1. Technical Field
This invention generally relates to pusher furnaces. More particularly, the invention relates to a method and apparatus for controlling the position of the sections of a pusher furnace in response to changes in temperature. Specifically, the invention relates to a compression system which engages at least one furnace section and applies pressure thereto to maintain contact between adjacent furnace sections in the pusher furnace.
2. Background Information
Pusher furnaces are designed in various lengths and may contain multiple heating and cooling sections as required by the application. These furnaces include a substantially continuous flat surface or a pair of slide rails running through the interior of the furnace. A plurality of pusher plates, carrying the material to be processed on their upper surfaces, are pushed sequentially along the flat surface and through the heating sections. Materials processed in this manner may include various materials required for electronic or ceramic components, as well as different metals that are to be annealed, sintered or de-waxed. In order to process a particular material properly, that material typically has to be subjected to very specific temperatures and atmospheric conditions as it passes through the furnace.
When the individual heating sections are heated, the overall length of the longitudinally extending furnace increases, sometimes by as much as several inches. Each heating section may be heated to a different temperature and consequently adjacent heating sections will likely expand to differing degrees. Furthermore, if the pusher furnace needs to be shut down in an emergency situation, for example, the various heating sections will tend to cool down at differing rates and, consequently, the heating sections may shrink to differing degrees. This difference in cooling rates can result in adjacent heating sections pulling apart from each other as they contract, thus creating gaps between the adjacent heating sections. Heat and gasses escape through these gaps, potentially causing damage to insulation within the sections and even potentially increasing the risk of catastrophic explosions. Even if the escaping heat and gasses do not cause explosions, they do cause a sudden change in the thermal and atmospheric conditions within the adjacent heating sections and thereby likely lead to damage of the materials being processed.
There is therefore a need in the art for a method and apparatus for keeping the heating sections in a pusher furnace substantially in contact with each other, thereby maintaining the temperature gradients over the entire length of the longitudinally extending furnace.
The present invention provides a furnace unit having first and second opposed ends and including a plurality of furnace sections each having a susceptor; wherein each susceptor abuts an adjacent susceptor; wherein the susceptors include first and last susceptors respectively adjacent the first and second ends of the furnace unit; a movable member which abuts the first susceptor for applying a force on the first susceptor toward the last susceptor whereby the movable member is adapted to keep the susceptors in abutment with each other during contraction of the susceptors during cooling thereof; and an actuator for moving the movable member.
The preferred embodiments of the invention, illustrative of the best mode in which applicant has contemplated applying the principles, are set forth in the following description and are shown in the drawings and are particularly and distinctly pointed out and set forth in the appended claims.
Referring to
Each heating section 12, 14 and 16 is substantially identically constructed. The following description relates to heating section 12, but applies generally to heating sections 14 and 16 as well. Heating section 12 includes an interior passageway 18 (
The susceptors 20 of adjacent heating sections 12, 14 and 16 must be kept in substantially continuous abutting contact with each other in order to prevent leakage of heat and process gasses from within passageway 18. Therefore, as may be seen from
A materials transport system extends through tunnel 34 and comprises a pair of spaced apart slide rails 36, 38 and a guide rail 40 disposed centrally between them. Slide rails 36, 38 and guide rails 40 are seated on susceptors 20 respectively within mating recesses 86A, 86B and 90 formed in a bottom wall 88 of susceptor 20. A plurality of pusher plates 42 are provided for transporting materials 44 through heating sections 12, 14 and 16. A pusher arm 46 is provided to push pusher plates 42, and therefore materials 44, into tunnel 34 and through heating sections 12, 14 and 16. Pusher plates 42 are slidably moved atop rails 36, 38 through tunnel 34 along a longitudinal axis of travel indicated at A-A in
First and second axially spaced and longitudinally elongated pedestals or supports 98A and 98B which are seated within induction coil 24. Supports 98 extend substantially the same length as susceptor 20 and insulation layers 22. Respective layers of graphoil 100A and 100B or a graphoil type material are seated respectively atop supports 98A and 98B along the length thereof in respective recesses formed therein. More particularly, bottom wall 88 of susceptor 20 is spaced upwardly of bottom insulation layers 22A to define a space 102 therebetween. Thus, susceptor 20 is supported entirely on layers of graphoil 100 and do not contact bottom insulation layers 22A. This arrangement helps to preserve bottom insulation layers 22A by eliminating the weight and friction thereon of susceptor 20 and any weight contributed thereto by top insulation layers 22B and any other related structure. This also eliminates degradation due to differing thermal expansion and contraction rates during heating and cooling of susceptor 20 and bottom insulation layers 22A which would occur if the susceptor were seated atop the insulation. Graphoil 100 provides a low-friction material which allows for the thermal expansion and contraction of susceptor 20 without substantial wear caused by the engagement therebetween. The arrangement of supports 98, layers 100 and related structure of the present invention is further described in the copending application entitled Furnace Alignment System, previously referenced herein.
