Compression Molding of Fiber Glass/Epoxy Handguards for the SFLM Advanced Combat Rifle — ARCCB-TR-89017
TECHNICAL REPORT ARCCB-TR-89017
COMPRESSION MOLDING OF FIBER
131
GLASS/EPOXY HANDGUARDS FOR THE
SFLM ADVANCED COMBAT RIFLE
SE
E)TC
KEVIN R. MINER
JECTE
SEP 0? 1989
JULY 1989
US ARMY ARMAMENT RESEARCH,
DEVELOPMENT AND ENGINEERING CENTER
. -CLOSE
COMBAT ARMAMENTS CENTER
BENET LABORATORIES
WATERVLIET, N.Y. 12189-4050
APPROVED FOR PUBLIC RELEASE; DISTRIBUTION UNLIMITED
89 9
06
006
DISCLAIMER
The findings in this report are not to be construed as an official
Department of the Army position unless so designated by other authorized
documents.
The use of trade name(s) and/or manufacturer(s) does not constitute
an official indorsement or approval.
DESTRUCTION NOTICE
For classified documents, follow the procedures in DoD 5200.22-M,
Industrial Security Manual, Section 11-19 or DoD 5200.1-R, Information
Security Program Regulation, Chapter IX.
For unclassified, limited documents, destroy by any method that will
prevent disclosure of contents or reconstruction of the document.
For unclassified,
no longer needed.
unlimited documents,
destroy when the report is
Do not return it to the originator.
SECURITY CLASSIFICATION OF THIS PAGE (Whm
Date Entered)
REPORT DOCUMENTATION PAGE
I.
REPORT NUMBER
CNSTRUCIONS
READCOMPLETING
FORM
BEFORE
2. GOVT ACCESSION NO.
3. RECIPIENT'S CATALOG NUMBER
ARCCB-TR-89017
S.
TITLE (and Subtitle)
4.
COMPRESSION MOLDING OF FIBER GLASS/EPOXY
TYPE OF REPORT & PERIOD COVERED
Final
HA NDGUARDS FCR THE SFLM ADVANCED COMBAT
6
6.
EFRIGOG ORG.
PERFORMING
8.
CONTRACT OR GRANT NUMBER(&)
PERFORMING ORGANIZATION NAME AND ADDRESS
10.
PROGRAM ELEMENT. PROJECT,
Army ARDEC
Benet Laboratories, SMCAR-CCB-TL
Watervliet, NY 12189-4050
AMCMS No. 6236.07.6270.U
PRON No. lA-8-3Z8CD-NMSC
RIFLE
7.
AUTHOR(s)
EO TNM
E
REPORT
NUMBER
Kevin R. Mliner
9.
U.S.
12.
CONTROLLING OFFICE NAME AND ADDRESS
II.
TASK
REPORT DATE
July 1989
U.S. Army ARDEC
Close Combat Armaments Center
Picatinny Arsenal, NJ 07806-5000
14.
AREA & WORK UNIT NUMBERS
IS. NUMBER OF PAGES
21
MONITORING AGENCY NAMF & ADONESS(if diffarent from Controlling Office)
IS.
SECURITY CLASS. (of this report)
UNCLASSIFIED
Sa.
16.
DISTRIBUTION
DECLASSIFICATION/OOWNGRADING
SCHEDULE
STATEMENT (of this Report)
Approved for public release; distribution unlimited.
17. DISTRIBUTION STATEMENT (o
the abatract entered In Block 20, if dltffrent from Report)
SUPPLEMENTARY NOTES
1.
KEY WORDS (Continue an revereo side If neceaniry and Identif by block nu.mber)
IS.
