Replaceable liner for powder coating apparatus

Information

  • Patent Grant
  • 6328224
  • Patent Number
    6,328,224
  • Date Filed
    Wednesday, February 5, 1997
    28 years ago
  • Date Issued
    Tuesday, December 11, 2001
    23 years ago
Abstract
A dispensing device for powder coating material includes an outer device portion having a first inner surface and a central passageway for mounting the outer portion on a rotary shaft for rotating the dispensing device. An inner portion of the dispensing device has a second outer surface shaped complementarily to the first surface and a somewhat bell- or cup-shaped third inner surface. Threaded fasteners retain the inner portion in the outer portion with the first and second surfaces in engagement. The outer portion is constructed from a first material having mechanical strength to withstand the stresses attending rotation of the dispensing device. The inner portion is constructed from a second material relatively more inert to the movement of the powder coating material across the third surface.
Description




BACKGROUND OF THE INVENTION




This invention relates to rotary coating material dispensers. It is disclosed in the context of a rotary dispenser for a stream of fluidized powder coating material. However, it is believed to have utility in other applications as well.




Various types and configurations of rotary coating material dispensers are known. There are, for example, the rotary coating material dispensers illustrated and described in U.S. Pat. Nos. 3,536,514; 4,037,561; 4,114,564; 4,381,079; 4,447,008; 5,353,995; and, 5,433,387; “Aerobell™ Powder Applicator ITW Automatic Division,” and, “Aerobell™ & Aerobell Plush™ Rotary Atomizer, DeVilbiss Ransburg Industrial Liquid Systems.” No representation is intended that a complete search has been made of the prior art, or that no better art references than those listed are available.




SUMMARY OF THE INVENTION




According to the invention, a dispensing device for a coating material includes an outer portion including a first, inner surface. The outer portion has a central passageway for mounting the outer portion on a rotary shaft for rotating the dispensing device. The dispensing device further includes an inner portion having a second, outer surface shaped complementarily to the first surface and a somewhat bell- or cup-shaped third, inner surface. Means are provided for retaining the inner portion in the outer portion with the first and second surfaces in engagement.




Illustratively, the outer portion is constructed from a first material having mechanical strength to withstand the stresses attending rotation of the dispensing device but being relatively less inert to the movement of coating material across it. The inner portion is constructed from a second material relatively more inert to the movement of coating material across the third surface.




Additionally illustratively, the first and second portions both extend to a circular discharge edge of the dispensing device.




Further illustratively, the apparatus comprises a third portion having a fourth surface cooperating with the circular discharge edge to define an annular discharge slot.




Additionally illustratively, the third portion is constructed from the second material.




Further illustratively, the means for retaining the inner portion in the outer portion comprises means for retaining the third portion in spaced apart relation to the second portion to define the annular discharge slot.











BRIEF DESCRIPTION OF THE DRAWINGS




The invention may best be understood by referring to the following detailed description and accompanying drawings which illustrate the invention. In the drawings:





FIG. 1

illustrates a longitudinal sectional view through a powder dispenser embodying the present invention;





FIG. 2

illustrates another longitudinal sectional view through a detail of the powder dispenser illustrated in

FIG. 1

;





FIG. 3

illustrates an exploded longitudinal sectional view through a detail of the powder dispenser illustrated in

FIG. 1

;





FIG. 4

illustrates an exploded longitudinal sectional view through a detail of the powder dispenser illustrated in

FIG. 1

;





FIG. 4



a


illustrates an enlarged fragmentary view of a detail of

FIG. 4

;





FIG. 5

illustrates a sectional view through the powder dispenser illustrated in

FIG. 1

, taken generally along section lines


5





5


of

FIG. 1

;





FIG. 6

illustrates a view of the powder dispenser illustrated in

FIG. 1

, taken generally along section lines


6





6


of

FIG. 1

;





FIG. 7

illustrates a sectional view through a detail of the powder dispenser illustrated in

FIG. 1

, taken generally along section lines


7





7


of

FIGS. 5-6

;





FIG. 8

illustrates a sectional view through the powder dispenser illustrated in

FIG. 1

, taken generally along section lines


8





8


of

FIG. 1

;





