U.S. patent application number 13/651814 was filed with the patent office on 2013-09-12 for out-of-autoclave and alternative oven curing using a self heating tool.
This patent application is currently assigned to ALLIANT TECHSYSTEMS INC.. The applicant listed for this patent is ALLIANT TECHSYSTEMS INC.. Invention is credited to George J. Glancy, David L. Johnson.
Application Number | 20130233476 13/651814 |
Document ID | / |
Family ID | 44800937 |
Filed Date | 2013-09-12 |
United States Patent
Application |
20130233476 |
Kind Code |
A1 |
Glancy; George J. ; et
al. |
September 12, 2013 |
OUT-OF-AUTOCLAVE AND ALTERNATIVE OVEN CURING USING A SELF HEATING
TOOL
Abstract
Method and apparatus for curing composite material to form
composite structures are provided. A curing tool in one embodiment
includes a curing tool that includes cured nano tube impregnated
resin. At least two conductors are formed in the nano tube
impregnated resin. The curing tool also includes a forming surface
portion. The forming surface portion includes cured composite
material of pre-preg material. The curing tool further includes at
least a first insulation layer that separates the cured composite
material from the nano tube impregnated resin.
Inventors: |
Glancy; George J.; (North
Ogden, UT) ; Johnson; David L.; (Roy, UT) |
|
Applicant: |
Name |
City |
State |
Country |
Type |
ALLIANT TECHSYSTEMS INC. |
Minneapolis |
MN |
US |
|
|
Assignee: |
ALLIANT TECHSYSTEMS INC.
Minneapolis
MN
|
Family ID: |
44800937 |
Appl. No.: |
13/651814 |
Filed: |
October 15, 2012 |
Related U.S. Patent Documents
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Application
Number |
Filing Date |
Patent Number |
|
|
12870556 |
Aug 27, 2010 |
8308889 |
|
|
13651814 |
|
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Current U.S.
Class: |
156/245 ;
156/349 |
Current CPC
Class: |
H05B 2203/013 20130101;
B29C 70/70 20130101; H05B 3/26 20130101; B29C 33/3807 20130101;
B29C 70/882 20130101; H05B 2203/017 20130101; B29C 70/30 20130101;
B29K 2105/167 20130101; B29K 2307/04 20130101; H05B 3/145 20130101;
H05B 2203/005 20130101; B29L 2031/757 20130101; B29C 70/021
20130101; H05B 2203/011 20130101; B29C 33/02 20130101; H05B 2214/04
20130101 |
Class at
Publication: |
156/245 ;
156/349 |
International
Class: |
B29C 70/02 20060101
B29C070/02 |
Goverment Interests
STATEMENT REGARDING FEDERALLY SPONSORED RESEARCH OR DEVELOPMENT
[0002] The United States Government may have certain rights to this
application under contract No. FA9453-06-D0368-0003.
Claims
1. A method of curing composite material to form a composite
structure, the method comprising: laying up and forming pre-preg
material on a forming surface of cured pre-preg material of a
composite structure forming tool; and passing current through nano
tube impregnated resin within the forming tool to heat the tool
internally to cure the pre-preg material.
2. The method of claim 1, wherein laying up and forming pre-preg
material further comprises: applying and pressing the pre-preg
material on the forming surface of the forming tool.
3. The method of claim 1, wherein passing current through the nano
tubes in the tool further comprises: creating a voltage potential
between adjacent conductive strips in the tool.
4. The method of claim 3, wherein creating the voltage potential
between adjacent conductive strips further comprises: coupling
alternating current to the conductive strips.
5. A curing tool comprising: cured nano tube impregnated resin; at
least two conductors formed in the nano tube impregnated resin; a
forming surface portion including cured composite material of
pre-preg material; and at least a first insulation layer separating
the cured composite material from the nano tube impregnated
resin.
6. The curing tool of claim 5, further comprising: a support base
portion of cured composite material; and at least one second
insulation layer separating the support base portion of the cured
composite material from the cured nano tube impregnated resin.
7. The curing tool of claim 6, wherein at least one of the first
and second insulation layers is a layer of cured glass ply.
8. The curing tool of claim 6, further comprising: the support base
portion, the at least second insulation layer and a portion of the
cured nano tube impregnated resin have aligned passages to the at
least two conductors; and a conductive wire for each aligned
passage, each conductive wire passing through associated aligned
passages, each conductive wire coupled to an associated
conductor.
