GB2467969A - Bearing support - Google Patents

Bearing support Download PDF

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Publication number
GB2467969A
GB2467969A GB0903058A GB0903058A GB2467969A GB 2467969 A GB2467969 A GB 2467969A GB 0903058 A GB0903058 A GB 0903058A GB 0903058 A GB0903058 A GB 0903058A GB 2467969 A GB2467969 A GB 2467969A
Authority
GB
United Kingdom
Prior art keywords
bore
bearing
adhesive
wall
diffuser
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.)
Granted
Application number
GB0903058A
Other versions
GB2467969B (en
GB0903058D0 (en
Inventor
David Ions
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.)
Dyson Technology Ltd
Original Assignee
Dyson Technology 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 Dyson Technology Ltd filed Critical Dyson Technology Ltd
Priority to GB0903058.6A priority Critical patent/GB2467969B/en
Publication of GB0903058D0 publication Critical patent/GB0903058D0/en
Priority to JP2011551525A priority patent/JP5535245B2/en
Priority to PCT/GB2010/050212 priority patent/WO2010097609A1/en
Priority to US12/707,380 priority patent/US9109626B2/en
Publication of GB2467969A publication Critical patent/GB2467969A/en
Application granted granted Critical
Publication of GB2467969B publication Critical patent/GB2467969B/en
Priority to JP2014088347A priority patent/JP5849325B2/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16CSHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C35/00Rigid support of bearing units; Housings, e.g. caps, covers
    • F16C35/04Rigid support of bearing units; Housings, e.g. caps, covers in the case of ball or roller bearings
    • F16C35/06Mounting or dismounting of ball or roller bearings; Fixing them onto shaft or in housing
    • F16C35/063Fixing them on the shaft
    • 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
    • F16C35/08Rigid support of bearing units; Housings, e.g. caps, covers for spindles
    • F16C35/12Rigid support of bearing units; Housings, e.g. caps, covers for spindles with ball or roller 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
    • F16C25/00Bearings for exclusively rotary movement adjustable for wear or play
    • F16C25/06Ball or roller bearings
    • F16C25/08Ball or roller bearings self-adjusting
    • F16C25/083Ball or roller bearings self-adjusting with resilient means acting axially on a race ring to preload the bearing
    • 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
    • F16C35/04Rigid support of bearing units; Housings, e.g. caps, covers in the case of ball or roller bearings
    • F16C35/06Mounting or dismounting of ball or roller bearings; Fixing them onto shaft or in housing
    • F16C35/067Fixing them in a housing
    • 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
    • F16C35/04Rigid support of bearing units; Housings, e.g. caps, covers in the case of ball or roller bearings
    • F16C35/06Mounting or dismounting of ball or roller bearings; Fixing them onto shaft or in housing
    • F16C35/07Fixing them on the shaft or housing with interposition of an element
    • F16C35/077Fixing them on the shaft or housing with interposition of an element between housing and outer race ring
    • 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
    • F16C19/00Bearings with rolling contact, for exclusively rotary movement
    • F16C19/02Bearings with rolling contact, for exclusively rotary movement with bearing balls essentially of the same size in one or more circular rows
    • F16C19/04Bearings with rolling contact, for exclusively rotary movement with bearing balls essentially of the same size in one or more circular rows for radial load mainly
    • F16C19/06Bearings with rolling contact, for exclusively rotary movement with bearing balls essentially of the same size in one or more circular rows for radial load mainly with a single row or balls
    • 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
    • F16C2226/00Joining parts; Fastening; Assembling or mounting parts
    • F16C2226/30Material joints
    • F16C2226/40Material joints with adhesive
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16CSHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C2360/00Engines or pumps
    • F16C2360/42Pumps with cylinders or pistons
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16CSHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C2360/00Engines or pumps
    • F16C2360/44Centrifugal pumps

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  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Mounting Of Bearings Or Others (AREA)

Abstract

A bearing support 1 comprising a body 2 through which a bore 3 extends and a plurality of grooves 4,5 formed in a wall 6 of the bore 3, each groove 4,5 extending from a first end 7 of the bore 3 and terminating prior to a second end 8 of the bore 3. A bearing 12 may be secured within the bearing support 1 by injecting adhesive 13 into one or more of the grooves 4,5. Also claimed is a diffuser (22 in Figure 4) which comprises the same features as does the bearing support and a compressor comprising a rotor mounted in such a diffuser.

