US2342556A - Method of making endless members for use in drafting units - Google Patents

Method of making endless members for use in drafting units Download PDF

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US2342556A
US2342556A US399756A US39975641A US2342556A US 2342556 A US2342556 A US 2342556A US 399756 A US399756 A US 399756A US 39975641 A US39975641 A US 39975641A US 2342556 A US2342556 A US 2342556A
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apron
drafting
draft
sheet
mandrel
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US399756A
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Rockoff Joseph
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Dayton Rubber Manufacturing Co
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Dayton Rubber Manufacturing Co
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    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C35/00Heating, cooling or curing, e.g. crosslinking or vulcanising; Apparatus therefor
    • B29C35/02Heating or curing, e.g. crosslinking or vulcanizing during moulding, e.g. in a mould
    • B29C35/0227Heating or curing, e.g. crosslinking or vulcanizing during moulding, e.g. in a mould using pressure vessels, e.g. autoclaves, vulcanising pans
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C43/00Compression moulding, i.e. applying external pressure to flow the moulding material; Apparatus therefor
    • B29C43/02Compression moulding, i.e. applying external pressure to flow the moulding material; Apparatus therefor of articles of definite length, i.e. discrete articles
    • B29C43/021Compression moulding, i.e. applying external pressure to flow the moulding material; Apparatus therefor of articles of definite length, i.e. discrete articles characterised by the shape of the surface
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C43/00Compression moulding, i.e. applying external pressure to flow the moulding material; Apparatus therefor
    • B29C43/32Component parts, details or accessories; Auxiliary operations
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C67/00Shaping techniques not covered by groups B29C39/00 - B29C65/00, B29C70/00 or B29C73/00
    • B29C67/0037Forming articles from a moulding composition enclosed in a deformable bag
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C69/00Combinations of shaping techniques not provided for in a single one of main groups B29C39/00 - B29C67/00, e.g. associations of moulding and joining techniques; Apparatus therefore
    • B29C69/001Combinations of shaping techniques not provided for in a single one of main groups B29C39/00 - B29C67/00, e.g. associations of moulding and joining techniques; Apparatus therefore a shaping technique combined with cutting, e.g. in parts or slices combined with rearranging and joining the cut parts
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C70/00Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
    • B29C70/04Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
    • B29C70/06Fibrous reinforcements only
    • B29C70/10Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres
    • B29C70/12Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres using fibres of short length, e.g. in the form of a mat
    • B29C70/14Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres using fibres of short length, e.g. in the form of a mat oriented
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29DPRODUCING PARTICULAR ARTICLES FROM PLASTICS OR FROM SUBSTANCES IN A PLASTIC STATE
    • B29D7/00Producing flat articles, e.g. films or sheets
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C2793/00Shaping techniques involving a cutting or machining operation
    • B29C2793/009Shaping techniques involving a cutting or machining operation after shaping
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C43/00Compression moulding, i.e. applying external pressure to flow the moulding material; Apparatus therefor
    • B29C43/22Compression moulding, i.e. applying external pressure to flow the moulding material; Apparatus therefor of articles of indefinite length
    • B29C43/24Calendering
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C48/00Extrusion moulding, i.e. expressing the moulding material through a die or nozzle which imparts the desired form; Apparatus therefor
    • B29C48/001Combinations of extrusion moulding with other shaping operations
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C48/00Extrusion moulding, i.e. expressing the moulding material through a die or nozzle which imparts the desired form; Apparatus therefor
    • B29C48/001Combinations of extrusion moulding with other shaping operations
    • B29C48/0019Combinations of extrusion moulding with other shaping operations combined with shaping by flattening, folding or bending
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C48/00Extrusion moulding, i.e. expressing the moulding material through a die or nozzle which imparts the desired form; Apparatus therefor
    • B29C48/001Combinations of extrusion moulding with other shaping operations
    • B29C48/0022Combinations of extrusion moulding with other shaping operations combined with cutting
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C48/00Extrusion moulding, i.e. expressing the moulding material through a die or nozzle which imparts the desired form; Apparatus therefor
