The present invention relates generally toward a rotary atomizer, and more particularly toward a rotary atomizer for a coating device.
In production paint settings, paint is applied to a workpiece using a rotary atomizer having an atomizer bell that spins at high speeds to atomize the paint being applied to the workpiece. This type of paint application device, in combination with generating an electrostatic field, has produced high quality paint finishes along with high paint transfer efficiencies. Generally, an atomizer bell is affixed to a rotating shaft that transfers rotational movement at high speed to the atomizer bell. A shaft receives rotational movement from a turbine or equivalent motor transferred through gears as is known in U.S. Pat. No. 5,816,508.
The rotating shaft and related drive mechanisms are generally concealed inside an atomizer housing where the shaft includes a distal end extending outwardly onto which the atomizer bell is affixed. As part of general production maintenance, the atomizer bell is typically removed from the assembly for cleaning or replacement with a new atomizer bell. This has generally been difficult to perform because the rotating shaft does not allow for the easy removal of the atomizer bell from the assembly.
U.S. Pat. No. 5,816,508 discloses one method of securing a rotatable shaft by affixing a push pin locking device to the housing of the atomizer. However, the drive mechanism of the disclosed rotary atomizer is quite complex requiring several gears to translate rotational movement to the atomizer bell. Therefore, it would be desirable to provide a compact simplified turbine design eliminating gear mechanisms while still providing the ability to lock the rotating shaft for easy removal of the atomizer bell.
A rotary atomizer assembly for applying paint to a workpiece includes a housing and an atomizer bell extending from the housing for atomizing paint being applied to the workpiece. A turbine is disposed within the housing and provides a bearing surface for a rotary shaft that the atomizer bell is affixed to. The rotary shaft is rotatably supported by the bearing surface and is coaxially aligned with the turbine. The shaft defines a distal end adapted to receive the atomizer bell and a proximal end adapted to be received by the turbine. A locking element is received by the turbine and extends through the housing. The locking element is moveable radially inwardly toward the rotary shaft and is engageable with the rotary shaft for locking the rotary shaft in a non-rotatable position.
The simplified design of the turbine and rotary shaft solves the problems associated with prior art rotary atomizer assemblies, which require independent gear mechanisms to drive the rotary shaft. The elimination of the gearing mechanisms reduces significantly the number of components necessary to rotate the atomizer bell at a high speed. Furthermore, a locking element now is capable of locking the rotary shaft to the turbine, which provides rotational movement to the rotary shaft enabling the atomizer bell to be easily removed from the assembly.
The rotary shaft 24 is coaxially aligned within the turbine 20 along axis A. The rotary shaft 24 includes a distal end 28 and a proximal end 30. The distal end 28 is adapted to receive the atomizer bell 14 in a fixed relationship. More specifically, the rotary shaft 24 defines a threaded surface 32 onto which the atomizer bell 14 is threadably received securing the atomizer bell 14 to the rotary shaft 24.
Turbine blades 34 circumscribe the rotary shaft 24 proximate the proximal end 30 of the rotary shaft 24. The turbine 20 defines an aperture 36, best shown in
A locking element 40 is received by the turbine 20 for securing the rotary shaft 24 in a non-rotatable position. The locking element 40 is actuated by depressing the button 16 disposed in the housing 12, which moves the locking element 40 radially inwardly to engage the rotary shaft 24 and the end plate 38 of the turbine 20. A spring element 42 biases the locking element 40 radially outwardly from the axis A allowing the rotary shaft 24 to rotate freely inside the turbine 20.
As best shown in
Referring to
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.
This application is a continuation-in-part of and claims the benefit of U.S. patent application Ser. No. 10/256,428, filed Sep. 27, 2002 now abandoned.
Number | Name | Date | Kind |
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4896834 | Coeling et al. | Jan 1990 | A |
4927081 | Kwok et al. | May 1990 | A |
5538189 | Rodgers | Jul 1996 | A |
5816508 | Hollstein et al. | Oct 1998 | A |
5862988 | Van der Steur | Jan 1999 | A |
6105886 | Hollstein et al. | Aug 2000 | A |
6284047 | Yoshida et al. | Sep 2001 | B1 |
Number | Date | Country |
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3912700 | Oct 1990 | DE |
WO9636438 | Nov 1996 | WO |
Number | Date | Country | |
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20050001057 A1 | Jan 2005 | US |
Number | Date | Country | |
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Parent | 10256428 | Sep 2002 | US |
Child | 10781596 | US |