Description

Bearing Support The present invention relates to a support into which a bearing may be secured by adhesive.
A rotor is typically mounted to a support by one or more bearings. Each bearing may be press fit into a bore within the support. However, this requires high-precision manufacturing of both the support and the bearing. As an alternative to press fitting, each bearing may be adhered within a bore of the support. However, there is often difficulty in ensuring that an even coverage of adhesive is provided between the bearing and the support. This difficulty is compounded by the fact that, once the bearing is seated within the bore, it is not easy to rotate the bearing relative to the support.
Insufficient or uneven coverage of adhesive may subsequently result in failure of the adhesive.
In a first aspect, the present invention provides a bearing support comprising a body through which a bore extends and a plurality of grooves formed in a wall of the bore, each groove extending from a first end of the bore and terminating prior to a second end of the bore.
The bore is dimensioned such that, when a bearing is seated within the bore, a clearance exits between the bearing and the wall of the bore. Once the bearing is seated within the bore, adhesive may be injected into one or more of the grooves. The grooves act to deliver the adhesive to the bottom of the bore. Owing to the clearance between the bearing and the wall of the bore, the adhesive wicks around the bottom of the bore. As adhesive continues to be injected into the grooves, the adhesive rises within the bore thereby driving out any air. The result is an even distribution of adhesive between the bearing and the wall of the bore.
The term bearing is intended encompasses both a single bearing (e.g. ball bearing, needle roller bearing or double row bearing) and a plurality of bearings forming part of a single bearing assembly (e.g. a bearing cartridge).
Each groove preferably extends in a direction parallel to a longitudinal axis of the bore.
Consequently, any adhesive injected into a groove is quickly delivered to the bottom of the groove. By delivering adhesive quickly to the bottom of the groove, the adhesive wicks first around the bottom of the bore. As further adhesive is delivered, the adhesive then rises from the bottom of the bore, thereby minimising the risk of trapped air.
The bore is ideally tapered towards the second end. This then has the advantage that, as the adhesive rises within the bore, the air is driven out into an expanding volume and thus the risk of air entrapment is further reduced. Furthermore, by having a tapered bore, the cured adhesive forms a wedge between the bearing and the bearing support.
This wedge acts to oppose axial thrust acting on the bearing relative to the bearing support.
The wall of the bore is preferably chamfered at the first end. The chamfered portion of the bore may then serve as a reservoir for the rising adhesive. Consequently, tight controls on the volume of adhesive injected into the grooves are not required. Instead, a fixed volume of adhesive can be injected that ensures good coverage without the danger of overfilling. Furthermore, the chamfered portion provides a relatively large region over which the adhesive can be initially cured, e.g. by UV light. The cured adhesive within the chamfered portion then acts to hold the bearing to the bearing support whilst the remainder of the adhesive within the bore cures, e.g. anaerobically. This then removes the danger of possible movement of the bearing relative to the bearing support during curing, which might otherwise result in a weak adhesive join.
Advantageously, the bearing support comprises two grooves located on opposite sides of the bore. By providing grooves on opposite sides of the bore, adhesive may be injected into one groove, which then wicks around the bore before bleeding into the second groove. This then encourages complete coverage of adhesive between the bearing and the wall of the bore. Moreover, the adhesive process is simplified since adhesive need only be injected into one groove.
Press fitting a bearing into a bore requires high-precision manufacturing of both the bearing and the support. As such, certain materials and processes are excluded from use since it is not possible to obtain the required tolerances. In contrast, the adhesive acts to absorb manufacturing tolerances in the bearing and/or the support. Accordingly, the bearing support may be formed of plastic using, for example, injection or compression moulding.
In a second aspect, the present invention provides a diffuser comprising a hub through which a bore extends and a plurality of grooves formed in a wall of the bore, each groove extending from a first end of the bore and terminating prior to a second end of the bore.
A rotor may then be adhered within the bore of the diffuser. Since the rotor is secured directly to the diffuser, accurate alignment of the rotor relative to the diffuser is made possible. In particular, the rotor may be adhered to the diffuser such that the rotor and diffuser are concentric. This in contrast to other compressors in which the rotor is not directly secured to the diffuser and thus geometric tolerances may result in misalignment of the rotor and diffuser. Additionally, the manufacture and assembly of the diffuser and rotor is made both simpler and cheaper.