    • B29C48/03Extrusion moulding, i.e. expressing the moulding material through a die or nozzle which imparts the desired form; Apparatus therefor characterised by the shape of the extruded material at extrusion
    • B29C48/07Flat, e.g. panels
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C48/00Extrusion moulding, i.e. expressing the moulding material through a die or nozzle which imparts the desired form; Apparatus therefor
    • B29C48/03Extrusion moulding, i.e. expressing the moulding material through a die or nozzle which imparts the desired form; Apparatus therefor characterised by the shape of the extruded material at extrusion
    • B29C48/07Flat, e.g. panels
    • B29C48/08Flat, e.g. panels flexible, e.g. films
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C53/00Shaping by bending, folding, twisting, straightening or flattening; Apparatus therefor
    • B29C53/56Winding and joining, e.g. winding spirally
    • B29C53/562Winding and joining, e.g. winding spirally spirally
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29KINDEXING SCHEME ASSOCIATED WITH SUBCLASSES B29B, B29C OR B29D, RELATING TO MOULDING MATERIALS OR TO MATERIALS FOR MOULDS, REINFORCEMENTS, FILLERS OR PREFORMED PARTS, e.g. INSERTS
    • B29K2021/00Use of unspecified rubbers as moulding material
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29LINDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULAR ARTICLES
    • B29L2007/00Flat articles, e.g. films or sheets
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10STECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10S264/00Plastic and nonmetallic article shaping or treating: processes
    • Y10S264/68Roll

Description

Feb. 22, 1944. l J, ROCKOFF 2,342,556
METHOD OF MAKING ENDLESS MEMBERS` FOB USE IN DRAFTING UNITS Original Filed Aug. 2, 1940 EEE Cw" T0 MGM TETE /V V EN TOR MJU ATfoRym/s Patented Feb. Z22, 1944 METHOD F MAKING ENDLESS MEMBERS FOR USE IN DRAFTING UNITS Joseph Rockoff, Dayton, Ohio, assignor to The Dayton Rubber Manufacturing Company, Dayton, Ohio, a corporation of Ohio Original application August 2,
1940, Serial No.
349,517. Divided and this application June 25, 1941, Serial No. 399,756
(Cl. IE- 59) 1 Claim.
This invention relates to textile drafting machinery, and more particularly to a method of making draft aprons.
In textile spinning machines comprising fiber drafting mechanism an endless belt or band member is used as a conveyor to carry the fibers along during the drafting stage. Where a threeroll long drafting system is employed a draft or transport apron is utilized to carry the fiber from the middle line drafting rolls to the front line drafting set of rolls. The maximum amount of drafting is done between these two sets of rolls and it is therefore necessary to transport the fibers across' the intervening gap between the rolls. The drafting aprons are required to operate under uniform tension and must run straight and true, tracking accurately without any tendency to run to one side or form uneven sides or crooked stretches.
Heretofore, draft aprons have been made of leather and similar material but it has been diilicult to provide an apron having uniform gauge thickness throughout its length so that difficulty has been encountered in maintaining a true running fiber transport apron. When the drafting apron, during operation of the fiberdrafting unit, does not run straight and true forming an angle to one side, the traversevv of the apron pulls the cotton or ber being drafted off to one side causing ineffective drafting and resulting in breakdowns. The fiber pulled through the narrow opening between the rolls is subjected to higher resistance and causes an extra pulling down or drafting of the fiber which results in overdrafting and frequent breakage of the fiber necessitating discarding of the draft aprons. n
It is an object of this invention -,to produce draft aprons which are substantially of uniform gauge thickness and can be duplicated throughout a large number of aprons and to provide a fiber transport apron which will operate under uniform tension, run straight and true, and possess a long life in service.
Another object of this invention is to provide a long draft apron made by a method of vulcanization of synthetic rubber composition or synthetic resin composition combined with fibers and which is substantially inextensible and which will have the proper degree of friction for accurately controlling the fibers during the drafting operation so as to produce a yarn winchv is even and regular in unit lengths.
Another object of this invention is to provide a.' method of making an improved draft fapron which is made of a combined synthetic rubber and fiber composition or a synthetic resin and fiber composition and is of substantially uniform gauge thickness throughout, possessing the proper coefficient of friction at its surface which will carry the fibers along through the drafting unit in a uniformly straight line, and which apron will operate in unison with the rest of the machine so that slippage resulting in off balance operation is not encountered.
Another object is to provide a method of making a draft apron compo-sed of vulcanized synthetic resin or vulcanized synthetic rubber combined with fibers to form a long staple inextensible material extending lengthwise of the circumference or periphery of the apron to produce a longitudinally ineXtensible apron having a working surface of sufcient coeflicient of friction to prevent slippage during operation.