9. The curing tool of claim 8, further comprising: a power supply
coupled to the plurality of conductive wires; and a controller
configured to control the power supply.
10. The curing tool of claim 9, wherein the controller is
configured to vary the power of the power supply to adjust heat
produced by the curing tool.
11. The curing tool of claim 9, wherein the power supply supplies
an alternating current.
12. The curing tool of claim 5, wherein the at least two conductors
are conductive strips positioned relatively parallel to each other
and spaced select distances apart.
Description
CROSS-REFERENCE TO RELATED APPLICATIONS
[0001] This application claims priority to co-pending U.S. patent
application Ser. No. 12/870,556 filed on Aug. 27, 2010, entitled
the same as above, is herein incorporated by reference.
BACKGROUND
[0003] Composite structures formed from pre-impregnated (pre-preg)
material are used in the formation of high strength-low weight
structures such as, but not limited to, parts used to build
aircraft and spacecraft. Pre-preg material is made of composite
fibers such as carbon, glass, aramid and the like, that are bonded
together with a resin that is activated with heat to cure. The
pre-preg material is typically supplied in sheets or plies. The
manufacturer then forms stacks of plies of pre-preg material on a
forming surface of a tool having a desired shape. Once the pre-preg
material is formed on the tool, the tool is placed in an autoclave
or conventional oven to cure the resin. The aerospace industry's
desire for increasingly larger structures has resulted in larger
autoclaves and conventional ovens needed to cure the pre-preg
material. The larger the autoclaves and conventional ovens, the
more costs associated with building and operating them.
[0004] For the reasons stated above and for other reasons stated
below which will become apparent to those skilled in the art upon
reading and understanding the present specification, there is a
need in the art for an effective and efficient method of forming
composite structures without the use of an autoclave or
conventional oven.
SUMMARY OF INVENTION
[0005] The above-mentioned problems of current systems are
addressed by embodiments of the present invention and will be
understood by reading and studying the following specification.
Embodiments of the present invention include both apparatuses and
methods. The following summary is made by way of example and not by
way of limitation. It is merely provided to aid the reader in
understanding some of the aspects of the invention.
[0006] In one embodiment, a method of curing composite material to
form a composite structure is provided. The method including,
laying up and forming pre-preg material on a forming surface of
cured pre-preg material of a composite structure forming tool and
passing current through nano tube impregnated resin within the
forming tool to heat the tool internally to cure the pre-preg
material.
[0007] In another embodiment, a curing tool is provided. The curing
tool includes cured nano tube impregnated resin. At least two
conductors are formed in the nano tube impregnated resin. The
curing tool also includes a forming surface portion. The forming
surface portion includes cured composite material of pre-preg
material. The curing tool further includes at least a first
insulation layer that separates the cured composite material from
the nano tube impregnated resin.
BRIEF DESCRIPTION OF THE DRAWINGS
[0008] The present invention can be more easily understood and
further advantages and uses thereof will be more readily apparent,
when considered in view of the detailed description and the
following figures in which:
[0009] FIG. 1 is a tool formation flow diagram of one embodiment of
the present invention;
[0010] FIG. 2 is a partial side perspective view illustration of
the formation of a support base portion of a tool of one embodiment
of the present invention;
[0011] FIGS. 3A-3I are partial side perspective views illustrating
the further formation of a heating tool of one embodiment of the
present invention;
[0012] FIG. 3J is a bottom perspective view of the tool with formed
passages of one embodiment of the present invention;
[0013] FIG. 3K is a cross-sectional end view of a heating tool of
one embodiment of the present invention;
[0014] FIG. 3L is a cross section end view of the heating tool of
FIG. 3H coupled to a controller and power source of one embodiment
of the present invention;
[0015] FIG. 3M is a side perspective view of the forming of
conductors in a heating tool of another embodiment of the present
invention;
[0016] FIG. 4 is a composite structure forming flow diagram of one
embodiment of the present invention;
[0017] FIG. 5A and 5B are partial side perspective views in forming
a composite structure on a self heated tool of one embodiment of
the present invention; and
[0018] FIG. 6 is a side perspective view of a lay up of the heating
tool of another embodiment; and
[0019] FIG. 7 is a tool formation flow diagram of the formation of
the tool of FIG. 6.
