Dynamic Stresses and Deformations Investigation of
the Below Knee Prosthesis using CT-Scan Modeling
Muhsin J. Jweeg
1, Abdulkareem Abdulrazzaq Ahumdany
2, Ali Faik Mohammed Jawad
31
Al-Farahidi University, Baghdad, Iraq, muhsinjj@gmail.com
2
University of Babylon College of Engineering Al-Musayab, Iraq, Alhumdany@yahoo.com
3Mechanical Engineering Department, College of Engineering, University of Kerbala, Iraq, alialrafiya@gmail.com
Abstract
— The main issue of this research to improve and develop the mechanical properties of the socket composite material for below-knee (BK) prosthesis; and study the stresses and deformations that are developed due to the dynamic loading caused in the gait cycle. The suggested composite material was consisting of the following layers (2perlon +1kevlar +1perlon +1kevlar +2perlon) as 7 layers and 3.5 mm thickness. This research involved two main parts experimental and numerical. The experimental parts investigation the ultimate tensile strength and modulus of elasticity, (187 MPa) and (1.78 GPa) respectively for the suggested material. The experimental part also included the measurement of the ground reaction force test (GRF). The results showed that the suggested socket was close to symmetrical by (96%) as compering with the intact leg. The numerical part depends on ANSYS 16.0 to calculate the dynamic stresses and deformation. Modeling of the socket was developed by using CT –Scan method and exported to ANSYS 16.0. The dynamic results showed that the maximum stresses (107 MPa) and the total deformation was (18 mm) for the suggestion socket when assuming the applying load as unit step. The dynamic load factor (DLF) was (1.18).Index Term
— Kevlar, Below Knee Prosthesis Dynamic Stress, CT Scan.I.
I
NTRODUCTIONThe modified for mechanical properties and behavior for
below knee prosthesis and socket part investigated from many
researchers at previous years. Therefore, more study gold to
increase strength for materials used for manufacturing the
socket. Then, can be using various way to modified the
mechanical properties and behavior for its parts, as, change the
reinforcement fiber types, change the reinforcement fiber
volume fraction, change the laminated sconces … etc.
Therefore, same researchers listing below shown same ways to
modified the strength and properties for materials used, as,
Firstly, M. J. Jweeg et. al, [1-3], from 2011 to 2017,
investigated the effect for materials properties changing on the
various mechanical properties and stress behavior for foot,
socket, and prosthetic below knee, in addition to, investigated
the creep and fatigue characterizations for materials used to
manufacture its parts, by using experimental and theoretical
techniques. After this, J. S. Chiad et. al, [4-5], at 2012 and
2018, investigated the vibration analysis for below knee and
stress distribution by using experimental techniques.
The, A. M. Takhakh et. al, [6-8], at 2013 and 2018, studied the
vibration and other mechanical properties and behavior for
various Orthosis part with various materials types parameters.
After this, J. K. Oleiwi, [9-10], at 2016 and 2018,
investigation the effect of materials properties with various
reinforcement effect on the stress analysis for various foot
and, prosthetic and biomechanical applications parts. Then, M.
A. Al-Shammari, [11-12], at 2017 and 2018, presented the
stress and fatigue analysis for knee prosthesis sockets with
various reinforcement materials effect experimentally. Also, at
2017, K. K. Resan, [13], investigated the effect of ultraviolet
radiation on the fatigue behavior of below-knee sockets, with
and with-out Heat effect, by using experimental technique.
Finally, M. Al-Waily, [14-17], at 2018, investigated for the
reinforcement fiber type effect on the various mechanical
behavior for foot and below knee, as stress and fatigue
behavior for materials used, in addition to, investigated the
tempratue effect on the fatigue behavior for foot part. Also,
the investigation included analysis for Biomechanical and gait
assessment for normal and Legs.
Therefore, in this work the ultimate tensile strength, the
modulus of elasticity and dynamic load factor for the
suggested marital will be determining. The material properties
will be inserted to the ANSYS 16.0. While the modelling of
the socket will be made by using CT-scan method.
When, the application of CT-Scan modeling has been used by
a few researches before, because of its difficulty. Diane Higgs
and Phavan Sanders [18] developed a design for below knee
prosthetic. The design was based on prescribed specification,
which includes manufacturing process, material, physical
actives data points were acquired from a CT scan of a residual
limb and allowance was made in pressure areas. Figure 1
shows the CT-scan slices for the tibia crest. The socket model
was imported into ANSYS 5.7 for finite element analysis.
