U.S. patent number RE32,772 [Application Number 06/842,191] was granted by the patent office on 1988-10-25 for method of manufacturing a composite reinforcing structure.
This patent grant is currently assigned to Polymer Composites, Inc.. Invention is credited to Ronald C. Hawley.
United States Patent |
RE32,772 |
Hawley |
October 25, 1988 |
Method of manufacturing a composite reinforcing structure
Abstract
A compound composite structure is a combination of plastics and
other materials forming a structure usable in the fabrication of
manufactured products or components. A compound composite structure
is composed of a thermoplastic resin material bonded to, by mixture
with, a composite reinforcing structure. The composite reinforcing
structure consists of fibers imbedded in a thermoplastic resin
material. The composite reinforcing structure may be formed by
passing extruded plastic resin material through a die which imbeds
fibers. The compound composite structure may be formed by mounting
a preformed composite reinforcing structure in a molding die and by
injecting thermoplastic resin material into the molding die.
Inventors: |
Hawley; Ronald C. (Winona,
MN) |
Assignee: |
Polymer Composites, Inc.
(Winona, MN)
|
Family
ID: |
26756450 |
Appl.
No.: |
06/842,191 |
Filed: |
March 21, 1986 |
Related U.S. Patent Documents
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Application
Number |
Filing Date |
Patent Number |
Issue Date |
|
|
75116 |
Sep 13, 1979 |
4312917 |
Jan 26, 1982 |
|
Reissue of: |
321375 |
Nov 16, 1981 |
04439387 |
Mar 27, 1984 |
|
|
Current U.S.
Class: |
264/108;
264/171.13; 264/136; 425/114; 425/112 |
Current CPC
Class: |
B29C
45/14631 (20130101); B29C 48/156 (20190201); B29C
48/05 (20190201) |
Current International
Class: |
B29C
47/02 (20060101); B29C 45/14 (20060101); B29C
047/02 () |
Field of
Search: |
;264/108,136,166,167
;156/166 ;425/113,114,505,112,115 |
References Cited
[Referenced By]
U.S. Patent Documents
Foreign Patent Documents
Primary Examiner: Thurlow; Jeffery
Attorney, Agent or Firm: Moore & Hansen
Parent Case Text
This is a division of application Ser. No. 75,116 filed Sept. 13,
1979, now U.S. Pat. No. 4,312,917 issued Jan. 26, 1982.
Claims
What is claimed is:
1. A method of manufacturing a composite reinforcing structure
comprising the steps of:
extruding a mass of fluid thermoplastic resin material in a
flowable state and having no discrete shape into and longitudinally
through an elongated, stationary die having no relatively movable
components, said die having a continuous, fully open central
passage extending longitudinally therethrough, and a plurality of
lobes projecting radially inwardly into said central passage from
spaced apart locations along the length of the inside, opposite
side walls of said central passage in interleaving relation to each
other to form a convoluted passage through which said thermoplastic
resin material flows;
simultaneously introducing a plurality of continuous lengths of
reinforcing fiber strands into said die central passage at
different locations therein;
separately passing each of said fiber strands longitudinally within
and along the length of said central passage over and between said
interleaving lobes in the presence of said flowing mass of
thermoplastic material to thoroughly contact and coat each of said
fiber strands with said thermoplastic material; and
drawing said thermoplastic resin material and said coated fiber
strands from said die, longitudinally thereof, to thereby produce a
solid plastic .[.rod.]. member having said fiber strands extending
longitudinally therein generally parallel to the longitudinal axis
of said .[.rod.]. member inside of said plastic material.
2. The method of claim 1 further including a step of mixing a
bonding additive with said thermoplastic resin material.
Description
BACKGROUND OF THE INVENTION
This invention relates generally to reinforced thermoplastic
structures and methods of manufacturing such structures. This
invention pertains particularly to compound composite structures in
which thermoplastic resin material is bonded to a preformed
composite reinforcing structure composed of fibers imbedded in
thermoplastic resin material.
