U.S. patent number 3,844,822 [Application Number 05/211,339] was granted by the patent office on 1974-10-29 for production of uniformly resin impregnated carbon fiber ribbon.
This patent grant is currently assigned to Celanese Corporation. Invention is credited to A. Evan Boss, Michael J. Ram, Thomas K. Reynolds.
United States Patent |
3,844,822 |
Boss , et al. |
October 29, 1974 |
PRODUCTION OF UNIFORMLY RESIN IMPREGNATED CARBON FIBER RIBBON
Abstract
An improved process is provided for the production of a
continuous length of a carbon fiber ribbon which is impregnated
with a tacky B-stage thermosetting resin. The fibrous ribbon
undergoing treatment is resin impregnated with a neat liquid resin
system of relatively high viscosity containing an A-stage
thermosetting resin through the application of a force sufficient
to bring the resin into intimate association with the individual
fibers of the ribbon. The resin impregnated ribbon is next
partially cured while continuously passing through a heating zone
as described while interposed between a pair of flexible endless
belts. The resulting ribbon is uniformly impregnated with a
thermosetting resin of a tacky B-stage consistency and may be
utilized in the formation of carbon fiber reinforced composite
structures by filament winding or other suitable techniques.
Inventors: |
Boss; A. Evan (Mountainside,
NJ), Ram; Michael J. (West Orange, NJ), Reynolds; Thomas
K. (Santa Monica, CA) |
Assignee: |
Celanese Corporation (New York,
NY)
|
Family
ID: |
22786514 |
Appl.
No.: |
05/211,339 |
Filed: |
December 23, 1971 |
Current U.S.
Class: |
427/377; 118/70;
118/59; 427/386 |
Current CPC
Class: |
B29C
70/04 (20130101); D01F 11/14 (20130101); B29K
2307/00 (20130101) |
Current International
Class: |
D01F
11/14 (20060101); D01F 11/00 (20060101); B44d
001/48 () |
Field of
Search: |
;117/119.6,161ZB,228,65.2,DIG.11 ;118/59,106 ;34/116 |
References Cited
[Referenced By]
U.S. Patent Documents
Foreign Patent Documents
|
|
|
|
|
|
|
710,750 |
|
Jun 1965 |
|
CA |
|
525,037 |
|
May 1956 |
|
CA |
|
791,598 |
|
Mar 1958 |
|
GB |
|
Primary Examiner: Martin; William D.
Assistant Examiner: Beck; Shrive P.
Claims
1. An improved process for the production of a uniformly resin
impregnated ribbon of a carbonaceous fibrous material which is
suitable for use in the manufacture of carbon fiber reinforced
composite structures comprising:
a. continuously conveying to an impregnation zone a carbonaceous
fibrous ribbon containing at least about 90 percent carbon by
weight,
b. forcing a liquid solventless system having a viscosity of about
500 to 10,000 cps, comprising an A-stage thermosetting resin into
intimate association with said carbonaceous fibrous ribbon while
present in said impregnation zone,
c. interposing said ribbon while in intimate association with said
solventless system between the outer surfaces of a pair of flexible
endless belts having a non porous surface and a width greater than
that of said ribbon,
d. continuously passing said ribbon in the direction of its length
while interposed between said flexible endless belts through a
substantially enclosed heating zone provided with a heated gaseous
atmosphere while substantially suspended therein wherein said belts
and said ribbon are looped in a single wrap about each of a
multiplicity of rotating parallel rollers wherein the inner
surfaces of said belts are in alternating contact with said rollers
as said belts and said ribbon progress through said heating zone
with said ribbon being out of contact with said rollers and wherein
said thermosetting resin in intimate association with said ribbon
is converted to a B-stage consistency,
e. continuously withdrawing said ribbon from said heating zone
while interposed between said outer surfaces of said pair of
flexible endless belts and while said thermosetting resin in
intimate association with said ribbon remains in a B-stage
consistency, and
f. separating said resulting resin impregnated carbonaceous fibrous
ribbon
2. An improved process according to claim 1 wherein said
carbonaceous fibrous ribbon comprises a plurality of substantially
parallel
3. An improved process according to claim 1 wherein said
carbonaceous
4. An improved process according to claim 1 wherein said
carbonaceous fibrous ribbon contains at least about 95 percent
carbon by weight and
5. An improved process according to claim 1 wherein said liquid
solventless system comprising an A-stage thermosetting resin has a
viscosity of about
6. An improved process according to claim 1 wherein said
solventless system comprising an A-stage thermosetting resin is
forced into intimate association with said carbonaceous fibrous
ribbon by passing said ribbon bearing said system upon its surface
through a pair of rotating parallel
7. An improved process according to claim 1 wherein said
solventless system
8. An improved process according to claim 7 wherein said epoxy
resin is a
9. An improved process according to claim 7 wherein said epoxy
resin is an epoxy novolac resin formed by the reacting of
epichlorohydrin with a
10. An improved process according to claim 1 wherein said resulting
uniformly resin impregnated carbonaceous fibrous ribbon contains
about 35 to 55 percent B-stage thermosetting resin by volume, and
about 45 to 65
11. An improved process for the production of a uniformly resin
impregnated ribbon of a carbonaceous fibrous material which is
suitable for use in the manufacture of carbon fiber reinforced
composite structures comprising:
a. continuously conveying to an impregnation zone a carbonaceous
fibrous ribbon containing at least about 90 percent carbon by
weight,
b. forcing a liquid solventless system having a viscosity of about
1,000 to 3,000 cps. comprising an A-stage thermosetting epoxy resin
and a curing agent for said resin into intimate association with
said carbonaceous fibrous ribbon while present in said impregnation
zone,
c. interposing said ribbon while in intimate association with said
solventless system between the outer surfaces of a pair of flexible
endless belts having a non porous surface and a width greater than
that of said ribbon,
d. continuously passing said ribbon in the direction of its length
while interposed between said flexible endless belts through a
substantially enclosed heating zone provided with a heated gaseous
atmosphere at a temperature of about 75.degree. to 175.degree. C.
