • F16C32/04Bearings not otherwise provided for using magnetic or electric supporting means
    • F16C32/0406Magnetic bearings
    • F16C32/0408Passive magnetic bearings
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16CSHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C32/00Bearings not otherwise provided for
    • F16C32/04Bearings not otherwise provided for using magnetic or electric supporting means
    • F16C32/0406Magnetic bearings
    • F16C32/0408Passive magnetic bearings
    • F16C32/0423Passive magnetic bearings with permanent magnets on both parts repelling each other
    • F16C32/0425Passive magnetic bearings with permanent magnets on both parts repelling each other for radial load mainly
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2260/00Function
    • F05D2260/30Retaining components in desired mutual position
    • F05D2260/37Retaining components in desired mutual position by a press fit connection
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2300/00Materials; Properties thereof
    • F05D2300/10Metals, alloys or intermetallic compounds
    • F05D2300/17Alloys
    • F05D2300/173Aluminium alloys, e.g. AlCuMgPb
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2300/00Materials; Properties thereof
    • F05D2300/50Intrinsic material properties or characteristics
    • F05D2300/502Thermal properties
    • F05D2300/5021Expansivity
    • F05D2300/50211Expansivity similar
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16CSHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C35/00Rigid support of bearing units; Housings, e.g. caps, covers

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Physics & Mathematics (AREA)
  • Electromagnetism (AREA)
  • Magnetic Bearings And Hydrostatic Bearings (AREA)

Abstract

The present invention provides a vacuum pump (1), preferably a turbomolecular pump, comprising a rotor shaft (9) configured to have one or more rotor blades (8) coupled thereto and the rotor shaft (9) defining a bearing well (7) containing, in an interference-fit configuration, a permanent magnetic bearing, wherein the magnetic bearing insert comprises one or more permanent magnet alloy rings (3,4,5) of a rotor bearing half of a permanent magnetic bearing and a radially outwardly extending sleeve (16) coupled thereto around an outer circumference of the or each said permanent magnet alloy ring (3,4,5), and an outer surface of the permanent magnetic bearing insert (3) engages with an inward facing wall of the bearing well (7) to provide an interference fit, wherein the radially outwardly extending sleeve (16) has a coefficient of thermal expansion that is at least substantially the same as the coefficient of thermal expansion of the material of the rotor shaft (9) defining the engaged bearing well wall.