FIG. 9

illustrates a side elevational view of certain details of the powder dispenser illustrated in

FIG. 1

;





FIG. 10

illustrates a view of the details of the powder dispenser illustrated in

FIG. 9

, taken generally along section lines


10





10


of

FIG. 9

;





FIG. 11

illustrates a fragmentary sectional view through a detail of the powder dispenser illustrated in

FIG. 1

, taken generally along section line


11


and the axis of

FIG. 8

;





FIG. 12

illustrates a fragmentary sectional view through a detail of the powder dispenser illustrated in

FIG. 1

, taken generally along section line


12


and the axis of

FIG. 8

;





FIG. 13

illustrates a fragmentary sectional view through a detail of the powder dispenser illustrated in

FIG. 1

, taken generally along section line


13


and the axis of

FIG. 8

;





FIG. 14

illustrates a sectional view through a detail of the powder dispenser illustrated in

FIG. 1

, taken generally along section lines


14





14


of

FIG. 1

;





FIG. 15

illustrates a fragmentary, exploded, partial longitudinal sectional view of a detail of the powder dispenser illustrated in

FIG. 1

;





FIG. 16

illustrates a fragmentary sectional view through a detail of the powder dispenser illustrated in

FIG. 1

, taken generally along section line


16


and the axis of

FIG. 8

;





FIG. 17

illustrates a fragmentary sectional view through a detail of the powder dispenser illustrated in

FIG. 1

, taken generally along section line


17


and the axis of

FIG. 8

;





FIG. 18

illustrates a fragmentary sectional view through a detail of the powder dispenser illustrated in

FIG. 1

, taken generally along section lines


18





18


of

FIG. 8

;





FIG. 19

illustrates a fragmentary sectional view through a detail of the powder dispenser illustrated in

FIG. 1

, taken generally along section line


19


and the axis of

FIG. 8

;





FIG. 20

illustrates a fragmentary sectional view through a detail of the powder dispenser illustrated in

FIG. 1

, taken generally along section line


20


and the axis of

FIG. 8

;





FIG. 21

illustrates a fragmentary sectional view through a detail of the powder dispenser illustrated in

FIG. 1

, taken generally along section line


21


and the axis of

FIG. 8

;





FIG. 22

illustrates a fragmentary sectional view through a detail of the powder dispenser illustrated in

FIG. 1

, taken generally along section line


22


and the axis of

FIG. 8

;





FIG. 23

illustrates an elevational view of a mounting plate for mounting the powder dispenser illustrated in

FIG. 1

; and,





FIG. 24

illustrates a sectional view through the mounting plate illustrated in

FIG. 23

, taken generally along section lines


24





24


of FIG.


23


.











DETAILED DESCRIPTION OF AN ILLUSTRATIVE EMBODIMENT




A rotary powder dispenser


38


according to the invention includes a manifold


40


. Manifold


40


illustratively is constructed from, for example, Acetron® GP general purpose acetal available from DSM Engineering Plastic Products, Incorporated, Reading, Pa. 19612-4235. An air turbine motor assembly


42


is mounted from a front side


44


of manifold


40


and extends forward therefrom. Motor assembly


42


includes a turbine motor housing


46


constructed from, for example


150


SA or


550


SA Delrin® material, a high voltage contact plate


48


constructed from, for example, aluminum, a turbine air nozzle plate


50


constructed from, for example, aluminum, an air turbine shaft


52


having a central axial passageway


54


therethrough, a thrust bearing spacer


56


and a turbine rotor


58


. The turbine motor assembly


42


can be, for example a part D1245-07 available from Westwind Air Bearings, Inc., 745 Phoenix Drive, Ann Arbor, Mich. 48108. A, for example, glass reinforced Delrin® feed tube


59


extends down the center of passageway


54


.