while substantially suspended therein wherein said belts and said
ribbon are looped in a single wrap about each of a multiplicity of
rotating parallel rollers wherein the inner surfaces of said belts
are in alternating contact with said rollers as said belts and said
ribbon progress through said heating zone with said ribbon being
out of contact with said rollers and wherein said thermosetting
epoxy resin in intimate association with said ribbon is converted
to a B-stage consistency,
e. continuously withdrawing said ribbon from said heating zone
while interposed between said outer surfaces of said pair of
flexible endless belts and while said thermosetting epoxy resin in
intimate association with said ribbon remains in a B-stage
consistency, and
f. separating said resulting epoxy resin impregnated carbonaceous
fibrous
12. An improved process according to claim 11 wherein said
carbonaceous fibrous ribbon comprises a plurality of substantially
parallel
13. An improved process according to claim 11 wherein said
carbonaceous
14. An improved process according to claim 11 wherein said
carbonaceous fibrous ribbon contains at least about 95 percent
carbon by weight and
15. An improved process according to claim 11 wherein said heated
gaseous atmosphere provided within said heating zone has a
temperature of about
16. An improved process according to claim 11 wherein said
solventless system comprising an A-stage thermosetting epoxy resin
and a curing agent for said resin is forced into intimate
association with said carbonaceous fibrous ribbon by passing said
ribbon bearing said system upon its surface
17. An improved process according to claim 11 wherein said epoxy
resin is a
18. An improved process according to claim 1 wherein said epoxy
resin is an epoxy novolac resin formed by the reacting of
epichlorohydrin with a
19. An improved process according to claim 11 wherein said
resulting uniformly epoxy resin impregnated carbonaceous fibrous
ribbon contains about 35 to 55 percent B-stage thermosetting epoxy
resin by volume, and about 45 to 65 percent carbon fiber by volume.
Description
BACKGROUND OF THE INVENTION
In the search for high performance materials, considerable interest
has been focused upon carbon fibers. The terms "carbon" fibers or
"carbonaceous" fibers are used herein in the generic sense and
include graphite fibers which consist substantially of carbon and
have a predominant X-ray diffraction pattern characteristic of
graphite. Amorphous carbon fibers, on the other hand, are defined
as fibers in which the bulk of the fiber weight can be attributed
to carbon and which exhibit a predominantly amorphous X-ray
diffraction pattern. Graphite fibers generally have a higher
Young's modulus than do amorphous carbon fibers and in addition are
more highly electrically and thermally conductive.
As is known in the art, numerous precedures have been proposed in
the past for the conversion of various organic polymeric fibrous
materials to a carbonaceous form while retaining the original
fibrous configuration essentially intact. Such procedures have in
common the thermal treatment of the fibrous precursor in an
appropriate atmosphere or atmospheres which is commonly conducted
in a plurality of heating zones, or alternatively in a single
heating zone wherein the fibrous material is subjected to
progressively increasing temperatures. See, for instance, U.S. Pat.
No. 3,539,295 to Michael J. Ram for a representative conversion
process.
Industrial high performance materials of the future are projected
to make substantial utilization of fiber reinforced composites, and
graphitic carbon fibers theoretically have among the best
properties of any fiber for use as high strength reinforcement.
Among these desirable properties are corrosion and high temperature
resistance, low density, high tensile strength, and high
modulus.
