US3060595A - Jet dryer - Google Patents
Jet dryer Download PDFInfo
- Publication number
- US3060595A US3060595A US819763A US81976359A US3060595A US 3060595 A US3060595 A US 3060595A US 819763 A US819763 A US 819763A US 81976359 A US81976359 A US 81976359A US 3060595 A US3060595 A US 3060595A
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- velocity
- area
- wall
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- expansion chamber
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Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F26—DRYING
- F26B—DRYING SOLID MATERIALS OR OBJECTS BY REMOVING LIQUID THEREFROM
- F26B21/00—Arrangements or duct systems, e.g. in combination with pallet boxes, for supplying and controlling air or gases for drying solid materials or objects
- F26B21/004—Nozzle assemblies; Air knives; Air distributors; Blow boxes
-
- D—TEXTILES; PAPER
- D21—PAPER-MAKING; PRODUCTION OF CELLULOSE
- D21F—PAPER-MAKING MACHINES; METHODS OF PRODUCING PAPER THEREON
- D21F5/00—Dryer section of machines for making continuous webs of paper
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F26—DRYING
- F26B—DRYING SOLID MATERIALS OR OBJECTS BY REMOVING LIQUID THEREFROM
- F26B13/00—Machines and apparatus for drying fabrics, fibres, yarns, or other materials in long lengths, with progressive movement
- F26B13/10—Arrangements for feeding, heating or supporting materials; Controlling movement, tension or position of materials
Definitions
- the apparatus of this invention is designed to avoid transverse exhaust of the spent gases present in constructions such as that shown in Dungler Patent No. 2,594,299.
- uniform drying is difiicult and practically impossible at high velocities because outer sections of the web being dried are exposed to greater quantities of air per second than the center of the web because the volume of air moving transversely of the web to the exhaust at each side of the apparatus increases outwardly from the center of the dryer to both sides, as the air from the side jets is added to the air exhausting from the center jets.
- edge drying i.e., the center of the web is not dried as rapidly as its edges.
- the gases are not exhausted across, but rather are exhausted in a direction perpendicularly away from the surface of the material being treated.
- the number of jets may be increased indefinitely in any direction without affecting the drying characteristics within any existing jet area.
- avoidance of transverse exhaust gas flow permits, by proper design of the spaces between the nozzles, an abrupt loss of velocity insuring that any benefits arising from the kinetic energy of the gas will be procured at or near the drying surface where the kinetic energy is dissipated.
- the exhaust ports may be readily so designed that after great loss of velocity, the air may still be exhausted at the identical rate at which it is introduced, and preferably at velocities great enough to permit utilization of an exhaust suction chamber of reasonable size leading through a closed return circuit containing a reheating unit.
- each nozzle as an individual unit, so to speak, and to handle every nozzle in the same manner as every other nozzle, so that cumulatively uniformity of drying results regardless of the number or extent of the nozzles and edgedrying (i.e., overdrying at the edges) is avoided.
- this includes providing, in the preferred form, a separate exhaust adapted to handle the total volume of air emanating from each separate nozzle.
- P16. 1 is a vertical cross-sectional view of a treating apparatus embodying the invention
- FIG. 2 is a plan view taken along the line 2-2 of FIG. 1;
- FIG. 4 is a cross-sectional view taken along the line 4-4 of FIG. 3.
- the treating chamber is in a form wherein a conveyor belt 10 which may be traveling continuously conveys materials through an inlet into the chamber 12, through the chamber and out an outlet 14.
- the remainder of the apparatus in this embodiment takes the form of a hood which includes side walls 16 and 18 and a top wall 20.
- Leading through the bottom wall 22 of the pressure chamber 36 are a series of spaced tubes which constitute the nozzles of the dryer. These nozzles 40 extend downwardly so that their orifices lie in a single plane spaced at short distance above the conveyor belt 10.
- the nozzles extend through the wall 42 through oversize apertures 44, which, in the form shown, comprise the exhaust ports leading back into the suction chamber.