Sam L. Phillips et al [19] Have made Eight varieties of lay-up
materials (fibers) each laminated separately with one of three
common resins (matrix), resulting in 24 combinations of
fiber/resin laminates. the weakest were laminates with fibers
of perlon or Nyglass stockinette, spectralon, nylon, and cotton,
ranging between 18 and 42 (MPa); the middle was fiberglass,
ranging between 67 and 109 MPa; the highest strengths were
found in carbon fiber laminates, ranging between 236 and 249
MPa. As shown in figure 2 (A and B) and figure 3 (A and B).
Fig.2 A: The average thickness for the sample set.
Fig. 2.B: The average weight for the sample set.
Fig. 3 A: Stress-strain curves for two samples
Fig. 3 B: Ultimate tensile strength of composites using three resins
II. EXPERIMENTAL PART
The experimental technique included manufacturing and
testing for the below knee structure with materials combined.
Where, the testing samples are manufacturing accordant to
ASTM stander, [20-29], with various composite combined
reinforcement effect.
The experimental part consists of manufacturing the below
knee prosthetics by using the following material and
equipment, knit from perlon, kevlar fibers, laminations resin
80:20 polyurethane, and, hardening powder.
II.1. Equipment of Manufacturing the Prosthetic Socket
Gypsum mold: Mold is made of gypsum material with an
external shape of parallelogram with dimensions of 12 cm 12
cm 30 cm. This mold underwent operations sculpt and refine
of the surface because the inner surface of the material to be
manufactured will take the form of the outer surface of the
mold see figure (4a). Vacuum system: It includes pipes and
vacuum pump. It is used for suction the air completely from
two possible gaps between the PVA and the gypsum mold and
between the inner and outer plies of PVA. There are several
benefits of vacuum system. In the first gap vacuuming gives a
perfect shape for gypsum mold and prevents creating bubbles
between the mold and PVA. For the second gap vacuum is
used to remove the air between the PVA and the part of
casting process. Moreover, vacuum process insures no bubbles
created during the casting process and insure the suitable
distribution of the risen throw all the layers figure (4b).
II.2 Procedure of Manufacturing Prosthetic Socket
The following steps were followed:
1.
Putting the first piece from the PVA on the gypsum molds
as shown in figure (2a) and suction the air between PVA
and gypsum by the vacuum system.
2.
Putting the first Knit of perlon as shown in figure (2b) that
density is 0.01331g /cm
23.
For available material Putting the mat from Kevlar fiber
with density is 1.44 g/cm
2.
4.
Putting the second Knit of perlon that density is 0.01331
g/cm
2and the second piece of PVA and suction the air
between two bags by the vacuum system. Mix the
laminations resin with hardening powder put this mixture
on these layers as distributed equally as shown in figure
(5d).
Fig 5: Procedure for made material of prosthetic socket
II.3. Tensile Test
yield stress and ultimate stress for each material used for
suggested prosthetic socket. Standard tensile test specimens
were cut from the final product according to the American
Society for Testing and Materials (ASTM) D638 [30-38].
Three specimens were cut for each lamination, [39-42], at the
workshop using a computer numeric control (CNC)
machine.as shown in figure 6 and figure 7.
Fig 6: Tensile test specimens and the dimensions for suggested material.
A. Before Testing B. After Testing
Fig 7: Tensile Test for suggestion material Before and After Test.
II.4. Free Vibration Test
The test can be Concisely into the following:
1.
The testing device consists of a special testing hammer,
accelerometer, amplifier and monitor as shown in Figure 8.
2.
The manufactured socket was fixed from the adaptor as a
boundary condition.
3.
The position of the nodes to be tested are marked as shown
in figure 9
4.
The testing hammer used to produce the natural frequency
by hitting the fixed socket a quick and strong hit; this
operation has been done fourth times for the same node but
the hit was in deferent direction.
5.
Finally, the frequency waves were recorded and saved in
USB flash memory.
Fig 8: The Natural Frequency Rig.
Fig 9: The markers of the tested nodes.
III. NUMERICAL ANALYSIS FOR BELOW KNEE
PROSTHETIC SOCKET
The finite element method (FEM) is extensively used in the
multi purposes fields in engineering and science, [43-51],
taking the advantage of the rapid development of digital
computers with large memory capacity, by fast computation.