Carbon fiber reinforced composites are commonly formed by coating
or impregnating carbon fibers with an uncured or partially cured
liquid thermosetting resinous material which is ultimately to serve
as the matrix or continuous phase in the composite article,
converting the resinous material present on the carbon fibers to a
tacky consistency through partial curing and/or evaporation of
solvent, molding or otherwise shaping the same into the desired
configuration, and fully curing the same to form a rigid monolithic
structure. Heretofore, a thermosetting resinous material has
commonly been applied to the carbon fibers from a solvent system
which has necessitated volatilization of the solvent during the
composite formation prior to complete curing. Additionally,
techniques have been proposed wherein the thermosetting resin is
applied from a liquid solventless system. Whenever filament winding
is utilized to shape the composite article, the resin impregnated
carbon fibers bearing a partially cured resin must by necessity be
provided in an appreciable length. The efficient uniform resin
impregnation, handling, and partial curing of continuous lengths of
carbon fibers particularly in ribbon form has been an elusive goal
when employing prior art technology. Arch ovens have been employed
wherein the resin impregnated ribbon is passed through a highly
elongated heating zone while supported upon one surface and the
solvent evaporated. The exposed surface accordingly tends to cure
at a different rate than the surface in contact with the support.
If the resin impregnated ribbon is unsupported over an appreciable
span, roping and/or splitting of the same commonly occurs. A
non-uniformly resin impregnated or nonuniformly partially cured
carbon fiber ribbon is incapable of yielding a carbon fiber
reinforced composite structure consistently exhibiting the required
tensile properties for many end use applications.
It is an object of the invention to provide an improved process for
the production of a carbon fiber ribbon which is uniformly
impregnated with a thermosetting resin which has a tacky B-stage
consistency and is suitable for use in the formation of carbon
fiber reinforced composite structures.
It is an object of the invention to provide an improved process for
production of a continuous length of a thermosetting resin
impregnated carbon fiber ribbon wherein the necessity to volatilize
a solvent from the resin system in contact with the ribbon is
eliminated.
It is an object of the invention to provide an improved process for
the production of a continuous length of a thermosetting resin
impregnated carbon fiber ribbon wherein the partial curing of the
resin is uniformly accomplished on a continuous basis within a
limited area while preserving intimate association between resin
and the carbon fiber ribbon.
It is another object of the invention to provide an improved
process for the production of a carbon fiber ribbon which is
uniformly impregnated with a thermosetting resin having a tacky
B-stage consistency wherein the single filament tensile properties
initially exhibited by the carbon fiber ribbon are substantially
unimpaired.
These and other objects, as well as the scope, nature, and
utilization of the invention will be apparent from the following
description and appended claims.
SUMMARY OF THE INVENTION
It has been found that an improved process for the production of a
uniformly resin impregnated ribbon of a carbonaceous fibrous
material which is suitable for use in the manufacture of carbon
fiber reinforced composite structures comprises:
a. continuously conveying to an impregnation zone a carbonaceous
fibrous ribbon containing at least about 90 percent carbon by
weight,
b. forcing a liquid solventless system having a viscosity of about
500 to 10,000 cps, comprising an A-stage thermosetting resin into
intimate association with the carbonaceous fibrous ribbon while
present in the impregnation zone,
c. interposing the ribbon while in intimate association with the
solventless system between the outer surfaces of a pair of flexible
endless belts having a width greater than that of the ribbon,
d. continuously passing the ribbon in the direction of its length
while interposed between the flexible endless belts through a
substantially enclosed heating zone provided with a heated gaseous
atmosphere while substantially suspended therein wherein the belts
and the ribbon are looped in a single wrap about each of a
multiplicity of rotating parallel rollers wherein the inner
surfaces of the belts are in alternating contact with the rollers
as the belts and the ribbon progress through the heating zone with
the ribbon being out of contact with the rollers and wherein the
thermosetting resin in intimate association with the ribbon is
converted to a B-stage consistency,
e. continuously withdrawing the ribbon from the heating zone while
interposed between the outer surfaces of the pair of flexible
endless belts and while the thermosetting resin in intimate
association with the ribbon remains in a B-stage consistency,
and
f. separating the resulting resin impregnated carbonaceous fibrous
ribbon from the flexible endless belts.
BRIEF DESCRIPTION OF DRAWING
The drawing is a schematic presentation of a representative
apparatus arrangement capable of carrying out the process of the
present invention.
DESCRIPTION OF PREFERRED EMBODIMENTS
The carbonaceous fibrous ribbon which serves as the starting
material in the present process contains at least about 90 percent
carbon by weight. The carbon fibers of the ribbon may exhibit
either an amorphous carbon or a predominantly graphitic carbon
X-ray diffraction pattern. In a preferred embodiment of the process
the carbon fibers contain at least about 95 percent carbon by
weight and exhibit a predominantly graphitic X-ray diffraction
pattern.
The width of the carbonaceous fibrous ribbon may conveniently vary
from about 0.5 to 12 inches, or more.
The carbonaceous fibrous ribbon may comprise a single flat tow of
continuous carbon filaments or a plurality of substantially
parallel multifilament fiber bundles which are substantially
coextensive with the length of the ribbon.
