Apparatus for generating a vortex for a vacuum cleaner
11109728 ยท 2021-09-07
Assignee
Inventors
Cpc classification
F04D29/287
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
A47L9/16
HUMAN NECESSITIES
F04D17/16
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F04D29/36
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
A47L9/1683
HUMAN NECESSITIES
International classification
A47L9/16
HUMAN NECESSITIES
F04D17/16
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F04D29/36
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
Abstract
An apparatus for generating a vortex in a collection vessel of a vacuum cleaner, using a blade assembly rotatably mountable in the collection vessel. By rotating the blade assembly, a vortex is generated inside the collection vessel, and enough suction is created to draw air through the entire system. The use of a blade assembly to generate the vortex may remove the need for an impeller external to the collection vessel, as the blade assembly may be capable of creating enough suction to draw air into the collection vessel. This may allow the vacuum cleaner to operate with lower noise.
Claims
1. An apparatus comprising: a collection vessel having therein a motor having a driving gear, a support member, and a blade assembly rotatably mounted in the collection vessel and including a driven gear, and a plurality of blades mounted to the support member, wherein the plurality of blades extends downwards from the support member to be spaced apart from one another in a circumferential direction of the blade assembly, the plurality of blades is rotated by the driven gear of the blade assembly engaged with the driving gear of the motor, to thereby generate a suction force and a vortex within the collection vessel, the collection vessel has an air inlet and an air outlet, the air inlet is configured to direct suctioned air and particles from a surface external to the apparatus into the collection vessel through the suction force generated by the blade assembly, and the air outlet is configured to direct the suctioned air out of the collection vessel through the blade assembly using the vortex generated by the blade assembly and the plurality of blades is movable relative to the support member.
2. The apparatus according to claim 1, wherein at least some of the plurality of blades are symmetrically disposed around a periphery of the support member.
3. The apparatus according to claim 1, wherein an angle of each of the plurality of blades relative to a direction of motion is adjustable.
4. The apparatus according to claim 3, further comprising a gear assembly configured to adjust the angle of the plurality of blades.
5. The apparatus according to claim 4, wherein the gear assembly comprises a plurality of first gears mounted to the support member, each of the plurality of first gears being connected to a respective one of the plurality of the blades by an axle.
6. The apparatus according to claim 5, further comprising a second gear arranged to mesh with each of the plurality of first gears and configured to adjust the angle of each of the plurality of blades by a same amount.
7. The apparatus according to claim 6, further comprising a third gear configured to mesh with the second gear.
8. The apparatus according to claim 1, wherein the plurality of blades comprising three blades.
9. The apparatus according to claim 1, wherein at least some of the plurality of blades have a symmetric aerofoil shape.
10. The apparatus according to claim 1, wherein at least some of the plurality of blades have a cambered aerofoil shape.
11. The apparatus according to claim 1, comprising a plurality of vanes around a periphery of the support member.
12. The apparatus according to claim 1, wherein the driven gear has a plurality of teeth around a periphery of the support member configured to engage with the driving gear of the motor.
13. A vacuum cleaner comprising: a collection vessel having therein a motor having a driving gear, a support member, and a blade assembly rotatably mounted in the collection vessel and including a driven gear, and a plurality of blades mounted to the support member, wherein the plurality of blades extend downwards from the support member to be spaced apart from one another in a circumferential direction of the blade assembly, the plurality of blades are rotated the driven gear of the blade assembly engaged with the driving gear of the motor, to thereby generate a suction force and a vortex within the collection vessel, the collection vessel has an air inlet and an air outlet, the air inlet is configured to direct suctioned air and particles from a surface external to the vacuum cleaner into the collection vessel through the suction force generated by the blade assembly, and the air outlet is configured to direct the suctioned air out of the collection vessel through the blade assembly using the vortex generated by the blade assembly, and wherein the support member has a central aperture, and the vacuum cleaner further comprises a filter above the central aperture arranged to remove fine particles from air exiting the collection vessel.
14. The vacuum cleaner according to claim 13, wherein the air inlet is located on a side of the collection vessel.
15. The vacuum cleaner according to claim 14, wherein the air inlet is located below the blade assembly.
16. The vacuum cleaner according to claim 14, wherein the air inlet is arranged such that the suctioned air is drawn into the collection vessel at an angle that is tangential to the wall of the vessel.
17. The vacuum cleaner according to claim 13, wherein the collection vessel comprises a collection chamber at the bottom for collecting dust.
Description
BRIEF DESCRIPTION OF THE DRAWINGS
(1) Embodiments of the invention will now be described by way of example with reference to the accompanying drawings, in which:
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DETAILED DESCRIPTION
(10)
(11) Referring to
(12) In another embodiment shown in
(13)
(14) Referring to
(15) The blade assembly 13 may be driven by a motor or other driving device (not shown). As the blade assembly 13 rotates relative to the collection vessel, the blades 13A, 13B, 13C cause the air inside the collection vessel 10 to flow in a vortex-like motion, thus generating a vortex. The vortex may force light particulates, e.g. hair, into the centre of the collection vessel 10, and heavy particulates to the collection vessel walls. The light particulates then travel along with the airflow up through the centre of the blade assembly 13 to the outlet 12, whilst the heavy particulates fall to the bottom of the collection vessel where they accumulate. This has the effect of separating heavy particulates from the airflow. The bottom of the collection vessel 14 may comprise a separate collection chamber for collecting the particulates, and the collection chamber may be detachable from the rest of the collection vessel 10 to allow for disposal of the accumulated particulates.