The bore preferably extends from a first side of the hub to a second side of the hub, and the diffuser comprises a plurality of vanes located on the second side of the hub. Each groove then extends from the first side and terminates prior to the second side of the hub. As a result, adhesive is injected into the grooves from a side of the hub opposite to that on which the vanes are located. This has the advantage that a rotor having an impeller may be secured to the diffuser. The rotor may therefore be dynamically balanced as a complete unit before being secured to the diffuser. This is contrast to other rotor-diffuser assemblies in which the shaft of the rotor must first be secured to the diffuser and then the impeller is subsequently secured to the shaft.
The bore is ideally tapered towards the second side of the hub. Consequently, as adhesive rises within the bore, air is driven out by the adhesive into an expanding volume and thus the risk of air entrapment is reduced. Furthermore, the adhesive forms a wedge that opposes axial thrust acting on the rotor when in operation.
In a third aspect, the present invention provides an assembly comprising a bearing secured within a bearing support, the bearing support comprising a body through which a bore extends and a plurality of grooves formed in a wall of the bore, each groove extending from a first end of the bore and terminating prior to a second end of the bore, and the bearing is secured within the bore by adhesive located between the bearing and the wall and within the grooves.
The bore is dimensioned (i.e. has a particular diameter andlor degree of taper) such that a clearance exists between the bearing and the wall of the bore. The bearing is secured to the support by adhesive that fills the clearance between the bearing and the wall.
In a fourth aspect, the present invention provides a compressor comprising a rotor mounted to a diffuser, the rotor comprising a shaft to which are mounted an impeller and a bearing, and the diffuser comprises a hub through which a bore extends and a plurality of grooves are formed in a wall of the bore, each groove extending from a first end of the bore and terminating prior to a second end of the bore, wherein the bearing is secured within the bore by adhesive located between the bearing and the wall and within the grooves.
The bore is dimensioned such that a clearance exists between the bearing and the wall of the bore. By providing a clearance, the rotor and the diffuser may be accurately aligned without the need for high-precision manufacturing. The adhesive then fills the clearance between the bearing and the wall of the bore so as maintain alignment of the rotor relative to the diffuser.
The bearing is preferably a bearing cartridge comprising a pair of spaced bearings surrounded by a sleeve, and the adhesive is located between the sleeve and the wall.
This then has the advantage that the rotor is supported over a relatively long length, thereby providing good stability. Moreover, the sleeve provides a relatively large surface over which the adhesive secures the rotor to the diffuser, and thus a good bond is formed between the rotor and the bearing support.
In a fifth aspect, the present invention provides a method of securing a bearing to a support, the method comprising: providing a bearing support, the bearing support comprising a body through which a bore extends and a plurality of grooves formed in a wall of the bore, each groove extending from a first end of the bore and terminating prior to a second end of the bore; inserting a bearing into the bore; and injecting adhesive into one or more of the grooves.
The bore is dimensioned such that a clearance exists between the bearing and the wall of the bore. This size of this clearance is ideally chosen so as to permit good wicking of the adhesive whilst simultaneously preventing the adhesive from seeping out through the bottom of the bore.
Preferably, at least one groove is precluded from adhesive injection. More preferably, for each groove into which adhesive is injected, an adjacent groove is precluded from adhesive injection. This then allows the adhesive injected into one groove to wick around the bore and bleed into an adjacent groove, thereby encouraging an even distribution of adhesive.
In order that the present invention may be more readily understood, embodiments of the invention will now be described, by way of example, with reference to the accompanying drawings, in which: Figure 1 is a plan view of a bearing support in accordance with the present invention; Figure 2 is a sectional view of the bearing support of Figure 1 along the line X--X; Figure 3 is a sectional view of a rotor secured within the bearing support of Figures 1 and 2; and Figure 4 is a sectional view of a compressor incorporating the bearing support of Figures 1 and 2.
The bearing support 1 of Figures 1 and 2 comprises a main body 2 through which a bore 3 extends. A pair of grooves 4,5 are formed along a wall 6 of the bore 3. The grooves 45 are located on opposite sides of the bore 3 and extend linearly in a direction parallel to the longitudinal axis of the bore 3. Moreover, each groove 4,5 extends from a first end 7 of the bore 3 and terminates prior to a second, opposite end 8 of the bore 3.
