Design and Fabricate Filament Winding Machine and Analysis of Cotton/Epoxy and Pandanus/Epoxy
This project concerned with filament wound cotton/epoxy and pandanus/epoxy composite tubes. Monofilament winding machine has been designed and fabricated. It is later used in fabricating the composite tubes. The performance of this machine was measured. The results revealed that the winding angl...
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| Format: | Thesis |
| Language: | English English |
| Published: |
1997
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| Subjects: | |
| Online Access: | http://psasir.upm.edu.my/id/eprint/10019/1/FK_1997_14_A.pdf |
| Summary: | This project concerned with filament wound cotton/epoxy and
pandanus/epoxy composite tubes. Monofilament winding machine has been
designed and fabricated. It is later used in fabricating the composite tubes. The
performance of this machine was measured. The results revealed that the winding
angle depended primarily on the carriage speed traversing at speed synchronised
with mandrel rotation. Also, the efficiency of the machine showed that winding at
high angles relative to rotational axis was very high (i.e. at 90° the efficiency is
100%). Winding at low angles (parallel to rotational axis) was difficult. The surface finish depended on the fibre tension, the wiping process and band formation 0. e.
smooth surface finish at 4.4 kN).
The behaviour of filament wound cotton/epoxy and pandanus/epoxy
composite tubes was studied experimentally. Circular cylindrical of cotton/epoxy
and pandanus/epoxy were loaded in uni-axial compression. The test results show
that cotton/epoxy hoop tubes the maximum strength was found to be 13kN and for
the 80° cotton/epoxy tubes was found to be 10.6kN. For the pandanus/epoxy hoop
tube the maximum strength was found to be 0.3kN. Flat specimens were also
prepared from wound tubes and loaded in uni-axial tension. The cotton/epoxy
composite tubes were tested under internal pressure. The results show that the
maximum pressure that the tube can be withstand was found to be 5 bar. Maximum
stress and maximum strain theories are used to predict the failure of these tubes.
Finite element method also used in the analysis of cotton/epoxy composite tubes.
The uni-axial tensile test results show that the mean modulus was found to be
3 867.6 MPa for the 80° laminated tensile test specimens and 1067.0 MPa for hoop
(90°) laminated tensile test specimens. The maximum strain mean in 80° and 90°
laminated tensile specimens are essentially the same (0.1). The urn-axial
compression test results show that in the condition of hoop (90°) laminated tubes
and 80° laminated tubes the load-displacement curve is linearly up to initial failure. |
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