The method is recognized as one of the most powerful
numerical methods because of its capabilities which include
complex geometrical boundaries and non-linear material
properties. In this work, FEM with the aid of ANSYS
workbench 16.0 software is used as a numerical tool to
illustrate the effect of the fatigue performance in a structure
element to determine the behavior of stress distributions
contour, total deformations, and areas of safety factor. The
general analysis by using ANSYS workbench version 16.0 has
three distinct steps they are, [52-58]:
1.
Building the geometry as a model.
2.
Applying the conditions of boundaries load and get the
solutions.
III.1. CT-Scan of the Below Knee Prosthesis
A below-knee amputee socket has been modeled by using
CT-scan method in AL-Kafeel hospital/kerbala/iraq, the obtaining
slice pictures from CT-Scan for the designed socket had been
exported to (Materialise Mimics Innovation Suite 17.0) where
the 3D modeling which created as shown in Figure 10. The
generated geometry was not uniform because of the stainless
steel adapter joint makes the X-Ray shuttering. As shown in
figure 11.
Fig.10: CT-scan generated geometry
Fig 11: The Shuttered Area Around the Socket Adapter
After making a lot of editing steps included erasing and
redrawing soothing and wrapping which makes the geometry
acceptable and ready to be analyzing, as in Fig. 12.
Fig. 12: The Final Shape of Socket. after editing.
III.2. Mesh of the Model
The meshing process has been done by choosing the volume,
and then the shape of element was selected as tetrahedron
(Automatic meshing), [59-70], for The prosthetic socket as
shown in figure 13. This meshing contains on 350000
elements according to, triangular method has been chosen
ANSYS elements and nodes counter.
Fig.13: The model of BK socket with meshing
IV. RESULT AND DISCUSSION
IV.1. Experimental Results
A.
Mechanical Properties
The mechanical properties as (σult and E) of each tested
spaceman material represent the average value for three
attempts are listed in Table. I. These properties will be used
later in the program ANSYS 16.0 to simulate the prosthetic
socket and analyze stress and deformation.
Table I
The mechanical properties of the material tested.
Material
suggested available
Ultimate stress σ ult (MPa)
177.9
33.65
Modulus of elasticity (E) (GPa)
1.87
0.941
B.
Natural Frequency Results
Natural frequency results were achieved at university of kuffa/
department of mechanical engineering, by testing ten different
positions and take the average results for each suggested node
it was about (69.3) as shown in figure (114) while the other
ten nodes result have listed in table II.
Table II
Ten Nods result for the socket
Nodes
No.
Natural Frequency (HZ)
1
68.665
2
69.275
3
69.58
4
67.749
5
70.496
6
`70.496
7
69.58
8
69.29
9
68.359
10
69.27
Average
69.276
C.
Gait Cycle Results
The results of a step for the two cases (available and suggested
socket) are summarized in Tables III and Table IV
respectively. The results include the prosthetic left leg (injured
leg) and right leg (intact leg) for two cases. For the step-strip
specification result the differences can be observed between
the injury leg and normal leg for the two cases (suggested and
available socket). The difference in the step length for the
suggested socket was (0 cm) while it was (6 cm) for the
available socket; this gives enhancement by (100 %). For the
step time difference, it was (0.02 sec) for the suggested socket
while it was (0.05 sec) for the available socket so it was
enhanced by (60%). Also the foot rotation angle difference for
first case was (0.9 deg), while its being (4.2 deg) for the
second case and thus it’s have been enhanced (78.5%).
The result that obtained in figure 15 and figure 16, have
shown that the difference in gait cycle length and single
support line was (10mm) and (4mm) respectively; for the
suggestion socket. While for the polypropylene socket it was
(37mm) and (47mm) respectively.
Table III
Step-Strip and gait cycle results for suggestion prostheses socket.
Table IV
Step-Strip specification and gait cycle results for available prostheses socket.
Fig 15: A) Gait line length. (B) Single support line, Anterior/posterior position and Lateral symmetry. For suggestion socket
Fig 16: (A) Gait line length. (B) Single support line, Anterior/posterior position and Lateral symmetry. for available socket.
IV.2. The Numerical Results
A.