Consequently, each groove 4,5 does not extend along the full length of the bore 3 but is instead closed at one end.
The bore 3 is tapered towards the second end 8, i.e. the diameter of the bore 3 at the first end 5 is greater than that at the second end 6. Additionally, the wall 6 of the bore 3 is chamfered 9 at the first end 7.
A method of securing of a bearing within the bearing support I will now be described with reference to Figure 3.
Figure 3 illustrates a rotor 10 comprising a shaft 11 to which a bearing 12 is mounted.
Although not shown, the shaft 11 of the rotor 10 is held in one half of a jig and the bearing support 1 is held in another half of the jig. The two halves of the jig are brought together such that the rotor 10 extends through the bearing support 1 and the bearing 12 is seated within the bore 3 of the support 1, as is illustrated in Figure 3. The two halves of the jig are aligned so as to ensure accurate alignment of the rotor 10 within the bearing support 1. The bore 3 is dimensioned (i.e. has a particular diameter and degree of taper) such that a clearance is achieved between the wall 6 of the bore 3 and the bearing 12, the importance of which is described below.
After the two halves of the jig have been brought together, adhesive 13 is injected into the open top of the first groove 4. The adhesive is a UV-curable anaerobic adhesive; however, alternative adhesives might equally be used. Under the influence of gravity, the adhesive 13 flows down to the closed end of the groove 4. From here, the adhesive 13 wicks between the bearing 12 and the wall 6 of the bore 3. The adhesive 13 wicks around the bottom of the bore 3 from the first groove 4 to the second groove 5.
The adhesive 13 then bleeds into and begins to fill the second groove 5. As the level of adhesive 13 in the second groove 5 rises, the level of adhesive 13 in the first groove 4 drops. The first groove 4 may therefore be regarded as a runner for the adhesive 13, and the second groove 5 may be regarded as a riser. As adhesive 13 continues to be injected into the first groove 4, the level of the adhesive 13 within the bore 3 and the grooves 4,5 rises. As the level of the adhesive 13 approaches the top of the bore 3, adhesive 13 begins to fill the chamfered portion of the bore 3. Injection of adhesive 13 into the first groove 4 is then halted. The net result is an even and continuous distribution of adhesive 13 between the bearing 12 and the wall 6 of the bore 3. Owing to the relatively small clearance between the bearing 12 and the bottom end 8 of the bore 3, no adhesive 13 seeps through the bottom of the bore 3. Finally, the adhesive 13 is cured.
For this particular type of adhesive, curing is achieved by illuminating the top end 7 of the bore 3 with UV light. This then cures the adhesive 13 within the chamfered portion of the bore 3. The remainder of the adhesive 13 along the length of the bore 3 then cures anaerobically.
The bore 3 is dimensioned (i.e. has a diameter and degree of taper) such that a relatively small clearance is achieved between the wall 6 of the bore 3 and the bearing 12. This clearance should be sufficiently large to encourage wicking of the adhesive 13 whilst ensuring that no adhesive 13 seeps through the bottom of the bore 3. For many types of adhesive, it is possible to have a sizeable clearance between the bearing 12 and the wall 6 of the bore 3 without the adhesive seeping out through the bottom of the bore 3.
However, as the size of the clearance increases, the amount of adhesive needed to secure the bearing 12 increases. Not only does this increase the cost of securing the bearing 12, but it also increases the length of time necessary to cure the adhesive 13.
Accordingly, the clearance is ideally no bigger than that necessary to achieve acceptable wicking times. The dimension of the bore 3 and the resulting clearance with the bearing 12 will therefore depend upon the choice of adhesive and in particular the viscosity of the adhesive. By way of example only, a difference in the diameters of the bore 3 and bearing 12 of between 0.3 mm and 0.5 mm has been found to work well for an adhesive having a viscosity of between 400 -600 mPa.s (Brookfield RVT, spindle 2 at 20 rpm, 25°C).
The bearing support 1 of the present invention provides significant advantages over conventional means of securement. In contrast to press fitting, a bearing 12 may be secured within the bearing support 1 without the need for high-precision manufacturing.
The bearing support 1 thus offers a cheaper method of securing and supporting a rotor 10. Furthermore, the bearing support 1 may be formed from materials and processes that would otherwise be precluded from use owing to the associated tolerances. In particular, the bearing support 1 may be formed of a plastic material using compression or injection moulding. The bearing support 1 therefore enables a rotor 10 to be supported and accurately aligned using cheaper materials and processes.
If the bearing 12 were secured within a conventional bore (i.e. a bore having no grooves), any adhesive injected into the top of the bore would wick slowly downwards.
