US3602416A - Method of collimating fibers - Google Patents

Method of collimating fibers Download PDF

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US3602416A
US3602416A US794901*A US3602416DA US3602416A US 3602416 A US3602416 A US 3602416A US 3602416D A US3602416D A US 3602416DA US 3602416 A US3602416 A US 3602416A
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roller
filaments
filament
fibers
rollers
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US794901*A
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Malcolm Basche
Urban E Kuntz
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Raytheon Technologies Corp
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United Aircraft Corp
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    • DTEXTILES; PAPER
    • D04BRAIDING; LACE-MAKING; KNITTING; TRIMMINGS; NON-WOVEN FABRICS
    • D04HMAKING TEXTILE FABRICS, e.g. FROM FIBRES OR FILAMENTARY MATERIAL; FABRICS MADE BY SUCH PROCESSES OR APPARATUS, e.g. FELTS, NON-WOVEN FABRICS; COTTON-WOOL; WADDING ; NON-WOVEN FABRICS FROM STAPLE FIBRES, FILAMENTS OR YARNS, BONDED WITH AT LEAST ONE WEB-LIKE MATERIAL DURING THEIR CONSOLIDATION
    • D04H3/00Non-woven fabrics formed wholly or mainly of yarns or like filamentary material of substantial length
    • D04H3/02Non-woven fabrics formed wholly or mainly of yarns or like filamentary material of substantial length characterised by the method of forming fleeces or layers, e.g. reorientation of yarns or filaments
    • D04H3/04Non-woven fabrics formed wholly or mainly of yarns or like filamentary material of substantial length characterised by the method of forming fleeces or layers, e.g. reorientation of yarns or filaments in rectilinear paths, e.g. crossing at right angles

Abstract

A method for collimating a plurality of filaments into parallel, side-by-side contiguous relation including passing the filaments around first and second rollers, the rollers having their axes perpendicular to, but noncoplanar with, each other whereby all but one filament will be subjected to sidewise forces.