Advanced Combat Rifle
Fiber Glass/Epoxy Composites
Composite Materials
A95"AC'
(Ctfinwe mr er
v
ef
nstmasy s
Compression Molding
Composites Fabrication
Filament Winding
-
ldetity by block nfibi)
A novel compression molding process was used to fabricate a lightweight, highstrength continuous filament fiber glass/epoxy handguard for the advanced
combat rifle. This process involved placing a filament wound preimpreanated
preform into a fiber glass/epoxy mold with a room temperature vulcanized (RTV)
rubber top cover and subjecting it to an autoclave cycle. A well-compacted
and durable structure was easily and quickly produced utilizing this technicue.
DO
,
147
mT0io
OF I Nov 4S Is OBSOLETE
UNCLASSIFIED
SECUIT'Y CLASSIFICATION OF ThIS PAGE (When Data Entered)
SECURITY CLASSIFICATION OF THIS PAGE(Whm Date Bnter)
SECURITY CLASSIFICATION OF THIS PAGE('When Data Entrd)
TABLE OF CONTENTS
Page
INTRODUCTION ...............................................................
1
PROCEDURE..................................................................
2
RESULTS .... ................................................................
5
CONCLUSIONS ................................................................
6
APPENDIX A ................................................................. 17
APPENDIX B ................................................................ 18
LIST OF ILLUSTRATIONS
1.
The serial flechette launch mechanism advanced combat rifle ...........
8
2.
The fiber glass/epoxy mold with caul plate and RTV top cover ..........
9
3.
RTV top cover and vacuum port ......................................... 10
4.
The aluminum master used to make the molds ............................
11
5.
Dimensions of the aluminum preform mandrel
............................
12
6.
The preimpregnated preform and finger rings ready to be
placed in the mold ....................................................
13
7.
Completed handguard halves ............................................ 14
8.
Completed handguard halves ............................................
15
9.
Handguard half subjected to three-point bend test .....................
16
B-1. Front view of the handguard half ...................................... 19
B-2. Side view of the handguard half ....................................... 20
~~~By
....
D.;ttb'
/A
INTRODUCTION
The task was presented by the Future Weapons Branch, U.S. Army ARDEC,
Picatinny Arsenal, New Jersey, to the Advanced Technology Branch, Benet
Laboratories, to fabricate a handguard for the serial flechette launch mechanism
(SFLM) advanced combat rifle (Figure 1).
This is an alternative to the existing
design found on the current combat rifle, the M16.
The handguard was made in
two parts, joined together over the proper location on the barrel of the rifle,
and held in position by end caps.
These caps had a groove in them which
accepted the end lips of the handguard halves and held the halves tightly
together as well as in position.
The handguard had to be lightweight, yet
strong and durable to withstand the rigors of field use.
The surface finish had
to be smooth with well-defined corners, fillets, and rounds.
resist moderate temperatures (150 0F-200*F) was essential.
The ability to
Vent holes were
allowed to relieve the heat buildup.
The proposed solution to the problem was to fabricate a fiber-reinforced
plastic handguard which would be lightweight and stronger than the previous allplastic handguard.
There are several possible configurations including chopped
fiber resin injection molding and cloth layup utilizing either prepreg or resin
transfer molding.
However, these processes required specialized and expensive
equipment unavailable for this project.
Another novel idea was filament winding or braiding a preform and molding
this preform to the proper shape.
This concept, initialized by Plastics
Technical Evaluation Center (PLASTEC), U.S. Army ARDEC, Picatinny Arsenal, New
Jersey, involves the use of a triaxial braider to wet braid a tube or "sock."
This resin-preimpregnated sock is folded lengthwise to form a double thickness
preform, put into a specially designed mold, and cured.
1
/
Under the action of
pressure during the curing process, the braided material is compressed into the
required shape and when comoleted the handguard half is removed, the flashing
trimmed, and the vent holes drilled.
The result is a molded part that contains
very few free edges, namely just the ends.
Free edges are the edges of a lami-
nate that have been cleanly cut or sheared exposing the individual ply edges to
the environment.
By themselves and by the action of moisture intrusion these
plies tend to separate causing delamination and part failure.