Description

PERMANENT MAGNETIC BEARING INSERT
Field
[001 ] The present invention relates to a magnetic bearing insert for a vacuum pump, a vacuum pump, particularly a turbomolecular pump, comprising the same, and a method of manufacturing a vacuum pump. The invention further provides the use of a neodymium magnet alloy in a permanent magnetic bearing insert or vacuum pump.
Background
[002] A vacuum pump typically comprises an impeller in the form of a rotor mounted on a shaft for rotation relative to a surrounding stator. In a turbomolecular pump, for example, sets of moving rotor blades are located on a shaft and are separated and moveable between stationary blades, in use, to compress gas and typically deliver it to an outlet pump, e.g. a rotary pump.
[003] A shaft is supported by two bearing arrangements located at or intermediate respective ends of the shaft. Typically, the upper bearing (that nearest the pump inlet) may be in the form of a magnetic bearing, and the lower bearing is in the form of a rolling bearing.
[004] The magnetic bearing is typically a passive magnetic bearing comprising an inner stator bearing half and an outer rotor bearing half, the outer rotor bearing half forming a part of the rotor shaft of the vacuum pump. The outer rotor bearing half typically comprises one or more ring shaped permanent magnets coaxially aligned with the axis of rotation of the rotor shaft and the inner stator bearing half.
[005] Typically, the permanent magnet rings in the inner stator bearing half and outer rotor bearing half are magnetised and disposed relative to each other in order to create repulsive forces between the two halves. Thus they may suspend the rotor radially. [006] Typically, the permanent magnet rings are made from a samarium-cobalt alloy, such as SmCos. Advantageously, these magnets are extremely resistant to demagnetisation, and show good temperature stability with maximum use temperatures typically between 250°C and 550 °C, and a Curie temperature from 700 °C to 800 °C.
[007] There is however a desire to move towards other magnet alloys, such as neodymium magnets, as they are magnetically stronger, facilitating the use of small magnets and ultimately more compact vacuum pump designs. Known vacuum pump designs and methods of manufacture have however been found to be unsuitable for successfully accommodating these alternative magnets in their bearings.
[008] The present invention addresses at least to a degree some or all of these problems with the prior art.
Summary
[009] Thus, in a first aspect, the present invention provides a vacuum pump, preferably a turbomolecular pump, comprising a rotor shaft configured to have one or more rotor blades coupled thereto and the rotor shaft defining a bearing well containing, in an interference-fit configuration, a permanent magnetic bearing insert.
[010] The magnetic bearing insert comprises one or more permanent magnet alloy rings of a rotor bearing half of a permanent magnetic bearing and a radially outwardly extending sleeve coupled thereto around an outer circumference of the or each said permanent magnet alloy ring.
[011 ] An outer surface of the permanent magnetic bearing insert engages with an inward facing wall of the bearing well to provide an interference fit.
[012] Preferably, the radially outwardly extending sleeve has a coefficient of thermal expansion that is at least substantially the same as (i.e. the same or greater than), preferably substantially the same as, the coefficient of thermal expansion of the material of the rotor shaft defining the engaged bearing well wall.
[013] In a related aspect, the invention further provides permanent magnetic bearing insert for a vacuum pump, the vacuum pump comprising a rotor shaft having one or more rotor blades coupled thereto and the rotor shaft defining a bearing well configured to receive the magnetic bearing insert in an interference-fit configuration.
[014] The magnetic bearing insert comprises one or more magnetized permanent magnet alloy rings of a rotor bearing half of a permanent magnetic bearing and a radially outwardly extending sleeve coupled thereto around an outer circumference of the or each said permanent magnet alloy ring.
[015] An outer surface of the permanent magnetic bearing insert is configured to engage with an inward facing wall of the bearing well following insertion therein.
[016] Typically, the sleeve of the permanent magnetic bearing insert will be generally tubular. The sleeve may extend from a proximal end to a distal end. When in situ in the rotor shaft of the vacuum pump, the proximal end is typically located towards a low pressure end of the rotor, whereas the distal end is typically located towards a relatively higher pressure section of the rotor.
[017] The sleeve of the permanent magnetic bearing insert may be a substantially plain cylinder or may include other features.
[018] One end of the sleeve may include a radially inwardly extending annular flange, or other abutment, for retaining the permanent magnet alloy ring(s). In use, a permanent magnet alloy ring may directly abut against the radially inwardly extending annular flange or other abutment. In some applications, this end may the proximal or low pressure end.
[019] Such radially inward extending annual flange or abutment may be integral part of the sleeve or may be in the form of a ring, or other insert, inserted in the sleeve to provide an abutment for the or each magnet(s). Said ring or insert may be held by a snap-fit or interference fit or other permanent or semi-permanent fixation. [020] In some applications an abutment ring, or other abutment insert, may be inserted at the opposite end to that of an integral ring to provide abutment to the magnet(s) so as to provide an abutment either side of the magnetic ring(s). Likewise, in some applications two abutment rings, or abutment inserts, may be inserted, each at the opposite ends of the sleeve. This arrangement may provide abutment to the magnetic ring(s) at both ends also.
[021 ] One end of the sleeve may include a funnelled entrance. This may assist with pushing the permanent magnet alloy rings into the funnel and/or forming an interference fit. In some applications the funnelled entrance may be at the distal or higher pressure end of the sleeve. Typically, before the permanent magnet alloy rings are inserted, the funnelled entrance is such that the internal diameter of the sleeve decreases from a diameter greater than that of the permanent magnet alloy ring(s) to a diameter that is smaller than that of the of the permanent magnet alloy ring(s). Once in situ the rings will typically be in an interference fit. An abutment ring, or other abutment insert, may be inserted through the funnelled entrance once the permanent magnet alloy ring(s) are in situ to improve the retention thereof.