A powder bell cup assembly


60


is threaded onto front end


62


of shaft


52


. Powder bell cup assembly


60


includes a bell cup


64


constructed from, for example, filled or unfilled polyetheretherketone (PEEK), a bell cup insert or liner


66


constructed from, for example, Teflon® or Delrin® material, and a diffuser


68


also constructed from, for example, Teflon® or Delrin® material, all held together by three equally circumferentially spaced slotted flat head screws


70


. Diffuser


68


illustratively is configured as illustrated and described in U.S. Ser. No. 08/377,816 filed Jan. 25, 1995, now U.S. Pat. No. 5,632,448 . The outer surfaces


74


of bell cup


64


are treated as described in U.S. Ser. No. 08/451,570 filed May 26, 1995, now U.S. Pat. No. 5,662,278, U.S. Ser. No. 08/437,218 filed May 8, 1995, now U.S. Pat. No. 5,633,306 and U.S. Ser. No. 08/451,541 filed May 26, 1995 now U.S. Pat. No. 5,622,563. These four applications are incorporated herein by reference. The material from which bell cup


64


is constructed accepts the above-identified treatment of its outside surfaces


74


well. The material from which the liner


66


is constructed has somewhat less susceptibility to impact fusion of many coating powders of the type being dispensed by dispenser


38


.




A somewhat projectile-shaped front shroud


74


having a shaping air ring cap


76


houses the forward part of manifold


40


, turbine motor assembly


42


, and most of powder bell cup assembly


60


except the forwardmost portions thereof, including the powder discharge slot


78


defined between liner


66


and diffuser


68


. Radially outwardly and axially extending ribs


80


provided on shroud


74


help define between shroud


74


and shaping air-ring cap


76


an annular shaping air slot which is provided with shaping air through passageways


81


,


82


,


84


provided in manifold


40


, turbine housing


46


, and front shroud


74


, respectively. The complementary, mating surfaces


86


,


88


of shroud


74


and manifold


40


are labyrinthine in configuration to provide longer pathways across the surfaces of these two components. This reduces the likelihood of tracking of the high magnitude electrical potential which is impressed upon, for example, high voltage contact plate


48


during operation of dispenser


38


back to, for example, grounded dispenser


38


support.




A rear manifold plate assembly


90


includes a rear manifold mounting flange


92


attached by three equally circumferentially spaced screws


94


to a rear manifold mounting plate


96


. The rearward surface


98


of plate


96


is finished flat and smooth. A generally right circular cylindrical rear shroud


100


is captured at its rearward extent in an annular groove


102


provided by adjacent surfaces of plate


96


and flange


92


and at its forward extent in an annular groove


104


provided on the rearwardly facing side of manifold


40


. Appropriate fittings and lines connect the respective fluidized PowDeR (fittings


96


-


1


and


40


-


1


and line


91


), powder cloud SHaPing air (fittings


96


-


3


and


40


-


3


and line


95


), turbine DRiVing air (fittings


96


-


2


and


40


-


2


and line


93


), turbine BeaRinG air


1


and


2


(fittings


96


-


4


-


1


,


96


-


4


-


2


,


40


-


4


-


1


and


40


-


4


-


2


and lines


97


and


103


) and turbine BRaKing air ports (fittings


96


-


5


and


40


-


5


and line


101


) on plate


96


and manifold


40


. Turbine air EXHaust ports


1


and


2


(ports


96


-


6


) in plate


96


vent turbine exhaust air from within rear shroud


100


. This air is exhausted from turbine


42


through mufflers


106


fitted to the two EXHaust ports (


40


-


6


) on manifold


40


.




FiberOptic speed control fittings (


40


-


7


and


96


-


7


) are provided on both manifold


40


and plate


96


. The FiberOptic speed control fitting


96


-


7


on plate


96


is intersected by a threaded bore


108


which extends into plate


96


from its edge


110


. A cap screw is threaded into bore


108


to provide for the precise location of an optical fiber terminal


114


at the flat surface


98


of plate


96


. This facilitates matching of the optical fiber terminal


114


to a lens mounted in a flat plate onto which plate


96


is mounted by bolts


116


for quick and easy replacement. This mechanism avoids the time consuming necessity of aligning terminal


114


with the lens if dispenser


38


should have to be removed for any reason including replacement by a similarly designed dispenser. The fluidized PowDeR (


96


-


1


), powder cloud SHaPing air (


96


-


3


), turbine DRiVing (air


96


-


2


), turbine BeaRinG air (


96


-


4


-


1


and


96


-


4


-


2


) and turbine BRaKing air (


96


-


5


) ports on surface


98


are provided with surrounding


0


-ring seals


99


.