(16) The rotation of the blade assembly 13 causes a pressure differential between the central region of the collection vessel 10, where there is relatively low pressure, and the side regions of the collection vessel 10, where there is relatively high pressure. This pressure differential has the effect of producing enough suction to draw air through the entire system. The apparatus may therefore be capable of both generating a vortex and producing enough suction to draw air into the apparatus. As such, there may be no need to provide an impeller external to the apparatus so that the apparatus may operate at a lower noise level. Additionally, since the means by which suction is generated is provided inside the collection vessel with the vortex, it may be possible to provide the same suction power with a smaller sized cyclonic vacuum cleaner.
(17) Referring again to
(18) The blades 13A, 13B, 13C may have an aerofoil shape, for example a symmetric aerofoil or a cambered aerofoil. Cambered aerofoils may include reflex aerofoils, wedge shaped aerofoils and flattened aerofoils, among many others. The shape of the blades is not limited to any specific shape, as long as they have the effect of producing a vortex when rotated.
(19) Furthermore, while the above embodiment refers to three blades, the invention is not limited thereto, and any number of blades may be provided as long as they are capable of generating a vortex. However, simulations show that three aerofoil blades symmetrically disposed around the periphery of a support member may provide improved results over other configurations.
(20)
(21) Referring to
(22) The blades 23A, 23B, 23C of the blade assembly 23 are mounted to and extend downwards from a support member 23D. In this embodiment, the blades, which have a cambered aerofoil shape, are fixed to the support member 23D so that they cannot move relative to the support member. The blades may be made of a substantially rigid material, or they may be made of a relatively flexible material so that, even if fixed in position, the blades may flex as they are rotated. However, the invention is not limited either to the blades being fixedly mounted or to the specific shape of the aerofoil, or to specific materials or rigidity.
(23) The support member 23D may be an annular ring, with the blades being fixed at an outer portion of the ring. The support member 23D may be integrally formed with the blades, for example by a moulding process. The support member 23D may have a central aperture 29 which allows air loaded with light particles to flow through the centre of the blade assembly 23 for filtration.
(24) As described above, the blades 23A, 23B, 23C are symmetrically disposed around the periphery of the support member 23D and the rotation of the support member about its central axis causes the blades 23A, 23B, 23C to move in a circle, thus generating a vortex. The principle of operation of the vortex and its effects are described above and will not be repeated here. A motor 24 may be provided adjacent to the blade assembly 23 and mechanically coupled to the blade assembly to drive its rotation. This may be achieved by engaging a driving gear 25 of the motor with a driven gear 26 of the blade assembly, the driven gear 25 comprising an annular ring disposed on top of the support member 23D, so that the gear teeth are exposed at the periphery of the support member. This configuration allows the central aperture 29 at the top of the blade assembly to be maintained clear to allow for the flow of air, but the configuration is not limited to this.
(25) In some embodiments, the blade assembly 23 may further comprise a plurality of vanes 27 around the periphery of the support member 23D.
(26) Referring to
(27) The blades 33A, 33B, 33C are symmetrically disposed around the periphery of the support member and the rotation of the support member 33D about its central axis causes the blades 33A, 33B, 33C to move in a circle, thus generating a vortex. The principle of operation of the vortex and its effects are described above and will not be repeated here. In this embodiment, the blades 33A, 33B, 33C have symmetric aerofoil shapes, and the collection vessel 10 may have a substantially cylindrical shape to facilitate the formation of a vortex.
(28) In this embodiment each of the blades 33A, 33B, 33C may be mounted to the support member 33D by a corresponding axle 35. Each of the axles 35 may pass through a corresponding hole in the support member 33D and extend into the leading edge side of a corresponding blade, thus fixing to the blade. The blade is mounted to the support member by a gear arrangement which is described in more detail below. The precise mounting arrangement of the axle to the blade and the blade to the supporting member is not limited to the above arrangement, as long as the rotation of the blade assembly 33 still generates a vortex.
(29) The angle of the blades 33A, 33B, 33C relative to their direction of motion may be adjusted by rotating the axles 35 to which they are attached. This may be achieved through the use of a gear assembly 34 comprising a control gear 34A, a coupling gear 34B and axle gears 34C. The control gear 34A meshes with the coupling gear 34B which is in turn meshed with the axle gears 34C. Each axle gear 34C is attached to a corresponding axle 35 which extends through the centre of the axle gear. Rotating the control gear 34A transfers torque to the coupling gear 34B which then simultaneously rotates the axle gears 34C. Since the axle gears 34C are attached to the axles 35, the axles also rotate. This alters the angle of each of the blades relative to their direction of motion by the same amount. As such, the angle of the blades relative to their direction of motion may be adjusted by turning a single control gear 34A.
(30) Although in this embodiment the blades are attached to the support member by axles, the invention is not limited to this. For example, the blades may be attached to the support member by an adhesive or one or more screws. Alternatively, the blades may be integrally formed with the support member, for example by a moulding process. In general, any method of attaching the blades to the support member may be used. This includes methods in which the blades are fixed relative to the support member and methods in which the blades can be moved relative to the support member.
(31)
(32) Referring to
(33) The blades may also be rotated to different positions in accordance with preset operating modes. Adjusting the angle of the blades 33A, 33B, 33C allows the movement of air within the collection vessel 10 to be controlled, for example to dislodge any trapped particulates that need moving, or to control the size of particulates which are separated from the airflow.
(34) Although a number of embodiments of the invention have been described above, it will be understood that many variations and modifications are possible without departing from the scope of the invention as defined in the claims. Furthermore, different features of the embodiments may be combined with one another or substituted for one another. For example, the blades used in the embodiment illustrated in