This application claims the priority of United Kingdom Application No. 1521892.8, filed Dec. 11, 2015, the entire contents of which are incorporated herein by reference.
The present invention relates to an electric motor.
Electric motors have an extremely wide range of applications, for example from electric drives for vehicles to powering air moving devices such as vacuum motors and fans, and also handheld power tools and other consumer products. With electric motors being incorporated into more and more consumer products, it is important to find ways in which the cost of the electric motor can be kept down where possible. In addition, particularly when being used in handheld products, it is important to find ways in which the size and weight of an electric motor can be minimised. Improvements to electric motors are required that allow for reductions in size, weight and cost of electric motors but without negatively affecting their performance.
Aspects of this invention provide an electric motor comprising: a frame; a rotor assembly comprising a magnet, a bearing assembly, an impeller, and a shaft; and a stator assembly comprising a stator core and a bobbin. The frame has an inner wall and an outer wall, the outer wall surrounds the inner wall and defines an annular channel between the inner wall and the outer wall, and diffuser vanes extending from the inner wall to the outer wall through the annular channel. The inner wall defines a bore for supporting the rotor assembly, and the outer wall defines a substantially cylindrical outer casing of the motor.
As a result, a motor can be achieved that requires fewer components. The inner wall of the frame supports the rotor assembly, and the inner and outer walls also define a diffuser channel through which the airflow generated by the impeller passes. As such, no separate rotor supporting part or diffuser is required. By reducing the number of components in the motor, the cost of the motor can be reduced, as well as its size and weight.
The bore may support the rotor assembly at the bearing assembly. As such, the rotor can be supported such that the rotor assembly is balanced within the motor. This can reduce imbalance of the motor, and will minimise unwanted vibration which can affect the performance of the motor, and could reduce its lifetime.
The bearing assembly may comprise a pair of bearings fixed to the shaft and a spring located between the two bearings. The spring can then act to apply a pre-load to the outer races of each of the bearings. This improves the bearings' performance, and reduces the risk of them failing at high speed.
The bearing assembly may be fixed within the bore, the inner wall acting as a protective sleeve around the bearing assembly. As a result, the bearing assembly does not need a separate protective sleeve. As such, the size and weight of the motor can be kept down. Furthermore, fewer components are required to make up the motor and so the cost of the motor can also be minimised.
The outer wall may extend beyond the inner wall in an axial direction in at least one of an upstream and a downstream direction. As a result, by having the inner wall shorter than the outer wall, space is made available within the axial length of the outer wall that can be used to enclose other components of the motor. This helps to make the motor more compact. Furthermore, less material is required to form the inner wall, and so the weight of the motor can be reduced.
The diffuser vanes may have tail portions that extend axially beyond the inner wall to the outer wall. As a result, the effective length of the diffuser can be maximised, while the overall size of the motor can be reduced.
The inner wall may comprise at least one lug extending in an axial direction from one end of the inner wall. As a result, other components of the motor can be fixed to the frame using the lug.
The stator assembly may comprise at least one recess for receiving the at least one lug. The stator assembly can therefore be fixed to the frame using the lug.
The inner wall may comprise an annular protrusion extending axially from one end of the inner wall, the annular protrusion being receivable within a recess in a hub of the impeller. This can create a labyrinth seal inside the hub of the impeller. This can prevent foreign objects from entering into the bearing assembly which could damage the rotor assembly and significantly reduce the lifetime of the motor.
The impeller may be an axial impeller formed of aluminium, and may comprise a hub and a plurality of blades attached to the hub. Aluminium is very light and strong, and so the impeller can remain strong enough to withstand forces associated with high-speed applications, but the weight of the motor can also be minimised. The hub may comprise a recess for receiving an axially extending annular protrusion of the inner wall.
The inner wall may have an outer diameter that substantially matches an outer diameter of the hub. This creates an evenly proportioned air channel through the motor which helps to minimise turbulence and pressure losses through the motor which can negatively affect the performance of the motor.
The frame may be formed of zinc. Zinc has the advantage that it is acoustically dull, and so the frame is able to at least partly absorb noise generated by the motor during use.
The frame may comprise an electrical connection portion formed in the outer wall. The electrical connection portion may be a spade terminal. The electrical connection portion may be a DC reference connection. As a result, no additional connector part is required, and therefore the number of components can be reduced. In turn this can help to minimise the cost of the motor and can also help to reduce the size of the motor.