[022] An end of the sleeve may include a tapered and I or stepped outer surface. This may assist with pushing the sleeve and/or bearing insert into the rotor shaft bearing well. In some applications the tapered and/or stepped outer surface may be located at the distal or higher pressure end of the sleeve. However, in other applications, for instance a bell-shaped rotor, the tapered and/or stepped outer surface may be located at a proximal or lower pressure end of the sleeve. Typically, before the sleeve and/or bearing insert is inserted into the bearing well, the tapered outer surface is such that the outer diameter of the sleeve increases from a diameter less that the inner diameter of the bearing well to a diameter great than the diameter of the bearing well. This may assist with pushing the sleeve and/or bearing insert into the bearing well and/or forming an interference fit.
[023] When in situ in the bearing well of the rotor shaft, an end of the bearing insert directly may abut against a radially inwardly extending annular flange formed within the rotor shaft. This may assist with the correct alignment of the rotor half of the permanent magnet bearing with the stator half of the permanent magnet bearing. [024] When the bearing insert is in situ in the bearing well of the rotor, an additional abutment ring or similar abutment insert(s) may be inserted in the rotor well so as to abut against the sleeve and/or the magnets. The additional abutment ring, or abutment insert, may compliment the interference fit between the sleeve and well to better hold the sleeve and/or the magnet rings in place.
[025] The bearing well is typically in the form of a cavity or recess in the rotor shaft. Typically, the bearing well is located at or towards a proximal, or lower pressure, end of the rotor shaft. Although, in embodiments, bearing well may be present at or towards the distal, relatively higher pressure, end of the rotor shaft, or at or towards both ends of the rotor shaft.
[026] The bearing well may be configured to slidably receive the bearing insert to achieve an intimate engagement about the entire circumference of the bearing insert. Typically, the bearing well has a generally circular cross-section along a length thereof. The fit between the bearing well and the bearing insert may be permanent or semipermanent. The fit may however be sufficient to maintain the position of the permanent bearing magnets during normal use of the vacuum pump.
[027] Typically, the bearing insert may comprise from about 1 to about 10 permanent magnet alloy rings, more preferably from about 2 to about 6 permanent magnet alloy rings, 2 to 4 permanent magnet alloys are particularly preferred.
[028] Preferably, the permanent magnet alloy ring(s) comprise a Neodymium Iron Boron (‘neodymium’) magnet, preferably Nd2Fei4B; or Samarium Cobalt, preferably SmCos, or Sm2Co17. Neodymium magnet(s) are particularly preferred. Typically, where a plurality of magnet alloy rings are present, each comprise substantially the same material.
[029] Preferably, the radially outwardly extending sleeve has a coefficient of thermal expansion that is at least substantially the same as the coefficient of thermal expansion of the material of the rotor shaft defining the engaged bearing well wall, preferably their coefficient of thermal expansion is substantially the same. [030] The invention further provides a rotor for a vacuum pump comprising a rotor shaft having one or more rotor blades coupled thereto and the rotor shaft defining a bearing well containing magnetic bearing insert in an interference-fit configuration.
[031 ] The magnetic bearing insert comprises one or more permanent magnet alloy rings of a rotor bearing half of a permanent magnetic bearing and a radially outwardly extending sleeve coupled thereto around an outer circumference of the or each said permanent magnet alloy ring.
[032] Preferably, the radially outwardly extending sleeve has a coefficient of thermal expansion that is at least substantially the same as the coefficient of thermal expansion of the material of the rotor shaft defining the engaged bearing well wall.
[033] Advantageously, the permanent magnetic bearing insert of the aspects of the invention facilitates the inclusion of a neodymium permanent magnet, and others, in the magnetic bearing of a vacuum pump.
[034] As will be appreciated, permanent magnets are typically brittle and cannot withstand high tensile loads without fracture. In order to contain tensile stress, rotor bearing half magnets are typically inserted into the rotor with an interference fit, generating an inward radial compressive fit on the rotor bearing half magnets.
[035] The material properties and sizes of the permanent magnets and the rotor are such that the magnets expand less with temperature and centrifugal force than the rotor, which is typically made from aluminium. This results in a decrease in the amount of compression exerted by the rotor on the rotor magnets during use.
[036] However, as will be understood, for the bearing to operate as intended the residual compressive action at maximum speed and temperature must still be sufficient for the rotor bearing half magnets to be retained by the rotor, all while keeping the tensile strain below a maximum allowed value for a given magnet (this may be referred to as a minimum compressing action). [037] In addition, the magnets may have a minimum fit requirement. The minimum fit between magnets is the fit that at maximum temperature and speed generates the minimum compressing action as described above.
[038] Additionally, tolerances in the magnets and in the rotor result in a max fit which may be defined as ‘the minimum fit requirement1 plus manufacturing tolerances.
[039] When the max fit condition occurs, the compressive stress on the magnets and the overall stress in the rotor are highest. This will typically be encountered when the rotor is not rotating and when the ambient temperature (and consequently the temperature of the rotor and bearing) is low (e.g. room temperature).
[040] Additionally, the magnets are typically inserted into the rotor by a press, with the rotor heated to a high temperature to minimise the press force required. The magnets may also be cooled to very low temperatures, such as in liquid nitrogen, to minimise the pressing force required. The maximum temperature the rotor can be heated to is often limited by material science issues and the pressing forces can also be limited by stress and practical considerations. Therefore, there is a limit in the max fit that can be achieved, which in turn limits the minimum fit requirement.
[041 ] The inventors have found that the use of neodymium, NdFeB, magnets especially, poses a particular challenge because of their relatively very low coefficient of thermal expansion and their susceptibility to demagnetisation at relatively low temperatures (e.g. from about 120 °C, depending on the grade).
[042] The minimum fit requirement is therefore much higher than with magnets like NdFeB, and the max fit that can be achieved is reduced because cooling the magnets during the fitting operation does not help (because of their negligible or negative coefficient of thermal expansion) and, depending on the rotor material, by the maximum temperature they can be exposed to before significant demagnetisation takes place.