- oversize apertures 44 comprise the exhaust ports leading back into the suction chamber.
- these are circular holes in the wall 42 but their dimensions are carefully chosen as will be hereinafter described, though their shape and locations in the wall 42 may be varied.
- the web treatment area the area or zone between the conveyor belt and the plane of the nozzle orifices.
- the passages between the nozzles and extending from the top of the web treatment zone to the partition Wall 42 will be referred to as the expansion chamber, indicated by reference 48.
- each tube can, for example be spaced at a distance of 1%. inches from the conveyor or at least from the material to be treated when it is placed on the conveyor.
- the total bore area of the entire 40 tubes will be 0.06676 square foot.
- the entire length of the chamber in the form shown is, say 2 ft. and the width of the belt is 1.0937 ft., so that the cross-sectional area of the Web under treatment in square feet is 2.1875.
- the partition wall is provided with apertures each of which is 1% inches in diameter equivalent in square feet to'.0.00690 which deducting the displacement of each /6 inch diameter tube through the center leaves the exhaust ports each with an area in square feet of 0.00476 and a total area of 40 0.00476 or 0.1904 sq. ft.
- the cross-sectional area of the expansion chamber as previously defined is therefore the area of web treatment (2.1875 sq. ft.) minus the displacement of 40 inch diameter tubes or 2.1021 sq. ft.
- the ratio of the jet tube blast area to the web treatment area is thus or 3.05% plus or minus.
- the ratio in percent of the exhaust areas to the web treatment area is thus .00476 40 (0.1904) divided by 2.1875 or 8.69% plus or minus. If the jet discharge velocity is, for example 8000 f.p.m., each jet will emit 8000 .001669 sq. ft. per minute or 13.352 c.f.m. and 40 jets will emit 534 c.f.m.
- the velocities at other points in the apparatus may be ascertained from the equation when V is the velocity in feet per minute, A is the crosssectional area in sq. ft. and Q is the cubic feet per minute, the 534 c.f.m. remaining constant throughout the apparatus.
- the effective height of the expansion chamber will be limited by the suction velocity contour lines.
- no contour line having a suction approach velocity greater than the desired minimum expansion chamber velocity should extend so far towards the web being treated as to unduly limit the height of the effective expansion chamber area and thus prevent attainment of the desired minimum expansion chamber velocity.
- the above relations may be further expressed as a desire on my part to have the total cross-sectional area of the orifices in a ratio to the total cross-sectional area of the expansion chamber which is as small as possible consistent with maintaining the overall compactness of the device.
- this will mean that expressed percentage-wise such ratio should be from 1 /2 to about 6%, being or 3.15% in the illustrative apparatus.
- the percent of the cross-sectional areas of the exhaust ports based upon the total web treatment area may run from about 1 /z% to as high as 18%, depending upon the permissible size of the suction chamber 46, being or 8.69% in the illustrative device.
- the extent to which the nozzles extend beyond the partition wall 42 controls the height of the web treating area.
- the expansion chamber is increased in height, other dimensions being constant; with the minimum expansion chamber velocity thus decreasing.
- the nozzle may extend from wall 42 as little as 25 percent of that distance.
- the pressure plenum chamber 30 and the suction chamber 46 are provided respectively with an inlet 50 from the fan and an outlet 52 to the fan of equal crosssectional area. As shown, both chambers are so dimensioned that the inlet 50 will supply gas at uniform rates to all 40 nozzles and the outlet pipe 52 will draw uniformly from all 40 exhaust ports 44, in accordance with known principles.
- nozzle orifices lie in a horizontal plane nor that they extend downwardly as distinguished from horizontally or upwardly.
- the entire unit may thus be turned about a horizontal axis or otherwise tipped so that the plane of the orifices will be parallel to any plane which constitutes the path of the material being treated.