Another object is to provide a method of making draft aprons comprising a vulcanized synthetic rubber composition or vulcanized resin composition including fibers wherein the desired thickness of the apron is built up by wrapping a thin sheet of substantially ineXtensible composition material on a mandrel or arbor until the desired thickness of the apron isy secured and thereafter curing the material to provide a belt or apron having the proper surface texture to provide a fairly high coefficient of friction.
Another object is to devise amethod of making draft aprons or belt-like conveyors which are substantially static free. oil proof, abrasive resistant, and will not be subject to cold flow in service, or become deformed or tacky when subjected to the temperature and atmospheric conditions maintained during the drafting operation.
Another object is the method of poducing an improved draft apron made of synthetic rubber compositions or synthetic resin compositions,`
containing fibrous material, shaped and treated to produce a substantially longitudinally inextensible apron which has favorable ageing properties and remains odorless when subjected to the temperature and atmospheric conditions during operation of the spinning machine. j
These and other objects and advantages will become apparent from the accompanying description taken in connection with the drawing.
This is a divisional of my co-pending application Serial No. 349,517, filed August 2, 1940.
For the purpose of illustrating my invention. the draft apron and method of making is shown as embodied in a three-roll drafting system.
This system is commonly referred to as the Saco-Lowell draft system. My invention, however, is not limited to this particular type of drafting system and is adapted for use in twoapron drafting systems, such as commonly employed in Whitin type drafting machines or other types of fiber drafting units where draft aprons are employed.
In the drawing, there is diagrammatically il- A lustrated the different steps performed in making the improved draft aprons of my invention. As a typical example, a longl draft apron is shown as used in a three-roll drafting system.
Figure 1 illustrates diagrammatically the initial step of calendering a synthetic rubber and fiber composition so as to produce a plastic unvulcanizecl sheet of the desired thickness and wherein the fibers are arranged parallel to each other throughout the length of the sheet.
Figure 2 is a perspective view illustrating the second step of Winding the above mentioned plastic unvulcanized calendered sheet of Figure 1 on a mandrel so that the fibers in the sheet are parallel to the circumference of the mandrel to provide an apron body of the desired gauge thickness.
Figure 3 diagrammatically illustrates the third step comprising wrapping the cloth or fabric jacket liner around the built-up apron body wound on the mandrel preparatory to vulcanizing the laminated sheet layers wound on the mandrel.
Figure 4 illustrates a vulcanizing chamber in elevation and partly in section in which the Wrapped draft apron material wound on the mandrel is placed for heat curing to an integral resilient body.
Figure 5 shows in perspective the step of removing the wrapper to leave an imprint or bead on the outer surface of the vulcanized apron body.
Figures 6 and 7 illustrate diagrammatically and in perspective the steps of removing the overlap portion to provide a vulcanized apron body having a uniform outer diameter and souffing off the surface by grinding or in any other manner, for example, by pickling, for producing a uniformly level rough surface having the desired coefficient of friction.
Figure 8 illustrates the step of cutting aprons of the desired width from the built-up vulcanized and ground body.
Figure 9 is an enlarged fragmentary detail view of a portion of the finished apron illustrating the relative position of the fibers of the apron material with respect to the longitudinal axis of the apron.
Figure 10 is an enlarged fragmentary sectional view showing the surface and interior structure of the finished apron product.
Figure 1l is adiagrammatic view in elevation illustrating the use of the apron in a three-rollV drafting machine assembly.
Referring to the drawing in detail, particularly Figures 1 to 9, there is illustrated the different steps to be performed in making the draft aprons of this invention. These steps comprise the following:
STEP I A stock mass I5 having fibers I6 intermixed therewith is passed through calendering rolls I8 so as to form a plastic unvulcanized sheet I9 of substantially uniform thickness wherein the fibersV I6 are arranged parallel and extend longitudinally of the sheet. This parallel arrangement of the fibers I6 in the sheet is an essential step in the method of making the improved draft apron of this invention, as in this way, a substantially inextensible composition apron is formed. The gauge thickness of the sheet i9 may be varied somewhat but as a typical example I form a sheet of from .013 to .015 thickness. The width of the sheet is a matter of choice and equipment available but for convenience in handling, the sheet may be approximately 28".
During calendering of the mass I5, the disarranged fibers I6 are swung around by the flowing current action created by the calendering rolls as the composition mass is drawn therebetween, so that the longitudinal axes of the fibers are arranged substantially parallel and at right angles to the axes of rotation of the calender rolls. This produces a sheet wherein the fibers extend parallel to the length of the composition sheet and are uniformly distributed.