Indeed, owing to the wicking length associated with the adhesive, it may prove impossible to deliver adhesive along the full length of the bearing. In addition, the adhesive would most likely trap pockets of air resulting in incomplete and uneven distribution of adhesive. Once the bearing 12 is seated within the bore, it is not easy to rotate the bearing 12 in order to obtain a more even distribution of adhesive. In particular, any attempt to rotate the shaft 11 of the rotor 10 will only cause the inner race of the bearing 12 to rotate relative to the outer race. During subsequent use of the rotor 10, any uneven distribution of adhesive may result in failure of the adhesive, causing the bearing 12 to separate from the support.
With the bearing support 1 of the present invention, a more complete and even coverage of adhesive 13 is achieved. This is made possible through the provision of grooves 4,5, which act to deliver adhesive 13 to the bottom of the bore 3 and bearing 12. Since adhesive is delivered to the bottom of the bore 3, the adhesive 13 first wicks around the bottom of the bore 3. As the adhesive 13 wicks around the bore 3, the adhesive 13 drives out any air between the bearing 12 and the wall 6 of the bore 3. By injecting adhesive 13 into only one of the grooves 4, air is driven by the adhesive 13 both upwards and into the other groove 5, which then acts as a flue for the air.
Consequently, no air is trapped by the adhesive 13. In addition to providing a more even coverage of adhesive 13, the time required for the adhesive 13 to wick between the bearing 12 and the wall of the bore 3 is significantly reduced.
The provision of a tapered bore 3 has two key benefits. First, by tapering the bore towards the bottom end 8 (i.e. the second end 8) of the bore 3, adhesive 13 rising within the bore 3 drives air upwards into an expanding volume and thus the risk of air entrapment is further reduced. Second, axial thrust acting on the rotor 10 creates a shearing force between the bearing 12 and the bearing support 1. By having a tapered bore 3, the cured adhesive 13 forms a wedge between the bearing 12 and the bearing support 1. This wedge then acts to oppose axial thrust operating in a direction from the top 7 to the bottom 8 of the bore 3. In spite of the aforementioned advantages, the taper in the bore 3 is not essential and may be omitted.
The chamfer 9 in the top end 7 (i.e. the first end 7) of the bore 3 similarly has two key benefits. First, the chamfer 9 acts as a reservoir for the rising adhesive 13.
Consequently, tight control on the volume of adhesive 13 injected into the groove 4 is not required. Instead, a fixed volume of adhesive 13 can be injected into the groove 4 that achieves good coverage without the risk of adhesive 13 spilling out of the bore 3 and on to the bearing 12. This naturally has benefits for automated assembly. Second, movement of the bearing 12 relative to the bearing support 1 during curing is likely to result in a weak adhesive join. The chamfer 9 provides a region over which a portion of the adhesive 13 can be cured quickly and easily, e.g. by UV light. The adhesive cured within the chamfered portion 9 of the bore 3 then acts to hold the bearing 12 to the bearing support 1 whilst the remainder of the adhesive 12 within the bore 3 cures, e.g. anaerobically. Consequently, relative movement of the bearing 12 and bearing support 1, as the adhesive 13 within the bore 3 is curing, is prevented. Again, whilst the chamfer 9 in the wall 6 of the bore 3 has particular benefits, the provision of a chamfer 9 is not essential and may be omitted.
In the example illustrated in Figure 3, the length of the bearing 12 is relatively short.
However, the bearing support 1 of the present invention is of particular benefit in securing bearings of longer length, e.g. bearing assemblies, needle roller bearings, double row bearings. When securing a longer-length bearing into a conventional bore, the likelihood of trapped air increases, as does the time required for the adhesive to wick. Moreover, as already noted above, it may not be possible to deliver adhesive along the full length of the bearing owing to the limited wicking length associated with the adhesive. In contrast, the bearing support 1 of the present invention is not so restricted. The grooves 4,5 provide means by which adhesive 13 can be delivered to the bottom of the bore 3. Consequently, even for an adhesive having a wicking length shorter than that of the bearing length, it is still possible to achieve an even distribution of adhesive 13 along the full length of the bearing 12.
The bearing support 1 may form any part of a structure to which a rotor is mounted. By way of example, Figure 4 illustrates a compressor 20 in which the bearing support I forms an integral part of a diffuser 22. In addition to the diffuser 22, the compressor 20 comprises a rotor 21 rotatably mounted to the diffuser 22.
The rotor 21 comprises a shaft 23 to which are secured an impeller 24 and a bearing cartridge 25. The bearing cartridge 25 comprises a pair of spaced bearings 26 preloaded by a spring 27 and surrounded by a sleeve 28.
The diffuser 22 comprises a hub 29 around which a plurality of vanes 30 are circumferentially spaced. The hub 29 serves as the body 2 of a bearing support I and includes a central bore 3. The bore 3 extends from a first side 31 (e.g. the upper side) to a second side 32 (e.g. the lower side) of the hub 29, the vanes 30 being located on the second side 32 of the hub 29. The bore 3 is tapered towards the second side 32 of the hub 29, and is chamfered around the end adjacent the first side 31 of the hub 29. A pair of grooves 4,5 are formed along a wall 6 of the bore 3 and extend from a first end 7 of the bore 3 and terminate prior to a second end 8 of the bore 3. More particularly, each groove 4,5 extends from the first side 31 and terminates prior to the second side 32 of the hub 29.