- Apparatus for gaseous treatment of a material comprising a casing having a plane wall forming a partition, said wall being perforated to define a plurality of spaced apertures forming exhaust ports lying in the plane of said wall, said apertures having a total area substantially less than the total area of said partition within said casing, a series of straight parallel tubes extending through said Wall away from said plane and terminating at and having orifices lying in a common plane spaced from but parallel to the plane of said exhaust ports for directing gaseous streams issuing from said orifices at a predetermined uniform velocity onto a material presented in opposition to said orifices, the space within said casing between said planes being obstructed solely by said tubes and forming an expansion chamber, having a depth equivalent to the distance between said planes and a transverse cross-sectional area which is uniform throughout its depth, into which the gases in said streams pass after they impinge on said material and through which they rise with velocities substantially reduced from said orifice velocity before they reach
- said casing has an inlet and an opposed aligned outlet adapted to permit a material to be treated to be passed into, through and out of said casing along a plane path parallel to the plane of said orifices and wherein said tubes extend from the plane of said partition towards said path at least 25% of the distance between said partition and said path, whereby the depth of said chamber is at least 5% of said distance.
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- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Textile Engineering (AREA)
- Drying Of Solid Materials (AREA)
Description
i as) 3,060,595 Patented Oct. 30, 1962 ice 3,060,595 JET DRYER William P. Dapses, North Attlehoro, Mass, assignor t Wolverine Equipment 60., Cambridge, Mass, a corporation of Massachusetts Filed June 11, 1959, Ser. No. 819,763 3 Claims. (Cl. 34-160) This invention reiates to apparatus useful in the treatment of materials with gaseous streams, including particularly the treatment of continuously fed sheet materials such as paper and cloth, and more specifically with socalled jet dryers which utilize high velocity gaseous jets for such treatment.
It is a main object of the invention to provide a gaseous treatment apparatus wherein impingement of gases may be accomplished simultaneously over a wide area of material to be treated while exposing all sections of the material to substantially uniform volumes of gas and while maintaining the impinging velocity so high that the temperature differential between the gas and any single limited area of the material is maintained as high as possible consistent with the maximum permissible gas temperature input.
To this end, the apparatus of this invention is designed to avoid transverse exhaust of the spent gases present in constructions such as that shown in Dungler Patent No. 2,594,299. In such constructions uniform drying is difiicult and practically impossible at high velocities because outer sections of the web being dried are exposed to greater quantities of air per second than the center of the web because the volume of air moving transversely of the web to the exhaust at each side of the apparatus increases outwardly from the center of the dryer to both sides, as the air from the side jets is added to the air exhausting from the center jets. This results in edge dryingi.e., the center of the web is not dried as rapidly as its edges.
According to this invention, the gases are not exhausted across, but rather are exhausted in a direction perpendicularly away from the surface of the material being treated.
Several advantages accrue. First, the number of jets may be increased indefinitely in any direction without affecting the drying characteristics within any existing jet area. Second, avoidance of transverse exhaust gas flow permits, by proper design of the spaces between the nozzles, an abrupt loss of velocity insuring that any benefits arising from the kinetic energy of the gas will be procured at or near the drying surface where the kinetic energy is dissipated. Lastly, the exhaust ports may be readily so designed that after great loss of velocity, the air may still be exhausted at the identical rate at which it is introduced, and preferably at velocities great enough to permit utilization of an exhaust suction chamber of reasonable size leading through a closed return circuit containing a reheating unit.
In short, it is an object of this invention to handle each nozzle as an individual unit, so to speak, and to handle every nozzle in the same manner as every other nozzle, so that cumulatively uniformity of drying results regardless of the number or extent of the nozzles and edgedrying (i.e., overdrying at the edges) is avoided. lnsofar as possible, this includes providing, in the preferred form, a separate exhaust adapted to handle the total volume of air emanating from each separate nozzle.