[043] The use of a sleeve may allow increased compression of the magnets, particularly when the magnets are inserted in the sleeve first and then the assembly formed by the sleeve and magnets is inserted into the rotor. [044] However, permanent magnetic bearing inserts made from materials having a relatively low coefficient of thermal expansion, like titanium, or, more specifically, lower than the rotor material (like stainless steel with an aluminium rotor), as seen in prior art, have been found to be inadequate for accommodate NdFeB magnets in rotor bearing wells, particularly aluminium rotor bearing wells.
[045] In fact, whilst the thermal expansion of these materials relative to the Neodymium magnets may be contained, the heating temperature required to shrink the magnets inside the sleeve and/or the pressing force required for the max fit condition may be inappropriately high and I or may lead to demagnetisation of the magnets. Likewise, the heating temperature required for the rotor to ensure the sleeve remains in contact during operation, particularly if the rotor is made in aluminium, may lead to weakening of the rotor.
[046] The inventors have found that by providing a permanent magnetic bearing insert comprising a radially outwardly extending sleeve which has a coefficient of thermal expansion that is at least substantially the same as the coefficient of thermal expansion of the material of the rotor shaft defining the cavity configured to receive the magnetic bearing insert, then appropriate levels of compression may maintained during and out of use, whereas an acceptable press-fit insert force may be employed without necessitating excessive heating of the magnets, sleeve and/or rotor. The invention may therefore facilitate the use of neodymium magnets in magnet bearings of vacuum pumps, in particular turbomolecular pumps, reducing the size of the magnets required and potentially the size of the bearing and/or vacuum pump.
[047] References herein to the coefficient of thermal expansion refer to the linear coefficient of thermal expansion (CLTE) measured at 20 °C (to = 20°C, ti = 100 °C). Throughout the specification, unless stated otherwise, all measurements are taken at 20 °C and standard atmospheric pressure (101325 Pa).
[048] The sleeve may have a coefficient of thermal expansion that is at least substantially the same as the coefficient of thermal expansion of the material of the rotor shaft defining the bearing well wall, preferably substantially the same as the coefficient of thermal expansion of the material of the rotor shaft as a whole. More preferably, the sleeve is made from the material defining the bearing well wall.
[049] Herein, substantially the same as may mean within about 10% of the given parameter, preferably within about 5% of the given parameter, more preferably within about 1 % of the given parameter.
[050] Preferably, the sleeve may have a coefficient of thermal expansion that is within about 1 .5 x10-6 K’1, preferably within about 0.25 x10-6 K-1 of the coefficient of thermal expansion of the material of the rotor shaft defining the bearing well wall.
[051 ] In embodiments, the coefficient of thermal expansion of the material of the rotor shaft defining the engaged bearing well wall is about 8.6 x1 O’6 K1 or greater, preferably about 10.1 K’1 or greater, preferably about 17.3 or greater, more preferably about 23 K’1 or greater.
[052] Preferably, the sleeve comprises a material with a linear coefficient of thermal expansion of about 20 x1 O’6 K-1 or greater, preferably about 23. x1 O’6 K1 or greater.
[053] Preferably, the sleeve comprises a material with a linear coefficient of thermal expansion of about 20 x1 O’6 K-1 or greater, preferably about 22 x1 O’6 K1 or greater, and the material of the rotor shaft defining the engaged bearing well wall a linear coefficient of thermal expansion of about 23x1 O’6 K-1 or greater, preferably about 23 x1 O’6 K’1 or greater.
[054] Typically, the sleeve is made from a non-ferromagnetic material.
[055] In embodiments, the sleeve is aluminium. Typically, the cavity is defined by an aluminium portion of the rotor shaft, preferably a high strength aluminium alloy.
[056] In particularly preferred embodiments both the insert sleeve and portion of the rotor shaft defining the rotor cavity for receiving the same are made from aluminium, preferably substantially the same aluminium alloy. For the avoidance of doubt, references to aluminium herein include aluminium alloy, that is to say an alloy in which aluminium is the predominant metal. The typical alloying elements are copper, magnesium, manganese, silicon, tin, nickel and zinc. The aluminium may be anodized or coated. 2000 and 7000 series aluminium alloys may be particularly suitable for the invention. Preferably substantially all of the rotor shaft is made from aluminium.
[057] Typically, the or each permanent magnet alloy ring is coupled to the sleeve by an interference fit. Preferably, the permanent magnet alloy ring(s) is coupled to the sleeve prior to the sleeve being inserted into the cavity of the pump rotor.
[058] In embodiments, the magnetic bearing insert is machined after the permanent magnet alloy ring is coupled to the sleeve, typically a radially outermost wall of the sleeve is machined once the magnet alloy ring is coupled to the sleeve. Typically, this in situ machining is the final machine of the sleeve. Machining the sleeve once the magnet is in situ may enable tighter tolerances to be achieved when compared to machining the individual components prior to their assembly.
[059] Similarly, the rotor may be machined once the insert is in situ. Typically, this will be the final machine of the rotor. Again, machining the rotor once the insert (including the ring magnet(s)) is in situ may enable tighter tolerances to be achieved when compared to machining the individual components prior to their assembly.
[060] For the avoidance of doubt, in all embodiments and aspects, the or each permanent magnet alloy ring may be magnetic. In embodiments, the or each permanent magnet alloy ring comprises a neodymium magnet alloy.
[061 ] A Neodymium magnet (also known as NdFeB, NIB or Neo magnet) is a permanent magnet made from an alloy of neodymium, iron, and boron to form typically the Nd2FeuB tetragonal crystalline structure. A Neodymium magnet is magnetised.
[062] In embodiments, the rotor shaft and one or more rotor blades are monolithic, i.e. in the form of a single piece of material. The rotor blades may extend radially outwardly from the rotor shaft in a series of axially separated substantially planar arrays. Rotor shafts of this construction may be referred to as a monobloc rotor(s).
[063] Alternatively, one or more of the rotor blades may form a part of an annular rotor blade array, or arrays, coupled to the rotor shaft by an interference fit. Typically, the annular rotor blade array(s) are coupled to the rotor once the bearing insert is in situ. Advantageously, this may facilitate introducing further compression to the permanent magnetic ring. Preferably, the rotor shaft is machined once the magnetic bearing insert is in situ but prior to coupling the rotor blade array(s) to said rotor shaft. Rotor shafts of this construction may be referred to as a multiblock rotor(s).
