High temperature rotating vacuum kiln and method for heat treating solid particulate material under a vacuum

Information

  • Patent Grant
  • 6271501
  • Patent Number
    6,271,501
  • Date Filed
    Friday, July 7, 2000
    24 years ago
  • Date Issued
    Tuesday, August 7, 2001
    23 years ago
Abstract
A rotating vacuum kiln and method for heat treating solid particulate material under vacuum conditions uses a rotating refractory metal cylindrical vessel with a cool inlet zone, hot intermediate zone, and cool exit zone, with a first series of inner radiation shields provided at the hot intermediate zone adjacent to the cool inlet zone and a second series of inner radiation shields provided at the hot intermediate zone adjacent the cool exit zone to protect those two zones from the high temperatures in the hot intermediate zone. Heat for the hot intermediate zone of the cylindrical vessel is provided indirectly by electrical resistance heaters that surround the vessel and outer radiation shields are provided about the heaters to direct heat to the cylindrical vessel.
Description




BACKGROUND OF THE INVENTION




The present invention relates to a rotary vacuum kiln and method for the treatment of solid particulate material under conditions of high temperature and under a high vacuum.




Solid particulate material must, at times, be treated under a vacuum at high temperatures in order to provide a desired product. In the manufacture of tantalum powders, for example, for use in capacitors, at one or more steps in processing, the powder is heat-treated in a vacuum furnace. Such treatment may be used to drive off residual impurities and to provide a flowable powder. A present processing system involves placement of a stack of trays containing tantalum powder into a vacuum furnace and heating the entire tray assembly. After a comparatively short heat treatment, in such a batchwise treatment, the entire tray assembly is cooled and a small amount of air is admitted until a layer of tantalum oxide has formed on the powder particle surfaces to prevent pyrophoric combustion of the powder upon subsequent exposure to air. Such a treatment is time-and energy-consuming and requires expensive equipment. Also, the fixed bed geometry of the treatment results in material near the outside of the bed being heated sooner and hotter than the material in the middle of the bed or tray stack. Heat transfer is also slow. In addition, since the material on the outside of the bed is heated more than that on the inside, uneven sintering can occur. A non-uniform product can result with various portions of the charge having different physical properties from others. If the material on the inside is not sufficiently sintered, the resultant product is fragile and a large proportion of this material turns to a dust during subsequent handling of the product. Such dust or fines must be recycled for reprocessing.




It is an object of the present invention to provide an apparatus for high temperature treatment of solid particulate material, while under a vacuum, by the use of a rotating kiln that will provide a more heat-treated uniform product.




It is another object of the present invention to provide a method for the continuous high temperature treatment of solid particulate material, such as tantalum powder, while under a vacuum, using a rotating kiln so as to provide a more uniform heat treated product.




SUMMARY OF THE INVENTION




A rotating vacuum kiln has a rotatable refractory metal cylindrical vessel that includes a cool inlet zone, a hot intermediate zone, and a cool exit zone. A gaseous exhaust conduit extends through an end wall of the cylindrical vessel through the cool exit zone and to the hot intermediate zone. A first series of inner radiation shields are provided in the cylindrical vessel at the hot intermediate zone adjacent to the cool inlet zone, and a second series of inner radiation shields are provided at the hot intermediate zone adjacent to the cool exit zone.




A first vacuum housing encloses a feed chute that directs solid particulate material to the cool inlet zone of the cylindrical vessel while under vacuum, while a second vacuum housing encloses a discharge chute for discharging treated material from the cylindrical housing while also under vacuum. Solid particulate material is moved through the rotating refractory metal cylindrical vessel by the use of screw flights attached to the inner surface of the vessel wall or by tilting the cylindrical vessel to allow flow by gravity.




The hot intermediate zone of the cylindrical vessel is indirectly heated by electric resistance heating bands which are provided, spaced from and along the hot intermediate zone, while outer radiation shields surround the heating bands and the cylindrical vessel along the hot intermediate zone. The use of the heating bands, radiation shields, and first and second series of inner radiation shields, concentrate the heat in the hot intermediate zone of the cylindrical vessel and shield the cool inlet zone, cool exit zone, and associated mechanical equipment, such as drive equipment and support equipment, from the high temperatures of the hot intermediate zone.