A method for producing solid rods by combining resin-impregnated,
longitudinally extending, parallel strands or roving of fibers to
form both the solid body or core of the rod as well as the outer
layer of material consisting of the longitudinally extending,
parallel fibers inbedded in plastic is disclosed by Leonard S.
Meyer in U.S. Pat. No. 3,470,051. The Meyer patent mentions a
method of applying an outer layer of parallel roving to the
exterior of a prefabricated solid core. However, Meyer does not
show a thermoplastic resin material bonded to a composite
reinforcing structure. Meyer relies on a proecss of coating fiber
strands with resin and later hardening the resin so that the fibers
will be imbedded in the resin in longitudinally extending, exactly
parallel relationship. Meyer discloses the use of an extrusion die
which acts to guide resin covered fibers and combine them into a
rod-like mass.
A method for encapsulating fibers in a collimated array within a
thermoplastic resin matrix is disclosed by Bear et al in U.S. Pat.
No. 3,635,879. The Baer process uses chopped glass strands in the
preparation of capsules which may be used as feed stock for an
extruder or molding apparatus. In U.S. Pat. No. 3,834,980, Hall
discloses a method of extruding a coating of thermoplastic polymer
over roving formed from fibrous strands. The Hall process is used
to form pellets which may later be blended with thermoplastic and
used in a molding process. A method of manufacturing plastic rods
having fiber strands extending continuously throughout the length
of the rod is shown by Koch in U.S. Pat. No. 2,625,498. The Koch
method submerges a bundle of strands into a bath of thermosetting
resin and then heats the bundle in a mold until the resin has
completely set or cured. A granule consisting of lengths of glass
roving coated with a molding plastic is described by Bradt in U.S.
Pat. No. 2,877,501. The Bradt capsules are intended for use as a
feed stock for an injection molding machine.
The prior art patents mentioned above do recognize the value of
using fiber strands to reinforce plastics. However, the prior art
does not show a method of adequately reinforcing thermoplastic
resin to allow the manufacture of satisfactory parts and
components. Particularly, the prior art does not show a
satisfactory method of imbedding aligned fibers inside intricate
part shapes. A satisfactory method of employing thermoplastic
resins in the production of high strength plastic parts is not
shown by the prior art. Also, the prior art does not show a simple
method of imbedding continuous length fiber strands in a
thermoplastic resin material using an extruder.
BRIEF SUMMARY OF THE INVENTION
Accordingly, it is an object of this invention to provide a
compound compsoite structure usable in the fabrication of
manufactured products or components.
Another object of this invention is to provide a method of bonding
thermopolastic resin material to a preformed composite reinforcing
structure. It is desirable to have a molding method which allows
the fabrication of high strength, precisely formed products or
components.
A further object of this invention is to provide a method for
forming a composite reinforcing structure by imbedding fibers in
extruded thermoplastic resin material. It is desirable to employ
such a method in which commercially standard extruders are utilized
without substantial modification to produce the composite
reinforcing structure.
Another object of this invention is to provide a method for
precisely locating and orienting a composite reinforcing structure
inside a compound composite structure. A precise method of locating
and orienting a reinforcing structure allows the efficient use of
materials such that only the highly stressed parts of a product or
component need be reinforced. By precisely locating and orienting
reinforcing structures, materials may be saved and the directional
sensitivity of some types of reinforcing structures may be
exploited to provide strength in products or components where
needed.
Still another object of the invention is to provide a method of
manufacturing parts and components using a compound composite
structure which allows fabrication at a high rate of speed.
Another object of this invention is to provide a compound composite
structure that is temperature resistant and which will not warp or
fracture when subjected to temperature changes.
Another object of this invention is to provide a composite
reinforcing structure which may be heated and reshaped to fit as an
insert in a molding die so that products or components having
irregular directional strength requirements may be formed as
compound composite structures.