[064] Often permanent magnets demonstrate anisotropic thermal expansion, whereby the value of the coefficient of the thermal expansion depends on the direction considered. Often the coefficient of the thermal expansion that has the most influence on the expansion of the diameters of the ring is the one in the circumferential or hoop direction. Preferably, the permanent magnet alloy ring has a coefficient of thermal expansion in such direction that is less than about 16 x1 O’6 K-1 More preferably below4 x10-6 K’1 and even more preferably below 1 x10-6 K’1. Preferably, such permanent magnet alloy rings are made in Neodymium Iron Boron. Preferably, the rings are magnetised either axially or radially.
[065] In a further aspect the invention provides method of manufacturing a vacuum pump, preferably a turbomolecular pump, according to the previous aspect. The pump comprises a rotor shaft configured to have one or more rotor blades coupled thereto and the rotor shaft defining a cavity for receiving a magnetic bearing insert.
[066] The method comprises the steps of a) providing a permanent magnetic bearing insert according to first aspect of the invention and b) inserting the magnetic bearing insert into the cavity of the rotor of the vacuum pump for receiving the same and forming an interference fit.
[067] In embodiments of the method, the permanent magnetic bearing insert is preassembled prior to step a) by inserting the permanent magnet alloy ring or rings into the sleeve to form an interference fit.
[068] In embodiments relating to multiblock rotor(s), one or more rotor blades are coupled to the rotor shaft, preferably using an interference fit, following step b). Preferably, the rotor shaft is machined after step b) in an intermediate step before the one or more rotor blades are coupled to the rotor shaft. [069] In embodiments, the permanent magnetic bearing insert is cooled and/or the portion of the rotor defining the cavity is heated prior to inserting the insert into the cavity.
[070] In a further aspect the present invention provides the use of a neodymium magnet alloy in a permanent magnetic bearing insert or vacuum pump, in particular in an insert or vacuum pump as previously described herein. The neodymium magnet alloy may be magnetic.
Figures
[071 ] The invention will now be described with reference to the following figures, which are intended to be non-limiting.
Fig. 1 shows a magnetic bearing insert according to the invention in situ in a monobloc turbomolecular pump rotor.
Fig. 2 shows a magnetic bearing insert according to the invention.
Fig. 3 shows a magnetic bearing insert according to the invention in situ in a multiblock turbomolecular pump rotor.
Fig. 4 shows a rotor bearing comprising a bearing insert according to the invention.
Detailed Description
[072] As illustrated in Fig.1 , the present invention provides a permanent magnetic bearing insert (2), preferably for a turbomolecular pump rotor (1). In the illustrated example, the magnetic bearing insert (2) is located towards a relatively low pressure end (6) of the rotor (1). The insert (2) is slidably installed in a magnetic bearing well (7) formed in the rotor (1). The bearing insert (2) is held in position within the bearing well (7) by an interference fit.
[073] In the illustrated embodiment, an interference fit is formed between a longitudinally extending, radially outwardly facing circumferential wall of the insert and a longitudinally extending radially inwardly facing wall of the bearing well. Typically, the interference fit is such that the bearing insert and/or the or each magnetic ring is in compression across the operating temperature range of the of rotor, for instance from about ambient temperature (e.g. 20 °C) to about 90 °C, or to about 120, for other applications. Typically, the interference fit is such that the bearing insert and/or the or each magnetic ring is in compression across the across the operating rotational speed of the rotor, for instance up to about lOOOOOrpm.
[074] The illustrated bearing well (7) includes a radially inwardly extending annular shoulder or ledge (15). Once inserted into the well, a distal end of the insert positively engages the shoulder or ledge (15). This may assist with the precise position of the bearing insert (2), and therefore the or each magnet ring (3, 4, 5), within the rotor (1). The bearing insert (2) is typically pushed into the bearing well (7) through the bearing well opening using a press.
[075] As better illustrated in Fig. 2, the sleeve opening may be in the form of a funnel (13). The opening of the funnel having an inner diameter substantially the same as or larger than the outer diameter of the or each magnet ring prior to insertion therein. The funnel end may have an inner diameter smaller than the outer diameter of the or each magnet ring prior to insertion therein. The funnelled entrance (13) to the sleeve facilitates inserting the or each magnet ring (3, 4, 5) into the sleeve.
[076] Similarly, in embodiments and as illustrated in in Fig. 2, the end of the sleeve may have a tapered (14) or stepped leading edge. The leading edge of the sleeve tapering from an outer diameter which is smaller than the inner diameter of the opening of the bearing well to an outer diameter which is greater than the inner diameter of the opening of the bearing well prior to insertion therein. Again, the tapered leading edge of the sleeve facilitates inserting the sleeve (16) into the bearing well (7).
[077] The sleeve (16) may further comprise a radially inwardly extending annular lip (12) at a second end opposite sleeve entrance (13). The annular lip (12) provides an abutment against which a magnet ring (3) of the bearing insert (2) may abut. This may assist with the accurate placement of the or each magnet ring within the sleeve, rotor and vacuum pump. [078] The rotor (1) illustrated in Fig.1 is of a monolithic construction. That is to say the rotor (1), including rotor blades (8), rotor shaft (9) and the rotor bearing well wall (10) are all formed from a single piece of material. In this instance, an aluminium alloy. A multicomponent rotor is also contemplated in which the rotor blades are coupled rotor shaft by an interference fit, typically once the bearing insert is in situ in the rotor bearing well. In said embodiments, the rotor shaft may be machined while the bearing insert is in situ but prior to coupling the rotor blades to the rotor shaft. This may improve tolerances.