In the latter embodiment the carbonaceous fiber bundles of the
ribbon may be provided in a variety of physical configurations. For
instance, the bundles of the ribbon may assume the configuration of
continuous lengths of multifilament yarns, tows, strands, cables,
or similar fibrous assemblages. The multifilament bundles are
preferably lengths of a continuous multifilament yarn. The fiber
bundles within the ribbon optionally may be provided with a twist
which tends to improve their handling characteristics. For
instance, a twist of about 0.1 to 5 tpi, and preferably about 0.3
to 1 tpi, may be imparted to each fiber bundle. Also, a false twist
may be used instead of or in addition to a real twist.
Alternatively, the fiber bundles may possess substantially no
twist.
Multifilament fiber bundles may be provided within the ribbon in a
substantially parallel manner in the substantial absence of bundle
crossovers to produce a flat ribbon. The number of parallel
multifilament bundles present within the carbonaceous ribbon may be
varied widely, e.g., from 6 to 1,000, or more. In a preferred
embodiment of the process a ribbon precursor is selected having a
weft pick interlaced with substantially parallel fiber bundles in
accordance with the teachings of commonly assigned U.S. Ser. No.
112,189, filed Feb. 3, 1971 of K. S. Burns, G. R. Ferment, and R.
C. Waugh which is herein incorporated by reference. It is not
essential, however, that the parallel fiber bundles or the
filaments of a flat tow be bound by any form of weft interlacement
when constructing carbon fiber tapes for resin impregnation in
accordance with the present invention.
The carbonaceous ribbon which serves as the starting material in
the present process may be produced in accordance with a variety of
techniques as will be apparent to those skilled in the art. For
instance, organic polymeric fibrous materials which are capable of
undergoing thermal stabilization may be initially stabilized by
treatment in an appropriate atmosphere at a moderate temperature
(e.g., 200.degree. to 400.degree. C.), and subsequently heated in
an inert atmosphere at a more highly elevated temperature, e.g.,
900 to 1,000.degree. C., or more, until a carbonaceous fibrous
material is formed. If the thermally stabilized material is heated
to a maximum temperature of 2,000.degree. to 3,100.degree. C.
(preferably 2,400.degree. to 3,100.degree. C.) in an inert
atmosphere, substantial amounts of graphitic carbon are commonly
detected in the resulting carbon fiber, otherwise the carbon fiber
will commonly exhibit a substantially amorphous x-ray diffraction
pattern.
The exact temperature and atmosphere utilized during the initial
stabilization of an organic polymeric fibrous material commonly
vary with the composition of the precursor as will be apparent to
those skilled in the art. During the carbonization reaction
elements present in the fibrous material other than carbon (e.g.,
oxygen and hydrogen) are substantially expelled. Suitable organic
polymeric fibrous materials from which the carbonaceous ribbon may
be derived include an acrylic polymer, a cellulosic polymer, a
polyamide, a polybenzimidazole, polyvinyl alchol, etc. Acrylic
polymeric materials are particularly suited for use as precursors
in the formation of the carbonaceous ribbon. Illustrative examples
of suitable cellulosic materials include the natural and
regenerated forms of cellulose, e.g., rayon. Illustrative examples
of suitable polyamide materials include the aromatic polyamides,
such as nylon 6T, which is formed by the condensation of
hexamethylenediamine and terephthalic acid. An illustrative example
of a suitable polybenzimidazole is poly-2,2'-m-phenylene-5,5'
bibenzimidazole. Preferred carbonization and graphitization
techniques for use in forming the carbonaceous ribbon are described
in commonly assigned U.S. Ser. Nos. 777,275, filed Nov. 20, 1968 of
Charles M. Clarke (now abandoned); 17,780, filed Mar. 9, 1970 of
Charles M. Clarke, Michael J. Ram, and John P. Riggs (now U.S. Pat.
No. 3,677,705); and 17,832, filed Mar. 9, 1970 of Charles M.
Clarke, Michael J. Ram, and Arnold J. Rosenthal. Each of these
disclosures is herein incorporated by reference.
The carbonaceous ribbon optionally may be surface treated in order
to improve its ability to bond to a thermosetting resinous
material. Conventional surface modification techniques may be
selected. Preferred surface modification treatments are disclosed
in commonly assigned U.S. Ser. Nos. 65,454 and 65,456, (now U.S.
Pat. No. 3,723,150) filed Aug. 20, 1970 of M. L. Druin, G. R.
Ferment, and N.V.P. Rao.
In the process of the present invention the carbonaceous ribbon is
continuously conveyed to the impregnation zone while in a flat
configuration. The ribbon may be conveyed in accordance with
conventional fiber advancing techniques, and is preferably under a
uniform tension across its width when it arrives at the
impregnation zone.
While present in the impregnation zone, a liquid solventless system
of a relatively high viscosity comprising an A-stage thermosetting
resin is forced into intimate association with the individual
fibers of the ribbon. The solventless system exhibits a viscosity
of about 500 to 10,000 cps. and preferably a viscosity of about
1,000 to 3,000 cps, during impregnation. It has been found that
such resin systems of relatively high viscosity are capable of
producing a more uniformly resin impregnated ribbon.