Briefly, this invention involves a compound composite structure
formed by bonding a thermoplastic resin material to a composite
reinforcing structure. A composite reinforcing structure may be
formed by imbedding long fibers in a first thermoplastic resin
material. The composite reinforcing structure is then used as
insert in an injection molding machine die so that a second
thermoplastic resin material may be molded around the composite
reinforcing structure. The first and second thermoplastic resin
materials should be compatible so that when the second
thermoplastic resin material is injected into the molding die, at
least a thin layer of the first thermoplastic resin material is
melted and becomes intermixed with the second thermoplastic resin
material. Thus, the second thermoplastic resin material becomes
bonded to the composite reinforcing structure in a zone of mixture
between the first and second thermoplastic resin material.
These and other objects and adantages of my invention will appear
more fully from the following description made in conjunction with
the accompanying drawings wherein like reference characters refer
to the same or similar parts throughout the several views.
BRIEF DESCRIPTION OF THE DRAWINGS
FIG. 1 shows a partially cut away perspective view of a compound
composite structure.
FIG. 2 shows a partly cut away side view of an injection molding
machine and mold die for production of compound composite
structures.
FIG. 3 shows a side view of an apparatus for extruding composite
reinforcing structures.
FIG. 4 is a partly cut away side view of an extrusion die for
producing composite reinforcing structures.
DESCRIPTION OF THE PREFERRED EMBODIMENT
FIG. 1 shows a compound composite structure which is designated
generally by the number 10. The compound composite structure shown
has a surface shape in the form of teeth 28 cut in a gear wheel 26
mounted on an axle 38. A bearing (not shown) may be mounted on
surface 30, and another bearing (not shown) may be mounted on
surface 32. Alternatively, separate bearing structures may be
omitted and surfaces 30 and 32 may themselves be used as bearing
surfaces mounted in suitably shaped bores (not shown) to form a
sleeve-type bearing. Thus the particular compound composite
structure 10 shown is a gear assembly which may be rotated about
axis 34 of axle 38 in the direction shown by arrow 36. However, my
inventon may be used in products or components having many
different shapes. The particular shape shown in FIG. 1 is presented
for illustrative purposes only, and indicate only one possible
shape a compound composite structure 10 may take.
The compound composite structure 10 consists of a second
thermoplastic resin material 18 bonded to a composite reinforcing
structure 12. The composite reinforcing structure 12 of FIG. 1 is
shown as a long solid circular cylindrical rod. However, composite
reinforcing structure 12 may have many different cross sectional
geometric shapes including such shapes as a square, rectangle,
triangle, "I" shape, or "[" shape. Also, composite reinforcing
structure 12 may have an elongated tubular shape with a hollow
center. Such elongated tubular shapes for composite reinforcing
structure 12 may have any of various cross sectional geometries
including circular, triangular, or rectangular.
The composite reinforcing structure 12 consists of fibers 14
imbedded in a first thermoplastic resin material 16. The second
thermoplastic resin material 18 is bonded to the composite
reinforcing structure 12 in a zone of mixture 20 where the first
thermoplastic resin material 16 is mixed with the second
thermoplastic resin material 18. While the boundaries of a zone of
mixture 20 may not be clearly defined in a compound composite
structure 10 because of the nature of the first thermoplastic resin
material 16 and the second thermoplastic resin material 18, at
least some mixture does exist in a zone of mixture 20 shown bounded
by first dotted line 22 and second dotted line 24 of FIG. 1.
Thermoplastic resin materials 16 and 18 may be any of various types
of thermoplastics, but material 16 need not be the same type of
thermoplastic as material 18. A partial list of types of
thermoplastics usable as material 16 or 18 would be: polypropylene,
polyethylene, various nylons, polycarbonate, styrene, styrene
acrylonitrile, acrylonitrile butadiene styrene, polysulfone,
various polyesters, polyurethane, polyphenylene sulfide, DuPont
Hytrel brand polyester elastomer, and various thermoplastic
rubbers. The second thermoplastic resin material 18 may consist of
an acetal resin or other self lubricating or low friction type
resin so that surfaces 30 and 32 may themselves be used as bearing
surfaces.