[079] The rotor blades (8) are arranged in a series of annular arrays extending radially outwardly from the rotor shaft (9). The size and pitch of the rotor blades will be determined according to the specific requirements of the pump in question; however, generally both the size and pitch of the rotor blades decrease from the lower-pressure end (6) of the rotor shaft (9) towards the relatively higher-pressure end (11 ) of the rotor shaft (10). The bearing well (7) is located towards the lower-pressure end of the rotor shaft (9) in the illustrated embodiment. The bearing insert and magnet ring(s) being held such they are essentially coaxial with the rotational axis (A) of the rotor shaft. In use, the bearing insert and magnet ring(s) rotate about the rotational axis (A) of the rotor shaft.
[080] The permanent magnetic bearing insert comprises a plurality of permanent magnet alloy rings (3, 4, 5), in this instance three. The exemplified permanent magnet alloy rings are made from a ferromagnetic material.
[081] Typically, the sleeve is a monolithic structure. Typically, the sleeve consists substantially of a single material, although, in embodiments, it may be coated and/or anodised.
[082] Preferably, the sleeve comprises, consists essentially of, or consists of aluminium, preferably an aluminium alloy selected from 2000 or 7000 series.
[083] Preferably, the or each magnet alloy ring comprises, consists essentially of, or consists of a ferromagnetic material, preferably Nd2Fei4B (neodymium magnet), SmCos, Sm(Co, Fe, Cu, Zr)?, preferably Nd2Fei4B or SmCos. A neodymium magnet is particularly preferred, particularly sintered neodymium alloy. The or each magnet alloy ring may be coated or plated, such as nickel or zinc plating, or a polymer and/or lacquer coating may be employed.
[084] Preferably the permanent magnet bearing and/or vacuum pump is configured such that the or each magnet alloy ring does not exceed about 120 °C during use.
[085] Preferably the magnet alloy has a Curie temperature from about 310 °C to about 370 °C.
[086] As described earlier, the invention further provides method of manufacturing a vacuum pump, preferably a turbomolecular pump. The pump comprises a rotor shaft configured to have one or more rotor blades coupled thereto and the rotor shaft defining a cavity for receiving a magnetic bearing insert.
[087] The method of the invention will generally comprise the steps of providing a permanent magnetic bearing insert according to the invention and inserting the magnetic bearing insert into the passive magnetic bearing cavity of the rotor of the vacuum pump to form an interference fit.
[088] Typically, the permanent magnetic bearing insert is preassembled prior to step being inserted into the rotor by first inserting the or each permanent magnet alloy ring into the sleeve and forming an interference fit therebetween. Typically, the or each ring is pushed into the sleeve using an external press. In embodiments, the permanent magnetic bearing insert is cooled and/or the portion of the rotor defining the cavity is heated prior to inserting the insert into the cavity.
[089] The sleeve may be machined once the magnet alloy rings are in situ. Typically, the surface of the sleeve which may form the interference fit with the rotor bearing well is machined, for instance a radially outwardly facing circumferentially extending outer face of the sleeve. Performing this machining step once the rings are in situ may reduce tolerances and/or ease manufacturing. Typically, this may be the final machining of the sleeve.
[090] Prior to insertion in the rotor, the insert may be cooled to a temperature below about 0 °C, preferably below about -50 °C, preferably below about -75 °C, for instance using either dry ice or liquid nitrogen. Preferably, the portion of the rotor defining the cavity is heated to a temperature of from about 100 °C to about 150 °C. Once in position the or each magnet alloy ring and the sleeve are allowed to reach ambient temperature.
[091 ] The rotor shaft may be machined once the insert is in situ therein, for example the surface of the rotor shaft which receives an annular array of rotor blades is machined in multiblock rotors. Performing this machining step once the insert is in situ may reduce tolerances and/or ease manufacturing. Typically, this may be the final machining of the rotor. Figure 3 shows a multiblock rotor according to the invention.
[092] In embodiments, one or more rotor blades, typically in the form of one or more annular arrays, are coupled to the rotor shaft, preferably using an interference fit, once the permanent magnetic bearing insert is in situ.
[093] A suitable vacuum pump for use with the permanent bearing inserts and rotor shafts described herein is the nEXT made by Edwards Vacuums.
[094] Figure 3 shows an embodiment of the invention in which the rotor (1 ) is a multiblock rotor. Similar or identical features are identified with corresponding numerals to Figures 1 and 2 respectively. In the illustrated embodiment of Figure 3, the rotor (1 ) comprises a rotor shaft (9) and plurality of separately formed annular arrays (17) of rotor blades (8) coupled thereto with an interference fit. The rotor blade annular arrays (17) may be provided as a single monolithic structure or a plurality of blocks of one or more annular arrays. The or each annular array block may itself be muti-array, having two or more arrays in a single monolithic structure, or a mono-array, having a single annular array.
[095] As described above, the preferably, in a multi-block rotor the rotor blades are coupled to the rotor shaft once the magnetic bearing insert is in situ. As this may allow for improved compression of the permanent magnetic bearing ring(s).
[096] Figure 4, shows an assembled permanent magnetic bearing comprising a bearing insert according to the invention. [097] As illustrated, the magnetic bearing comprises an inner stator bearing half and an outer rotor bearing half, the outer rotor bearing half forming a part of the rotor shaft of the vacuum pump. The illustrated outer rotor bearing half comprises three ring shaped permanent magnets (3,4,5) provided in a permanent magnet bearing insert according to the invention. The bearing insert, and ring-shaped magnets, are substantially coaxially aligned with the axis (A) of rotation of the rotor shaft (9). The bearing further comprises an inner stator bearing half also comprising three ring shaped permanent magnets (18,19,20).
[098] The illustrated permanent magnet rings (18, 19, 20) in the inner stator bearing half and permanent magnet rings in the outer rotor bearing half (3, 4, 5) are magnetised and disposed relative to each other in order to create repulsive forces between the two halves. Thus they suspend the rotor shaft (9) radially.
[099] It will be appreciated that various modifications may be made to the embodiments shown without departing from the spirit and scope of the invention as defined by the accompanying claims as interpreted under patent law.
Key
1 Turbomolecular pump rotor
2 Magnetic bearing insert
3 Magnet ring
4 Magnet ring
5 Magnet ring
6 Low pressure end of the rotor
7 Bearing well
8 Rotor blade
9 Rotor shaft
10 Rotor bearing well wall
11 High-pressure end
12 Annular lip
13 Funnelled entrance
14 Tapered sleeve end
15 Shoulder / ledge
16 Sleeve
17 Annular array
18 Magnet ring
19 Magnet ring
20 Magnet ring