The molded edges,
however, do not delaminate.
This quick, easy, and inexpensive L mpression molding technique was the
chosen method of manufacture.
However, after initial experimentation with
resin-impregnated braided fiber glass socks, it was found that they were
extremely difficult to handle.
The weave simply fell apart when handled, indi-
cating the need for a more workable material form.
The use of commercially
available preimpregnated fiber glass roving to filament wind a preform was
explored with success.
The filament wound preform proved to be easy to work
with, quickly produced, and could be refrigerated for extended periods of time.
PROCEDURE
The compression molding technique involved placing a form of preimpregnated
fiber glass/epoxy material into a mold.
The mold was subsequently placed into
an autoclave where heat and pressure were applied to compact and form the
handguard half.
The molds were made from a fiber glass/epoxy tooling material
produced by Fiberite Corporation, Winona, Minnesota.
The part and the fiber
glass molds were the same material and had the same heatup and cooldown rate
which provided good anti-distortion characteristics.
The molds were also light
and could easily be brought to temperature, thus saving labor and process time.
A long tool life could be expected with these molds.
2
Since the mold had only three major components, the function was quite
simple (see Figure 2).
The mold body contained a female cavity surrounded by a
channel which was ported to a vacuum pump.
The cavity accepted the
preimpregnated form and provided the proper dimensions to the finished part.
An
aluminum caul plate sat on a positioning shelf in the mold body and was used to
provide a flat molded edge on the part.
the vacuum pump through this plate.
The vacuum channel was also ported to
A room temperature vulcanized (RTV) sili-
cone rubber top cover was then placed over the caul plate effectively sealing
the part and vacuum chamber (see Figure 3).
in plaster molds supplied by PLASTEC.
These were made by molding the RTV
The top cover provided the proper form
for the inside of the handguard and was pliable allowing the external pressure
from the autoclave to transfer to the part.
The action of the vacuum chamber
allowed any gasses generated during the curing process to bleed off.
The manufacture of the molds was a laborious, yet straightforward process.
An aluminum master of the handguard half, supplied by PLASTEC, was used as a
mold for the tool.
This master was positioned onto an aluminum plate upon which
bars were affixed to provide the vacuum channel in the tool (see Figure 4).
After a release agent was sprayed onto the master, a gel coat of the special
epoxy molding resin was applied.
This was followed by several layers of both
fine and coarse fiber glass/epoxy preimpregnated cloths that built up a mold
thickness of about 0.25 inch.
A debulking procedure was then performed on the
uncured mold assembly to squeeze out trapped air and to compact the laminate.
Following this, a more coarse prepreg cloth was applied and the part was prepared for curing under vacuum and pressure.
Detailed information on the lami-
nate and curing techniques can be found in Appendix A.
3
The molding preforms consisted of uncured preimpregnated continuous filament
fiber glass/epoxy material with a forest green pigment.
This roving was fila-
ment wound onto an aluminum cylinder of specific dimensions (see Figure 5) providing the proper size and shape for the preform.
helical wraps were first applied.
Two layers of ± 45-degree
This wrap was subsequently parted in two by
slicing the laminate lengthwise 180 degrees apart.
The halves were then joined
to make a preform four layers thick which was placed into the mold.
The raised portions of the handguards were finger grips and were made in a
unique way.
num cylinder.
A 0.25-inch thick layer of 90-degree wrap was wound onto the alumiThis layer was then sliced into 0.25-inch wide ring segments
which were removed from the cylinder, cut into approximately 2-inch lengths, and
inserted into the finger grip grooves in the mold prior to the insertion of the
preform.
Under the heat and pressure of the curing process these ring segments
were formed into the shape of the finger grips and bonded securely to the main
body of the part.
As noted in the detailed drawings in Appendix B, the upper portion of the
handguard was thicker than the rest of the part.
This was accounted for by
adding extra prepreg material in that area of the mold in the layup phase.
