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THE USE OF FINITE THE USE OF FINITE ELEMENTS IN ELEMENTS IN SURGICAL SURGICAL PROCEDURES PROCEDURES
Djenane C. Pamplona
Laboratory of Membranes and Biomembranes
Civil Engineering Department Catholic University of Rio de Janeiro - Brazil
THE USE OF FINITE THE USE OF FINITE ELEMENTS IN ELEMENTS IN - - PowerPoint PPT Presentation
Civil Engineering Department Catholic University of Rio de Janeiro - Brazil THE USE OF FINITE THE USE OF FINITE ELEMENTS IN ELEMENTS IN SURGICAL SURGICAL PROCEDURES PROCEDURES Djenane C. Pamplona Laboratory of Membranes and Biomembranes
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Civil Engineering Department Catholic University of Rio de Janeiro - Brazil
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Obtain extra skin to reconstruct
breast reconstruction; eliminating tattoos and scars; extra skin with the desired
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To understand the behavior of the skin under expansion. To identify the the material parameters for the skin under
To help doctors to know the number and shape of the
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Expansion of the scalp Filling the expander
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Measuring pressure. Connecting the syringe.
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Volume ( ml)
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W : Constitutive Relation. a and b : Parameters of the material. I1: First principal invariant of the Cauchy-Green deformation tensor.
1
t
G ( t ) : Relaxation function
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Circular skin expander
Triangular and quadrilateral membrane and fluid elements.
Boundary Condition
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Using the least-square fit procedure minimizing the error, the material coefficients at the first stage (volume 80 – 110 ml) are : a= 0.213 MPa and b=31.5.
0,00 0,50 1,00 1,50 2,00 2,50 3,00 3,50 70,00 80,00 90,00 100,00 110,00 120,00 Volume (ml) Pressure (N/cm2) Experimental C1 C2 C3 C4 C5
The same procedure was used in the following stages, until volume from 538 ml is reached.
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Constant a scalp
0.000 0.500 1.000 1.500 2.000 2.500 3.000 0.00 0.50 1.00 1.50
Current volume/initial volume (X100)
Constant a (MPa)
Experimental
Constant b scalp
0.0 20.0 40.0 60.0 80.0 0.00 0.50 1.00 1,50
Current volume / initial volume (X100) Constant b experimental Fase Vfinal/Vo a (Mpa) b A 80 x x x 1 80 110 0.28 0.213 31.5 2 110 140 0.35 0.222 33.4 B 140 380 x x x 3 380 425 1.06 0.986 51.3 4 425 465 1.16 1.298 75.2 5 465 500 1.25 1.463 134.5 6 500 538 1.35 1.787 120.5 initial - final
Experimental results - Pacient 1
Volume (ml) Constants Fase Vfinal/Vo a (Mpa) b A 214 x x x 1 214 254 0.85 0.636 42.6 2 254 298 0.99 0.491 48.2 3 298 338 1.13 1.007 49.8 4 338 376 1.25 1.500 65.6
Experimental results Pacient 2
Volume (ml) initial - final Constants
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Patient 2 Patient 3 Patient 4 Patient 5 Patient 1
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The numerical model developed was successful in its
It was possible to understand the limiting stress during the
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Different regions: Scalp: more rigid larger values for constant a. Abdomen and leg : similar values for constant a. A parammetric study involving the thickness of the skin: showed the necessity to have it correctly measured during the surgery. Fatty regions: It was verified the importance of the amount of fatty tissue in the behaviour of the skin expansion.
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More patients, with different regions of the body,
discriminating race and age must be done..
Experimental study to verify the importance of the elastic
foundation (fatty base) in the expansion.
Reliable skin thickness to work with.. Measure the relaxation process. Propose number, shape and size of the skin expander for
doctors.
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B C A
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i i i
2 2 1 N 1 i 2 i
α α α =
= τ −
N 1 i t i R
i
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(h = 6 mm; 8 mm in the scar)
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Maximum stresses (N/cm2)
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Maximum stresses (N/cm2)
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The breast is composed basically by mammary glands in the internal part of the breast. The fatty tissue is responsible for the rest of the composition. The proportion of each one differs from
The glandular tissue is more rigid than the fatty.
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Areola Infra mammary fold
Three points are marked forming a triangle around the areola of the breast and two points more in the infra mammary fold, considered a constraint. The incisions are made according to the figure.
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A B
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Ogden
= α α α
2 1 i 3 2 1 2 i i
i i i
µ1 (kPa) α1 Fatty Tissue* 1.8567 18.1468 Skin 0.803 6.8206 Mammary Glands* 9.0657 25.0000 MATERIAL
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3 breast.
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(yellow)
The model for the breast has 5844 elements (C3D4). MOD2a MOD2b
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Maximum stresses (N/cm2)
T=0: lying and upright position. 3 weeks
Nipple
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Maximum stresses (N/cm2)
T=0: lying and upright position. 3 weeks
Nipple
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