Claims

What is claimed:
1 . A vacuum pump, preferably a turbomolecular pump, comprising a rotor shaft configured to have one or more rotor blades coupled thereto and the rotor shaft defining a bearing well containing, in an interference-fit configuration, a permanent magnetic bearing insert, wherein the magnetic bearing insert comprises one or more permanent magnet alloy rings of a rotor bearing half of a permanent magnetic bearing and a radially outwardly extending sleeve coupled thereto around an outer circumference of the or each said permanent magnet alloy ring, and an outer surface of the permanent magnetic bearing insert engages with an inward facing wall of the bearing well to provide an interference fit, wherein the radially outwardly extending sleeve has a coefficient of thermal expansion that is at least substantially the same as the coefficient of thermal expansion of the material of the rotor shaft defining the engaged bearing well wall.
2. The vacuum pump according to claim 1 , wherein the radially outwardly extending sleeve has a coefficient of thermal expansion that is substantially the same as the coefficient of thermal expansion of the material of the rotor shaft defining the engaged bearing well wall.
3. The vacuum pump according to claim 1 or claim 2, wherein the or each permanent magnet alloy ring is coupled to the sleeve by an interference fit.
4. The vacuum pump according to any preceding claim wherein the permanent magnet alloy ring is coupled to the sleeve prior to the sleeve being inserted into the bearing well of the pump rotor.
5. The vacuum pump according to any preceding claim wherein the magnetic bearing insert is machined after the permanent magnet alloy ring is coupled to the sleeve.
6. The vacuum pump according to any one of claims 3 or 4, wherein the rotor is final machined after fitting the insert.
7. The vacuum pump according to any preceding claim, wherein the bearing well is defined by an aluminium portion of the rotor shaft; and/or wherein the sleeve is aluminium.
8. The vacuum pump according to any preceding claim, wherein the permanent magnet alloy ring has a coefficient of thermal expansion in the circumferential direction of less than about 4x10"6 K’1.
9. The vacuum pump according to any preceding claim wherein the or each permanent magnet alloy ring comprises a neodymium magnet magnetised either in the axial or radial direction.
10. The vacuum pump according to any preceding claim wherein the rotor shaft and one or more rotor blades are monolithic, and/or wherein one or more of said rotor blades forms a part of an annular rotor blade array coupled to the rotor shaft by an interference fit.
11 . A method of manufacturing a vacuum pump, preferably a turbomolecular pump, according to any one of claims 1 to 10, the pump comprising a rotor shaft configured to have one or more rotor blades coupled thereto and the rotor shaft defining a bearing well for receiving a magnetic bearing insert, the method comprising the steps of: a. providing a permanent magnetic bearing insert comprising one or more permanent magnet alloy rings of a rotor bearing half of a permanent magnetic bearing and a radially outwardly extending sleeve coupled thereto around an outer circumference of the or each said permanent magnet alloy ring, and b. inserting the magnetic bearing insert into the rotor bearing well of the vacuum pump rotor and forming an interference fit, and wherein the radially outwardly extending sleeve has a coefficient of thermal expansion that is at least substantially the same as, preferably substantially the same as, the coefficient of thermal expansion of the material of the rotor shaft defining the engaged bearing well wall, optionally wherein the permanent magnetic bearing insert is cooled and/or the portion of the rotor defining the bearing well is heated prior to inserting the bearing insert into the bearing well.
12. The method of claim 11 wherein the permanent magnetic bearing insert is preassembled prior to step a) by inserting the permanent magnet alloy ring into the sleeve and forming an interference fit, and/or wherein one or more rotor blades are coupled to the rotor shaft following step b).
13. A permanent magnetic bearing insert for a vacuum pump, the vacuum pump comprising a rotor shaft having one or more rotor blades coupled thereto and the rotor shaft defining a bearing well configured to receive the magnetic bearing insert in an interference-fit configuration, wherein the magnetic bearing insert comprises one or more permanent magnet alloy rings of a rotor bearing half of a permanent magnetic bearing and a radially outwardly extending sleeve coupled thereto around an outer circumference of the or each said permanent magnet alloy ring, and an outer surface of the permanent magnetic bearing insert is configured to engage with an inward facing wall of the bearing well following insertion therein, wherein the radially outwardly extending sleeve has a coefficient of thermal expansion that is at least substantially the same, preferably substantially the same, as the coefficient of thermal expansion of the material of the rotor shaft defining the engaged bearing well wall.
14. A vacuum pump according to any one of claims 1 to 10 comprising a permanent magnetic bearing insert according to claim 13.
15. The use of an neodymium magnet alloy in a vacuum pump according to claims 1 to 10 or 14 or permanent magnetic bearing insert according to claim 13; or the use of a neodymium magnet in a vacuum pump according to any one of claims 1 to 10.
EP24729342.6A 2023-06-08 2024-05-14 Permanent magnetic bearing insert Pending EP4724706A1 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
GB2308520.2A GB2630786A (en) 2023-06-08 2023-06-08 Permanent magnetic bearing insert
PCT/GB2024/051248 WO2024252121A1 (en) 2023-06-08 2024-05-14 Permanent magnetic bearing insert