A
0.5 by 0.25-inch strip of unidirectional preimpregnated fiber glass/epoxy,
referred to as a rib, was laid into the mold, sandwiched between the two layers
of the preform, and extended its entire length.
This provided the required
thickness for the top of the handguard and also gave longitudinal strength and
stiffness.
The three parts of the handguard before cure, the preform, the finger
rings, and the rib, were positioned into the mold using heat from a hot-air heat
gun to soften the prepreg material to the point where it could be worked into
4
the mold shape (see Figure 6).
The excess material extending beyond the upper
flat surface of the mold was cut away with a razor.
Care was taken to ensure
that an adequate amount of the prepreg material extended into the zone of the
end lip, since this lip alone held the handguard halves together and onto the
gun.
When the preform, rings, and rib were positioned and worked to remove
excess air pockets, the aluminum caul plate and the RTV top cover were
installed.
It should be noted that the caul plate not only provided a flat
molded surface for the halves to be joined, but also formed the positioning
holes required to properly position the halves onto the gun.
This was
accomplished by inserting four pins in the caul plate at the proper location.
When assembled, the molds were put into an autoclave in a group of four to
cure the part.
The cure cycle involved heating to 250°F while maintaining a
pressure of 100 psi in a nitrogen environment.
The molds were then
disassembled, the handguard halves removed, and the flashing trimmed.
The
completed handguards are shown in Figures 7 and 8.
The drilling of the vent holes and the installation of irternal heat
shields were performed by the Future Weapons Branch.
These heat shields pro-
vided protection from excessive heat buildup during firing.
Also, the vent hole
edges were sealed with an epoxy resin to prevent delamination.
RESULTS
The compression molding procedure produced a solid, well-compacted
handguard with a good surface finish and well-defined corners and rounds.
finger grips bonded securely to the body and blended in very well.
The
Good end lip
integrity was evident with fibers extending into this zone providing the
required strength.
This was verified by subjecting the handguard half to a
simple three-point compression test with the end lips supported as shown in
5
Figure 9.
A 355-pound load was required to initiate failure of the part with a
midpoint deflection of 0.45 inch.
strength and durability.
This should give some indication of its
The handguard weighed only 134 grams per half, meeting
the lightweight criterion.
The compression molding technique produced a good quality part that conformed to all critical design tolerances.
Slight dimensional instability
resulted from the use of the flexible RTV silicone rubber top cover, but this
did not affect the function or appearance of the handguard and could be
neglected.
An extremely slight axial bow was discovered that produced a small
gap at both ends between two mating handguards.
stresses produced by the mold cur
This was traced to residual
cycle which distorted the mold.
However,
when the handguards were assembled onto the rifle, this axial bow proved to be
beneficial by providing a spring effect that tightened the coupling with the
metal end caps.
This allowed the handguards to mate together very well when
installed on the rifle.
CONCLUSIONS
The compression molding process successfully provided a well-compacted
structure adhering to strict dimensional tolerances.
The fine details of the
handguard were generated without difficulty and without resin or fiber-rich
areas.
The novel approach of filament winding a continuous filament fiber
glass/epoxy preimpregnated preform with integrated finger ring portions proved
to be an easy, although laborious procedure.
Mold wear was evident early in
mold production, but this was due to inadequate part extraction techniques.
Howevp - , when these were corrected, the molds showed little wear and could be
expected to produce hundreds of parts before replacement.
6
It should be understood that the process described herein was experimental
with the objective to produce a small quantity of a newly designed part.
Major
production of a continuous filament/plastic handguard may be accomplished in a
much more inexpensive and timely manner.
However, this process was accomplished
in the projected time and cost frames, which was the objective here.
The
compression molding process produced a good quality, lightweight, and strong
fiber glass/epoxy handguard.
7
L
.0
2
0
V
~0
U
=
U,
U
2
U
4-.
.4-.