Static Results
The equivalent Von-Mises Stresses analysis gives a
knowledge on the amounts of stress and deformation
generated by the interface pressure in the socket. The highest
stress value was 107 MPa in the socket made from the
suggested material as shown in figure (17) while the total
deformation was not exceeding 21 mm in some thin area as
shown in figure (18).
Fig. 17: Von-Mises stress of suggested prosthetic socket material
Fig. 18: Total deformation for suggested prosthetic socket material
B.
Dynamic Results
The dynamic analyses is the actual state for the all movement
application so to make that available for the prosthetics socket
it has been assumed to cases the first was subjected the socket
to unit step force its value was 700 N as shown in figure 19
(from the GRF test). The obtained results for the first case
showed that the maximum stress was 107 Mpa as shown in
figure (20). While the total deformation was 24 mm as shown
in figure (21). Also figure (22) and figure (23) showing the
stress and deformation verses time curves during one second.
Fig. 19: Unit Step force during 1 second for both sockets.
Fig. 20: The equivalent stress at the last second for the unit step force.
Fig. 21: The total deformation in the last second for the unit step force.
Fig. 22: Dynamic stresses during 1 second for the unit step force.
While in the second case it was assume that force as sinusoidal
as show in figure (24). The second case showed that the
maximum developed stress and deformation was 147 Mpa and
22 mm respectively at 0.8 second as shown in figure (25) and
figure (26). While the stress-time and deformation-time curve
s have shown in figure (27) and figure (28) respectively.
The dynamic load factor has been calculated by dividing the
dynamic stress on static stress
DLF= dynamic stress (MPa))/ (static stress (MPa)
It is find that DLF does not exceed (1.188) for the suggested
socket material.
Fig.24: Sinusoidal force during 1 second.
Fig.25: The maximum stress value at 0.8 second.
Fig 26: The deformation value at 0.8 second.
Fig. 27: Stress-time curve for the sinusoidal force.
Fig. 28: Deformation-time curve for the sinusoidal force.
V. CONCLUSIONS
The following points are concluded as follows,
1.
To have a uniform solidification the ambient temperature
should be more than 24o C for the lamination risen 80:20.
2.
The mechanical proprieties for the suggestion material (2
perlon +1 kevlar + 1 perlon +1 kevlar +2 perlon) show
better results than available material (polypropylene).
Where the ultimate tensile strength and modulus of
elasticity are increased by (428.6%) and (98.7%)
respectively.
3.
CT-scan method was very powerful in FEL modeling
geometry compared to the normal geometry representation
of the socket.
4.
From the gait cycle results, it was observed that the
suggested socket prostheses decrease the butterfly
parameters, the difference between the injury leg and the
intact leg. the butterfly parameters and the gait cycle step
time enhanced by (60 %).
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[51] Ragad Aziz Neama, Maher A.R. Sadiq Baghdadi, Muhannad Al-Waily ‘Effect of Blank Holder Force and Punch Number on the Forming Behavior of Conventional Dies’ International Journal of Mechanical & Mechatronics Engineering IJMME-IJENS, Vol. 18, No. 04, 2018. [52] Ehab N. Abbas, Muhsin J. Jweeg, Muhannad Al-Waily ‘Analytical and
Numerical Investigations for Dynamic Response of Composite Plates Under Various Dynamic Loading with the Influence of Carbon Multi-Wall Tube Nano Materials’ International Journal of Mechanical & Mechatronics Engineering IJMME-IJENS, Vol. 18, No. 06, pp. 1-10, 2018.
[53] Muhsin J. Jweeg, Zaid S. Hammoudi, Bassam A. Alwan ‘Optimised Analysis, Design, and Fabrication of Trans-Tibial Prosthetic Sockets’ IOP Conference Series: Materials Science and Engineering, 2nd International Conference on Engineering Sciences, Vol. 433, 2018. [54] Ayad M. Takhakh, Saif M.Abbas, Aseel.K. Ahmed ‘A Study of the
Mechanical Properties and Gait Cycle Parameter for a Below-Knee Prosthetic Socket’ IOP Conference Series: Materials Science and Engineering, 2nd International Conference on Engineering Sciences, Vol. 433, 2018.
[55] Mohsin Abdullah Al-Shammari, Sahar Emad Abdullah ‘Stiffness to Weight Ratio of Various Mechanical and Thermal Loaded Hyper
Composite Plate Structures’ IOP Conference Series: Materials Science and Engineering, 2nd International Conference on Engineering Sciences, Vol. 433, 2018.