The solventless system comprising an A-stage thermosetting resin is
a flowable liquid and is substantially uncured during the
impregnation step. Such a material when exposed to heat hardens or
sets to a rigid solid consistency designated as a C-stage thermoset
resin, and may not subsequently be rendered plastic or flowable
upon the reapplication of heat. The curing or hardening of the
thermosetting resin is brought about by heat-promoted chemical
changes which result in the formation of a compact, often
cross-linked system. It is accordingly essential that thermosetting
resins be molded to the desired configuration prior to the point in
time when the curing reaction has progressed to the C-stage. A
B-stage thermosetting resin is defined as a partially cured
thermosetting resin which has neither the consistency of a flowable
liquid, nor the consistency of a rigid solid. A B-stage
thermosetting resin is accordingly soft and tacky in its
consistency and may be readily molded. Upon the passage of time
even at room temperature, a B-stage thermosetting resin will assume
a C-stage consistency.
The solventless system applied in the impregnation zone may
comprise the A-stage thermosetting resin, one or more curing agents
for the thermosetting resin, one or more accelerators and one or
more solid particulate inert fillers. Conventional solvents such as
acetone which may dissolve the A-stage thermosetting resin are to
be avoided, since upon evaporation such solvents tend to produce
strength-reducing voids, and also lengthen the period of time
required for the A-stage thermosetting resin to assume a B-stage
consistency within the heating zone (described in detail
hereafter). If desired, various modifiers or diluents of the
reactive type may be present within the solventless system since
such components form a permanent portion of the hardened thermoset
resin, and it is not essential to evaporate the same during the
curing reaction.
The resin employed in the solventless system may generally be
selected from those thermosetting resins utilized in the production
of fiber reinforced composites by prior art techniques. It is, of
course, necessary that a substantially uncured thermosetting resin
be selected which inherently possesses the required viscosity at
the impregnation temperature or which may be modified to possess
the required viscosity at the impregnation temperature by the
addition of a reactive modifier or diluent. Illustrative examples
of suitable thermosetting resins for use in the present process
include epoxy resins, phenolic resins, polyester resins,
polyimides, etc.
An epoxy resin is the preferred thermosetting resin for use in the
process of the invention. The epoxy resins utilized in the present
invention are most commonly prepared by the condensation of
bisphenol A (4,4' isoproplidene diphenol) and epichlorohydrin.
Also, other polyols, such as aliphatic glycols and novolac resins
may be reacted with epichlorohydrin for the production of epoxy
resins suitable for use in the present process provided the
resinous products possess or can be modified to possess the
requisite viscosity characteristics. Numerous reactive diluents or
modifiers which are capable of increasing the flow properties of
uncured epoxy resins are well known and include butyl glycidyl
ether, higher molecular weight aliphatic and cycloaliphatic
monoglycidyl ethers, styrene oxide, aliphatic and cycloaliphatic
diglycidyl ethers, and mixtures of the above.
In a preferred embodiment of the invention epoxy resins are
selected which possess terminal epoxide groups and are condensation
products of bisphenol A and epichlorohydrin of the following
formula: ##SPC1##
where n varies between zero and a small number less than about 10.
When n is zero, the resin is a very fluid light-colored material
which is substantially the diglycidyl ether of bisphenol A. As the
molecular weight increases, so generally does the viscosity of the
resins. Accordingly, the particularly preferred liquid epoxy resins
generally possess an n value averaging less than about 1.0.
Illustrative examples by standard trade designations of
particularly useful commercially available epoxy resins include:
Epi-Rez 508 and Epi-Rez 510 (Celanese Coatings) ERLA 2256 (Union
Carbide), ERLA 4617 (Union Carbide), and Epon (Shell) epoxy
resins.
Epoxy novolac resins formed by the reacting of epichlorohydrin with
phenol-formaldehyde resins are also particularly preferred
thermosetting resins. An illustrative example of a highly useful
resin is Epi-Rez 5155 epoxy novolac resin (Celanese Coatings).
A variety of epoxy resin curing agents may be employed in
conjunction with the epoxy resin. The curing or hardening of the
epoxy resin typically involves further reaction of the epoxy or
hydroxyl groups to cause molecular chain growth and cross-linking.
The term "curing agent" as used herein is accordingly defined to
include the various hardeners of the co-reactant type. Illustrative
classes of known epoxy curing agents which may be utilized include
aliphatic and aromatic amines, polyamides, tertiary amines, amine
adducts, acid anhydrides, acids, aldehyde condensation products,
and Lewis acid type catalysts, such as boron trifluoride. The
preferred epoxy curing agents for use with the epoxy resin are acid
anhydrides (e.g. hexahydrophthalic acid and
methylbicyclo[2.2.1]heptene-1,1-dicarboxylic anhydride isomers
marketed under the designation Nadic Methyl Anhydride by the Allied
Chemical Company), and aromatic amines (e.g., meta-phenylene
diamine and dimethylaniline).