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 following accompanying drawings, in which:
For the sake of clarity, the term “axial” is intended to mean in the direction of an axis running along a rotational axis of the motor as depicted by axis A-A in
The frame 10 is formed of zinc and can be formed, for example, by machining or die-casting, or a combination method using both machining and die-casting. Zinc is an acoustically dull material and so a zinc frame 10 is able to effectively absorb acoustic frequencies generated by the motor 1 during use. The zinc frame 10 therefore acts to reduce the overall level of noise generated by a product inside of which the motor 1 is incorporated.
The diffuser vanes 13 extend between the inner wall 11 and the outer wall 12, and extend along substantially the whole length of the inner wall. In addition, the diffuser vanes 13 have tail portions 18 that extend axially downstream beyond the inner wall to the outer wall. The diffuser vanes 13 are therefore longer at a radially outer part of the annular channel 14 than at a radially inner part of the annular channel 14. This has the benefit that the diffuser vanes have a longer effective length acting on the airflow whilst still allowing the size and weight of the motor to be kept to a minimum by reducing the axial length of the inner wall 11.
The inner wall 11 is cylindrical and defines a bore 15. The inner wall 11 can support the rotor assembly 20 within the bore 15 when the motor 1 is assembled. In addition, the inner wall has a lug 16 that extends from one end of the inner wall 11 in an axial direction. In particular the lug 16 extends axially in a downstream direction. The lug 16 provides a mounting point onto which the stator assembly 40 can be easily mounted in order that the stator assembly 40 can be secured to the frame 10.
The inner wall 11 has an axially extending annular protrusion 17 which extends from an end of the inner wall 11 in an opposite direction to the lug 16. This axially extending annular protrusion 17 can be received into a complimentary recess on the impeller 24 to form a labyrinth seal. This will be described in more detail below with reference to
The rotor assembly 20 comprises a shaft 21, a magnet 22, a bearing assembly 23 and an impeller 24. A cross-section through the rotor assembly 20 is shown in
As described above, the rotor assembly 20 is supported in the frame 10 by the inner wall 11. The bearing assembly 23 is fixed inside the bore 15 of the inner wall 11 such that the inner wall 11 of the frame 10 acts as a protective sleeve around the bearing assembly 23. This eliminates the need for the bearing assembly 23 to have a separate protective sleeve, and helps to reduce the size and weight of the motor 1. The outer races of the bearings 25a, 25b are fixed to the inside circumference of the inner wall 11 in the bore 15, and can be fixed, for example, by adhesive.
The impeller 24 shown in the Figures is an axial impeller with a plurality of blades 27 spaced circumferentially around, and extending radially out from, a central hub 28. During use, as each blade 27 spins it creates sound waves at a particular frequency. It is therefore possible to design the impeller in such a way as to reduce its acoustic impact. The impeller 24 shown in
The impeller 24 is formed by machining aluminium. Aluminium is a very light material and therefore by using it to form the impeller 24 this helps to counteract some of the additional weight included in the motor 1 by using zinc to create the frame 10. The motor 1 described herein is intended to be run at rotational speeds of around 75 to 110 krpm. The magnitude of the forces acting on the impeller 24 at these high speeds are very great. Thankfully, despite being light, aluminium is also very strong and so the impeller 24 is capable of withstanding these large forces when it rotates at high speed.
The bobbin assembly 44 comprises recesses 46 that are configured to align with the lugs 16 on the frame 10 such that the stator assembly 40 can be fixed to the frame 10. The lugs 16 are receivable into the recesses 46, and can be fixed in place using adhesive and/or interference fit.
The bearing assembly 23 comprises a pair of bearings 72a, 72b, and a spring 73 separating the bearings 72a, 72b. The spring 73 acts to pre-load each of the outer races of the bearings 72a, 72b to reduce wear of the bearings during use. Washers may also be provided between the spring 73 and each of the bearings 72a, 72b.
Whilst particular embodiments have thus far been described, it will be understood that various modifications may be made without departing from the scope of the invention as defined by the claims.
