The Rinne and Weber tests help distinguish between a conductive hearing loss (CHL) and sensorineural Hearing Loss (SHL).These tests should be carried out with a full examination of the cranial nerves or the ear.Patients with bilateral loss or mixed losses are better assessed with formal pure tone audiometry.They are most useful in patients with unilateral hearing loss which is purely conductive or purely sensorineural.The tuning fork tests provide a reliable clinical method for assessing hearing loss.How to do Rinne and Weber tuning fork tests for doctors, medical student finals, OSCEs and MRCP PACES 19(16), 3455 (2019)īukhari, S.A.R., Saleem, M.M., Hamza, A., Bazaz, S.A.: A novel design of high resolution MEMS gyroscope using mode-localization in weakly coupled resonators.Tuning Fork Tests (Rinne’s and Weber’s tests) Li, Z., Gao, S., Jin, L., Liu, H., Guan, Y., Peng, S.: Design and mechanical sensitivity analysis of a MEMS tuning fork gyroscope with an anchored leverage mechanism. Electronic, Dev (1993)Ĭao, L., Li, J., Liu, X., Sun, F.Y.: Research on an anchor point lever beam coupling type tuning fork micro-gyroscope. Gabrielson, T.G.: Mechanical-thermal noise in micromachined acoustic and vibration sensors. Masu, K., Machida, K., Yamane, D., Ito, H., Ishihara, N., Chang, T.-F.M., Sone, M., Shigeyama, R., Ogata, T., Miyake, Y.: (Invited) CMOS-MEMS based microgravity sensor and its application. Handtmann, M., Aigner, R., Meckes, A., Wachutka, G.K.M.: Sensitivity enhancement of MEMS inertial sensors using negative springs and active control. Petritoli, E., Leccese, F., Leccese, M.: Inertial navigation systems for UAV: Uncertainty and error measurements. ElsevierĮl-Sheimy, N., Youssef, A.: Inertial sensors technologies for navigation applications: state of the art and future trends. He, Q., Zeng, C., He, X., Xu, X., Lin, Z.: Measurement, undefined 2018, Calibrating accelerometers for space-stable inertial navigation systems at system level. Nusbaum, U., Rusnak, I., Klein, I.: Angular accelerometer-based inertial navigation system. Guan, Y., Gao, S., Jin, L., Cao, L.: Design and vibration sensitivity of a MEMS tuning fork gyroscope with anchored coupling mechanism. Zhou, X., Xiao, D., Wu, X., Wu, Y., Hou, Z., He, K., Li, Q.: Stiffness-mass decoupled silicon disk resonator for high resolution gyroscopic application with long decay time constant (8.695 s). Sonmezoglu, S., Alper, S., Akin, T.: An automatically mode-matched MEMS gyroscope with wide and tunable bandwidth. Park, B., Han, K., Lee, S., Yu, M.-J.: Analysis of compensation for a g-sensitivity scale-factor error for a MEMS vibratory gyroscope. Tatar, E., Mukherjee, T., Fedder, G.K.: Stress effects and compensation of bias drift in a MEMS vibratory-rate gyroscope. Prikhodko, I., Zotov, S., Trusov, A., Shkel, A.M.: Foucault pendulum on a chip: rate integrating silicon MEMS gyroscope. Guan, Y., Gao, S., Liu, H., Jin, L., Niu, S.: Design and vibration sensitivity analysis of a MEMS tuning fork gyroscope with an anchored diamond coupling mechanism. Yang, C., Li, H.: Digital control system for the MEMS tuning fork gyroscope based on synchronous integral demodulator. Nguyen, M.N., Ha, N.S., Nguyen, L.Q., Chu, H.M., Vu, H.N.: Z-axis micromachined tuning fork gyroscope with low air damping. Wu, J., Zhou, Z., Fourati, H., Cheng, Y.: A super fast attitude determination algorithm for consumer-level accelerometer and magnetometer. Pang, G., Liu, H.: Evaluation of a low-cost MEMS accelerometer for distance measurement. Ma, W., Lin, Y., Liu, S., Zheng, X., Jin, Z.: A novel oscillation control for MEMS vibratory gyroscopes using a modified electromechanical amplitude modulation technique. Passaro, V.M.N., Cuccovillo, A., Vaiani, L., De Carlo, M., Campanella, C.E.: Gyroscope technology and applications: a review in the industrial perspective. Söderkvist, J.: Micromachined gyroscopes. Xia, D., Yu, C., Sensors, L.K.: undefined,: the development of micromachined gyroscope structure and circuitry technology. Yazdi, N., Ayazi, F., Najafi, K.: Micromachined inertial sensors.
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