These and other advantages and objects of the invention will be discussed in more detail in connection with a description of the accompanying drawings wherein:
P16. 1 is a vertical cross-sectional view of a treating apparatus embodying the invention;
FIG. 2 is a plan view taken along the line 2-2 of FIG. 1;
FlG. 3 is an enlarged cross-sectional detail taken of a portion of FIG. 1, with a part broken away; and
FIG. 4 is a cross-sectional view taken along the line 4-4 of FIG. 3.
In the embodiments shown, the treating chamber is in a form wherein a conveyor belt 10 which may be traveling continuously conveys materials through an inlet into the chamber 12, through the chamber and out an outlet 14. The remainder of the apparatus in this embodiment takes the form of a hood which includes side walls 16 and 18 and a top wall 20. An intermediate internal wall 22, forms the bottom wall of a pressure plenum chamber 39. Leading through the bottom wall 22 of the pressure chamber 36 are a series of spaced tubes which constitute the nozzles of the dryer. These nozzles 40 extend downwardly so that their orifices lie in a single plane spaced at short distance above the conveyor belt 10.
A lower partition wall 42 extends horizontally across the chamber at a certain distance above the single plane of the jet orifices which distance will be more fully described hereinafter. Suffice it to say for the moment that the wall 42 defines with the side walls .and the intermediate wall 22 a suction plenum chamber 46.
The nozzles extend through the wall 42 through oversize apertures 44, which, in the form shown, comprise the exhaust ports leading back into the suction chamber. In the form shown these are circular holes in the wall 42 but their dimensions are carefully chosen as will be hereinafter described, though their shape and locations in the wall 42 may be varied.
For the purposes of discussion the area or zone between the conveyor belt and the plane of the nozzle orifices will be referred to as the web treatment area. The passages between the nozzles and extending from the top of the web treatment zone to the partition Wall 42 will be referred to as the expansion chamber, indicated by reference 48. t
For further purposes of discussion, and as shown in FIG. 2, a description will be given of a 40-nozzle chamber wherein, as shown in FIG. 2, the nozzles in each successive row are offset or staggered so that the nozzle centers are spaced laterally in successive rows by a distance equal to the diameter of the bores of the tubes.
If the outside diameter of each tube is /6 inch, they can, for example be spaced at a distance of 1%. inches from the conveyor or at least from the material to be treated when it is placed on the conveyor.
Assuming that the cross-sectional area of the bore of each tube is in square feet 0.001669, the total bore area of the entire 40 tubes will be 0.06676 square foot. The entire length of the chamber in the form shown is, say 2 ft. and the width of the belt is 1.0937 ft., so that the cross-sectional area of the Web under treatment in square feet is 2.1875.
With the /6 inch outside diameter tubes the partition wall is provided with apertures each of which is 1% inches in diameter equivalent in square feet to'.0.00690 which deducting the displacement of each /6 inch diameter tube through the center leaves the exhaust ports each with an area in square feet of 0.00476 and a total area of 40 0.00476 or 0.1904 sq. ft.
The cross-sectional area of the expansion chamber as previously defined is therefore the area of web treatment (2.1875 sq. ft.) minus the displacement of 40 inch diameter tubes or 2.1021 sq. ft.
The ratio of the jet tube blast area to the web treatment area is thus or 3.05% plus or minus. The ratio in percent of the exhaust areas to the web treatment area is thus .00476 40 (0.1904) divided by 2.1875 or 8.69% plus or minus. If the jet discharge velocity is, for example 8000 f.p.m., each jet will emit 8000 .001669 sq. ft. per minute or 13.352 c.f.m. and 40 jets will emit 534 c.f.m.
The velocities at other points in the apparatus may be ascertained from the equation when V is the velocity in feet per minute, A is the crosssectional area in sq. ft. and Q is the cubic feet per minute, the 534 c.f.m. remaining constant throughout the apparatus.
