SEPARATOR FOR VACUUM CLEANER

Abstract

The present invention relates to a separator for vacuum cleaners operating on the basis of a liquid bath, the liquid bath serving as pre-separation and as a dumping area for the aspirated particles. It consists of segments (7), each of the segments (7) being formed as a radially flat ring (13) that is centrally secured to a hub (11) via radial supports (12) and having blades (8) extending equidistantly and substantially perpendicularly to the surface of the ring (13). The blades (8) are positioned on each individual segment (7) in a way that a gap (9) is formed between each two adjacent blades (8) of each segment (7). When individual segments (7) are stacked one over another, the blades (8) of one segment (7) extend into the gaps (9) between the blades (8) of the next segment (7), such that a newly formed gap (91) is formed between the two adjacent blades (8) of the assembled separator (1). In a preferred embodiment, the separator (1) consists of two end segments (71, 72) and at least one intermediate segment (73), the first end segment (71) preferably having the radially flat ring (13) provided with an integrated sealing ring (30), and the second end segment (72) having the radially flat ring (13) provided with an integrated bottom (20).

Claims

1. A separator for vacuum cleaners operating on the basis of a liquid bath, the liquid bath serving as pre-separation and as a dumping area for the aspirated particles and the air flow being generated by a turbine wheel (2) in a housing (4), the separation being achieved by a centrifugal separator (1), the separator (1) consisting of at least two segments (7), each of the segments (7) being formed as a radially flat ring (13) that is centrally secured to a hub (11) via radial supports (12) and having blades (8) equidistantly formed and substantially perpendicularly to the surface of the ring (13), said blades (8) extending from the outer circumference of the ring (13) towards the interior, and the blades (8) being positioned in a way that an angle (a) is present in the opposite direction (10) of rotation between the radial direction (R) and the direction (A) of the blade (8), said angle being in the range 0 to 40 angular degrees, and each of the segments (7) having an axially formed hub (11) with an opening for attaching the separator (1) to the shaft of the motor (3), characterized in that the blades (8) are positioned on each individual segment (7) in a way that a gap (9) is formed between each two adjacent blades (8) of each segment (7), wherein, when individual segments (7) are stacked one over another, the blades (8) of one segment (7) extend into the gaps (9) between the blades (8) of the next segment (7), such that a newly formed gap (91) is formed between the two adjacent blades (8) of the assembled separator (1).

2. A separator according to claim 1, characterized in that the minimum width of the gaps (9) is 1.2 to 3.5 of the maximum thickness of the blade (8) and the minimum width of the newly formed gaps (91) is 0.1 to 1.25 of the maximum thickness of the blade (8).

3. A separator according to claim 1, characterized in that the blades (8) have basically a profile of an aircraft wing, wherein a front side (81) of the blade (8) is cut at an angle of about 15 to 45 angular degrees with respect to the tangent of the circumference, and tails (82) of the blades (8) are formed as a sharp edge.

4. A separator according to claim 1, characterized in that the blades (8) are provided at their upper edge with projections (14), the radially flat rings (13) are provided in the gaps (9) with recesses (15), wherein, when the segments (7) are assembled, the projections (14) on the blades (8) engage the recesses (15) on the radially flat rings (13).

5. A separator according to claim 1, characterized in that the height of the hub (11) is approximately identical to the height of the blades (8) and positioning connectors (16) are formed on the hub (11) of each segment (7) for engagement of the blades (8) of one segment (7) into the gaps (9) between the blades (8) of another segment (7), when the segments (7) are being assembled.

6. A separator according to claim 1, characterized by consisting of a first end segment (71), a second end segment (72), and at least one intermediate segment (73).

7. A separator according to claim 6, characterized in that the intermediate segment (73) is provided with blades (8) on both sides of the radially flat ring (13).

8. A separator according to claim 7, characterized in that the blades (8) on either side of the radially flat ring (13) are arranged so as to be offset on one side of the radially flat ring (13) towards the blades (8) on the other side of the radially flat ring (13) by one half of the gap (9).

9. A separator according to claim 7, characterized in that the blades (8) on both sides of the radially flat ring (13) are aligned one above the other.

10. A separator according to claim 6, characterized in that the first end segment (71) and the second end segment (72) are provided with blades (8) only on one side of the radially flat ring (13), wherein the first end segment (71) is provided with blades (8) on the side of the radially flat ring (13) facing away from the turbine wheel (2) and the second end segment (72) is provided with blades (8) on the side of the radially flat ring (13) facing the turbine wheel (2).

11. A separator according to claim 6, characterized in that the first end segment (71) and the second end segment (72) are formed as stand-alone elements, a bottom (20) and a sealing ring (30) being formed as stand-alone elements.

12. A separator according to claim 6, characterized in that the first end segment (71) preferably has the radially flat ring (13) provided with an integrated sealing ring (30), and the second end segment (72) has the radially flat ring (13) provided with an integrated bottom (20).