The mass l5 may comprise any suitable material which, when formed into a belt has the following characteristics: considerable iiexibility and a high coefficient of friction; favorable ageing properties such as maintenance of its thickness; resistant to cracking, therefore, having a long life; substantially free from static; resistant to oil and to abrasives; will now cold flow or stretch in service or become deformed or tacky when subjected to the temperature at high humidity conditions present during the drafting operation lperiod. A number of materials will satisfy these requirements and good results are obtainable by using synthetic rubber and synthetic resin compositions containing vegetable fibers such as cotton or synthetic fibers such as rayon, nylon, etc. The presence of these fibers in the rubber material greatly enhances the tensile strength of the apron or belt formed and renders the completed apron substantially inextensible while the yieldability of the apron is not appreciably affected. The textile fibers materially reinforce the body `of the apron and Iprovide a long-wearing straightrunning draft apron. The following are examples of the synthetic rubber and synthetic resin type of composition which may be used for the apron material, but it will be understood that the invention is not limited to these compositions or mixtures:
Composition #1 (using Neoprene) Parts by Weight Neoprene type G Zinc oxide 10 Light magnesium oxide 10 Cumar 2 Whiting 20 Cotton seed oil 5k Cotton fiber 30 Vulcanizing: 30 minutes at 300 F. steam cure. Composition #2 (using Perbunan) Vulcanizing: 30 minutes at 300 F. steam cure.
Composition #3 (using Thiolcol)l Vulcanizing: 30 minutes at 300 F. steam cure.
Composition #4 (using flexible Glyptal) f Parts by Weight Soft Glyptal resin (General Electric 1353 U Resin) 89 Neoprene binder1 l0 A Flexible Bakelite resin l Cotton fiber 30 Vulcanizing: 120 minutes at 300 F. dry heat.
1The neoprene binder mentioned in the immediately :more formula is preferably composed of ythe following materials Parts by Weight Neoprene type E 60.3
itharge 10.07 Sulfur STEP II After forming the thin plastic unvulcanized sheet I9 a mandrel or arbor 2l is selected having the desired inner diameter of the drafting apron to be formed and the sheet I9 is wound spirally around the mandrel 2l, as shown in Figure 2, until an apron body of the desired thickness is built up. The sheet is Wound on the mandrel so that the fibers i6 are parallel to the circumference of the mandrel whereupon the finished product will be substantially inextensible. In order to prevent wrinkles during the winding of the sheet onto the mandrel, the sheet stock is placed on a folded liner or similar material 22 and the mandrel rolled on this when the stock is wound around the mandrel.
One side of the sheet stock is thoroughly swabbed with solvent, such as benzol or the like cleaning substance. In order to start the sheet stock around the mandrel 2! the end of the sheet is skived, as shown at 24 in Figure 2, and is swabbed lightly with solvent and stuck to the mandrel by rolling the mandrel back on the skived end portion. The other side of the Skived end is thoroughly swabbed with solvent and allowed to dry. After the desired thickness of the composition body is rolled up on the mandrel, the last turn, or layer, of the sheet stock is stitched or suitably secured down at the end and about 1/8 beyond the seam the excess sheet stock is trimmed off.
STEP III The tightly wound plastic unvulcanized sheet stock on the mandrel of Step II is provided with a wrapper or jacket 25 of relatively coarse fabric or similar woven material so as to leave 'an imprint on the outer surface of the wound stock. The wrapper is started around the laminated layers on the mandrel with a light tension and after two or three rounds the maximum tension is applied to the wrapper for the remainder of the operation. Preferably two layers of butted frictional bead tape are @und around the matcrial to be vulcanized. The second layer is positioned so as to cover the butted portions of the first layer. l
STEP IV l After the built-up apron body has been wrapped, the mandrel and overlaid composition material are placed in a steam vulcanizer and vulcanized under heat to a unitary belt or Aapron structure. Preferably the curing or vulcanizing step comprises subjecting thevmaterial to a temperature of approximately 300 degrees F. for from l5 to 40 minutes, depending on the kind of composition. When using a flexible glyptal composition as in the case of Composition #4 given above, the vulcanizing time is extended to approximately minutes. Steam or dry heat may be utilized for effecting the vulcanization.
STEP V After vulcanization, the composition material Wrapper is removed leaving the imprint of the fabric or texture of the wrapper on the outer surface of the molded apron body, as illustrated in Figure 5.