Description

United States Patent Malcolm Basche West Hartford;
Urban E. Kuntz. East Hartford, both 01, Conn.
Jim. 19, 106') Aug. 31. 1971 United Alt-craft Corporation East Hartlord, Conn.
Inventors Appl Nu, llled Patented Asslgnee METHOD OF COLLlMATlNG FIBERS l Chim,3Draw1ng Figs.
U.S.Cl 226/196, 19/65 T, 156/161, 156/181 Int. Cl ..B65h-23/26,
DOlh 13/02, B65h57/14 FieldofSearch 156/181,
Relerences Clted UNITED STATES PATENTS Schmidt Smith Smith Remr Tarbell Gallagher.... Balch et a1.
FOREIGN PATENTS Great Britain Primary Examiner-Carl D. Quarforth Assistant Examiner-Roger S. Gaither Attorney-John D. Del Ponti 226/196 X 19/65 '1 19/65 T l9/66T 19/65 T ABSTRACT: A method for collimating a plurality of filaments into parallel, side-by-side contiguous relation including passing the filaments around first and second rollers, the rollers having their axes perpendicular to, but noncoplanar with, each other whereby all but one filament will be subjected to sidewise forces.
PATENTED was] IBYi 3,602,416
SHEET 1 [IF 2 INVENTORS MALCOLM BASCHE URBAN E. KUNTZ ATTORNEY PATENTEU M1831 \sn 3.602.416
SHEEI 2 0r 2 F/GJ METHOD OF COLLIMATING FIBERS BACKGROUND OF THE INVENTION 5 This invention relates to the production of multiple fiber composite tape and more particularly relates to means for collimating a plurality of individual filaments into a parallel sideby-side relationship to facilitate the production of unidirectional fiber-reinforced composites.
It is known that fiber strengthening offers the potential of significant improvements in the fabrication of composite materials. The concept of fiber strengthening is based on the fact that materials produced in fibrous form frequently exhibit a higher elastic modulus and a higher strength than the corresponding materials in bulk. In order to exploit the attractive physical properties of continuous filamentary materials however, it is necessary to gather the fibers together into a composite structure in such a way that failure in several isolated fibers will not be transmitted to .the surrounding fibers and further, to distribute the load with reasonable uniformity over the entire fiber bundle. One method of achieving this result is to gather the fibers into a collimated relationship and infiltrate them with matrix material to form a monolayer tape.
One of the paramount problems in continuously producing unidirectionally reinforced composite tapes resides in the inherent difficulty of incorporating the fibers into the matrix material. There are basically two ways in which continuous filaments may be incorporated into the matrix in a parallel, uniformly spaced fashion. One way is to precision align the filaments in noncontacting relation prior to encasement and to control their spacing by tension means until the matrix material is applied. Because of the elaborate and intricate equipment necessary to maintain exact spacing, this procedure is unsatisfactory and is generally considered commercially unattractive. The other general method involves precoating each individual filament with matrix material so that the fibers can subsequently be aligned in side-by-side contacting relation with the filaments being spaced apart by the thickness of the coatings. Although this procedure has done away with the problem of spacing maintenance it has generated new problems, one of which is the assiduous requirement that the apparatus be capable of causing the individual, precoated filaments to continuously assume and maintain intimate side-byside contact in a monoplanar configuration. The prior art has shown apparatus for collimating filaments together into a ribbon, however, these prior techniques incorporate specialized components, often unreliable, as for example concave roller or toothed comb elements in order to achieve the aforesaid collimation.
Exemplary of the prior art teachings are those shown in Letters Patent U.S. Pat. No. 3,009,5[2 issued to Guay on Nov. 2|, I961 and US. Pat. No. 3,258,378 issued to Kelsey on June 28, I966. The Guay patent teaches the use of a concave highly polished roll across which a plurality of filaments are pulled under tension in order that the filaments will come together under the influence of a sidewise pressure. Unfortunately, the operation of the Guay device frequently resulted in the filaments riding one over the other. One of the disadvantages of the Guay device can be traced to the use therein of a collimating roller with a nonconstant diameter so that adjacent fibers, in passing thereover, are subjected to different circumferential speeds and hence imbalances in filament tension and sidewise pressure effects. The Kelsey patent, in an effort to resolve the problems of the Guay device, taught that a tiltable comb could be utilized. in conjunction with a tension inducing roller pair, to position the filaments adjacent to each other without the generation of any sideways pressure at all. The Kelsey teaching requires that the toothed comb be maintained at a precise inclination so that the cosine of the angle of tilt of the comb multiplied by the spacing of the threads be equal to the widths of the threads. To this end, a micrometric screw adjustment was provided.
The present invention. while utilizing some of the concepts underlying both the Guay and the Kelsey processes, produces monolayer tapes by a distinct and different process and by an improved and simplified apparatus without the necessityfor concave rollers, adjustable toothed combs or any other specializedequipment at all. I
SUMMARY OF THE INVENTION 2 I The present invention relates to a means for collimating a plurality of filaments into a parallel side-by-s'iderelationship preparatory to integration into monolayer tape product without necessitating the use of concave roller or toothed comb elements. The technique includes an improved process and' apparatus whereby adjacent filaments initiating from diverse sources are automatically made to assume a continuous contacting relation by the exertion of a sidewise pressure induced by the juxtaposed relation of a sequence of rollers.
According to one aspect of this invention, a plurality of continuous filaments each issuing from a separate feed source are sequentially passed around a pair of cylindrical rollers, the rollers being so located with respect to each other that the filaments issuing from the first roller are subjected to sidewise forces and are naturally made to assume an intimate state of contact whereby high quality is assured without the necessity for critical production control. One advantageous feature of the present apparatus is the fact that substantially all contact with the fibers during the orientation period is a rolling contact so that the likelihood of wear and damage to both the fiber and the equipment is minimized.
BRIEF DESCRIPTION OF THE DRAWINGS FIG. 1 is a schematic perspective view of typical apparatus used in the practice of the invention;
FIG. 2 is a plan view of a portion of the apparatus shown in FIG. I; and
FIG. 3 is a plan view of the rollers shown in FIG. 2 but with their axes in a nonperpendicular orientation.