A generally right rectangular cylindrical boss


120


is provided on the forward or inside surface


122


of plate


96


. A generally right circular cylindrical relief


124


is provided on the rearward surface of manifold


40


directly opposite boss


120


. An ITW Ransburg MICRO-PAK™ high voltage transformer and cascade-type voltage multiplier


126


is captured between boss


120


and relief


124


. The floor


128


of relief


124


is labyrinthine to complement the configuration of high magnitude potential output end


130


of high voltage multiplier


126


. Again, this configuration provides longer pathways across the surfaces of multiplier


126


and manifold


40


from the high magnitude potential terminal


131


of multiplier


126


to ground. Manifold


40


, turbine motor assembly


42


and front shroud


74


are supported from rear manifold plate


96


by four equally circumferentially spaced support rods


132


which have threaded ends for threading into complementarily threaded holes


133


provides therefor in manifold


40


. Support rods


132


are attached to plate


96


by cap screws


135


.




Bearing air is supplied to the turbine


42


air bearing through the


1


BRG port. The


2


BRG port couples the air bearing to a pressure sensing switch, not shown. If the switch senses the loss of pressure in the air bearing, the flows of fluidized powder coating material and driving air are halted and the turbine


42


is permitted to coast to a stop in an effort to save the turbine


42


.




Low alternating current voltage, for example 12 VAC-30 VAC, is supplied through the LowVoltage connector


96


-


8


on plate


96


to the low voltage terminals of multiplier


126


. LowVoltage connector


96


-


8


is also held in place by a cap screw (not shown) threaded into a bore


137


in the edge


110


of plate


96


. Bore


137


intersects the bore into which connector


96


-


8


is fitted. A, for example, phosphor bronze, wire


136


has several coils of compression spring


138


formed at one end thereof. The end


140


of wire


136


opposite spring


138


fits into the cavity in multiplier


126


in which terminal


131


is provided. The spring


138


is compressed in contact with high voltage contact plate


48


during assembly of turbine


42


to manifold


40


.




BeaRinG air for turbine


42


is supplied from fitting


40


-


4


-


1


through passageways


144


to the air bearing


145


of turbine


42


. This bearing air is sensed through passageways


146


by the above mentioned air BeaRinG pressure sensing switch connected to fitting


40


-


4


-


2


. If BeaRinG air pressure is present at fitting


40


-


4


-


2


, DRiVing air for turbine


42


flows forward through fitting


40


-


2


and passageways


150


from which it flows through the turbine


42


nozzles


152


and against the blades of the turbine rotor


58


to rotate rotor


58


and the powder bell cup assembly


60


mounted on the end


62


of shaft


52


.




Turbine


42


rotation rate signals are coupled back through, for example, a DeVilbiss Ransburg model LSMC 5003 inductive-to-fiber optic signal transmitter


156


which generates a pulse of light each time it senses the passage of a small magnetic disk (not shown) mounted in the rearwardly facing surface of rotor


58


facing transmitter


156


. This signal is transmitted through fiber optic coupler


114


to surface


98


of plate


96


for further transmission through, for example, another similar fiber optic coupler (not shown) to turbine


42


speed control equipment (not shown) which controls the supply of DRiVing air to fitting


96


-


2


, thereby controlling the turbine


42


rotation rate.




BRaKing air to slow the turbine


42


rotation rate is supplied from fitting


40


-


5


through passageways


160


to a braking air nozzle


162


which directs braking air, when it is supplied to fitting


40


-


5


at braking air buckets formed in the rearwardly facing surface of rotor


58


.




Exhaust air from the low pressure side


164


of turbine


42


is exhausted through passageways


40


-


6


and mufflers


106


into rear shroud


100


. From shroud


100


, the exhaust air is vented through the


1


EXHaust and


2


EXHaust ports in plate


96


. In this way, the turbine


42


exhaust is conducted in a direction away from the area radially directly outwardly from slot


78


where the dispensed powder cloud is formed and sustained, rather than being exhausted in a direction generally toward the powder cloud.