[56] Marwah Mohammed Abdulridha, Nasreen Dakel Fahad, Muhannad Al-Waily, Kadhim K. Resan ‘Rubber Creep Behavior Investigation with Multi Wall Tube Carbon Nano Particle Material Effect’ International Journal of Mechanical Engineering and Technology (IJMET), Vol. 09, No. 12, pp. 729-746, 2018.
[57] Fahad M Kadhim, Jumaa S Chiad, Ayad M Takhakh ‘Design And Manufacturing Knee Joint for Smart Transfemoral Prosthetic’ IOP Conference Series: Materials Science and Engineering, International Conference on Materials Engineering and Science, Vol. 454, 2018. [58] H. J. Abbas, M. J. Jweeg, Muhannad Al-Waily, Abbas Ali Diwan
‘Experimental Testing and Theoretical Prediction of Fiber Optical Cable for Fault Detection and Identification’ Journal of Engineering and Applied Sciences, Vol. 14, No. 02, pp. 430-438, 2019.
[59] Najdat A. Mahmood, Muhsin J. Jweeg, Mumtaz Y. Rajab ‘Investigation of partially pressurized thick cylindrical shells’ Modelling, simulation & control. B. AMSE Press, Vol. 25, No. 03, pp. 47-64, 1989.
[60] Maher A.R. Sadiq Al-Baghdadi ‘A CFD Study of Hygro-Thermal Stresses Distribution in PEM Fuel Cell During Regular Cell Operation’ Renewable Energy Journal, Vol. 34, No. 03, pp.674-682, 2009. [61] Maher A. R. Sadiq Al-Baghdadi ‘A CFD Analysis of Transport
Phenomena and Electrochemical Reactions in a Tubular-Shaped Ambient Air-Breathing PEM Micro Fuel Cell’ HKIE Transactions Hong Kong Institution of Engineers, Vol. 17, No. 02, 2010.
[62] Luay S. Al-Ansari, Muhannad Al-Waily, Ali M. H. Yusif ‘Vibration Analysis of Hyper Composite Material Beam Utilizing Shear Deformation and Rotary Inertia Effects’ International Journal of Mechanical & Mechatronics Engineering IJMME-IJENS, Vol. 12, No. 04, 2012.
[63] Muhsin J. Jweeg, Ali S. Hammood, Muhannad Al-Waily ‘A Suggested Analytical Solution of Isotropic Composite Plate with Crack Effect’ International Journal of Mechanical & Mechatronics Engineering IJMME-IJENS, Vol. 12, No. 05, 2012.
[64] Ahmed Hasson, Muhsin J. Jweeg ‘Soil organic carbon sequestration under pastures in arid region’ Nature Environment and Pollution Technology, Vol. 12, No. 01, pp. 57-62, 2013.
[65] Ekhlas M. Alfayyadh, Sadeq H. Bakhy, Yasir M. Shkara ‘A New Multi-Objective Evolutionary Algorithm for Optimizing the Aerodynamic Design of HAWT Rotor’ ASME 2014 12th Biennial Conference on Engineering Systems Design and Analysis, ESDA 2014, 2014. [66] Muhannad Al-Waily, Zaman Abud Almalik Abud Ali ‘A Suggested
Analytical Solution of Powder Reinforcement Effect on Buckling Load for Isotropic Mat and Short Hyper Composite Materials Plate’ International Journal of Mechanical & Mechatronics Engineering IJMME-IJENS, Vol. 15, No. 04, 2015.
[67] Muhsin J. Jweeg ‘A Suggested Analytical Solution for Vibration of Honeycombs Sandwich Combined Plate Structure’ International Journal of Mechanical & Mechatronics Engineering IJMME-IJENS, Vol. 16, No. 02, 2016.
[68] Jumaa S. Chiad, Fadhel Abbas Abdulla ‘Effect of Number and Location of Dampers on Suspension System for Washing Machine’ International Journal of Mechanical Engineering and Technology (IJMET), Vol. 09, No. 08, pp. 794-804, 2018.
[69] Sihama I. Salih, Jawad Kadhim Oleiwi, Sajid Abd Alkhidhir ‘Comparative study of some mechanical properties of hybrid polymeric composites prepared by using friction stir processing’ Journal of Advanced Research in Dynamic and Control Systems, Vol. 10, No. 02, Special Issue, 2018.