13. A separator according to claim 7, characterized in that the radial supports (12) are shaped so as to cover 50 to 100% of the total height of the hub (11) along the hub (11), while the height of the radial supports (12) decreases towards the ring (13).

Description

[0013] The invention will be described in more detail by way of an embodiment and the accompanying drawings representing in:

[0014] FIG. 1 Embodiment of a separator and turbine assembly,

[0015] FIG. 2 Disassembled separator in perspective view (“exploded view”),

[0016] FIG. 3 Segment of the separator, top view,

[0017] FIG. 4 Assembled separator.

[0018] An assembly consisting of a separator 1 and a turbine wheel 2 with a motor 3 within a housing 4 is the basis of operation of a liquid-bath based vacuum cleaner. In principle, the vacuum cleaner operates in a way that the motor 3 on its shaft drives the turbine wheel 2 and the separator 1. The assembly and the operation are illustrated in FIG. 1. The turbine wheel 2 generates negative pressure, as a result, a flow including a mixture of air, water droplets and other impurities is created which is directed towards the separator 1 in the direction of arrow 5. As the separator 1 rotates at high speed, droplets and other impurities having a high specific weight, due to centrifugal force, cannot enter the separator 1 or can do so only exceptionally. The air having a low specific weight, however, enters the separator 1 due to the pressure generated by the turbine wheel 2, the air is drawn in by the turbine wheel 2 and blown into the room. Droplets and other impurities that accidentally penetrate the separator 1 are rotated in the separator 1 by means of radial supports 12 and ejected from the separator 1 by centrifugal force as indicated by arrow 6.

[0019] The structure and the operation of the separator will be explained by way of drawings.

[0020] The separator 1 of the invention illustrated in FIGS. 2 to 4 preferably has a cylindrical shape and consist of segments 7, each of the segments 7 being formed as a radially flat ring 13 that is centrally secured to a hub 11 via radial supports 12 and having separator blades 8 equidistantly formed substantially perpendicularly to the surface of the ring 13, such that a gap 9 is formed between each two adjacent blades 8 of each segment 7, and the blades 8 are positioned on each individual segment 7 in a way that, when individual segments 7 are stacked one over another, the blades 8 of one segment 7 extend into the gaps 9 between the blades 8 of the next segment 7, such that a newly formed gap 91 is formed between the two adjacent blades 8 of the assembled separator 1. Each of the segments 7 has an axially formed hub 11 with an opening for attaching the separator 1 to the shaft of the motor 3.

[0021] On the radially flat ring 13, the separator blades 8 extend from the outer periphery of the ring 13 inwards and are positioned in a way that an angle α is present in the opposite direction of rotation between the radial direction R and the direction A of a blade, with the angle α being in the range 0 to 40 angular degrees. The direction of rotation is indicated by arrow 10.

[0022] The minimum width of each gap 9 is approximately 1.2 to 3.5 of the maximum thickness of the blade 8. The widths of the gaps 9 are preferably identical.

[0023] The blades 8 have their front side 81, i. e. outer side, sharply truncated. The blades 8 have basically a profile of an aircraft wing, however, experiments have shown that particles get better deflected if the front side 81 of the blade 8 is cut at an angle of about 15 to 45 angular degrees with respect to the tangent of the circumference. So, the front side of a blade 8 physically deflects, hits particles and water from the separator 1.

[0024] The thickness of the blades 8 continuously decreases towards a tail 82 i. e. the end of the blades 8 in the interior of the separator, so that the tails 82 of the blades 8 are formed as a sharp edge which reduce the accumulation of dirt on the blades 8 of the separator 1.

[0025] The blades 8 are provided at their upper edge with projections 14, the radially flat rings 13 are provided in the gaps 9 with recesses 15 so that, when the segments 7 are assembled, the projections 14 on the blades 8 engage the recesses 15 on the radially flat rings 13, the blades 8 being thus still additionally fixed.

[0026] When two adjacent segments 7 are assembled, the blades 8 of a first segment 7 engage the gaps 9 between the blades 8 of another segment 7, preferably the centre of the gaps 9, so when two adjacent segments 7 are assembled, a newly formed gap 91 is formed between two adjacent blades 8 of the assembled separator 1. The minimum width of the newly formed gap 91 is between 0.1 to 1.25 of the maximum thickness of the blade 8. The widths of the newly formed gaps 91 are preferably identical.

[0027] The engagement of the blades 8 of one segment 7, when assembling the segments 7, with the gaps 9 between the blades 8 of another segment 7, is ensured by positioning connectors 16 formed on the hub 11 of a respective segment 7.

[0028] The separator preferably consists of a first end segment 71, a second end segment 72, and at least one intermediate segment 73.

[0029] The first end segment 71 is the segment abutting the turbine wheel 2, the second end segment 72 is the segment the most distant from the turbine wheel 2.

[0030] The intermediate segment 73 of the separator 1 is provided with blades 8 on both sides of the radially flat ring 13. In one embodiment shown in FIGS. 2 and 3, the blades 8 on either side of the radially flat ring 13 are arranged so as to be offset on one side of the radially flat ring 13 towards the blades 8 on the other side of the radially flat ring 13. The blades 8 are preferably offset by half the width of the gap 9.