[0020] In accordance with common practice, the various described
features are not drawn to scale but are drawn to emphasize specific
features relevant to the present invention. Reference characters
denote like elements throughout Figures and text.
DETAILED DESCRIPTION
[0021] In the following detailed description, reference is made to
the accompanying drawings, which form a part hereof, and in which
is shown by way of illustration specific embodiments in which the
invention may be practiced. These embodiments are described in
sufficient detail to enable those skilled in the art to practice
the invention, and it is to be understood that other embodiments
may be utilized and that changes may be made without departing from
the spirit and scope of the present invention. The following
detailed description is, therefore, not to be taken in a limiting
sense, and the scope of the present invention is defined only by
the claims and equivalents thereof.
[0022] Embodiments of the present invention provide methods and
apparatuses for fabricating molds, forms, or mandrels (that can be
generally referred to as a tool) that are self heating. Hence, in
embodiments, a tool is provided that includes an internal heating
source. Embodiments allow composite structures to be cured on the
same tool as they were fabricated on without the need for an
autoclave or an oven. Hence, large out-of-autoclave structures are
cured while sitting on a production floor thereby eliminating size
constraints on autoclaves and ovens. Also, embodiments of the self
heating tools allow for the mass production of smaller composite
parts. Rather than stacking hundreds of uncured parts into an
autoclave in a time-consuming process, each part could have its own
self heating tool. Each self heating tool can be heated on the
production floor thereby providing an efficient part flow through
the manufacturing plant.
[0023] In embodiments, a tool is formed with resin impregnated with
nano tubes. The nano tubes in embodiments are electrically
conductive. In one embodiment the nano tubes used to impregnate the
resin are carbon nanofibers (nano tubes). Passing current through
the resin results in heat being generated due to electrical
resistance in the nano tube impregnated resin. In embodiments, by
varying the electrical power, the amount of heat created by the
tool is varied. Moreover, in embodiments, conductive strips, such
as, but not limited to, copper strips are embedded in the cured
nano tube impregnated resin. An electrical potential is created
between adjacent conductive strips (conductive strips that are near
each other) which cause a current to pass through the nano tube
impregnated resin. In an embodiment, an alternating current (AC) is
applied to the adjacent conductive strips to produce the current
through the nano tube impregnated resin.
[0024] Referring to FIG. 1, a formation flow diagram 100 of one
embodiment is illustrated. The formation flow diagram 100 is
described below in concert with illustrations in FIGS. 2 through
3I. In forming a tool, a first step is determining what resin is
compatible with a heat range needed to cure pre-preg material (out
of autoclave material) used to form a composite structure (102).
Then it is determined what the nano tube percentage should be in
relation to the resin (104). The percentage ratio is based on a
desired outcome (desired heat to be generated by a tool). The nano
tubes are then mixed with the resin to form carbon nano tube
impregnated resin (106). A type of resin that can be used is
K-factor resin provided by Boyce Components LLC. Example nano tubes
used are carbon nano tubes provided by Polygraf Products which is a
part of Applied Sciences Inc.
[0025] A foundation for the nano tube impregnated resin has to be
provided to form the self heating tool. In one embodiment, plies of
pre-preg material 204a, 204b, 204c are laid up and formed on a
mandrel 202 (108). The plies of pre-preg material form a support
base portion 204. In one embodiment six to eight layers (plies) of
carbon pre-preg material are used to form the support base portion
204 which is approximately 0.180 to 0.250 inches thick. FIG. 2
illustrates ply layers 204a, 204b and 204c being applied to the
mandrel 202. In one embodiment, the ply layers of pre-preg material
204a, 204b and 204c include carbon fibers. The plies that make up
the support base portion 204 are then cured (110). After the
support base portion 204 is cured, a first insulation layer 300 is
applied (112). This is illustrated in FIG. 3A. In one embodiment,
the first insulation layer 300 is a dry woven glass layer 300 that
is laminated on the support base portion 204. The insulation layer
(dry woven glass layer 300) is then cured on the support base
portion 204 (113). The thickness of the insulation layer 300 in one
embodiment is in the range of 0.003 to 0.005 inches.