DESCRIPTION OF THE PREFERRED EMBODIMENTS Referring now to the drawings, wherein like numbers indicate like elements, a series of supply rolls or spools 10 are provided as a convenient source of filaments 12. The filaments l2 assume a rolling contact with a pair of cylindrical rollers 14 and 16 and pass therearound as shown. The roller 14 acts as a spacing idler or guide roller while the roller I6 acts as a collimating roller when the rollers are critically disposed in a particular angular relationship, as hereinafter described, so that the filaments are induced to issue from the roller 16 as a monolayer of contiguous and coplanar collimated fibers. The fibers are subsequently transfixed into permanently collimated relation by means of a matrix overcoat applied by passage through a resin pot I8 and curing furnace 20. A detailed example of a practical coating apparatus is described in copending application Ser. No. 752,080 entitled Process for Coating Filaments with a Resin and Apparatus Therefor" filed Aug. 12, 1968 and sharing a common assignee with the instant invention. After coating and curing, the resulting unidirectional fiber reinforced tape is passed over a guide roller 22 and stored on a takeup reel 24.
The spools 10 are preferably arranged in banks with each bank of spools having the spools positioned with their axes parallel but at staggered elevations as shown in the drawings. However, it will be appreciated that so long as the spools 10 are sufficiently staggered to prevent filament interference, they may be arranged in any practical configuration. The number of supply spools utilized is a matter of choice with an upper quantity limit being determined by the axial length of the rollers 14 and 16.
As hereinbefore suggested, the angular relation of the idler l4 and the collimating roller 16 is precise and crucial. The two rollers must be disposed so that a sidewise pressure will be exerted on all but one of the filaments. In particular, the rollers must be disposed with their axes perpendicular to each other. Such a relationship assures that all of the filaments 12 will automatically be made to assume side-by-side contact on the collimating roller 16. It will be appreciated that one of the advantages of the instant invention is that if one of the filaments breaks during the operation, the remaining fibers will seek intimacy and close the gap created thereby, thus salvaging what would otherwise be unacceptable tape. That two common rollers could produce such dramatic results in terms of collimating efficiency was a discovery totally unexpected, particularly in view of the prior art techniques. The discovery is best explained with reference to FIG. 2 wherein is shown the two rollers positioned with their axes mutually perpendicular but not coplanar. Because of this roller relationship, only one of the filaments, designated by the numeral 12', can make an angle of 90 with the axis of the collimating roller 16. All of the other filaments 12" make angles which are either less than or greater than 90. As the filaments are pulled over the collimator l6 and cause it to rotate, a point P representing the point of initial contact between the roller and the filament 12" is caused to move. As the roller rotates, the point P on the roller moves to P while the corresponding point P on the filament moves to P". There is thus a relative axial slip P'-P" which, since there is friction between the filament and the roller, will cause a sidewise force to act on each filament 12" tending to displace them towards the base fiber 12'. As the filaments come together into a monolayer of parallel fibers, the sidewise forces will diminish but will nevertheless act to maintain the fibers in abutting contact since the filament diameter, while small, is still finite and all but the base filament will have an angle with the axis of roller by which it differs slightly from 90. As can be seen from the foregoing, one of the advantages inherent in the system resides in the fact that the automatic diminution of sliding contact between fiber and roller acts as a safeguard to keep the fibers from riding up over one another.
In contrast to the aforesaid concept and, as can be seen in FIG. 3, when the axes of rollers 14 and 16 are not mutually perpendicular, there exists a situation where more than one filament can be simultaneously perpendicular to the axis of the roller 16. As a result, the filaments will not seek intimacy with each other and will instead be spaced apart by an exact amount dependent upon the departure from mutual perpendicularity of the rollers 14 and 16. It is only when the rollers are disposed in the critical relation as heretofore described that all of the filaments will assume, in a monolayer, a continuously contacting collimated relation.
in one investigation with the apparatus as shown in FIG. 1, l0 fibers of 4 mil boron filament precoa'ted with a 0.2-0.4 mil coating of polyimide resin were passed through a rod-sealed mercury wipe resin pot at a speed of 400-800 ft./hour. The precoated boron filaments assumed a contiguous collimated relation with no spacing detectable therebetween so that after the application of the resin overcoat, the resulting tape displayed fibers that were evenly and uniformly spaced with no boron to boron contact. The tape was tested and had a tensile strength of 198,000 p.s.i. and a 36x10? p.s.i. modulus.
While for the sake of clarity and brevity, the foregoing description has been made with respect to specific examples, processes and parameters, these specific embodiments will be understood to be illustrative only, and no limitation is intended thereby. It should for example be understood that the instant method and apparatus for collimating fibers is applica ble to all kinds of filaments whether or not precoated. Various other modifications and alternatives will be evident to those skilled in the art within the true spirit and scope of the invention as set forth in the appended claims.
What is claimed is:
l. A method of collimating a plurality of continuous filaments into parallel side-by-side contiguous relationship which comprises,
providing first and second cylindrical rollers with the axis of one roller perpendicular to, but not coplanar, with the axis of the other roller, supplying a plurality of at least three individual and noncontiguous filaments to be guided around each roller under tension,
passing the tensioned filaments around the first roller in a generally parallel, side-by-side relationship such that no one tensioned filament overlays any other tensioned filament when passing around the first roller,
extending the tensioned filaments towards said second roller whereby only one of the filaments extending from said first roller to said second roller will be perpendicular to the axis of the second roller and the remaining extended filaments on either side of said one filament will be urged towards a relationship with the axis of the second roller,
and further passing the extended filaments around the second roller to form a monolayer of parallel filaments.