A method of heating a solid particulate material to high temperatures includes providing a rotating refractory metal cylindrical vessel having a cool inlet zone, hot intermediate zone and cool exit zone, with a first series of inner radiation shields at the hot intermediate zone adjacent the cool inlet zone and a second series of inner radiation shields at the hot intermediate zone adjacent the cool exit zone. Solid particulate material is moved through the rotating refractory metal cylindrical vessel while under a vacuum from the cool inlet zone and heated to a temperature of between about 1000° to 1700° C. in the hot intermediate zone and then discharged from the cool exit zone of the rotating refractory metal cylindrical vessel.











BRIEF DESCRIPTION OF THE DRAWINGS




The present invention will be more readily understood by reference to the following description of embodiments thereof and the accompanying drawings, wherein:





FIG. 1

is a longitudinal sectional view of a rotating refractory metal cylindrical vessel of the rotating vacuum kiln of the present invention;





FIG. 2

is a longitudinal sectional view through another embodiment of a rotating vacuum kiln of the present invention;





FIG. 3

is a view taken along lines III—III of

FIG. 2

;





FIG. 4

is a view taken along lines IV—IV of

FIG. 2

; and





FIG. 5

is a schematic view of the rotating vacuum kiln of

FIG. 1

illustrating the systems for feeding and discharging material under vacuum.











DETAILED DESCRIPTION




The rotating vacuum kiln of the present invention enables the heating of solid particulate material to a high temperature, for heat treatment or sintering under high vacuum conditions.




Referring now to the drawings,

FIG. 1

illustrates an embodiment of a rotary vacuum kiln


1


of the present invention having a rotating refractory metal cylindrical vessel


2


having an inner wall


3


and an outer wall


4


, the rotating refractory metal cylindrical vessel


2


having a cool inlet zone


5


, a hot intermediate zone


6


, and a cool exit zone


7


. A means


8


for charging a solid particulate material is provided on the cool inlet zone


5


of the cylindrical vessel


2


, such as a feed chute


9


, which feeds the material to a mixing and charging conduit


10


attached to the cylindrical vessel


2


, that communicates with the cool inlet zone


5


, the feed chute


9


and mixing and charging conduit


10


enclosed in a first vacuum housing


11


. The mixing and charging conduit


10


includes an inclined wall


12


on the cylindrical vessel


2


that acts as a dam to prevent solid particulate material from escaping from the mixing and charging conduit


10


rather than moving towards the cool inlet zone


5


of the cylindrical vessel


2


, which inclined wall


12


receives and encloses the discharge end


13


of the feed chute


9


. Feed chute


9


also has an outwardly flared section


14


at the upper end to receive solid particulate material. The cool exit zone


7


of the cylindrical vessel


2


has an end wall


15


with a gaseous exhaust conduit


16


passing through the wall


15


, and a discharge chute


17


communicating with the cylindrical vessel


2


at the cool exit zone


7


, the discharge chute


17


having an open receiving end


18


within the cool exit zone


7


for receiving solid particulate material therefrom and a discharge end


19


for discharging solid particulate material therefrom. The discharge end


19


of discharge chute


17


is enclosed in a second vacuum housing


20


.




Extending through the end wall


15


of the cylindrical vessel


2


, the gaseous exhaust conduit


16


receives gases from the cylindrical vessel


2


and passes the same to a gaseous discharge conduit


21


, while gaseous discharge conduit


21


is connected to a vacuum line


22


that is, in turn, connected to a vacuum pump


23


. The gaseous exhaust conduit


16


is preferably concentric with an axis a of the cylindrical vessel


2


, extends through the cool exit zone


7


, and has an open end


24


disposed in the intermediate hot zone


6


of the cylindrical vessel


2


.




A first series of inner radiation shields


25


is provided at the hot intermediate zone


6


adjacent to the cool inlet zone


5


of the cylindrical vessel


2


so as to reduce the flow of heat from the intermediate hot zone


6


to the cool inlet zone


5


of the cylindrical vessel


2


. The first series of inner radiation shields


25


are secured to the inner wall


3


, such as by spokes


27


that (

FIG. 2

) extend towards the inner wall and are welded, such as at


28


to the inner wall


3


.




A second series of inner radiation shields


29


is provided in the hot intermediate zone


6


adjacent to the cool exit zone


7


of the cylindrical vessel


2


so as to reduce the flow of heat from the intermediate zone


6


to the cool exit zone


7


. The second series of inner radiation shields


29


are secured to the outer wall


31


of the gaseous exhaust conduit


16


, such as by welds


32


. The second series of inner radiation


29


shields the cool exit zone


7


from the high temperatures of the intermediate hot zone


6


of the cylindrical vessel


2


. A series of short screw flights


33


may be provided in the cool inlet zone


5


, intermediate hot zone


6


, and cool exit zone


7


, secured to the inner wall


3


such as by welds


34


, to move solid particulate material through the rotating refractory metal cylindrical vessel.