Number | Date | Country | Kind |
---|---|---|---|
1521892 | Dec 2015 | GB | national |
Number | Name | Date | Kind |
---|---|---|---|
3495111 | Haydon | Feb 1970 | A |
3593049 | Dittrich | Jul 1971 | A |
4166265 | Reynolds et al. | Aug 1979 | A |
4333026 | Bock | Jun 1982 | A |
4927367 | Salvagno | May 1990 | A |
5019737 | Bruno | May 1991 | A |
5943760 | Barzideh et al. | Aug 1999 | A |
RE36545 | Steiner | Feb 2000 | E |
7345386 | Dano | Mar 2008 | B2 |
8157524 | Nicgorski | Apr 2012 | B2 |
8395289 | Tian | Mar 2013 | B2 |
10184487 | Hayamitsu | Jan 2019 | B2 |
10309420 | Johnson | Jun 2019 | B2 |
20010005943 | Fukumoto | Jul 2001 | A1 |
20030098660 | Erdman et al. | May 2003 | A1 |
20060280630 | Lee | Dec 2006 | A1 |
20070280829 | Stevens | Dec 2007 | A1 |
20090142204 | Yamamoto et al. | Jun 2009 | A1 |
20090191055 | Li | Jul 2009 | A1 |
20100117468 | Kurita | May 2010 | A1 |
20100158679 | Aust | Jun 2010 | A1 |
20110074230 | Hasegawa | Mar 2011 | A1 |
20120267972 | Leung | Oct 2012 | A1 |
20130270945 | Ziegler | Oct 2013 | A1 |
20130302146 | Dyson | Nov 2013 | A1 |
20140050600 | Kodato et al. | Feb 2014 | A1 |
20140183991 | Kulkarni et al. | Jul 2014 | A1 |
20140265700 | Patterson | Sep 2014 | A1 |
20140328684 | King | Nov 2014 | A1 |
20150093271 | Hiromoto | Apr 2015 | A1 |
20150351599 | Park | Dec 2015 | A1 |
20160204676 | Ziegler | Jul 2016 | A1 |
20170108010 | Johnson | Apr 2017 | A1 |
20170164711 | Childe | Jun 2017 | A1 |
20170170709 | Barnes et al. | Jun 2017 | A1 |
20180100517 | Sawada | Apr 2018 | A1 |
Number | Date | Country |
---|---|---|
1928346 | Mar 2007 | CN |
206272382 | Jun 2017 | CN |
37 10 622 | Oct 1988 | DE |
1 437 817 | Jul 2004 | EP |
2 667 995 | Apr 1992 | FR |
2 248 728 | Apr 1992 | GB |
2 362 268 | May 2005 | GB |
2467966 | Aug 2010 | GB |
2513661 | Nov 2014 | GB |
2513664 | Nov 2014 | GB |
S48-19392 | Jun 1973 | JP |
54-48306 | Apr 1979 | JP |
60-134401 | Sep 1985 | JP |
S63-183400 | Nov 1988 | JP |
3-203547 | Sep 1991 | JP |
10-191590 | Jul 1998 | JP |
2000-245109 | Sep 2000 | JP |
2002-171704 | Jun 2002 | JP |
2008-312272 | Dec 2008 | JP |
2012-87748 | May 2012 | JP |
2014-37817 | Feb 2014 | JP |
2015-92810 | May 2015 | JP |
48-19392 | Feb 2018 | JP |
2410818 | Jan 2011 | RU |
19483 | Dec 2006 | UA |
2008041353 | Apr 2008 | WO |
WO-2008041353 | Apr 2008 | WO |
Entry |
---|
Received STIC search report from EIC 2800 searcher Samir Patel dated Sep. 21, 2018. |
International Search Report and Written Opinion dated Mar. 14, 2017, directed to International Application No. PCT/GB2016/053704; 12 pages. |
Search Report dated May 25, 2016, directed to GB Application No. 1521892.8; 2 pages. |
Notification of Reason for Rejection dated Sep. 18, 2018, directed to JP Application No. 2016-240188; 8 pages. |
Official Action dated Apr. 3, 2019, directed to RU Application No. 2018125059; 11 pages. |
The First Office Action dated Sep. 29, 2018, directed to CN Application No. 201611140022.3; 16 pages. |
Notification of Reason for Rejection dated Sep. 28, 2020, directed to JP Application No. 2016-240188; 13 pages. |
Notification of Reason for Rejection dated Jul. 20, 2020, directed to JP Application No. 2019-163193; 4 pages. |
Number | Date | Country | |
---|---|---|---|
20170170709 A1 | Jun 2017 | US |