The solventless system comprising an A-stage thermosetting may be
provided at a moderately elevated temperature during the
impregnation step of the process in order to impart the required
viscosity to the same. The exact temperature selected will vary
with the specific system selected as will be apparent to those
skilled in the art. Resin system temperatures commonly range from
about 25.degree. to 100.degree. C. at the time of impregnation.
Those resin systems which exhibit a substantial pot life at the
impregnation temperature are preferred.
The technique utilized to force the resin system into intimate
association with multifilament fiber bundles of the ribbon may be
varied. It is essential, however, that the impregnation technique
selected results in no substantial diminution of the tensile
properties of the carbonaceous bundles. In a preferred embodiment
of the process the resin system is initially applied to the ribbon
by briefly passing the ribbon through a vessel containing the same,
and the ribbon bearing the resin system adhering to its surface is
next passed between a pair of parallel nip rollers. In addition to
immersion the resin initially may be satisfactorily applied by
spraying, extruding, etc., prior to passage between a pair of nip
rollers. One of the nip rollers optionally may be provided with a
flat groove corresponding in width to the width of the ribbon, and
the other nip roller provided with a substantially matching raised
surface which in combination with the grooved roller provides a
rectangular gap for the ribbon. The force exerted by such nip rolls
causes the resin system to flow throughout the ribbon.
Alternatively, the impregnation step may be accomplished through
the use of poltrusion or other application technique capable of
bringing out the desired impregnation.
The carbonaceous ribbon while in intimate association with the
solventless system is next interposed between the outer surfaces of
a pair of flexible endless belts. The belts preferably have smooth
nonporous surfaces, are relatively thin so as to permit efficient
heat transfer therethrough in the heating zone as described
hereafter, and are capable of being readily stripped from a ribbon
impregnated with a tacky thermosetting resin. The belts are capable
of withstanding the temperatures employed in the subsequent heating
zone, are capable of withstanding wash solvents, and may be formed
from a variety of materials. Preferred endless belts are formed
from fiberglass reinforced polytetrafluoroethylene sheets having a
thickness of about 0.005 to 0.030 inch. Flexible endless belts
alternatively may be formed from flexible metallic strips or other
fiber reinforced flexible resinous materials. The width of the
endless belts is greater than the width of the ribbon interposed
therebetween (e.g., 0.5 to 2 inches or wider), so that the ribbon
has each of its surfaces completely covered by the endless belts.
The ribbon is preferably interposed substantially at the center of
each belt and is aligned in parallel with the edges of the
belts.
While interposed between the flexible belts, the resin impregnated
ribbon is continuously passed in the direction of its length
through a substantially enclosed heating zone provided with a
heated gaseous atmosphere wherein the belts and the ribbon are
looped in a single wrap about each of a multiplicity of rotating
spaced parallel rollers wherein the inner surfaces of the belts are
in alternating contact with the rollers as the belts and the ribbon
progress through the heating zone. The heating zone may be
relatively compact and provided with a plurality of pairs of spaced
parallel rollers. As the belts and ribbon pass through the heating
zone as a unitary body, the impregnated ribbon remains between the
belts at a fixed location in the absence of sliding contact and is
substantially suspended within the heating zone. As the belts and
ribbon intermittently pass over the rotating rollers a flexing
action occurs and pressure is exerted on alternating sides of the
ribbon which further improves the uniformity of the resin
distribution throughout the ribbon. Each side of the ribbon is
uniformly heated at the same temperature while passing through the
heating zone.
The nature of heated gaseous atmosphere within the heating zone may
be varied. For instance, ordinary air may be employed.
Alternatively, inert gases such as nitrogen may serve as the
gaseous atmosphere. The gas is preferably preheated prior to
introduction into the heating zone such as by passing over
electrical resistance heaters. Additionally, the gas is preferably
circulated within the heating zone by continuously introducing and
withdrawing a portion of the same.
While present in the heating zone, the thermosetting resin in
intimate association with the ribbon is converted to a tacky
B-stage consistency. The temperature of the gaseous atmosphere of
the heating zone, as well as the residence time during which the
ribbon is within the heating zone will vary depending upon the
specific thermosetting resin undergoing partial curing. Heating
zone temperatures of about 75.degree. to 175.degree. C. are
commonly selected, and preferably the temperature of the gaseous
atmosphere within the heating zone is maintained at about
100.degree. to 150.degree. C. Satisfactory residence times in which
to accomplish the desired partial curing within the heating zone
commonly range from about 2 to 30 minutes, an preferably about 10
to 15 minutes.