Each individual heating section 12, 14 and 16 is programmed to heat up to a specific predetermined temperature, this temperature being potentially as high as 2200° C. or 4352° F. Each individual heating sections 12, 14 and 16 may also include a variety of different materials from those used in adjacent sections. These differing materials typically have respective coefficients of thermal expansion which differ from one another. As a result of the plurality of different factors affecting each section, each of the susceptors 20 will tend to heat up and cool down at a different rate than the susceptors in the adjacent heating sections and will consequently expand and contract at a different rate than the susceptors 20 in the heating sections disposed adjacent thereto. Furnace 10 may expand several inches in length because of the extremely high temperatures used in heating sections 12, 14 and 16. In a furnace of 60 feet in length, this expansion has been found to be as much as four inches.
Prior to heating of heating sections 12, 14 and 16, the susceptors 20 and the associated insulation 22 are interlocked in the manner shown in
Consequently, in accordance with a specific feature of the present invention, pusher furnace 10 is provided with a compression system, generally indicated at 50 to keep the susceptors 20 of adjacent heating sections 12, 14 and 16 interlocked with each other. Compression system 50 applies pressure to the susceptors 20 as required and thereby maintains the integrity of furnace 10 even though it may undergo a number of heating and cooling cycles.
Compression system 50 includes a plurality of pressure sensitive, torque electric actuators or hydraulic cylinders 52, a movable member in the form of a floating compression plate 54, a slide pin assembly 56 and, spaced a distance therefrom, a stationary member which in this instance is end wall 48. A compression spool 58 of slide pin assembly 56 is free to slide backward and forward on a pin 60 thereof. Furthermore, compression plate 54 has an annular flange or insert 62 that projects toward and substantially matches the face of the susceptor 20a of the first heating section 12. Thus, like the joints between adjacent susceptors 20, insert 62 and susceptor 20a form therebetween an overlapping shiplap joint. When compression plate 54 and susceptor 20a are engaged, they provide a positive, gas-tight seal which keeps all the process gasses internally within the heated chamber 12. Compression plate 54 includes an aperture 64 therethrough, which is substantially continuous with passageway 18 in heating section 12 and consequently with tunnel 34. Similarly, a stationary member, i.e., wall 48 is sealed with the susceptor of last heating section 16 in like manner to compression plate 54 and susceptor 20a. Second aperture 47 through end wall 48 is also substantially continuous with tunnel 34. Slide rails 36, 38 and guide rail 40 extend through apertures 64 and 47. Aperture 64 allows pusher plate 42, carrying the unprocessed materials 44 thereon, to be pushed into heating section 12 by pusher arm 46 and second aperture 47 allows pusher plate 42 carrying the now-processed materials 44 to exit heating section 16. Compression system 50 further includes a movement sensor in the form of a linear transducer 66 which measures the distance the compression plate 54 moves forwardly or rearwardly in response to actuation of cylinders 52. Compression system 50 is preferably also provided with one or more pressure sensors 66 (
The compression system 50 substantially keeps the shiplap joints between adjacent susceptors 20, and preferably the shiplapped layers of insulation 22 as well, tightly engaged and sealed and, through the linear transducer 66 and pressure and temperature sensors 66 and 68 monitors the thermal heating and cooling and related expansion and contraction of furnace 10 and activates and deactivates the hydraulic cylinders 52 as required. The sensors are linked into the controls of compression system 50 so that system 50 automatically applies more or less pressure to the susceptors 20 as they contract or expand. The potential formation of gaps between heating sections 12 and 14, and 14 and 16 is thereby substantially reduced.
The compression system 50 is preferably automated, but functions in the following manner. First, the thermal expansion coefficients and the temperature to which each section is to be heated is used to calculate the expansion/shrinkage profile for each susceptor in each of sections 12,14 and 16. The various induction coils are then powered to inductively heat the various susceptors within the furnace in order to heat the furnace to the operating temperature. During the heating of the furnace, the total expansion of the susceptors is measured via the use of transducer 66 or a similar sensor. When heating sections 12, 14 and/or 16 of furnace 10 cool down for one reason or another, a plurality of sensors provided on each of the individual heating sections 12, 14 and 16, in conjunction with the sensors provided on compression system 50 send a signal to the compression system control center. The control center actuates the hydraulic cylinders 52 to move as indicated at Arrow B in
When furnace 10 is fired up, the susceptors 20 will begin to expand once more. As they expand, the sensors on heating sections 12, 14 and 16 and the linear transducer 66 and sensors on compression system 50 feed information to the compression system controls which then retract cylinders 52 in response to the rate of expansion. This causes compression plate 54 to move in the direction opposite to the direction of travel through furnace 10. When susceptors 20 within furnace 10 are fully expanded, cylinders 52 cease to move. Thus all joints between adjacent susceptors are kept fully interlocked and the heat and process gasses are contained within tunnel 34. If desired, plate 54 may apply pressure on susceptor 20a toward the susceptor 20 in section 16 while moving away from the susceptor 20 of section 16.
In the foregoing description, certain terms have been used for brevity, clearness, and understanding. No unnecessary limitations are to be implied therefrom beyond the requirement of the prior art because such terms are used for descriptive purposes and are intended to be broadly construed.
Moreover, the description and illustration of the invention is an example and the invention is not limited to the exact details shown or described.
This application claims priority from U.S. provisional application Ser. No. 60/748,872 filed Dec. 7, 2005; the disclosure of which is incorporated herein by reference.
Number | Date | Country | |
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60748872 | Dec 2005 | US |