Fibers 14 are shown in FIG. 1 as a collection of long,
substantially straight, substantially parallel strands aligned in
the direction parallel to axis 34 of axle 38. This arrangement of
fibers 14 substantially strengthens the axle 38 in a direction
parallel to axis 34. The presence of fibers 14 causes compound
composite structure 10 to have anisotropic mechanical properties
and to have an increased strength, stiffness, flexural modulus, or
tensile modulus. Fibers 14 may be composed of any of many different
types of materials including such types as: glass, carbon,
graphite, DuPont Kevlar brand aramid fibers, various ceramics, and
various metals. My compound composite structure may also be formed
using a collection of fibers 14 which are randomly oriented, woven
or twisted together. The volumetric amount of fibes 14 relative to
the volumetric amount of first thermoplastic resin material 16
present in the composite reinforcing structure 12 is not a fixed
proportion. Enough resin material 16 should be present to
thoroughly cover each of the fibers 14 so that fibers 14 are
embedded in the material 16. The volumetric proportion between
fibers 14 and material 16 may be adjusted and optimized for the
particular product or component to be manufactured as a compound
composite structure 10. It is expected that increasing the
proportion between the volume of fibers 14 and the volume of
material 16 will increase the strength and other mechanical
properties of the compound composite structure 10.
For best performance, the temperature coefficient of expansion for
the second thermoplastic resin material 18 should be the same as
that for the first thermoplastic resin material 16. As the
temperature is increased or decreased, the first thermoplastic
resin material 16 and the second thermoplastic resin material 18
can be expected to expand or contract. If the materials 16 and 18
expand different amounts when the temperature is changed, the
compound composite structure 10 may fracture, become warped, or
undergo some other kind of structural damage. A temperature
coefficient of expansion is a measure of the amount of expansion a
material undergoes when exposed to changes in temperature. Matching
the temperature coefficient of expansion for the materials 16 and
18 will result in a compound composite structure 10 which is less
likely to be damaged by changes in temperature.
The thermoplastic resin materials 16 and 18 may be augmented by
ingredients added to improved performance or reduce cost. Fillers
may be added to material 16 or 18 to extend the volume of the
material 16 or 18 and thus reduce cost by replacing thermoplastic
with less expensive fillers. Such fillers may include various types
of minerals such as talc. Reinforcement substances such as short
lengths of glass, carbon or graphite fiber may be added to material
16 or 18 to change the mechanical properties of the material 16 or
18, such as increase the mechanical strength or elastic modulus.
Stabilizers may be added to material 16 or 18 to prevent the change
of material 16 or 18 when exposed to environmental stimuli. Such
stabilizers may prevent burning of material 16 or 18 when exposed
to flame or may prevent chemical changes in material 16 or 18 when
exposed to sunlight. Bonding additives may be added to material 16
or 18 to improve the amount of mixing and bonding between material
16 and material 18. Such bonding additives as silane may be used to
improve compatibility between material 16 and material 18 such that
material 18 readily mixes with material 16.
A compound composite structure 10 may also be formed which has more
than one composite reinforcing structure 12. A structure 10 may
have more than one reinforcing structure 12 to provide increased
strength in more than one direction. Thus a designer may position a
plurality of reinforcing structure 12 inside a compound composite
structure 10 to reinforce the highly stressed areas of compound
composite structure 10. The use of a plurality of composite
reinforcing structures 12 would be particularly advantageous in the
construction of products or components formed as compound composite
structures 10 having a shape subject to a plurality of localized
stress concentrations.
FIG. 2 shows a commercially standard injection molding machine
which has been denoted generally by the number 60. The injection
molding machine 60 has a screw shaft 64 mounted inside a barrel 62.
Threads 66 are mounted on screw shaft 64 and define a chamber 68
having a helical shape inside the barrel 62. Hopper 70 is mounted
on barrel 62 and allows feedstock 71 to be dropped into chamber 68.
As screw shaft 64 is rotated in direction 92, feedstock 71 is
conveyed from hopper 70 to nozzle 76 of barrel 62. Feedstock 71 is
heated by frictional forces resulting when screw shaft 64 is
rotated and is also heated by heater 72 and heater 74. Heater 72
and heater 74 are preferably electrical resistance heaters mounted
on the barrel 62.