Publications (1)

Publication Number Publication Date
EP4724706A1 true EP4724706A1 (en) 2026-04-15

Family

ID=87291478

Family Applications (1)

Application Number Title Priority Date Filing Date
EP24729342.6A Pending EP4724706A1 (en) 2023-06-08 2024-05-14 Permanent magnetic bearing insert

Country Status (4)

Country Link
EP (1) EP4724706A1 (en)
CN (1) CN121285697A (en)
GB (1) GB2630786A (en)
WO (1) WO2024252121A1 (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN121356281B (en) * 2025-12-18 2026-03-27 中国科学院电工研究所 A lightweight permanent magnet propulsion motor resistant to high and low temperatures and low air pressure

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2009092039A (en) * 2007-10-11 2009-04-30 Nabtesco Corp Two-stage screw type vacuum pump
JP2009092040A (en) * 2007-10-11 2009-04-30 Nabtesco Corp 2-stage vacuum pump
GB2467966B (en) * 2009-02-24 2013-04-03 Dyson Technology Ltd Rotor assembly
DE102014105581A1 (en) * 2014-04-17 2015-11-05 Pfeiffer Vacuum Gmbh vacuum pump
GB2578899B (en) * 2018-11-13 2021-05-26 Edwards Ltd Vacuum pump
GB2601320B (en) * 2020-11-25 2023-04-26 Edwards S R O Rotor assembly for a turbomolecular pump

Also Published As

Publication number Publication date
CN121285697A (en) 2026-01-06
WO2024252121A1 (en) 2024-12-12
GB2630786A (en) 2024-12-11
GB202308520D0 (en) 2023-07-26

Similar Documents

Publication Publication Date Title
US8344576B2 (en) Electric motor rotor
CN215870980U (en) Motor, rotor hole alignment device and air diffuser
CN101845987B (en) Seal device of compressor side shaft of exhaust gas turbocharger
US20150222164A1 (en) Electric motor rotor
EP2942537B1 (en) Bearing sleeve for air bearing
US7075204B2 (en) Threaded inner sleeve for generator magnet
EP4724706A1 (en) Permanent magnetic bearing insert
US7854059B2 (en) Apparatus for assembling rotor of permanent magnet motor
US20120243986A1 (en) Turbo machine
CN108900018A (en) Rotate electricapparatus
US9771938B2 (en) Rotary device having a radial magnetic coupling
CN109790847B (en) Modular turbo-compressor shaft
US20190238016A1 (en) Rotor for an electric machine, electric machine with the rotor and to method for producing the rotor
US8167576B2 (en) Method for manufacturing the rotor assembly of a rotating vacuum pump
EP1521348A3 (en) Electrical machine
CN105103410A (en) Rotor shaft of high speed permanent magnet motor
JP6284495B2 (en) Method for the production of a rotor device for a vacuum pump and a rotor device for a vacuum pump
US6551191B2 (en) Coupling apparatus
CN111371213A (en) Compressor rotors, compressors and refrigerant circulation systems
JP3144272U (en) Turbo molecular pump
JP2002070787A (en) Vacuum pump
CN111365293B (en) Compressor rotor, compressor and air conditioning equipment
CN209344880U (en) Compressor rotor, compressor and refrigerant circulation system
US7565731B2 (en) Methods of manufacturing a rotor assembly
EP3728857B1 (en) Magnetic shield for a vacuum pump

Legal Events

Date Code Title Description
STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: UNKNOWN

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: THE INTERNATIONAL PUBLICATION HAS BEEN MADE

PUAI Public reference made under article 153(3) epc to a published international application that has entered the european phase

Free format text: ORIGINAL CODE: 0009012

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: REQUEST FOR EXAMINATION WAS MADE

17P Request for examination filed

Effective date: 20251215

AK Designated contracting states

Kind code of ref document: A1

Designated state(s): AL AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC ME MK MT NL NO PL PT RO RS SE SI SK SM TR