Claims (1)

1. A method of collimating a plurality of continuous filaments into parallel side-by-side contiguous relationship which comprises, providing first and second cylindrical rollers with the axis of one roller perpendicular to, but not coplanar, with the axis of the other roller, supplying a plurality of at least three individual and noncontiguous filaments to be guided around each roller under tension, passing the tensioned filaments around the first roller in a generally parallel, side-by-side relationship such that no one tensioned filament overlays any other tensioned filament when passing around the first roller, extending the tensioned filaments towards said second roller whereby only one of the filaments extending from said first roller to said second roller will be perpendicular to the axis of the second roller and the remaining extended filaments on either side of said one filament will be urged towards a 90* relationship with the axis of the second roller, and further passing the extended filaments around the second roller to form a monolayer of parallel filaments.
US794901*A 1969-01-29 1969-01-29 Method of collimating fibers Expired - Lifetime US3602416A (en)

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Cited By (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4699683A (en) * 1986-02-07 1987-10-13 The Boeing Company Multiroving fiber laminator
US4724024A (en) * 1984-05-23 1988-02-09 U.S. Philips Corporation Method of bonding optical fibers to form a flat cable
US4894105A (en) * 1986-11-07 1990-01-16 Basf Aktiengesellschaft Production of improved preimpregnated material comprising a particulate thermoplastic polymer suitable for use in the formation of substantially void-free fiber-reinforced composite article
US5128198A (en) * 1986-11-07 1992-07-07 Basf Aktiengesellschaft Production of improved preimpregnated material comprising a particulate thermoplastic polymer suitable for use in the formation of a substantially void-free fiber-reinforced composite article
WO1994005499A1 (en) * 1992-09-09 1994-03-17 Clock Spring Company L.P. High tensile strength composite reinforcing bands and methods for making same
CN1041015C (en) * 1993-08-24 1998-12-02 钟表弹簧公司 High tensile strength composite reinforcing bands and methods for making same
US20050066493A1 (en) * 2003-09-26 2005-03-31 Celanese Acetate, Llc Method and apparatus for making an absorbent composite
US20090079998A1 (en) * 2007-09-22 2009-03-26 The Boeing Company Method and apparatus for measuring the width of composite tape
US20090211698A1 (en) * 2008-02-27 2009-08-27 The Boeing Company Reduced complexity automatic fiber placement apparatus and method
US20100006205A1 (en) * 2008-07-08 2010-01-14 The Boeing Company Method and apparatus for producing composite structures
US20100193103A1 (en) * 2009-01-31 2010-08-05 The Boeing Company Automated fiber placement using networked autonomous vehicles
US20100224716A1 (en) * 2009-03-09 2010-09-09 The Boeing Company Simplified fiber tensioning for automated fiber placement machines
US20100230043A1 (en) * 2009-03-13 2010-09-16 The Boeing Company Method and Apparatus for Placing Short Courses of Composite Tape
US20110114265A1 (en) * 2008-01-02 2011-05-19 The Boeing Company Graphite Tape Supply and Backing Paper Take-Up Apparatus
US8464773B2 (en) 2007-07-27 2013-06-18 The Boeing Company Tape removal apparatus and process