The intermediate hot zone


6


of the cylindrical vessel


2


is heated by use of an indirect heat source, such as electrical resistance heating bands


35


which are spaced from and encircle the outer wall


4


of the cylindrical vessel


2


. The heating bands


35


extend along the length of the intermediate hot zone


6


and are energized through an electric current fed from a source (not shown) through electrical leads


36


. In order to concentrate and direct the heat from the electrical resistance heating bands


35


towards the outer wall


4


of cylindrical vessel


2


, at least one radiation shield


37


and preferably a series of radiation shields


37




a


to


37




f


(FIG.


2


), are provided which are positioned concentrically about and spaced from the electrical resistance heating bands


35


and the intermediate hot zone


6


of the cylindrical vessel


2


and encircle and enclose the same. The radiation shields


37




a


-


37




f


are enclosed within a shield housing


38


.




The cool inlet zone


5


of the cylindrical vessel


2


may be provided with the series of short cool inlet zone screw flights


33


which are secured to the inner wall


3


, such as by welds


34


, and which extend from the inner wall


3


and will serve to move solid particulate material from the mixing and charging conduit


10


to the intermediate hot zone while a plurality of inwardly directed mixing flanges


39


may be provided on the inner wall


40


of the mixing and charging conduit


10


to mix solid particulate material fed thereto and charge the same to the cool short inlet zone screw flights


33


.




Because the intermediate hot zone


6


of the cylindrical vessel


2


, heating bands


35


and radiation shields


37


are contained in shield housing


38


and the first series of inner radiation shields


25


and second series of inner radiation shields


29


retain the heat within the intermediate hot zone, water cooled spool sections


41


may be used to enclose outer wall


4


of the cool inlet zone


5


and cool exit zone


7


, and the spool sections may be made of less expensive ferrous alloys rather than a refractory metal as is required for the cylindrical vessel


2


. The cylindrical vessel


2


may be rotated such as by use of a motor


42


, having a shaft


43


with gears


44


that engage with a ring gear


45


carried by the cylindrical vessel


2


, with the gears


44


contained within first vacuum housing


11


and shaft


43


passing through a seal


46


secured in a wall of the housing


11


.




The end wall


15


of the cylindrical vessel


2


and the outer end


47


of the gaseous exhaust conduit


16


are also enclosed in a third vacuum housing


48


, with discharge chute


19


passing through the lower wall


49


of third vacuum housing


48


into the second vacuum housing


20


. The gaseous exhaust conduit


16


preferably has a plurality of baffles


50


connected to the inner wall


51


, such as by welds


52


which are offset and spaced from each other along the horizontal axis a so as to provide a tortious path for gases flowing therethrough.




In order to maintain the interior i of the cylindrical vessel


2


under vacuum, while treating solid particulate material therein, the source of vacuum, vacuum pump


23


pulls a vacuum through vacuum line


22


, gaseous discharge conduit


21


, gaseous exhaust conduit


16


, the interior i of cylindrical vessel


2


, second vacuum housing


20


and first vacuum housing


11


, with seals and bearings provided where necessary to keep leakage within acceptable limits, as is known to one skilled in the art. To assist in maintaining the vacuum within the system, and particularly within the interior i of the cylindrical vessel


2


, a series of sealable feed hoppers and sealable discharge hoppers are provided, as shown in FIG.


5


. As schematically illustrated, for charging the cylindrical vessel


2


, solid particulate material to be treated is fed through a feed line


53


, through a sealable inlet valve


54


, to an initial feed chute


55


, contained within a first feed housing


56


having a feeder


57


which cooperates with a second sealable valve


58


. Second sealable valve


58


feeds to a second feed chute


59


which is contained within a first roughing vacuum feed housing


60


that is connected through line


61


to a source of vacuum, such as pump


62


, and which has a feeder


63


which cooperates with a third sealable valve


64


. Third sealable valve


64


feeds to an intermediate transfer feed chute


65


contained in an intermediate feed housing


66


that has an intermediate feeder


67


which cooperates with a fourth sealable valve


68


. Fourth sealable valve


68


feeds to a further feed chute


69


which is contained within a housing


70


that is connected through line


71


to a source of vacuum, such as pump


72


, and which has a feeder


73


which cooperates with a sealable valve


74


which cooperates with the first vacuum housing


11


so as to feed solid particulate material therefrom through outwardly flared section