Sprue plug 78 is mounted in right mold half 80 and abuts against
nozzle 76. Right mold half 80 is placed next to left mold half 82
so as to define a cavity 84. Right mold half 80 has a right insert
support 88 which is preferably a cylindrical bore with a flat
bottom. Similarly, left mold half 82 has a left insert support 90
which is preferably a cylindrical bore with a flat bottom. Insert
86 is preferably a cylindrical rod and is placed inside cavity 84
and is mounted between right insert support 88 and left insert
support 90.
In practice, a preformed composite reinforcing structure (see
structure 12 of FIG. 1) is used as an insert 86 and is placed
between right mold half 80 and left mold half 82. The position of
insert 86 is stabilized by support 88 and support 90. When insert
86 is in place, a thermoplastic resin material (see material 18 of
FIG. 1) is used as a feedstock 71 and is placed in hopper 70. Screw
shaft 64 is then rotated in direction 92 to cause the feedstock 71
to move along barrel 62 and be heated by frictional forces and by
heaters 72 and 74. The heated feedstock 71 passes through nozzle 76
and is injected into sprue plug 78. The heated feedstock 71 passes
from sprue plug 78 and completely fills cavity 84. The feedstock 71
has a temperature sufficient to cause the feedstock 71 to bond to
the composite reinforcing structure insert 86. Bonding is best
achieved when at least a thin layer of insert 86 is caused to melt
by the heated feedstock 71. When a portion of insert 86 melts, the
feedstock 71 mixes with the melted portion of insert 86 and a
strong bond results between insert 86 and the feedstock 71. After
the materials inside cavity 84 are allowed to cool, right mold half
80 is separated form left mold half 82 and the finished part is
removed form inside cavity 84.
As described above, a plurality of composite reinforcing structures
(see structure 12 of FIG. 1) may be used to construct compound
composite structures. Such a plurality of composite reinforcing
structures would be provided by additional inserts similar to
insert 86. Also, additional inserts could be mounted in additional
supports similar to supports 88 and 90.
Although insert 86 is shown in FIG. 2 as a solid cylindrical rod,
insert 86 may have any geometric shape and may be constructed as a
hollow tube. Insert 86 is a composite reinforcing structure (see
structure 12 of FIG. 1) and it is preferable that insert 86 be
formable when heated. That is, it is preferable to have an insert
86 which can be formed to a desired shape before insert 86 is
mounted between the mold halves 80 and 82. Users of my process of
manufacturing compound composite structures need keep on hand heat
deformable composite reinforcing structures of only a few standard
shapes. Products or components formed as a compound composite
structure requiring an insert 86 having an irregular shape may be
manufactured by a process including a step of forming a composite
reinforcing structure having a standard shape into the inset 86
having the desired shape. To be heat deformable, insert 86 should
preferably comprise a thermoplastic resin material which yields
plastically at elevated temperatures without cracking, crazing or
undergoing chemical changes.
The apparatus shown in FIG. 2 and the method described above may be
used to mold compound composite structures having both a high
strength and a precisely controlled shape. The method described
above utilizes thermoplastics which are molded into shape using
heat. The molding process produces a product having a very
precisely controlled shape. The use of a reinforced insert produces
a product having a greater strength or elastic modulus. The molding
process can be utilized to manufacture products at a high rate of
speed.
FIG. 3 shows an apparatus for the production of composite
reinforcing structures and includes a commercially standard
extruder machine designated generally by the number 120. The
extruder machine 120 has a screw shaft 124 mounted inside a barrel
122. Hopper 126 allows feedstock 127 to be passed inside barrel
122. Heater 130 is preferably an electrical resistance heater
mounted outside barrel 122. The feedstock 127 passes through barrel
122, is heated by heater 130, exits through barrel flange 128, and
enters die flange 132. Upper die half 134 mates witih lower die
half 136. Die halves 134 and 136 are mounted between flange 132 and
forming die 150. Heaters 133 are a plurality of heating elements
mounted in upper die half 134 or lower die half 136. Heaters 133
are preferably electrical resistance heaters formed in the shape of
elongated cylindrical rods. Pressure sensor 137 is shown mounted in
lower die half 136 near forming die 150.