Since the ribbon is positioned between the endless belts as it
passes through the heating zone, no splitting of roping of the
ribbon occurs as is common in the prior art when a resin
impregnated ribbon is passed across an unsupported span. The
overall dimensious of the heating zone may be substantially
reduced. Additionally, any volatile components of the resin system,
e.g., curing agents, are retained within the ribbon by the
adjoining belts, thereby making possible uniform curing of the
thermosetting resin to the desired tacky consistency. Since the
endless belts have a width greater than that of the ribbon, the
resin system never contacts the rotating rollers present within the
heating zone.
The resulting ribbon is continuously withdrawn from the heating
zone while interposed between the flexible belts prior to a point
in time when the thermosetting resin is advanced to a hard
non-tacky C-stage consistency. The resin in intimate association
with the ribbon remains in a tacky B-stage consistency at the time
of its withdrawl from the heating zone.
The resin impregnated carbonaceous ribbon is next separated from
the flexible endless belts and may be collected or directly
utilized in the formation of carbon fiber reinforced composite
structures. The endless belts following separation from the resin
impregnated ribbon may be washed with an appropriate solvent (e.g.,
acetone or methylene chloride) to remove any adhering resin and
returned for further use.
The uniformly resin impregnated carbon fiber ribbons formed in the
present process preferably contain about 35 to 55 percent partially
cured thermosetting resin by volume (preferably about 40 to 45
percent by volume) and about 45 to 65 percent carbon fiber by
volume (preferably about 55 to 60 percent by volume).
The resin impregnated ribbon following its separation from the
endless flexible belts may be positioned upon releasable interlay,
such as silicone coated release paper, and collected by winding
upon a flanged bobbin or other support where it may be stored for
future use. The resulting ribbons commonly exhibit an extended
shelf life at ambient conditions. For instance, epoxy impregnated
ribbons commonly may be stored as long as several days at room
temperature while still retaining a B-stage consistency. If stored
under refrigeration (e.g. at about 0.degree. C.), such ribbons
commonly exhibit a considerably longer shelf life (e.g., up to
about 90 days or more). The exact shelf life will vary with the
thermosetting resin selected.
The resin impregnated ribbons produced in the present process find
particular utility in the production of high performance composite
structures which are highly useful in the aerospace industry. For
instance, impellers, turbine blades, and similar lightweight
structural components may be formed by conventional filament
winding, molding, or shaping techniques.
A representative apparatus arrangement for carrying out the process
of the present invention is illustrated in the drawing.
Carbonaceous ribbon having a width of 2.75 inches is continuously
unwound from flanged bobbin 2 which is free to rotate about its
central axis. The carbonaceous ribbon consists of 300 continuous
multifilament yarn bundles which are arranged in parallel with each
yarn bundle containing about 400 filaments, having a twist of about
0.5 tpi, exhibiting a total denier of about 400, and a
predominantly graphitic X-ray diffraction pattern. The yarn bundles
are derived from an acrylonitrile homopolymer and contain in excess
of 99 percent carbon by weight. An interlay 4 of Kraft paper is
also continuously unwound from flanged bobbin 2 and is received by
interlay takeup 6 which is rotated about its axis by a driven
constant speed AC motor (not shown) having a spring-tensioned
friction plate. The unwinding of carbonaceous ribbon 1 from flanged
bobbin 2 is accordingly assisted by the rotation of interlay takeup
6 which exerts a pulling force on interlay 4.
The carbonaceous ribbon 1 following unwinding from flanged bobbin 1
passes over three grooved idler rolls 8, 10, and 12 which serve to
center the ribbon, eliminate splits, and equalize yarn density
across the web. Each of the grooved idler rolls 8, 10, and 12 has
groove width of 2.75 inches, a groove depth of 0.25 inch, and a
diameter within the groove of 3 inches. After leaving grooved idler
roller 12 the carbonaceous ribbon is wrapped about a series of four
tensioning rollers 14, 16, 18, and 20 each having a 6 inch
diameter, which apply a uniform tension to the ribbon. The tension
is adjusted by varying the weight 22 on dancer arm 24 as the ribbon
passes about idler rolls 26, 28, and 30 each having a diameter of 6
inches. Dancer arm 24 controls the speed of tensioning rollers 14,
16, 18, and 20 as well as the speed of upper nip roller 35 with all
five of these rollers being driven by the same variable speed motor
(not shown) by means of a chain drive (not shown).
After leaving idler roller 30, the carbonaceous ribbon passes about
a driven grooved dip roller 34 which is partially immersed in
vessel 36 which contains a liquid solventless system containing an
A-stage thermosetting resin and a curing agent for the resin. The
driven grooved dip roller 34 has groove width of 2.75 inches, a
groove depth of 0.125 inch, and a diameter within the groove of 3
inches. The carbonaceous ribbon bearing a coating of the
solventless system next passes between a pair of driven parallel
nip rollers 35 and 38. The nip rollers 35 and 38 serve to force the
resin system comprising an A-stage thermosetting resin into
intimate association with the multifilament fiber bundles of the
ribbon. Dip roller 34, vessel 36, and nip rollers 35, and 38 are
internally heated by a recirculating ethylene glycol-water solution
which aids in maintaining the solventless resin system at the
desired viscosity.