14


to feed chute


9


and then to the cool inlet zone


5


of the cylindrical vessel


2


. For discharging treated solid particulate material from the cylindrical vessel


2


, the treated material is fed by the rotating refractory metal cylindrical vessel


2


into the open end


18


of discharge chute


17


into second vacuum housing


20


, and through a first sealable discharge valve


75


into intermediate discharge chute


76


contained in a housing


77


that has an intermediate discharge feeder


78


which cooperates with a second sealable discharge valve


79


. Second sealable discharge valve


79


feeds to a second discharge chute


80


which is contained in roughing discharge housing


81


that has a discharge line


82


for reducing the vacuum in the roughing discharge housing


81


through reduction valve


83


, and which has a discharge feeder


84


which cooperates with final discharge sealable valve


85


to discharge the material from the system.




The operation of the rotating vacuum kiln


1


of the present invention is as follows. With motor


42


activated, the cylindrical vessel


2


is rotated by means of gears


44


meshing with gear ring


45


and upon activation of the vacuum pump


23


, the system including vacuum line


22


, gaseous discharge conduit


21


, interior of housing


50


, gaseous exhaust conduit


16


, discharge chute


17


, interior of second discharge housing


20


, the interior i of cylindrical vessel


2


, mixing and charging conduit


10


, and the interior of first vacuum housing


11


are placed under a vacuum as is desired for a particular treatment. The electrical resistance heating bands


35


are activated to heat the hot intermediate zone


6


of the cylindrical vessel


2


to the desired temperature, with radiation shields


37


retaining such heating. At this stage, solid particulate material to be treated is provided in further feed chute


69


, with the interior of housing


70


, with sealable valves


68


and


74


closed, subjected to a vacuum comparable to that within the cylindrical vessel


2


, by means of vacuum pump


72


. Upon opening of sealable valve


74


, solid particulate material is fed by feeder


73


to the feed chute


9


through outwardly flared section


14


and passes by gravity through the feed chute


9


to the mixing and charging conduit


10


. In mixing and charging conduit


10


, which is connected to, and rotating with, the cylindrical vessel


2


, the solid particulate matter is mixed, by contact with and tumbling by flanges


39


on inner wall


40


, while the inclined wall


12


prevents material escaping and urges the material into the cool inlet zone


5


of the cylindrical vessel


2


. The solid particulate material in cool inlet zone


5


is moved by the short cool inlet zone screw flights


33


to, and through, the hot intermediate zone


6


, while heating the material to the desired temperature. The hot material is then transferred, by short intermediate hot zone screw flights


33


, towards the open receiving end


18


of discharge chute


17


, with the hot material then fed through discharge chute


17


to housing


20


for discharge from the system. During the operation of the rotating vacuum kiln


1


, the first series of inner radiation shields


25


shields the cool inlet zone


5


from the high temperature of the hot intermediate zone


6


, while the second series of inner radiation shields


29


shields the cool exit zone


7


from that high temperature.




The present invention uses the above described rotating refractory metal cylindrical vessel


2


in heat-treating of solid particulate material. Solid particulate material is charged, under vacuum, to the cool inlet zone


5


of the rotating refractory metal cylindrical vessel


2


. which has a cool inlet zone


5


, hot intermediate zone


6


and cool exit zone


7


, and a first series of inner radiation shields


25


at the hot intermediate zone


6


adjacent to the cool inlet zone


5


, and a second series of inner radiation shields


29


at the hot intermediate zone


6


adjacent to the cool exit zone


7


. The solid particulate material is moved through the rotating refractory metal cylindrical vessel


2


while under a vacuum and heated in the hot intermediate zone


6


to a temperature of between about 1000° to 1700° C. in the hot intermediate zone


6


and then discharged from the cool exit zone


7


.




The heat treatment of solid particulate material according to the present invention is carried out under vacuum conditions and can be carried out at a vacuum below about 0.001 Torr and as low as of about 10


−4


Torr or lower, with residence times in the hot intermediate zone


6


of between about 0.3 to 2.0 hours. With the use of the first and second series of radiation shields


25


and


29


. with temperatures of between about 1000°-1700° C. preferably 1400°-1600° C. in the hot intermediate zone


6


. the temperatures in the cool inlet zone


5


and the cool exit zone


7


would be about 300° C. or below.