In use, a first thermoplastic resin material is dropped into hopper
126 as feedstock 127 for extruder machine 120. The feedstock 127 is
conveyed inside barrel 122 by screw shaft 124 and is heated by
frictional forces inside barrel 122 and by heater 130. The
feedstock 127 is extruded through barrel flange 128 and die flange
132 into upper die half 134 and lower die half 136. Fiber strand
142 feeds from reel 144 through feed port 138 into the upper die
half 134. Similarly, fiber strand 146 feeds from reel 148 through
feed port 140 into upper die half 134. Feedstock 127 is heated
inside die halves 134 and 136 by heaters 133. Fiber strands 142 and
146 become imbedded in the feedstock 127 and are extruded from
forming die 150 to create formed extrusion 152. Pressure sensor 137
senses the extrusion pressure near forming die 150 to allow control
to be exerted over the rate of extrusion by controlling the
rotational speed of screw shaft 124. That is, pressure sensor 137
is positioned near forming die 150 so that extruder machine 120 can
be operated to produce formed extrusion 152.
After leaving forming die 150, formed extrusion 152 enters sizing
die 154. Sized extrusion 156 leaves sizing die 154 as an extrusion
having a control shape. Sized extrusion 156 enters cooling chamber
158. Cooled extrusion 160 is pulled from cooling chamber 158 by
pulling track 162 mounted on rollers 164 and pulling track 166
mounted on rollers 168. Tracks 162 and 166 also create pulling
forces which act to pull formed extrusion 152 from forming die 150
and act to pull sized extrusion 156 from sizing die 154. Cooled
extrusion 160 is cut to length by cutting device 170. The apparatus
shown in FIG. 3 thus produces lengths or extruded material
corresponding to the composite reinforcing structure 12 of FIG. 1
and coresponding to the insert 86 of FIG. 2.
FIG. 4 shows an enlarged view of a portion of the apparatus of FIG.
3. Feed port 140 is constructed in the same way as feed port 138.
It should be understood that this invention can be practiced using
a plurality of feed ports. The number of feed ports used would vary
with the number of fiber strands to be embedded and the feed ports
may be mounted in the upper die half 134 or the lower die half 136.
Feed port 138 includes a sleeve 200 mounted in upper die half 134.
Feed port member 138 is slidably mounted in sleeve 200. Feed port
member 138 is split into at least two pieces, here shown as pieces
202 and 204. Feed port member 138 has a bore 206 passing
longitudinally therethrough. Bore 206 is preferably shaped as a
right cylindrical cone opening away from the upper die half 134.
Fiber strand 142 passes through bore 206 and enters passage 210
between upper die half 134 and lower die half 136. When knots or
other imperfections are encountered in fiber strand 142, feed port
member 138 may be slidably pulled from sleeve 200 along the path
shown by arrow 208 to allow such knots or imperfections in fiber
strand 142 to pass through bore 206 by separating piece 202 from
piece 204. When such knots or imperfections in fiber strand 142
have passed through bore 206 and entered passage 210, feed port
member 138 may be pushed back in sleeve 200 in the direction shown
by arrow 208. Thus feed port 138 allows for continuous production
of formed extrusion 152 even when knots or imperfections exist in
fiber strand 142.
A series of lobes 212, 214 and 216 are formed in uppe die half 134
and lower die half 136 such that passage 210 takes a convoluted
route. The function of lobes 212, 214 and 216 is to cause fiber
strands 142 and 146 to be passed over at least one lobe such that a
thermoplastic resin material (not shown) inside passage 210
thoroughly contacts each of the fiber strands 142 and 146. By
drawing the fiber strands 142 and 146 over the lobes 212, 214 and
216, thorough contact between a thermoplastic resin material and
the fiber strands 142 and 146 is asssured. Pressure sensor 137
measures the pressure of a thermoplastic resin material inside
passage 210.
It is anticipated that various changes may be made in the shape,
construction and operation of the invention as disclosed herein
without departing from the spirit and scope of the invention as
defined by the following claims.
* * * * *