Calculations show that with wall 42 spaced 5 /4 above the conveyor so that the nozzles project 4 elow the wall, the velocity through exhaust ports of these dimensions, with a nozzle emission velocity of 8000 f.p.m. will be about 28-00 f.p.m. and the velocity in the expansion chamber will be no greater than about 250 f.p.m. The depth of the expansion chamber is of importance in my construction from the standpoint that as the air ap proaches each exhaust port there is an induced suction approach velocity which is, I believe, controlled by the equation where V equals the center line velocity in f.p.m.; X equals the distance from the orifice in feet; Q represents cubic feet per minute and A equals the area of the orifice in square feet.
Thus a velocity of 2800 f.p.m. through the exhaust port will cause a velocity of 810 f.p.m. at a distance of /2 inch below the port, of 400 f.p.m. at a distance of inch below the port and velocities of 238 f.p.m. at a distance of 1 inch below the port. It is desirable therefore, and for best results essential, to have the expansion chamber of such a height that the influence of the suction approach velocity does not interfere with the purposes of the expansion chamber. In other words, suflicient expansion chamber or deceleration height should be provided to secure the desired minimum expansion chamber velocity, before the air velocity is subjected to increase due to the suction approach velocity. Otherwise, the effective height of the expansion chamber will be limited by the suction velocity contour lines. Hence no contour line having a suction approach velocity greater than the desired minimum expansion chamber velocity should extend so far towards the web being treated as to unduly limit the height of the effective expansion chamber area and thus prevent attainment of the desired minimum expansion chamber velocity.
The above relations may be further expressed as a desire on my part to have the total cross-sectional area of the orifices in a ratio to the total cross-sectional area of the expansion chamber which is as small as possible consistent with maintaining the overall compactness of the device. In general this will mean that expressed percentage-wise such ratio should be from 1 /2 to about 6%, being or 3.15% in the illustrative apparatus. On the other hand, the percent of the cross-sectional areas of the exhaust ports based upon the total web treatment area may run from about 1 /z% to as high as 18%, depending upon the permissible size of the suction chamber 46, being or 8.69% in the illustrative device.
The extent to which the nozzles extend beyond the partition wall 42 controls the height of the web treating area. In general, as the nozzles are lengthened, the expansion chamber is increased in height, other dimensions being constant; with the minimum expansion chamber velocity thus decreasing. However, depending upon the distance between wall 42 and the web being treated, the nozzle may extend from wall 42 as little as 25 percent of that distance.
The pressure plenum chamber 30 and the suction chamber 46 are provided respectively with an inlet 50 from the fan and an outlet 52 to the fan of equal crosssectional area. As shown, both chambers are so dimensioned that the inlet 50 will supply gas at uniform rates to all 40 nozzles and the outlet pipe 52 will draw uniformly from all 40 exhaust ports 44, in accordance with known principles.
It should be understood that it is not essential that the nozzle orifices lie in a horizontal plane nor that they extend downwardly as distinguished from horizontally or upwardly. The entire unit may thus be turned about a horizontal axis or otherwise tipped so that the plane of the orifices will be parallel to any plane which constitutes the path of the material being treated.
What is claimed is:
1. Apparatus for gaseous treatment of a material comprising a casing having a plane wall forming a partition, said wall being perforated to define a plurality of spaced apertures forming exhaust ports lying in the plane of said wall, said apertures having a total area substantially less than the total area of said partition within said casing, a series of straight parallel tubes extending through said Wall away from said plane and terminating at and having orifices lying in a common plane spaced from but parallel to the plane of said exhaust ports for directing gaseous streams issuing from said orifices at a predetermined uniform velocity onto a material presented in opposition to said orifices, the space within said casing between said planes being obstructed solely by said tubes and forming an expansion chamber, having a depth equivalent to the distance between said planes and a transverse cross-sectional area which is uniform throughout its depth, into which the gases in said streams pass after they impinge on said material and through which they rise with velocities substantially reduced from said orifice velocity before they reach the suction velocity contour lines of said exhaust ports.