[0026] Once the first dry woven glass layer 300 has been cured, a
first coat of carbon nanotube impregnated resin 302a is applied
over the dry woven glass layer 300 (114). This is illustrated in
FIGS. 3B and 3C. In one embodiment, a sponge brush 304 is used to
apply the first coat of carbon nano tube impregnated resin 302a to
the first dry woven glass layer 300. In one embodiment, the first
coat of carbon nano tube impregnated resin 302a is applied with a
uniform thickness of approximately 10 to 11 mils. The desired
spacing of the conductive strips 306 to be used in the tool is then
determined (116). In one embodiment, the conductive strips 306
(conductors) are made of a metal such as copper. The conductive
strips 306 are then placed on a surface of the first coat carbon
nano tube impregnated resin 302a (118) as illustrated in FIG. 3D. A
second coat of carbon nano tube impregnated resin 302b is then
applied over the first coat of carbon nano tube impregnated resin
302a and the conductive strips 306 (120). The first and second
coats of carbon nano tube impregnated resin 302a and 302b are then
cured (122). The tool in this state is illustrated in FIG. 3F.
Although, the conductive strips 306 are illustrated above as being
substantially straight in the embodiment illustrated in FIGS. 3D
and 3E, in other embodiments, the conductive strips 306a can take
any shape as needed to distribute the heat in the tool 350 as
desired. For example, in FIG. 3M the conductive strips 306a and
306b are patterned to achieve a desired heating distribution.
[0027] A second insulation layer 310 is laminated then laid up and
laminated on the carbon nano tube impregnated resin 302b (124).
This layer of the insulation 310 is then cured (125). In one
embodiment, the second insulation layer 310 is a dry woven glass
layer 310 having a thickness in the range of 0.003 to 0.005 inches.
The addition of the second insulation layer 310 is illustrated in
FIG. 3G. Once the second insulation layer 310 has been formed, ply
layers 312a and 312b of pre-preg material are laid up (126) and
cured (126) to form a tool forming surface 312 of the tool 350. The
lying up of the ply layers 312a and 312b are illustrated in FIG. 3H
and the formed tool forming surface 312 is illustrated in FIG. 3I.
FIG. 3I also illustrates the layers of a formed tool 350 in an
embodiment. In one embodiment, the ply layers of pre-preg material
312a and 312b include carbon fibers. Moreover, the number of ply
layers 312a and 312b used to form the tool forming surface portion
312 can vary depending on a desired outcome. In one embodiment, the
thickness of the tool forming surface 312 is in a range of 0.035 to
0.040 inches. Although, the formed tool 350 illustrated in FIG. 3I
is generally C-shaped, the tool can have any desired
cross-sectional shape desired depending on the application.
Moreover, the tool can be straight along its length, it can be
curved along its length and its cross-sectional geometry can vary
along its length. Hence, any shaped tool is contemplated and tool
350 of FIG. 3I is merely an example of one shape of a tool used to
form a C-shaped composite structure.
[0028] In one embodiment, the tool 350 is removed from the base
mold 124 once the tool is formed. Bores 330 are then selectively
formed through the base support portion 204, the first insulation
layer 300 and the first cured carbon nano tube impregnated resin
302a to the conducting strips 306 (130). This is illustrated in
FIG. 3J and FIG. 3K. In one embodiment, a Dremel.RTM. power tool by
the Robert Bosch Tool Corporation, or similar tool, is used to make
the bores through the tool 350 to the respective conducting strips
306. Conductive wires 340 are then coupled to the conductive strips
306 (132) as illustrated in FIG. 3L. FIG. 3L further illustrates, a
power source 342 coupled to the conductive wires 340 and a
controller 344. The controller 344 is designed to control the power
source 342. As stated above, in one embodiment, the power source
342 provides an alternating current (AC) to respective conductive
strips 306 to heat up the tool 350. As illustrated in FIG. 3L, the
first and second insulation layers 300 and 310 insulate the
conductors 306 and nano tube impregnated resin 302a from the
material that makes up the support base portion 204 and the tool
forming surface portion 312. This prevents the support base portion
204 and the tool forming surface portion 312 from passing current
out of the tool 350. This would be an issue in an embodiment where
the support base portion 204 and the tool forming surface 312
include conductive material such as carbon fibers. The insulation
layers 300 and 310 also help prevent the nano tube impregnated
resin from spreading onto the composite material of the support
base portion 204 and the tool forming surface portion 312 during
formation of the tool.