The carbonaceous ribbon 40 in intimate association with the resin
system comprising an A-stage thermosetting resin is next interposed
between a pair flexible endless belts 44 and 45. The endless belts
44 and 45 are non-porous, have widths of 4 inches, and are composed
of polytetrafluoroethylene coated fiberglass. Spring mounted idler
rollers 46 and 48 facilitate the interpositioning of the ribbon 40
between belts 44 and 45. The impregnated carbonaceous ribbon
interposed between the belts passes as a flat unitary structure 50
over compression plate 52 and into heating zone 54.
The heating zone 54 is provided in a forced air convection oven
measuring 3 .times. 3 .times. 2 feet having a top to bottom air
flow. Cantilevered within the heating zone 54 are eight oven
rollers 56, 58, 60, 62, 64, 66, 68, and 70 having diameters of 6
inches which are driven by a common motor (not shown) at a constant
speed. The resin impregnated ribbon while interposed been the belts
and present in heating zone 54 is successively wrapped about each
of oven rollers 56, 58, 60, 62, 64, 66, 68, and 70. The driven
rollers 56, 58, 60, 62, 64, 66, 68 and 70 within the heating zone
54 are rotated at the same rate as grooved dip roller 34 and lower
nip roller 38. While passing through heating zone 54 the
thermosetting resin in intimate association with the carbonaceous
ribbon is advanced to a tacky B-stage consistency, and it is in
this state when it exits from heating zone 54 at opening 72.
After passing between a pair of driven exit nip rollers 74 and 76,
which are rotating at the same rate as the oven rollers, the
resulting carbonaceous ribbon 78 is separated from the endless
flexible belts 42 and 44. The exit nip rollers 74 and 76 serve to
isolate the tension exerted upon the ribbon within the oven from
the takeup winding tension. The belts 42 and 44 pass through belt
washing pans 80 and 82 containing a solvent for the resin system
where any adhering resin is removed by the aid of rotating brushes.
Uniform tension is maintained upon endless belts 42 and 44 by
dancer arm assemblies 84 and 86.
A releasable paper interlay 88 is continuously unwound from reel 90
and contacts the surface of idler roller 92 prior to the arrival of
the resulting thermosetting resin impregnated carbonaceous ribbon
78. The interlay 88 bearing the tacky thermosetting resin
impregnated carbonaceous ribbon 78 next passes about tensioning arm
94 and is wound upon flanged bobbin 96.
The following examples are given as more specific illustrations of
the invention. It should be understood, however, that the invention
is not limited to the specific details set forth in the examples.
Reference is made in the examples to the drawing.
EXAMPLE I
The solventless system provided in dip pan 36 contained 100 parts
by weight of epoxy novolac resin formed by reacting epichlorohydrin
with a phenol-formaldehyde resin, and 88 parts by weight of an
anhydride curing agent. The solventless system at room temperature
(i.e., 25.degree. C.) exhibited a viscosity of about 100,000 cps.
Internally heated dip roller 34, vessel 36, and nip rollers 35 and
38 were maintained at 50.degree. C. during the resin impregnation
step at which temperature the resin system exhibited a viscosity of
about 1,000 cps. The gap between nip rollers 35 and 38 was 0.008
inch.
The carbonaceous ribbon was passed through apparatus at a rate of
20 inches per minute, and was present in heating zone 54 for a
residence time of 13.5 minutes which was maintained at a uniform
temperature of 132.degree. C.
The resulting carbonaceous ribbon was uniformly impregnated with
the tacky B-stage epoxy resin and consisted of about 42.6 percent
of volume resin, and about 57.4 percent by volume carbon fiber.
EXAMPLE II
The solventless system provided in dip pan 36 contained 100 parts
by weight of epoxy resin formed by reacting bisphenol A with
epichlorohydrin, and 35 parts by weight of an amine curing agent.
The solventless system at room temperature (i.e., 25.degree. C.)
was substantially non-flowable. Internally heated dip roller 34,
vessel 36, and nip rollers 35 and 38 were maintained at 78.degree.
C. during the resin impregnation step at which temperature the
resin system exhibited a viscosity of about 2,000 cps. The gap
between nip rollers 35 and 38 was 0.010 inch.
The carbonaceous ribbon was passed through the apparatus at a rate
of 20 inches per minute, and was present in heating zone 54 for a
residence time of 13.5 minutes which was maintained at a uniform
temperature of 125.degree. C.
The resulting carbonaceous ribbon was uniformly impregnated with
the tacky B-stage epoxy resin and consisted of about 45 percent by
volume resin, and 55 percent by volume carbon fiber.
Although the invention has been described with preferred
embodiments, it is to be understood that variations and
modifications may be resorted to as will be apparent to those
skilled in the art. Such variations and modifications are to be
considered within the purview and scope of the claims appended
hereto.
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