The rotor 21 is mounted to the diffuser 22 in the manner described above with reference to Figure 3. In particular, the rotor 21 and diffuser 22 are each held in one half of ajig.
The two halves of the jig are aligned and brought together, thereby ensuring that the rotor 21 is accurately aligned relative to the diffuser 22. Adhesive 13 is then injected into one of the grooves 4. As the level of adhesive 13 rises and begins to fill the chamfered portion 9 of the bore 3, injection of adhesive 13 into the groove 4 is halted, and the adhesive 13 is cured.
The bearing cartridge 25, in having two spaced bearings 26, supports the rotor 21 over a relatively long length and thus provides good stability. Moreover, the sleeve 28 of the bearing cartridge 25 provides a single, relatively large surface over which the rotor 21 may be secured to the diffuser 22.
In providing a diffuser 22 that incorporates a bearing support 1, accurate alignment of the rotor 21 relative to the diffuser 22 is made much simpler. In particular, the rotor 21 can be secured directly to the diffuser 22 such that the rotor 21 and diffuser 22 are concentric. This in contrast in to other compressors in which the rotor is not directly secured to the diffuser and thus geometric tolerances may result in misalignment of the rotor and diffuser. Furthermore, in providing a diffuser 22 that serves as a bearing support 1, the manufacture and assembly of the compressor 20 is made both simpler and cheaper.
Each groove 4,5 extends from a first side 31 of the diffuser 22, whilst the vanes 30 are located on an opposite, second side 32 of the diffuser 22. Consequently, adhesive 13 is injected into the groove 4 from a side 31 of the diffuser 22 opposite to that on which the vanes 30 are located. This has the advantage that a rotor 21 having an impeller 24 may be secured to the diffuser 22. The rotor 21 may therefore be dynamically balanced as a complete unit before being secured to the diffuser 22. This is contrast to a compressor in which the shaft must first be secured to the diffuser and then the impeller is subsequently secured to the shaft.
During operation of the compressor 20, the rotor 21 experiences axial thrust due to pressure differentials between the two sides 31,32 of the diffuser 22 and between the front and rear sides of the impeller 24. The axial thrust acts on the rotor 21 in a direction from the first side 31 to the second side 32 of the diffuser 22 (i.e. in a downward direction for the compressor 20 illustrated in Figure 4). By tapering the bore 3 in the diffuser 22, the cured adhesive 13 forms a wedge between the bearing cartridge 25 and the diffuser 22. Since the bore 3 is tapered towards the second side 32 of the diffuser 22, axial thrust on the rotor 21 is opposed by the wedge of adhesive 13.
In each of the embodiments described above, the bearing support 1 has only two grooves 4,5. Additional grooves may, however, be provided in the wall 6 of the bore 3.
By providing additional grooves, adhesive 13 may be injected into more than one groove and thus adhesive delivery times may be shortened. This may prove particularly useful when using a relatively viscous adhesive or if the bore 3 and bearing 12 have relatively large surface areas. Although adhesive 13 may be injected into more than one groove, at least one groove is ideally precluded from adhesive injection so as to allow air to be driven into the precluded groove. Indeed, for each groove into which adhesive 13 is injected, an adjacent groove is ideally precluded from adhesive injection.
Although at least one groove is ideally precluded from adhesive injection, adhesive 13 may nevertheless be injected into all grooves 4,5 of the bearing support 1. This continues to provide the benefit of delivering adhesive 13 to the bottom of the bore 3.
The adhesive 13 then wicks around the bottom of the bore 3, and as more adhesive 13 is injected, the level of adhesive 13 rises within the bore 3 thereby driving air out.
However, injecting adhesive 13 into all grooves 4,5 may increase the risk of air entrapment, particularly if the adhesive 13 has a relatively high viscosity. Any increased propensity to air entrapment may be addressed by injecting the adhesive 13 into the grooves 4,5 at a slower rate (thereby giving the adhesive 13 sufficient time to wick fully around the bore 3 before the level of adhesive 13 rises) or by increasing the clearance between the bearing 12 and the wall 6 of the bore 3 (e.g. by increasing the diameter andlor the degree of taper in the bore 3).
With the bearing support 1 of the present invention, a rotor 10,21 may be secured in a manner that ensures accurate alignment without the need for high-precision manufacturing. The bearing support 1 thus provides a cheaper means for securing a rotor 10,21 without compromising on alignment. Moreover, the bearing support 1 ensures that a complete and even distribution of adhesive 13 between the support 1 and a bearing 12,25 of the rotor 10,2 1 may be achieved over a relatively short timescale.

