Patent Grant
7036750
This application claims priority to German Patent Application No. DE 102 33 198.7 file Jul. 22, 2002.
The invention concerns a rotary atomizer for coating work pieces according to the preamble of claim 1.
Painting systems use known rotary atomizers, which have a so-called bell-shaped plate that is driven by a compressed-air turbine at high rpm. The bell-shaped plate is usually shaped like a truncated cone and expands in the direction of spraying, with the coating agent to be applied being accelerated in the truncated cone-like bell-shaped plate due to centrifugal forces in the axial direction and particularly in the radial direction, so that a conical spray stream is produced at the stub edge of the bell-shaped plate.
Furthermore, to form the spray stream it is known to blow so-called steering air onto the outer surface of the bell-shaped plate, with the steering air influencing the direction of the paint particles sprayed at the stub edge of the bell-shaped plate. By controlling the amount and the speed of the blown steering air, the shape of the spray stream, and thus the spray stream width, can be adjusted.
It is further known from DE 102 02 712 to direct two steering air streams, which can be controlled separately from each other, onto the spray stream.
For the known rotary atomizers of the previously described type, the steering air is supplied by a steering air line, which runs within the housing of the rotary atomizer towards the outside, between the housing wall and the compressed air turbine. In contrast, the steering air line meets an inlet in the mounting-side end surface of the rotary atomizer, the position of which is predetermined by corresponding connections in the attachment flange of the associated coating machine, such as, e.g., a painting robot, and thus cannot be changed.
A first disadvantage of the previously described guidance of the steering air line within the rotary atomizer, towards the outside between the housing wall and the compressed air turbine, is the fact that the housing diameter of the rotary atomizer is increased by the required cross section of the steering air line, with the installation space available for the compressed air turbine being reduced by the steering air line.
Another disadvantage of the known arrangement of the steering air line is that the steering air line must be first redirected, starting from the connection in the mounting-side end surface, in order to be able to guide it past the compressed air turbine on the outside. This guidance of the steering air line is poor in terms of flow dynamics, however, because the flow resistance is increased by the changes in direction of the steering air and undesired resonance effects can also appear within the steering air line, which produce worse painting results.
The invention is therefore based on the problem of optimizing the known rotary atomizer, described in the introduction, with reference to the required installation space and in terms of the flow dynamics.
The problem is solved, starting from the known rotary atomizer described in the introduction, according to the preamble of claim 1, by the characterizing features of claim 1 and by a bearing unit with the features of claim 15.
The invention includes the general technical teaching of arranging the steering air line, not towards the outside between the housing wall of the rotary atomizer and the compressed air turbine, but instead further inside in the radial direction.
Preferably, the steering air line in this way passes axially, at least in part, through a bearing unit of the compressed air turbine, so that the steering air line does not have to be guided around the compressed air turbine on the outside in a complicated way. Therefore, the bearing unit of the compressed air turbine preferably has an axial through hole, which forms a part of the steering air line.
Usually, the compressed air turbine consists of two approximately cylindrical sections with different outer diameters, with the turbine wheel being arranged in the section with the larger outer diameter. Preferably, the steering air line runs axially through the section of the bearing unit with the greater outer diameter, and opens on the side toward the bell-shaped plate into a so-called air space, which surrounds on the outside the section of the bearing unit having a smaller outer diameter. From this so-called air space, the steering air is then guided through one or more holes arranged in the bearing unit to the steering air outlet, with this hole starting from an opening in the surface shell of the bearing unit and running to a hole in the end surface of the bearing unit on the bell-shaped plate side.
In one variant of the invention, this hole runs at an acute angle to the axis of rotation of the bell-shaped plate, and is essentially without bends.
In contrast, in another variant of the invention this hole in the bearing unit starts from the end surface of the bearing unit on the bell-shaped plate side, and first runs parallel to the axis of rotation of the bell-shaped plate and then opens into a needle hole that runs radially and that opens into the air space at the surface shell of the bearing unit.
Preferably, the steering air line runs essentially without bends at least over a large part of its length in order to optimize fluidic properties of the flow of the steering air.
In addition, the steering air line preferably has an essentially constant cross-sectional area at least over a large part of its length in order to achieve uniform flow of the steering air within the steering air line.