Cited By (27)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4724024A (en) * 1984-05-23 1988-02-09 U.S. Philips Corporation Method of bonding optical fibers to form a flat cable
US4699683A (en) * 1986-02-07 1987-10-13 The Boeing Company Multiroving fiber laminator
US4894105A (en) * 1986-11-07 1990-01-16 Basf Aktiengesellschaft Production of improved preimpregnated material comprising a particulate thermoplastic polymer suitable for use in the formation of substantially void-free fiber-reinforced composite article
US5128198A (en) * 1986-11-07 1992-07-07 Basf Aktiengesellschaft Production of improved preimpregnated material comprising a particulate thermoplastic polymer suitable for use in the formation of a substantially void-free fiber-reinforced composite article
US5677046A (en) * 1992-09-09 1997-10-14 Clock Spring Company L.P. High tensile strength composite reinforcing bands
US5518568A (en) * 1992-09-09 1996-05-21 Fawley; Norman C. High tensile strength composite reinforcing bands and methods for making same
WO1994005499A1 (en) * 1992-09-09 1994-03-17 Clock Spring Company L.P. High tensile strength composite reinforcing bands and methods for making same
US5683530A (en) * 1992-09-09 1997-11-04 Clock Spring Company, L.P. Reinforcement methods utilizing high tensile strength composite bands
CN1041015C (en) * 1993-08-24 1998-12-02 钟表弹簧公司 High tensile strength composite reinforcing bands and methods for making same
US20050066493A1 (en) * 2003-09-26 2005-03-31 Celanese Acetate, Llc Method and apparatus for making an absorbent composite
US6983520B2 (en) * 2003-09-26 2006-01-10 Celanese Acetate, Llc Method and apparatus for making an absorbent composite
US8464773B2 (en) 2007-07-27 2013-06-18 The Boeing Company Tape removal apparatus and process
US20090079998A1 (en) * 2007-09-22 2009-03-26 The Boeing Company Method and apparatus for measuring the width of composite tape
US8345269B2 (en) 2007-09-22 2013-01-01 The Boeing Company Method and apparatus for measuring the width of composite tape
US8272419B2 (en) 2008-01-02 2012-09-25 The Boeing Company Graphite tape supply and backing paper take-up apparatus
US20110114265A1 (en) * 2008-01-02 2011-05-19 The Boeing Company Graphite Tape Supply and Backing Paper Take-Up Apparatus
US20090211698A1 (en) * 2008-02-27 2009-08-27 The Boeing Company Reduced complexity automatic fiber placement apparatus and method
US8557074B2 (en) 2008-02-27 2013-10-15 The Boeing Company Reduced complexity automatic fiber placement apparatus and method
US9884472B2 (en) 2008-02-27 2018-02-06 The Boeing Company Reduced complexity automatic fiber placement apparatus and method
US20100006205A1 (en) * 2008-07-08 2010-01-14 The Boeing Company Method and apparatus for producing composite structures
US8986482B2 (en) 2008-07-08 2015-03-24 The Boeing Company Method and apparatus for producing composite structures
US20100193103A1 (en) * 2009-01-31 2010-08-05 The Boeing Company Automated fiber placement using networked autonomous vehicles
US20100224716A1 (en) * 2009-03-09 2010-09-09 The Boeing Company Simplified fiber tensioning for automated fiber placement machines
US8308101B2 (en) 2009-03-09 2012-11-13 The Boeing Company Simplified fiber tensioning for automated fiber placement machines
US8490910B2 (en) 2009-03-09 2013-07-23 The Boeing Company Simplified fiber tensioning for automated fiber placement machines
US20100230043A1 (en) * 2009-03-13 2010-09-16 The Boeing Company Method and Apparatus for Placing Short Courses of Composite Tape
US8454788B2 (en) 2009-03-13 2013-06-04 The Boeing Company Method and apparatus for placing short courses of composite tape

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