Claims (21)

  1. CLAIMS1. A bearing support comprising a body through which a bore extends and a plurality of grooves formed in a wall of the bore, each groove extending from a first end of the bore and terminating prior to a second end of the bore.
  2. 2. A bearing support as claimed in claim 1, wherein each groove extends in a direction parallel to a longitudinal axis of the bore.
  3. 3. A bearing support as claimed in claim 1 or 2, wherein the bore is tapered towards the second end.
  4. 4. A bearing support as claimed in any one of the preceding claims, wherein the wall of the bore is chamfered at the first end.
  5. 5. A bearing support as claimed in any one of the preceding claims, wherein the support comprises two grooves located on opposite sides of the bore.
  6. 6. A bearing support as claimed in any one of the preceding claims, wherein the bearing support is formed of plastic.
  7. 7. A diffuser comprising a hub through which a bore extends and a plurality of grooves formed in a wall of the bore, each groove extending from a first end of the bore and terminating prior to a second end of the bore.
  8. 8. A diffuser as claimed in claim 7, wherein the bore extends from a first side of the hub to a second side of the hub, each groove extends from the first side and terminates prior to the second side, and the diffuser comprises a plurality of vanes located on the second side of the hub.
  9. 9. A diffuser as claimed in claim 8, wherein the bore is tapered towards the second side of the hub.
  10. 10. An assembly comprising a bearing secured within a bearing support, the bearing support comprising a body through which a bore extends and a plurality of grooves formed in a wall of the bore, each groove extending from a first end of the bore and terminating prior to a second end of the bore, and the bearing is secured within the bore by adhesive located between the bearing and the wall and within the grooves.
  11. 11. An assembly as claimed in claim 10, wherein the bore is dimensioned such that a clearance exists between the bearing and the wall of the bore, and the adhesive is located within the clearance between the bearing and the wall.
  12. 12. A compressor comprising a rotor mounted to a diffuser, the rotor comprising a shaft to which are mounted an impeller and a bearing, and the diffuser comprises a hub through which a bore extends and a plurality of grooves are formed in a wall of the bore, each groove extending from a first end of the bore and terminating prior to a second end of the bore, wherein the bearing is secured within the bore by adhesive located between the bearing and the wall and within the grooves.
  13. 13. A compressor as claimed in claim 12, wherein the rotor and diffuser are concentric.
  14. 14. A compressor as claimed in claim 12 or 13, wherein the bearing is a bearing cartridge comprising a pair of spaced bearings surrounded by a sleeve, and the adhesive is located between the sleeve and the wall.
  15. 15. A method of securing a bearing to a support, the method comprising: providing a bearing support, the bearing support comprising a body through which a bore extends and a plurality of grooves formed in a wall of the bore, each groove extending from a first end of the bore and terminating prior to a second end of the bore; inserting a bearing into the bore; and injecting adhesive into one or more of the grooves.
  16. 16. A method as claimed in claim 15, wherein the bore is dimensioned so as to permit wicking of the adhesive between the bearing and the wall.
  17. 17. A method as claimed in claim 15 or 16, wherein at least one groove is precluded from adhesive injection.
  18. 18. A method as claimed in claim 17, wherein for each groove into which adhesive is injected, an adjacent groove is precluded from adhesive injection.
  19. 19. A bearing support substantially as hereinbefore described with reference to and illustrated in the accompanying drawings.
  20. 20. A diffuser substantially as hereinbefore described with reference to and illustrated in the accompanying drawings.
  21. 21. A compressor substantially as substantially as hereinbefore described with reference to and illustrated in the accompanying drawings.
GB0903058.6A 2009-02-24 2009-02-24 Bearing support Active GB2467969B (en)