This is preferably assisted in that the steering air line has an essentially constant, and preferably obstacle-free, interior shape at least over a large part of its length.
In an advantageous refinement of the invention, preferably at least two steering air outlets are provided to form the spray stream, with the steering air outlets preferably being arranged at a different radial distance from the axis of rotation of the bell-shaped plate. The individual steering air outlets are preferably supplied with steering air by separate steering air lines, which provides a great amount of freedom in terms of the shape of the spray stream.
One of the steering air lines can be arranged in the conventional way, described in the introduction, towards the outside between the housing wall and the compressed air turbine, while another steering air line is arranged in the previously described way, according to the invention, farther inside at a distance from the housing wall.
Other advantageous refinements of the invention are characterized in the subordinate claims or are described in more detail in the following, together with the description of the preferred embodiment of the invention with reference to the drawing.
Other advantages of the present invention will be readily appreciated as the same becomes better understood by reference to the following detailed description when considered in connection with the accompanying drawings wherein:
The cross section reproduced in
For assembling the rotary atomizer 1, this has on its mounting-side end surface an attachment flange 2 with an attachment pin 3, which enables mechanical attachment to a robot arm of a painting robot.
A conventional truncated cone-like, bell-shaped plate 4 can be formed on the rotary atomizer 1. This bell-shaped plate is illustrated here only with dashed lines, and is driven by a compressed air turbine 5 at high rpm during operation of the rotary atomizer 1. The rotation of the bell-shaped plate 4 leads to the condition that the coating agent introduced into the interior of the bell-shaped plate 4 is accelerated in the axial direction and especially in the radial direction, and is sprayed at a stub edge of the bell-shaped plate.
The drive of the compressed air turbine 5 is achieved by compressed air, which is guided from the painting robot via the attachment flange 2, with the supply of drive air not being illustrated here for simplification.
Furthermore, for shaping the spray stream discharged from the bell-shaped plate 4, a so-called steering air ring 6 is provided that is arranged in the end surface, on the bell-shaped plate side, of a housing 7 of the rotary atomizer 1. In the steering air ring 6, there are several steering air nozzles 8, 9 aligned in the axial direction, by means of which, during operation of the rotary atomizer 1, a steering air current can be blown in the axial direction towards the outside onto the conical surface shell of the bell-shaped plate 4. Depending on the amount and speed of the steering air blown from the steering air nozzles 8, 9, the spray stream is shaped and the desired stream width is set.
The supply of steering air for the two steering air nozzles 8, 9 is achieved via corresponding flange openings 10, 11 that are arranged in the attachment flange 2 of the rotary atomizer 1. The position of each flange opening 10, 11 within the end surface of the attachment flange 2 is given by the position of corresponding connections on the associated attachment flange of the painting robot.
The outer steering air nozzle 8 is supplied in the conventional way, described in the introduction, by a steering air line 12 that is guided along the outside of the compressed air turbine 5 between the housing 7 and the compressed air turbine 5. For this purpose, the flange opening 10 opens first into an axial needle hole 13, which then transitions into a radial needle hole 14, which finally opens at the outside of a valve housing 15 into an intermediate space between the housing 7 and the valve housing 15. The steering air is then led past the compressed air turbine 5 into a so-called air space 16, from where it is finally led through needle holes 17 in the steering air ring 6 to the steering air nozzle 8.
In contrast, the supply of steering air for steering air nozzle 9 is realized through a steering air line 18, which starts from the flange opening 11 in the attachment flange 2 in the axial direction and runs without bends through the valve housing 15. In addition, the steering air line 18 also runs in the axial direction through a bearing unit 19 of the compressed air turbine 5. The radial distance of the steering air line 18 from the axis of rotation of the bell-shaped plate 4 is greater than the outer diameter of the turbine wheel, which is not shown for simplification, so that the steering air line 18 runs on the outside of the turbine wheel. On the bell-shaped plate side, the steering wheel line 18 then opens into another air space 20 that is arranged between an essentially cylindrical section 21 of the compressed air turbine 5 and a cover 22 surrounding this section.
In the surface shell of the section 21 are several holes 23 that open into the end surface, on the bell-shaped plate side, of the compressed air turbine, and finally into the steering air nozzles 9. The holes 23 in the section 21 of the compressed air turbine 5 consist of a radial needle hole starting from the surface shell of the section 21 and an axial needle hole starting from the end surface on the bell-shaped plate side of section 21, which enables simple assembly.
