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ABSTRACT
The terrorist operations, the wars and the incidents led to an increase
in the number of amputations in Iraq. Prosthetic limbs are manufactured to
compensate for the missing parts of the human body. However, the most
common type of lower limb is Trans-tibial (Below Knee).
In this work, design and analysis of below knee BK Prosthetic Socket is
discussed with the aim of selection of material, and manufacturing of
socket. Four groups Composite materials used for manufacturing BK
prosthetic socket by using vacuum molding technique with various volume
fractions are studied. The first group consists of eight layers (2-layers of
carbon and 6-layers of perlon with Vf=0.409) with acrylic resin, the second
group consists of eight layers (2-layers of carbon and 6-layers of perlon
with Vf=0.24) with acrylic resin, The third group consists of twelve layers
(4-layres of carbon and 8-layers of perlon) with acrylic resin, and four
group consists of acrylic resin only. The study was conducted
experimentally, analytically, and numerically.
The experimental work involves determination of physical, mechanical and
fatigue properties of composite material used for manufacturing below knee
prosthetic sockets. Two models Trans-Tibial prosthetic sockets with (3) mm
thickness were manufactured from Composite material (12-Layers) and
subjected to Force Plate testing and F-socket testing to determine ground
reaction force and pressure interface at socket/stump region.
The analytical work discusses the friction effect on normal stress at
interface. A simplified lower limb model was applied to analyze the effect
of frication. MATLAB Program was utilized to calculate the pre-pressure,
pressure and shear stress at stump/socket region by solving the equations.The finite element method (ANSYS-15) w s utilized for the analyzing and
evaluating of the fatigue properties by observing the, maximum principal
stress, the total deformation and safety factor.
The results showed the mechanical properties (ultimate strength and
Young s modulus) are increasing with the increasing volume frication at
constant perlon and carbon fiber layers.
The results showed that the composite materials achieve a large increment
in mechanical properties such as (ultimate strength, Young s modulus,
Flexural strength and flexural modulus ) which were increased to a
percentage of (124%), (7.2%), (95.9%), and (83.87%), in composite
material (12-Layers) as compared with composite material(8-Layers with
volume fraction=0.409). However, The ultimate tensile strength and the
modulus of elasticity of composite materials (12-Layers) are higher than
those of the composite materials (8-Layers with volume fraction=024) by
100% and 185% respectively, and by 444% and 274% for pure acrylic
lamination. The fatigue limit for 12-Layers (perlon and carbon) is 63 MPa.
Result of F-socket apparatus, four specific areas of the BK prosthetic socket
which experienced pressures in excess of 100 kPa were identified. The
highest pressure at socket/stump region was 200 kPa in patella tendon area
for long socket.
The results show that the maximum principal stress, deformation and safety
factor are equal to 37 MPa, 8.48 mm and 1.7 respectively for long socket
and 26 MPa, 4.59 mm and 1.83 respectively for standard socket.
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