STEP VI In order to provide a smooth uniform outside diameter apron body, the overlap portion 21, formed where the end layerportion is united to the under iayer of vulcanized material, is placed on a lathe or suitable mechanism and the overlap abraded oif by applying an abrading means 29, as illustrated in Figure 6. For abrading the overlap there may be used sandpaper or metal cloth wrapped around a small block and the overlap at the seam ground off to produce a curvature at the point of the seam which is the same as the rest of the outside cover portion of the apron body.
STEP VII In this step, the outer surface of the apron body is scuffed off to remove any burr-like projections and to produce an apron having a uniform outside diameter that is slightly rough, as illustrated at 30 in Figure l0. The texture of the outer surface comes from the imprint of the jacket wrapper Wound around the material before vulcanization and which imprint is modied by grinding in Step VI, as illustrated at 34 in Figure 9, to provide a draft apron having the proper coefcient of friction at its surface so as to avoid any slippage of the draft apron during use.
STEP VIII After the surface has been properly ground, the apron is cut at the desired width by mounting the mandrel on a lathe and applying the cutting knife or knives 32. Preferably, the vulcanized apron material is removed from the mandrel by directing a light blast of air underneath the cover at one end and progressively stripping the vulcanized sleeve-like body off from the mandrel, The material is then slipped over a wooden core, placed on a lathe, and cut to the desired width of draft apron, as illustrated in Figure 8. During the manufacture of the draft aprons the material is carefully gauged so as to produce a belt or apron having uniform thickness throughout and of the desired inside diameter or circumference.
In Figure ll the use of the finished draft apron 35 is illustrated in a three-roll drafting unit. In this type of unit only one apron is used which is fairly thin in thickness and is guided and held in place by an idler roller 36. This idler roller maintains the tension uniform and guides the apron through the operating cycle. A driven roll 38 runs the draft apron and a Weighted covered idler roll `411 cooperates with the driven roll 38 over which the draft apron is moved. The apron passes forward over the nose or pinch bar member 42 and continues around the idler tension roller 36. A slip or pencil roll 44 engages the apron as it passes over the pinch bar 42 during the drafting operation. The purpose of this pencil roll is to keep the fibers down onto the apron and to deliver them in a uniform layer to the nal drafting roll which is not shown but which is positioned immediately to the left of the pencil roll 44. The driven roll 38 may be suitably knurled or fluted in order to Contact the inside surface of the apron and drive the same.
The making of the draft aprons by the process described provides an improved method whereby each succeeding apron can be made of the same gauge thickness, length and Width throughout a large number of aprons. This is an important improvement in the making of draft aprons since any substantial variation in gauges in the different aprons results in inefficient and troublesome operations during the drafting process.
The surface texture of the aprons may be provided with a suicient coefficient of friction by grinding, pickling or any other means to drive the top roll 40 and also to prevent slippage of the pencil roll 44 when the aprons are used in a three-roll drafting unit.
When using the aprons of this invention in Whitin frames, the cloth markings provide proper coefficient of friction on the surface of the aprons to effect proper driving of the drafting apron and associated upper apron without slippage.
l It will be understood that this invention is not limited to the specific method steps and structure of the apron as described by me but modified to suit different conditions and uses as required.
Having thus fully described my invention, what I claim as new and desire to secure by Letters Patent, is:
An improved method of making an endless mem-ber for use in drafting units comprising the steps of (a) calenderingal synthetic rubber mass having fibers interspersed therein to form a sheet of said rubber mass and arrange the fibers therein longitudinally of the sheet, (b) Winding said sheet on a mandrel with the bers in the rubber material extending parallel to the circumference of said mandrel to provide a built-up apron body of the desired thickness, (c) Wrapping the outer surface of said wound sheet with a wrapper of coarse textile material, (d) vulcanizing said wrapped material, (e) removing the wrapper from the vulcanized material to leave an imprint of the wrapper on the surface, (f) grinding the surface to provide an apron body having a uniform outer diameter with a slightly rough surface, (g) removing said ground material from the mandrel and placing it on a core and cutting the apron material to the desired Width to provide a finished apron product.
JOSEPH ROCKOFF.