One advantage of the previously described arrangement of the additional steering air line 18 is the fact that the diameter of the housing 7 of the rotary atomizer 1 is not enlarged by the additional steering air line 18, and also the construction space available for the compressed air turbine 5 is not reduced by the steering air line 18.
Another advantage of the steering air line 18 according to the invention can be seen in the bend-free guidance of the steering air current, which is optimized in terms of flow.
The invention has been described in an illustrative manner, and it is to be understood that the terminology which has been used is intended to be in the nature of words of description rather than of limitation.
Obviously, many modifications and variations of the present invention are possible in light of the above teachings. It is, therefore, to be understood that within the scope of the appended claims, wherein reference numerals are merely for convenience and are not to be in any way limiting, the invention may be practiced otherwise than as specifically described.
| Number | Date | Country | Kind |
|---|---|---|---|
| 102 33 198 | Jul 2002 | DE | national |
| Number | Name | Date | Kind |
|---|---|---|---|
| 4376135 | Patel et al. | Mar 1983 | A |
| 4521462 | Smythe | Jun 1985 | A |
| 4572437 | Huber et al. | Feb 1986 | A |
| 4589597 | Robisch et al. | May 1986 | A |
| 4684064 | Kwok | Aug 1987 | A |
| 4715314 | Ramseier et al. | Dec 1987 | A |
| 4852810 | Behr et al. | Aug 1989 | A |
| 4887770 | Wacker et al. | Dec 1989 | A |
| 4919333 | Weinstein | Apr 1990 | A |
| 4927081 | Kwok et al. | May 1990 | A |
| 4944459 | Watanabe et al. | Jul 1990 | A |
| 4955960 | Behr et al. | Sep 1990 | A |
| 5011086 | Sonnleitner et al. | Apr 1991 | A |
| 5078321 | Davis et al. | Jan 1992 | A |
| 5127125 | Skibowski | Jul 1992 | A |
| 5294217 | Talacko et al. | Mar 1994 | A |
| 5300006 | Tanaka et al. | Apr 1994 | A |
| 5397063 | Weinstein | Mar 1995 | A |
| 5622563 | Howe et al. | Apr 1997 | A |
| 5632448 | Alexander et al. | May 1997 | A |
| 5633306 | Howe et al. | May 1997 | A |
| 5662278 | Howe et al. | Sep 1997 | A |
| 5683032 | Braslaw et al. | Nov 1997 | A |
| 5704977 | Baumann et al. | Jan 1998 | A |
| 5865380 | Kazama et al. | Feb 1999 | A |
| 6037010 | Kahmann et al. | Mar 2000 | A |
| 6090450 | Kahmann et al. | Jul 2000 | A |
| 6508610 | Dietrich | Jan 2003 | B1 |
| 6589348 | Ott | Jul 2003 | B1 |
| Number | Date | Country |
|---|---|---|
| 41 05 116 A 1 | Aug 1992 | DE |
| 43 42 128 | Jun 1995 | DE |
| 196 10 588 A 1 | Sep 1997 | DE |
| 197 09 988 A 1 | Oct 1998 | DE |
| 197 42 588 | Apr 1999 | DE |
| 198 30 029 A 1 | Jan 2000 | DE |
| 199 09 369 A 1 | Sep 2000 | DE |
| 199 37 425 A 1 | Mar 2001 | DE |
| 100 33 986 A 1 | Jan 2002 | DE |
| 100 63 234 C 1 | Jul 2002 | DE |
| 101 30 173 A 1 | Jan 2003 | DE |
| 102 02 712 | Jul 2003 | DE |
| 0 767 005 | Apr 1997 | EP |
| 0 904 848 | Mar 1999 | EP |
| 0 967 016 | Dec 1999 | EP |
| 1 108 475 | Jun 2001 | EP |
| 1 114 677 | Jul 2001 | EP |
| 1 172 152 | Jan 2002 | EP |
| WO 9422589 | Oct 1994 | WO |
| Number | Date | Country | |
|---|---|---|---|
| 20040129799 A1 | Jul 2004 | US |