[0031] The blades 8 on either side of the radially flat ring 13 can also be arranged in a different way, for instance the blades 8 on both sides of the radially flat ring 13 can be arranged without an offset, they are aligned one above the other.

[0032] In the longitudinal cross-section of FIG. 1, the radial supports 12 are shaped so as to cover 50 to 100% of the total height of the hub 11 along the hub 11, while their height decreases towards the ring 13. The radial supports 12 act as an additional turbine that ejects particles and liquid from the separator that could possibly penetrate the separator. The height of the hub 11 is approximately identical to the height of the blades 8.

[0033] The first end segment 71 and the second end segment 72 are provided with blades 8 only on one side of the radially flat ring 13. The first end segment 71 is provided with blades 8 on the side of the radially flat ring 13 facing away from the turbine wheel 2. The second end segment 72 is provided with blades 8 on the side of the radially flat ring 13 facing the turbine wheel 2.

[0034] According to one embodiment, the first end segment 71 and the second end segment 72 can be formed as stand-alone elements, a bottom 20 and a sealing ring 30 also being formed as stand-alone elements. In this case, both end segments 71, 72 are formed as a radially flat ring 13 that is centrically attached to the hub 11 through radial supports 12. In this case, the radial supports 12 and the hub 11 are adequately adapted not to obstruct the fitting of the sealing ring 30 and the bottom 20 on the end segments 71, 72.

[0035] The first end segment 71 preferably has the radially flat ring 13 provided with an integrated sealing ring 30, and the second end segment 72 has the radially flat ring 13 provided with an integrated bottom 20. In this way, fewer pieces are needed to produce the separator, as the sealing ring 30 and the bottom 20 need not be separately manufactured, and the relationship between the structural strength of the separator and the material consumption is improved.

[0036] In the embodiment shown in the figures, the separator according to the invention consists of five segments, namely, a second end segment 72 with an integrated bottom 20, three intermediate segments 73, and a first end segment 71 with an integrated sealing ring 30, all segments being assembled one on another and mutually positioned with positioning connectors 16 provided on the hub 11 of each segment 73, 71, 72. In this embodiment, the positioning connectors 16 are made as matching projections on the upper portion of the hub 11 and recesses on the lower portion of the hub 11 of each segment 73, 71, 72 of the separator 1.

[0037] So, the separator 1 consists of a second end segment 72 with an integrated bottom 20, to which a first intermediate segment 73 is arranged in a corresponding position determined by the positioning connectors 16, such that the blades 8 of the first intermediate segment 73 that are provided at the bottom side of the radially flat ring 13, are positioned in the centre of the gaps 9 between the blades 8 which are provided on the radially flat ring 13 of the second end segment 72. The second end segment 73 is placed onto the first intermediate segment 73 and positioned by positioning connectors 16, such that the blades 8 of the second intermediate segment 73 that are provided at the bottom side of the radially flat ring 13, are positioned in the centre of the gaps 9 between the blades 8 which are provided on the upper side of the radially flat ring 13 of the first intermediate segment 73. The number of intermediate segments 73 corresponds to the capacity of the separator 1. The separator 1 terminates at the upper portion with a first end segment 71 with an integrated sealing ring 30, such that the blades 8 of the first end segment 71 are positioned in the centre of the gaps 9 between the blades 8 which are provided on the upper side of the radially flat ring 13 of the last intermediate segment 73. When the separator 1 is assembled, a newly formed gap 91 is formed between two adjacent blades 8 of the assembled separator 1.

[0038] When the separator 1 rotates, the air enters the interior due to the negative pressure generated by the turbine wheel 2. Droplets, dust and other impurities are largely deflected by the blades 8 due to their large specific weight. Droplets, dust, and other impurities incidentally entering the separator 1 are further rotated by the radial supports 12 and ejected from the separator 1 between the blades 8. The blades 8 have basically the profile of an aircraft wing, but their outer edge is not aerodynamic, it is cut at the outer ends to a sharp edge at an angle, so as to deflect particles of impurities and liquids away from the separator, thereby preventing the impurities from settling. The construction according to the invention is mechanically solid, since the radially flat ring 13 is suspended at several points on the radial supports 12 and the blades 8 on the radially flat ring 13. The separator 1 is thus not subject to deformation due to centrifugal force. In this embodiment, the separator consists of segments 73, 71, 72, this is why the moulding tools can be simple. By varying the number of segments, any heights are possible, thereby increasing the capacity of the separator 1. It goes without saying that the invention also includes a separator made as one integral piece over the entire height.

[0039] The separator of the invention provides minimal gaps between the blades 8 and a large total surface of the gaps between the blades 8.

[0040] The invention has been described by way of one embodiment, however, it goes without saying that all structures, in which the separator has blades, wherein the blades of one segment engage between the blades of another segments, fall within the scope of the invention.