When heat-treating of tantalum powder, for example, temperatures in the 1500° C. range would be required in the hot intermediate zone


6


and the rotating refractory metal cylindrical vessel


2


would be composed of a refractory metal, such as molybdenum, tantalum, tungsten, or a refractory metal alloy such as a molybdenum alloy containing minor amounts of titanium and zirconium. The term refractory metal, as used herein, is used to designate a metal which will last for sufficient periods of time at temperatures in range of up to about 1700° C. without deleterious effects. Where tantalum is to be treated, for example, the cylindrical vessel


2


could be formed from a molybdenum alloy containing minor amounts of titanium and zirconium, with an inner liner of tantalum which would contact the hot solid particulate material being treated though the cylindrical vessel


2


. and with tantalum screw flights


33


welded to the inner liner on the wall


3


of the cylindrical vessel


2


and stitch-welded to each other so as to avoid differential expansion problems. A preferred embodiment would be “TEM”, which is an alloy of molybdenum with about 0.5% titanium and 0.08% zirconium. A preferred liner material is tantalum when processing tantalum powder.




The residence time in the cylindrical vessel


2


can be adjusted as desired by the pitch. height and cylindrical vessel rotation speed. In some instances. as shown in FIG.


1


. the use of screw flights


33


may be avoided if the cylindrical vessel


2


is positioned at a downward angle from the cool inlet zone


5


to the cool exit zone


7


and the material allowed to assume its natural angle of rill under rotation, and the material will move the same through the cylindrical vessel


2


.




Feeding of the cylindrical vessel


2


is carried out by feeding solid particulate material through feed line


53


and through open valve


54


into initial feed hopper or chute


55


at atmospheric pressure. Valve


54


is then closed and the material transferred by feeder


57


through opened valve


58


into second feed chute


59


. With valve


58


and valve


64


in closed position, a partial vacuum is provided in housing


60


through line


61


by activation of vacuum pump


62


. When the desired partial vacuum is achieved, valve


64


is opened and feeder


63


feeds the material to intermediate transfer feed chute


65


. Valve


64


is then closed and valve


68


opened, and the material, under partial vacuum, is fed by intermediate feeder


67


into further feed chute


69


. With valves and with vacuum pump


72


activated, a vacuum that approaches the high vacuum desired in the cylindrical vessel


2


is applied and feeder


73


used to discharge the material to feed chute


9


through flared section


14


. In the heat-treating of tantalum powder, a vacuum in the refractory metal cylindrical vessel


2


of about 0.001 Torr or below would be provided. In discharge of treated material from the cylindrical vessel


2


, a reverse procedure is carried out, where treated solids from the cylindrical vessel


2


are discharged therefrom through discharge chute


76


into second vacuum housing


20


. With second discharge valve


79


closed, the first discharge valve


75


is opened and the material fed to intermediate discharge chute


76


. First discharge valve


75


is then closed and second discharge valve


79


opened as that material is fed by intermediate discharge feeder


78


into second discharge chute


80


. With final discharge valve


85


in closed position, second discharge valve


79


is then closed and vacuum released through line


82


and reduction valve


83


. The material may be discharged into a further rotating drum (not shown) at atmospheric pressure where cooling and passivation would be effected. With the vacuum released, and a small amount of air injected to form an oxidized coating on the material, final discharge valve


85


may then be opened and the treated material removed for use.



Claims
  • 1. A method of heating a solid particulate material to a temperature of 1000° to 1700° C. under a vacuum comprising:producing a rotating refractory metal cylindrical vessel having inner and outer walls, a cool inlet zone, a hot intermediate zone, and a cool exit zone, a first series of inner radiation shields at said hot intermediate zone adjacent said cool inlet zone and a second series of inner radiation shields at said hot intermediate zone adjacent said cool exit zone, moving solid particulate matter through said rotating refractory metal cylindrical vessel while under a vacuum; heating said solid particulate metal to a temperature of 1000° to 1700° C. in said hot intermediate zone; and discharging said heated solid particulate material from said cool exit zone.
  • 2. The method as defined in claim 1 wherein said vacuum is at 0.001 Ton or below.
  • 3. The method as defined in claim 1 wherein said solid particulate material is tantalum powder.
  • 4. The method as defined in claim 3 wherein said vacuum is at 0.001 ton or below.
  • 5. The method as defined in claim 3 wherein the residence time of said tantalum powder in the hot intermediate zone is between about 0.3 to 2.0 hours.
  • 6. The method as defined in claim 3 wherein said temperature is between about 1400° to 1600° C.
Parent Case Info

The present application is a divisional of prior U.S. patent application Ser. No. 09/100,970 filed Jun. 22, 1998, now U.S. Pat. No. 6,105,272.

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Entry
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