The powder cloud is shaped by SHaPing air supplied through fitting


96


-


3


, line


95


, fitting


40


-


3


and passageways


81


,


82


and


84


.




Referring now to

FIGS. 23-24

, a mating plate


200


has a flat forward surface


202


facing the rearward surface


98


of plate


96


. Threaded openings


204


are circumferentially equally spaced around surface


202


for receiving cap screws


206


in flange


92


. Tightening of cap screws


206


in openings


204


compresses the O-rings


99


between surfaces


98


and


202


around mating fluidized PowDeR, DRiVing air, SHaPing air, BeaRinG air


1


and


2


, BRaKing air, FiberOptic and EXHaust air


1


and


2


openings in both of plates


96


and


200


. This constructions effectively seals each of these passageways anytime the two plate


96


,


200


are so secured to each other, and permits the quick and easy disconnection, reconnection and, if necessary or desirable, replacement of dispenser


38


with another dispenser of like or similar configuration.




Because the fluidized powder supplied to fitting


96


-


1


is somewhat penetrating, the configuration of the PowDeR fitting


96


-


1


of the quick disconnect


96


,


200


is somewhat different. Specifically, fitting


96


-


1


includes a nipple


210


provided with an additional O-ring seal


99


. The nipple


210


of fitting


96


-


1


slides into, and is sealed by this additional


0


-ring


99


within, a relief


212


provided for the nipple


210


in surface


202


of plate


200


. Plate


200


is mounted on any desired type of mounting, such as a stand, reciprocator, booth wall or the like, which presents powder bell cup assembly


60


at a suitable position adjacent articles to be coated by powder coating material to be dispensed therefrom.



Claims
  • 1. A dispensing device for a coating material, the dispensing device including an outer portion including a first, inner surface, the outer portion having a central passageway for mounting the outer portion on a rotary shaft for rotating the dispensing device, and an inner portion having a second, outer surface shaped complementarily to the first surface and a somewhat bell- or cup-shaped third, inner surface, and means for retaining the inner portion in the outer portion with the first and second surfaces in engagement.
  • 2. The apparatus of claim 1 wherein the outer portion is constructed from a first material having mechanical strength to withstand the stresses attending rotation of the dispensing device but being relatively less inert to the movement of coating material across it, and the inner portion is constructed from a second material relatively more inert to the movement of coating material across the third surface.
  • 3. The apparatus of claim 1 wherein the first and second surfaces both extend to a circular discharge edge of the dispensing device.
  • 4. The apparatus of claim 3 further comprising a third portion having a fourth surface cooperating with the circular discharge edge to define an annular discharge slot.
  • 5. The apparatus of claim 4 wherein the third portion is constructed from the second material.
  • 6. The apparatus of claim 1 wherein the second surface extends to a circular discharge edge of the dispensing device, the apparatus further comprising a third portion having a fourth surface cooperating with the third surface to define an annular discharge slot and the means for retaining the inner portion in the outer portion comprises means for retaining the third portion in spaced apart relation to the second portion to define the annular discharge slot.
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Number Name Date Kind
2690901 McCormack Oct 1954
2989241 Badger Jun 1961
3111179 Albers et al. Nov 1963
3263127 Point et al. Jul 1966
3536514 LaFave et al. Oct 1970
3870232 Lacchia Mar 1975
4024815 Platsch May 1977
4037561 LaFave et al. Jul 1977
4114564 Probst Sep 1978
4116384 Lacchia Sep 1978
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4235381 Vila Nov 1980
4381079 Allen Apr 1983
4447008 Allen May 1984
4788933 Buschor Dec 1988
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4993645 Buschor Feb 1991
5022590 Buschor Jun 1991
5240185 Kaiju et al. Aug 1993
5323547 Kaiju et al. Jun 1994
5335828 Kaiju et al. Aug 1994
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5443387 Howe et al. Aug 1995
5632448 Alexander et al. May 1997
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Number Date Country
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Non-Patent Literature Citations (2)
Entry
Aerobell™ Powder Applicator ITW Automatic Division.
Aerobell™ & Aerobell Plus™ Rotary Atomizer, DeVilbiss Ransburg Industrial Liquid Systems.