Priority Applications (5)

Application Number Priority Date Filing Date Title
GB0903058.6A GB2467969B (en) 2009-02-24 2009-02-24 Bearing support
JP2011551525A JP5535245B2 (en) 2009-02-24 2010-02-10 Bearing support
PCT/GB2010/050212 WO2010097609A1 (en) 2009-02-24 2010-02-10 Bearing support
US12/707,380 US9109626B2 (en) 2009-02-24 2010-02-17 Bearing support
JP2014088347A JP5849325B2 (en) 2009-02-24 2014-04-22 Assembly having a bearing, compressor, and method for fixing the bearing

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB0903058.6A GB2467969B (en) 2009-02-24 2009-02-24 Bearing support

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GB2467969A true GB2467969A (en) 2010-08-25
GB2467969B GB2467969B (en) 2013-06-12

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WO2012107736A1 (en) * 2011-02-08 2012-08-16 Dyson Technology Limited Rotor for a turbomachine
GB2493972A (en) * 2011-08-26 2013-02-27 Dyson Technology Ltd Rotor assembly having a component secured to a bore by two adhesives
US9169843B2 (en) 2011-08-26 2015-10-27 Dyson Technology Limited Turbomachine
US9410442B2 (en) 2011-08-26 2016-08-09 Dyson Technology Limited Turbomachine
US9863429B2 (en) 2011-08-26 2018-01-09 Dyson Technology Limited Rotor assembly for a turbomachine
US9926940B2 (en) 2009-02-24 2018-03-27 Dyson Technology Limited Rotor assembly
DE102017129803A1 (en) * 2017-12-13 2019-06-13 Vorwerk & Co. Interholding Gmbh Bearing unit for supporting a shaft, in particular a shaft of an electric motor
WO2019166776A1 (en) * 2018-03-01 2019-09-06 Dyson Technology Limited An electric motor
US11658540B2 (en) 2018-03-01 2023-05-23 Dyson Technology Limited Assembling method of a rotor to an electric motor frame

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GB2571557B (en) * 2018-03-01 2020-09-30 Dyson Technology Ltd A method of mounting a rotor assembly to a frame of an electric motor
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WO2007003153A1 (en) * 2005-06-30 2007-01-11 Geräte- und Pumpenbau GmbH Dr. Eugen Schmidt Assembly and method for mounting a pump bearing in/on plastic coolant pump housings
JP2007211960A (en) * 2006-02-13 2007-08-23 Hitachi Powdered Metals Co Ltd Bearing unit and its manufacturing method
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US9926940B2 (en) 2009-02-24 2018-03-27 Dyson Technology Limited Rotor assembly
CN103348143B (en) * 2011-02-08 2016-08-10 戴森技术有限公司 Rotor for a turbomachine
CN103348143A (en) * 2011-02-08 2013-10-09 戴森技术有限公司 Rotor for a turbomachine
US9624941B2 (en) 2011-02-08 2017-04-18 Dyson Technology Limited Rotor for a turbomachine
WO2012107736A1 (en) * 2011-02-08 2012-08-16 Dyson Technology Limited Rotor for a turbomachine
EP2562426A3 (en) * 2011-08-26 2015-04-15 Dyson Technology Limited Rotor assembly for a turbomachine
US9410553B2 (en) 2011-08-26 2016-08-09 Dyson Technology Limited Rotor assembly for a turbomachine
US9410442B2 (en) 2011-08-26 2016-08-09 Dyson Technology Limited Turbomachine
US9169843B2 (en) 2011-08-26 2015-10-27 Dyson Technology Limited Turbomachine
GB2493972B (en) * 2011-08-26 2014-12-03 Dyson Technology Ltd Rotor assembly for a turbomachine
US9863429B2 (en) 2011-08-26 2018-01-09 Dyson Technology Limited Rotor assembly for a turbomachine
GB2493972A (en) * 2011-08-26 2013-02-27 Dyson Technology Ltd Rotor assembly having a component secured to a bore by two adhesives
US11668322B2 (en) * 2011-08-26 2023-06-06 Dyson Technology Limited Turbomachine
DE102017129803A1 (en) * 2017-12-13 2019-06-13 Vorwerk & Co. Interholding Gmbh Bearing unit for supporting a shaft, in particular a shaft of an electric motor
WO2019166776A1 (en) * 2018-03-01 2019-09-06 Dyson Technology Limited An electric motor
GB2571555B (en) * 2018-03-01 2021-02-24 Dyson Technology Ltd An electric motor
US11658540B2 (en) 2018-03-01 2023-05-23 Dyson Technology Limited Assembling method of a rotor to an electric motor frame

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Publication number Publication date
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GB0903058D0 (en) 2009-04-08

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