-c
C-,
'4-
L
U,
I-
L
C,
U-
8
0
(~)
00
4~!
0-
-~-:
4
U
4'
0
0
L.
'4-
U-
9
44
LL
100
4
-P
S
i,)
L
"0
S=
L
0
L
0
('3
0
-,-
'a-
0
U,-
i
i
-o
0
0
4,
*0
00';
0.
0
04,
q*fl
0
4
-o
0
f
0
0.
vp~
0
4,
*1
0
00
00
0
I-
13
V
L
V
V
~I)
4-,
0.
0
w
L
'4-
14
Figure 8.
Completed handguard halves.
15
LOAD
Figure 9.
Handguard half subjected to three-point bend test.
16
APPENDIX A
Material
Preform, rings, and rib:
E-glass continuous filament preimpregnated with Fiberite Corp. 7714 forest
green-pigmented epoxy resin.
Molds:
Fiberite Corp. Toolrite tooling molding system containing MXB-7620/7500 and
MXB-7620/1597 preimpregnated cloth and MXR-7675 and MXR-7676 gel coat resin.
Autoclave Procedure
Molds:
Debulk with 20-inch vacuum at 150°F for 1 hour.
and 100 psi pressure at 200 to 210°F for 4 hours.
Cure under 20-inch vacuum
Postcure mold unsupported at
150OF for 1 hour, 200OF for 1 hour, 2750F for 1 hour, and 350 to 375°F for 2
hours.
Handquards:
Apply 20-inch vacuum and 100 psi pressure.
hours.
17
Heat to 2500F and hold for 2
APPENDIX B
Detailed Drawings
This appendix contains the front and side view sketches of the handguard
half.
18
Lc-)
L
E'4-
190
0
rr
C=U
C=,
1C=1
C=~
20
TECHNICAL REPORT INTERNAL DISTRIBUTION LIST
NO. OF
COPIES
CHIEF, DEVELOPMENT ENGINEERING DIVISIOV'
ATTN: SMCAR-CCB-D
-DA
-DC
-OP
-DR
-OS (SYSTEMS)
1
1
1
I
1
1
1
CHIEF, ENGINEERING SUPPORT DIVISION
ATTN: SMCAR-CCB-S
-SE
1
1
-DM
CHIEF, RESEARCH DIVISION
ATTN: SMCAR-CCB-R
-RA
-RM
-RP
-RT
2
1
1
1
1
TECHNICAL LIBRARY
ATTN: SMCAR-CCB-TL
5
TECHNICAL PUBLICATIONS & EDITING SECTION
ATTN: SMCAR-CCB-TL
3
DIRECTOR, OPERATIONS DIRECTORATE
ATTN: SMCWV-OD
1
DIRECTOR, PROCUREMENT DIRECTORATE
ATTN: SMCWV-PP
1
DIRECTOR, PRODUCT ASSURANCE DIRECTORATE
ATTN: SMCWV-QA
1
NOTE:
PLEASE NOTIFY DIRECTOR, BENET LABORATORIES, ATTN:
ANY ADDRESS CHANGES.
SMCAR-CCB-TL, OF
TECHNICAL REPORT EXTERNAL DISTRIBUTION LIST
NO. OF
COPIES
NO. OF
COPIES
ASST SEC OF THE ARMY
RESEARCH AND DEVELOPMENT
ATTN: DEPT FOR SCI AND TECH
THE PENTAGON
WASHINGTON, D.C. 20310-0103
ADMINISTRATOR
DEFENSE TECHNICAL INFO CENTER
ATTN: DTIC-FDAC
CAMERON STATION
ALEXANDRIA, VA 22304-6145
COMMANDER
US ARMY ARDEC
ATTN: SMCAR-AEE
SMCAR-AES, BLDG. 321
SMCAR-AET-O, BLDG. 351N
SMCAR-CC
SMCAR-CCP-A
SMCAR-FSA
SMCAR-FSM-E
SMCAR-FSS-D, BLDG. 94
SMCAR-IMI-I (STINFO) BLDG. 59
PICATINNY ARSENAL, NJ 07806-5000
COMMANDER
ROCK ISLAND ARSENAL
ATTN: SMCRI-ENM
ROCK ISLAND, IL 61299-5000
12
COMMANDER
US ARMY TANK-AUTMV R&D COMMAND
ATTN: AMSTA-DDL (TECH LIE!