2. Apparatus as claimed in claim 1 wherein said casing has an inlet and an opposed aligned outlet adapted to permit a material to be treated to be passed into, through and out of said casing along a plane path parallel to the plane of said orifices and wherein said tubes extend from the plane of said partition towards said path at least 25% of the distance between said partition and said path, whereby the depth of said chamber is at least 5% of said distance.
3. Apparatus as claimed in claim 1 wherein said tubes extend generally perpendicularly through the apertures in said wall and are spaced from the walls of said apertures to define with the walls of the apertures the exhaust ports in said wall.
References Cited in the file of this patent UNITED STATES PATENTS 2,042,610 Littleton June 2, 1936 2,701,452 Hopkins Feb, 8, 1955 2,807,892 Gerrish Oct. 1, 1957 2,878,583 Spooner Mar. 24, 1959 2,919,495 Underhay et a1 Jan. 5, 1960 UNITED STATES PATENT OFFICE CERTIFICATE OF CORRECTION Patent No 3,060,595 October 30, 1962 William P Dapses It is hereby certified that error appears in the above numbered patent requiring correction and that the said Letters Patent should read as corrected below.
Column 2 lines 46, 57, and 60, for "5/6", each occurrence, read 5/8 Signed and sealed this 30th day of April 1963.
(SEAL) Attestz' DAVID L. LADD Commissioner of Patents ERNEST W. SWIDER Attesting Officer
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
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US819763A US3060595A (en) | 1959-06-11 | 1959-06-11 | Jet dryer |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
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US819763A US3060595A (en) | 1959-06-11 | 1959-06-11 | Jet dryer |
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US3060595A true US3060595A (en) | 1962-10-30 |
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US819763A Expired - Lifetime US3060595A (en) | 1959-06-11 | 1959-06-11 | Jet dryer |
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Cited By (13)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3199224A (en) * | 1962-04-03 | 1965-08-10 | Wolverine Equipment Co | Apparatus for treating continuous length webs comprising high velocity gas jets |
US3359648A (en) * | 1965-04-05 | 1967-12-26 | Overly S Inc | Dryer with vacuum bar sheet feeder |
US3386714A (en) * | 1966-06-22 | 1968-06-04 | Ralph B. Rose Sr. | Dryer for printed sheets |
US3398467A (en) * | 1967-06-14 | 1968-08-27 | Wolverine Corp | Parallel tube gaseous jet apparatus with multisize tube bores |
US3518815A (en) * | 1968-05-24 | 1970-07-07 | Environmental Research Corp | Aerosol sampler |
JPS5131167U (en) * | 1974-08-29 | 1976-03-06 | ||
US4012209A (en) * | 1976-04-05 | 1977-03-15 | The United States Of America As Represented By The United States Energy Research And Development Administration | Liquid film target impingement scrubber |
FR2568358A1 (en) * | 1984-07-30 | 1986-01-31 | Oreal | Method for treating, in particular for drying, objects or materials, device for implementation of this method, in particular drying hood for hair |
US4868999A (en) * | 1987-03-20 | 1989-09-26 | C.D. High Technology | Apparatus and method for production of asphalt pavement having high recycled asphalt content |
WO2007065654A1 (en) * | 2005-12-06 | 2007-06-14 | Goller Textilmaschinen Gmbh | Drying and/or fixing device |
US8061055B2 (en) * | 2007-05-07 | 2011-11-22 | Megtec Systems, Inc. | Step air foil web stabilizer |
WO2013045026A1 (en) * | 2011-09-29 | 2013-04-04 | Karlsruher Institut für Technologie | Device for transferring heat or mass, comprising hexagonal jet nozzles, and method for treating surface layers |
