Polish J. of Environ. Stud. Vol. 15 No. 4A (2006), 140-142 Modelling of Some Mechanical Malfunctions of the Human Tympanic Membrane E. Skrodzka, J. Modáawska Institute of Acoustics, A. Mickiewicz University, PoznaĔ, Poland Abstract Many researchers have reported mechanical damages of a human tympanic membrane (TM) in the form of a rupture. Some forms of cicatrices and bosses were also observed on the TM. Ruptures and cicatrices can be treated as TM’s mechanical modifications. We present numerical models of the human TM with such modifications. The Finite Element Method was used as a numerical tool. The aim of our work was to simulate mechanical behaviour of the TM with a rupture and with an additional mass. Results of vibrational analysis for the structurally modified models were compared to results obtained from the physiological model. The main characteristics predicted from the modified TM’s have shown that all modifications affected calculated curves in all investigated cases. Keywords: tympanic membrane, structural modifications, mechanical behaviour Introduction Mechanical damages or dysfunctions of a human tympanic membrane (TM) can be acquired or related to biochemical malfunctions [1, 2]. Many researchers have reported acquired mechanical damages in the form of a rupture. The TM rupture may be caused by impact noise (i.e. explosions). Some forms of cicatrices and bosses of different origin were also observed on the TM [1]. Both ruptures and cicatrices can be treated as mechanical malfunctions of the TM. There are many numerical models of the TM and the whole middle ear in the physiological state as well as many models including dysfunctions of the ossicular chain [3]. However, there have been no reports about modelling of mechanical malfunctions of the TM. The aim of our work was to numerically simulate mechanical behaviour of the TM with a rupture and with an additional mass. Such modelling may help better understanding of some mechanical malfunctions of the TM. Numerical models of the TM with ruptures and additional mass The human TM was modeled as a semi-conical threedimensional structure with dimensions as well as isotropic material constants chosen to be realistic, or to be similar to those known from experiments. Details of the physiological model were described in our previous work, [4]. The physiological model was structurally modified by adding holes and mass. All ruptures and bosses were placed anterior-inferior portion of the TM. The area of ruptures was 2.2*10-6 m2 (small hole), 4.8*10-6 m2 (medium hole), 13.4*10-6 m2 (big hole) and 16.2*10-6 m2 (huge hole). Two kinds of bosses were modeled. Their physical parameters differed from those of the physiological TM (density ȡ=1.2*103 kg/m3, pars tensa Young’s modulus of elasticity E=3.3*107 (N/m2), total mass 8.2*10-6 kg, total area 70*10-6 m2). The thin and long bosses were modeled for the following values of physical parameters: ȡ1=1.8*103 kg/m3 and E1 = 5.0*107 N/m2 (boss 1); ȡ2 = 2.6*103 kg/m3, Modeling of Some Mechanical… 141 a) b) c) d) Fig. 1. (a) Input-output characteristics for models with holes; (b) input-output characteristics for models with bosses; (c) transfer functions for models with holes; (d) transfer functions for models with bosses for selected points on the TM 142 Skrodzka E., Moádawska J. E2= 7.2*107 N/m2 (boss 2); ȡ3=3.5*103 kg/m3, E3=9.7*107 N/m2 (boss 3). Additional mass was 9.36*10-6 kg (boss 1; 114.2% of the physiological model mass), 8.90*10-6 kg (boss 2; 108.5 % of the physiological model mass) and 8.50*10-6 kg (boss 3; 103.7 % of the physiological model mass) respectively. The thick and short bosses were modeled for the following parameters: ȡ1=1.8*103 kg/m3 and E1= 5.0*107 N/m2 (boss 1a); ȡ2=2.6*103 kg/m3, E2= 7.2*107 N/m2 (boss 2a); ȡ3=3.5*103 kg/m3, E3=9.7*107 N/m2 (boss 3a). Additional mass was 9.28*10-6 kg (boss 1a; 113.2 % of the physiological model mass); 8.85*10-6 kg (boss 2a; 107.9 % of the physiological model mass) and 8.48*10-6 kg and (boss 3a; 103.4 % of the physiological model mass). The Finite Element Method (FEM) was applied to modeling the dynamic behavior of the modified TMs [5]. Frequency response analysis based on modal superposition was used to solve the steady state response of the structure subjected to harmonic loading. In this research the NE/NASTRAN v.8.3K solver for FEM [6] together with FEMAP v.8.3.0.1 pre- and post processor [7] was used, and both programs were run on PC Pentium IV, 2.4 GHz. Results and discussion The TM models were tested by calculations of the dynamic characteristics (input-output functions) and velocity in points (model nodes). Calculations were compared to results obtained from the normal-functioning model of the TM, [4]. Point no. 1 was chosen on the pars tensa portion, point no. 2 – on the pars flaccida portion, point no. 3 – on the manubrium. The model was loaded by sinusoidal pressure of frequency 0.5, 0.8. 1, 1.5, 2, 3, 4, 5, 6 and 7 kHz, applied perpendicular to model surface. Applied sound pressure levels along the main axis of symmetry were 20-110 dB SPL, with 10 dB step. Examples of calculated input-output functions are presented in Fig.1a (ruptures) and Fig. 1b (bosses). Results are presented for chosen frequencies 0.5 kHz and 2 kHz as the frequency band limited by them is the most important for speech intelligibility. All presented input-output functions show linear behaviour, as it has been expected for the TM and the linear model. However, results obtained from models with holes are significantly different from those of the normal TM model and they depend on the observation point, frequency and the area of rupture. Results for bosses are more consistent – for all chosen physical parameters the input output functions are higher than the curve for the normal TM. Examples of calculated velocity for selected points vs. load frequency for ruptures are shown in Fig. 1c (ruptures) and Fig. 1d (bosses). Results are presented for 60 and 90 dB SPL. All curves obtained for modified models are generally higher than curves for the normal TM in lower frequencies (up to 2-3 kHz). The greatest effect is observed for big and huge holes as it could be expected [1]. For bosses results are more uniform, the smallest effect was observed for boss 3, the highest for boss 3a. Physical parameters of bosses were chosen arbitrary, as no literature data are available now. None of the chosen set of physical parameters of bosses has secured normal functioning of the TM. Velocities of the TM motion higher than normal may influence signal processing on higher stages of the auditory system. Conclusions Our numerical simulations have shown that all structural modifications of the TM affected calculated curves in most cases. It is worthwhile to add that physical parameters of the physiological tympanic membrane are relatively well described, but such parameters for bosses have not been described yet. Therefore, they were estimated to be close to reality in the best possible way. The results seem to be reasonable and although the models have some limitations they may be used in further investigation of the TM malfunctions caused by physical changes or damages like cicatrices or physiological covering of TM fistulas by isotropic membranes after acoustic trauma. In the latter case the fibrous structure of the tympanic membrane is probably not recovered. The results of modelling clearly show that the vibrations on impaired membranes are quite different from that of the normal TM and they may be used for improving the hearing-aid fitting process. References 1. 2. 3. 4. 5. 6. 7. Pruszewicz A.: Zarys audiologii klinicznej, Wyd. Ak. Med. w Poznaniu. PoznaĔ, 2000. ĝliwiĔska-Kowalska M., Audiologia kliniczna, Mediton. àódĨ, 2005. Koike T., Wada H., Kobayashi T.: Modeling of the human middle ear using finite-element method, J. Acoust. Soc. Am., 111, 1306-1317, 2002. Skrodzka E., Modáawska J.: Modal analysis of the human tympanic membrane of the middle ear using Finite-Element Method, Archives of Acoustics (in press), 2006. Bathe K.J.: Finite Element Procedures, Prentice Hall: New Jersey, 1996. NE/NASTRAN v.8.User`s Manual, Noran Engineering Inc: Los Alamitos, 2001. FEMAP v.8.1, User Guide, SDRC: Exton, 2001.
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