WARREN, MI 48397-5000
1
1
1
1
1
1
1
1
2
DIRECTOR
US ARMY BALLISTIC RESEARCH LABORATORY
ATTN: SLCBR-DD-T, BLDG. 305
1
ABERDEEN PROVING GROUND, MD 21005-5066
DIRECTOR
US ARMY MATERIEL SYSTEMS ANALYSIS ACTV
ATTN: AMXSY-MP
1
ABERDEEN PROVING GROUND, MD 21005-5071
COMMANDER
HQ, AMCCOM
ATTN: AMSMC-IMP-L
ROCK ISLAND, IL 61299-6000
NOTE:
DIRECTOR
US ARMY INDUSTRIAL BASE ENGR ACTV
ATTN: AMXIB-P
ROCK ISLAND, IL 61299-7260
COMMANDER
US MILITARY ACADEMY
ATTN: DEPARTMENT OF MECHANICS
WEST POINT, NY 10996-1792
US ARMY MISSILE COMMAND
REDSTONE SCIENTIFIC INFO CTR
ATTN: DOCUMENTS SECT, BLDG. 4484
REDSTONE ARSENAL, AL 35898-5241
2
COMMANDER
US ARMY FGN SCIENCE AND TECH CTR
ATTN: DRXST-SD
220 7TH STREET, N.E.
CHARLOTTESVILLE, VA 22901
COMMANDER
US ARMY LABCOM
MATERIALS TECHNOLOGY LAB
ATTN: SLCMT-IML (TECH LIB)
WATERTOWN, MA 02172-0001
2
1
PLEASE NOTIFY COMMANDER, ARMAMENT RESEARCH, DEVELOPMENT, AND ENGINEERING
CENTER, US ARMY AMCCOM, ATTN: BENET LABORATORIES, SMCAR-CCB-TL,
WATERVLIET, NY 12189-4050, OF ANY ADDRESS CHANGES.
TECHNICAL REPORT EXTERNAL DISTRIBUTION LIST (CONT'D)
NO. OF
COPIES
NO. OF
COPIES
COMMANDER
US ARMY LABCOM, ISA
ATTN: SLCIS-IM-TL
2800 POWDER MILL ROAD
ADELPHI, MO 20783-1145
COMMANDER
US ARMY RESEARCH OFFICE
ATTN: CHIEF, IPO
P.O. BOX 12211
RESEARCH TRIANGLE PARK, NC
1
1
COMMANDER
AIR FORCE ARMAMENT LABORATORY
ATTN: AFATL/MNF
EGLIN AFB, FL 32542-5434
METALS AND CERAMICS INFO CTR
BATTELLE COLUMBUS DIVISION
505 KING AVENUE
COLUMBUS, OH 43201-2693
27709-2211
DIRECTOR
US NAVAL RESEARCH LAB
ATTN: MATERIALS SCI & TECH DIVISION
CODE 26-27 (DOC LIB)
WASHINGTON, D.C. 20375
NOTE:
COMMANDER
AIR FORCE ARMAMENT LABORATORY
ATTN: AFATL/MN
EGLIN AFB, FL 32542-5434
1
1
PLFASE NOTIFY COMMANDER, ARMAMENT RESEARCH, DEVELOPMENT, AND ENGINEERING
BENET LABORATORIES, SMCAR-CCB-TL,
CENTER, US ARMY AMCCOM, ATTN:
WATERVLIET, NY 12189-4050, OF ANY ADDRESS CHANGES.