US399756A 1940-08-02 1941-06-25 Method of making endless members for use in drafting units Expired - Lifetime US2342556A (en)

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US399756A US2342556A (en) 1940-08-02 1941-06-25 Method of making endless members for use in drafting units

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Cited By (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2451046A (en) * 1944-09-20 1948-10-12 Johns Manville Method of coupling pipe
US3642559A (en) * 1970-02-20 1972-02-15 William S Stokes Membrane-lined structural panel
US3663350A (en) * 1970-01-12 1972-05-16 William S Stokes Membrane system
US4439391A (en) * 1979-06-26 1984-03-27 International Paper Company Polymeric sheets
EP0136867A2 (en) * 1983-09-30 1985-04-10 AlliedSignal Inc. Rollers with oriented fibre reinforcement and method of making them
US4551297A (en) * 1983-09-14 1985-11-05 J. H. Benecke Gmbh Method of making an embossing cylinder
US4552713A (en) * 1983-02-04 1985-11-12 Jamak, Inc. Method of forming an improved handgrip having non-slip features
US4581189A (en) * 1981-09-14 1986-04-08 Minnesota Mining And Manufacturing Company Method of making a belt for belt-driven recording tape pack
US4634484A (en) * 1984-02-20 1987-01-06 J.H. Benecke Gmbh Method for the production of an embossing roller for the continuous embossing of the surface of a thermoplastic film
WO1991015356A1 (en) * 1990-04-06 1991-10-17 Applications Mecaniques Et Robinetterie Industrielle (A.M.R.I.) Process for improving mechanical and sealilng properties and of elastomeric sealing packings, and packings obtained by said process
US5131891A (en) * 1991-02-04 1992-07-21 Gigatek Memory Systems Limited Partnership Highly durable tape cartridge drive belt
US5304267A (en) * 1991-05-14 1994-04-19 Heidelberg Harris Gmbh Method of making a gapless tubular printing blanket
US5489631A (en) * 1990-04-06 1996-02-06 Ksb S.A. Process for improving the mechanical and sealing properties of elastomer gaskets, joints and seals and the seal obtained with this process
US5686158A (en) * 1991-11-21 1997-11-11 Jmk International, Inc. Low specific gravity silicone rubber golf club grip
US5989481A (en) * 1996-06-18 1999-11-23 You; Daniel H. Golf club shaft manufacturing process

Cited By (17)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2451046A (en) * 1944-09-20 1948-10-12 Johns Manville Method of coupling pipe
US3663350A (en) * 1970-01-12 1972-05-16 William S Stokes Membrane system
US3642559A (en) * 1970-02-20 1972-02-15 William S Stokes Membrane-lined structural panel
US4439391A (en) * 1979-06-26 1984-03-27 International Paper Company Polymeric sheets
US4581189A (en) * 1981-09-14 1986-04-08 Minnesota Mining And Manufacturing Company Method of making a belt for belt-driven recording tape pack
US4552713A (en) * 1983-02-04 1985-11-12 Jamak, Inc. Method of forming an improved handgrip having non-slip features
US4551297A (en) * 1983-09-14 1985-11-05 J. H. Benecke Gmbh Method of making an embossing cylinder
US4766996A (en) * 1983-09-30 1988-08-30 Garrett Aerospace Rollers with oriented fiber reinforcement and method
EP0136867A2 (en) * 1983-09-30 1985-04-10 AlliedSignal Inc. Rollers with oriented fibre reinforcement and method of making them
EP0136867A3 (en) * 1983-09-30 1987-06-03 The Garrett Corporation Rollers with oriented fibre reinforcement and method of making them
US4634484A (en) * 1984-02-20 1987-01-06 J.H. Benecke Gmbh Method for the production of an embossing roller for the continuous embossing of the surface of a thermoplastic film
WO1991015356A1 (en) * 1990-04-06 1991-10-17 Applications Mecaniques Et Robinetterie Industrielle (A.M.R.I.) Process for improving mechanical and sealilng properties and of elastomeric sealing packings, and packings obtained by said process
US5489631A (en) * 1990-04-06 1996-02-06 Ksb S.A. Process for improving the mechanical and sealing properties of elastomer gaskets, joints and seals and the seal obtained with this process
US5131891A (en) * 1991-02-04 1992-07-21 Gigatek Memory Systems Limited Partnership Highly durable tape cartridge drive belt
US5304267A (en) * 1991-05-14 1994-04-19 Heidelberg Harris Gmbh Method of making a gapless tubular printing blanket
US5686158A (en) * 1991-11-21 1997-11-11 Jmk International, Inc. Low specific gravity silicone rubber golf club grip
US5989481A (en) * 1996-06-18 1999-11-23 You; Daniel H. Golf club shaft manufacturing process

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