PL442797A1 (en) * | 2022-11-14 | 2024-05-20 | Dworek Polski Spółka Jawna Koziński Jacek, Rybak Grzegorz | Effusion dryer |
Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2042610A (en) * | 1933-06-17 | 1936-06-02 | Corning Glass Works | Method and apparatus for tempering glass |
US2701452A (en) * | 1950-07-28 | 1955-02-08 | Flakice Corp | Tube ice-making apparatus |
US2807892A (en) * | 1954-03-16 | 1957-10-01 | Wolverine Equipment Co | Dryers |
US2878583A (en) * | 1954-12-17 | 1959-03-24 | Spooner Dryer & Eng Co Ltd | Drums for the temperature treatment of materials |
US2919495A (en) * | 1954-04-15 | 1960-01-05 | Bowater Res & Dev Co Ltd | Process of papermaking |
-
1959
- 1959-06-11 US US819763A patent/US3060595A/en not_active Expired - Lifetime
Patent Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2042610A (en) * | 1933-06-17 | 1936-06-02 | Corning Glass Works | Method and apparatus for tempering glass |
US2701452A (en) * | 1950-07-28 | 1955-02-08 | Flakice Corp | Tube ice-making apparatus |
US2807892A (en) * | 1954-03-16 | 1957-10-01 | Wolverine Equipment Co | Dryers |
US2919495A (en) * | 1954-04-15 | 1960-01-05 | Bowater Res & Dev Co Ltd | Process of papermaking |
US2878583A (en) * | 1954-12-17 | 1959-03-24 | Spooner Dryer & Eng Co Ltd | Drums for the temperature treatment of materials |
Cited By (13)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3199224A (en) * | 1962-04-03 | 1965-08-10 | Wolverine Equipment Co | Apparatus for treating continuous length webs comprising high velocity gas jets |
US3359648A (en) * | 1965-04-05 | 1967-12-26 | Overly S Inc | Dryer with vacuum bar sheet feeder |
US3386714A (en) * | 1966-06-22 | 1968-06-04 | Ralph B. Rose Sr. | Dryer for printed sheets |
US3398467A (en) * | 1967-06-14 | 1968-08-27 | Wolverine Corp | Parallel tube gaseous jet apparatus with multisize tube bores |
US3518815A (en) * | 1968-05-24 | 1970-07-07 | Environmental Research Corp | Aerosol sampler |
JPS5131167U (en) * | 1974-08-29 | 1976-03-06 | ||
US4012209A (en) * | 1976-04-05 | 1977-03-15 | The United States Of America As Represented By The United States Energy Research And Development Administration | Liquid film target impingement scrubber |
FR2568358A1 (en) * | 1984-07-30 | 1986-01-31 | Oreal | Method for treating, in particular for drying, objects or materials, device for implementation of this method, in particular drying hood for hair |
US4868999A (en) * | 1987-03-20 | 1989-09-26 | C.D. High Technology | Apparatus and method for production of asphalt pavement having high recycled asphalt content |
WO2007065654A1 (en) * | 2005-12-06 | 2007-06-14 | Goller Textilmaschinen Gmbh | Drying and/or fixing device |
US8061055B2 (en) * | 2007-05-07 | 2011-11-22 | Megtec Systems, Inc. | Step air foil web stabilizer |
WO2013045026A1 (en) * | 2011-09-29 | 2013-04-04 | Karlsruher Institut für Technologie | Device for transferring heat or mass, comprising hexagonal jet nozzles, and method for treating surface layers |
PL442797A1 (en) * | 2022-11-14 | 2024-05-20 | Dworek Polski Spółka Jawna Koziński Jacek, Rybak Grzegorz | Effusion dryer |
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Owner name: FIRST NATIONAL BANK OF BOSTON, THE, 100 FEDERAL ST Free format text: SECURITY INTEREST;ASSIGNOR:WOLVERINE CORPORATION, A MA CORP.;REEL/FRAME:004171/0618 Effective date: 19830824 |
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AS | Assignment |
Owner name: WOLVERINE CORPORATION, MASSACHUSETTS Free format text: ASSIGNMENT OF ASSIGNORS INTEREST.;ASSIGNOR:FIRST NATIONAL BANK OF BOSTON, THE;REEL/FRAME:005941/0741 Effective date: 19910906 |