[0029] Referring to FIG. 4, an illustration of a composite
structure forming flow diagram 400 is illustrated. The flow diagram
400 is described in concert with FIGS. 5A and 5B. The process
starts by laying up and forming pre-preg material on the tool
(402). In one embodiment, this is done by applying one or more
layers of pre-preg material on the tool forming surface portion 312
of the tool 350 and pressing the one or more layers of pre-preg
material onto the tool forming surface portion 312 of the tool 350
to form the pre-preg material into the shape of the tool forming
surface portion 312. An example of laying up a layer of ply
material 500 on a tool 350 is illustrated in FIG. 5A. Any method
known in the art to lay up and form the pre-preg material 500 on
the tool 350 can be used. An example method of laying up and
forming pre-preg material on a tool is illustrated in commonly
assigned U.S. Pat. No. 7,249,943 entitled "Apparatus for Forming
Composite Stiffeners and Reinforced Structures" that issued on Jul.
31, 2007 and U.S. Pat. No. 7,513,769 entitled "Apparatus and
Methods for Forming Composite Stiffeners and Reinforcing
Structures" that issued on Apr. 7, 2009 both of which are
incorporated herein by reference. Moreover, any other method of
laying up and forming the pre-preg material on a tool can be used,
such as hot drape forming and other methods known in the art. Once
the pre-preg material is positioned on the tool, the power source
342 provides power to the conductive strips 306 in the tool 350
(404). An example, of the power source 342 coupled to heat a tool
350 is illustrated in FIG. 5B. In FIG. 5B pre-preg material on the
tool 350 is cured to form a composite structure 550. In particular,
the heat of the tool 350, as a result of the power being supplied
to conductors (conductive strips) in the tool 350, cures the
pre-preg material (404) to form the composite structure 550. In one
embodiment, a vacuum bag system known in the art is used to compact
the pre-preg material during curing (403). Once the pre-preg
material is cured, the formed composite structure 550 is removed
from the tool 350 (406).
[0030] Referring to FIG. 6, a lay up (formation) of the tool 350 of
another embodiment is illustrated. In this embodiment the tool is
formed on a master 602 (mandrel) in an opposite manner as the
embodiment discussed above. In this embodiment, the master 602 is
generally in the shape of the part to be made on the heated tool
305. Hence, the formation of the tool on a mandrel can be made in
different ways. One advantage to the formation of the tool 350 as
illustrated in FIG. 6 is that the tool forming surface portion 312
will be relatively smooth and provide a good surface on which to
form the composite structures. Conversely, a surface of the support
base portion 102 will be rougher due to the use of one or more
vacuum bags used to cure the tool 350.
[0031] FIG. 7 illustrated a tool formation flow diagram 700
pursuant to the lay up illustrated in FIG. 6. The flow diagram 700
starts similar to the flow diagram 100 described above. The resin
is selected (102). The nano tube percentage is selected (104). The
nano tubes and resin are mixed to form the nano tube impregnated
resin 302 (106). Plies of pre-preg material are layed up on the
master (708). The plies are then cured (710) to form the tool
forming surface portion 312 on a surface of the master 702. A first
insulation layer 300 is then laminated on a back side of the tool
forming surface portion 312 (712). The first insulation layer 300
is then cured (713). A first coat of nano tube resin 302a is then
applied to the cured first insulation layer 300 (714). It is then
determined what the spacing should be for the conductive strips
(716). The conductive strips 306 are then placed on the first coat
of nano tube resin 302a (718). A second coat of nano tube resin
302b is then applied covering the conductive strips 306 (720). The
nano tube resin 302a and 320b is then cured (722). A second layer
of insulation 310 is then laminated over the nano tube resin 302a
and 320b (724). The insulation layer 310 is then cured (725). Plies
of pre-preg material are then layed up on the second layer of
insulation 310 (726). The plies of pre-preg material are then cured
to form the support base portion (128). Bores are then formed
through the support base portion 204 to the conductive strips (130)
as described above in regards to FIG. 3J. Conductive wires are then
coupled to the conductive strips (132). As understood in the art,
curing of the various materials to make the tool 350 may include
various forms of vacuum bagging techniques.
[0032] Although specific embodiments have been illustrated and
described herein, it will be appreciated by those of ordinary skill
in the art that any arrangement, which is calculated to achieve the
same purpose, may be substituted for the specific embodiment shown.
This application is intended to cover any adaptations or variations
of the present invention. Therefore, it is manifestly intended that
this invention be limited only by the claims and the equivalents
thereof.
* * * * *