• 한국소음진동공학회:학술대회논문집
• /
• 한국소음진동공학회 2002년도 추계학술대회논문집
• /
• pp.705-710
• /
• 2002

Magnetostrictive materials are used low frequency sonar transmitter instead of piezoelectric materials. But it is difficult to analyze due to the nonlinearity and hysteresis of magnetostrictive materials. This paper deals with the program development for the finite element modeling of magnetostrictive tonpilz transducers and for analyzing their acoustic characteristics. To take into account the nonlinearity of magnetostrictive materials, the magnetic field calculation is separated form the displacement calculation, and a curve fitting is adopted for the nonlinear behavior of the magnetic and mechanical strain fields. At first, the magnetic field is obtained by using a commercial FEM software and the displacement of the transducer is calculated by plugging the obtained magnetic field into forcing term. To verity the accuracy of the developed program, a comparison is made with a commercial code, ATILA.

• 한국소음진동공학회:학술대회논문집
• /
• 한국소음진동공학회 2004년도 춘계학술대회논문집
• /
• pp.568-574
• /
• 2004

On-line phase tracking of an extrinsic Fabry-Perot interferometer (EFPI) and experimental vibration control of a composite beam with a sensing-patch are investigated. We propose a sensing-patch for the compensation of the interferometric non-linearity. In this paper, a sensing-patch that comprises an EFPI and a piezo ceramic(PZT) is fabricated and the characteristics of the sensing-patch are experimentally investigated. A simple and practical logic is applied for the real-time tracking of optical phase of an interferometer. Experimental results show that the proposed sensing-patch does not have the non-linear behavior of conventional EFPI and hysteresis of piezoelectric material. Moreover, it has good strain resolution and wide dynamic sensing range. Finally, the vibration control with the developed sensing-patch has been performed using Fuzzy logic controller, and the possibility of sensing-patch as a sensoriactuator is considered.

• 한국정밀공학회지
• /
• 제23권4호
• /
• pp.139-145
• /
• 2006

This paper presents the design and manufacturing of a sensor using SAW and delay line in order to measure temperature. SAW sensors having single and double electrodes are manufactured on the $128^{\circ}YX-LiNbO_3$ substrate, and its process is addressed. Before manufacturing, the device is simulated using a commercial finite element program. The frequency responses of the saw sensor on the temperature change is measured. Since the center frequency on the temperature change from $-30^{\circ}C$ to $80^{\circ}C$ is linearly changed, the saw sensor is applicable to measure the temperature change or strain variation.

• 한국전기전자재료학회:학술대회논문집
• /
• 한국전기전자재료학회 2003년도 춘계학술대회 논문집 디스플레이 광소자분야
• /
• pp.96-99
• /
• 2003

본 논문에서는 수치 해석 방법을 이용하여 $In_{x}Ga_{1-x}N/GaN$ (x=0.06~0.1) 양자우물 구조의 에너지 준위를 계산하였다. InGaN 벌크 샘플(bulk sample)의 PL(photoluminescence) 데이터로부터 bowing factor를 결정한 후 InGaN의 유효 에너지 밴드갭을 계산하였고, InGaN/GaN 양자우물 구조의 전도대와 가전자대의 오프셋(offset)을 0.67/0.33으로 정하였다. 다음으로, 양자화 효과에 의한 에너지 변위와 압전장(piezoelectric field)을 제외한 양축 압축 변형(biaxial compressive strain)에 의한 에너지 변위를 고려하여 기저준위 전자와 heavy hole(le-1hh)간의 천이 에너지를 계산하였다. 계산된 천이 에너지는 PL로 측정한 천이 에너지에 비해 약 9~15 meV 크게 관찰되었는데, 이것은 InGaN/GaN 양자우물 계면에 발생하는 압전장 때문인 것으로 생각된다.

• Transactions on Electrical and Electronic Materials
• /
• 제6권1호
• /
• pp.6-9
• /
• 2005

Aging characteristics of 0.2PMN-0.8PZT multilayer ceramic actuators (MCA) has been investigated by applying both triangular wave function for unpoled and unipolar wave for poling. P-E hysteresis loops of the MCA had been distorted after about 90 million cycles running in triangular wave function. Effective electromechanical coupling coefficient was calculated in resonant and anti resonant frequencies. And pseudo-piezoelectric constant $d_{33}$ was also estimated from the strain versus electric field characteristics. The crack growth of MCA was clearly observed along to the boundary between electrode and inactive area. That results were thought due to the internal tensile stress came from both actuation of $d_{33}$ mode and motion of Poisson ratio.

• 한국소음진동공학회:학술대회논문집
• /
• 한국소음진동공학회 2011년도 추계학술대회 논문집
• /
• pp.236-241
• /
• 2011

An active trailing-edge flap blade named as Seoul National University Flap (SNUF) blade is designed for reducing helicopter vibratory loads and the relevant aeroacoustic noise. Unlike the conventional rotor control, which is restricted to 1/rev frequency, an active control device like the present trailing-edge flap is capable of actuating each individual blade at higher harmonic frequencies i.e., higher harmonic control (HHC) of rotor. The proposed blade is a small scale blade and rotates at higher RPM. The flap actuation components are located inside the blade and additional structures are included for reinforcement. Initially, the blade cross-section design is determined. The aerodynamic loads are predicted using a comprehensive rotorcraft analysis code. The structural integrity of the active blade is verified using a stress-strain recovery analysis.

• 한국전기전자재료학회:학술대회논문집
• /
• 한국전기전자재료학회 1998년도 춘계학술대회 논문집
• /
• pp.33-36
• /
• 1998

This paper is a study on a linear ultrasonic motor with a first longitudinal$(L_1)$ and fourth bending $(B_4)$ double-mode rectangular plate. The stator vibrator is composed of an elastic material plate and of a piezo-ceramic element having a motion by electrical excitation. Each strain vector differs by $90^{\circ}$ generate travelling wave with the elliptical displacement motion of a point on the surface. To magnify displacement of longitudinal direction in elliptical displacement motion, the motor has a mechanism of the.displacement enlargement. In this paper, the vibration shape of the stator is simulated using the finite element method. A detailed model considered of the piezoelectric effect and of the exact geometry of the stator is used to calculate the displacement. The position of displacement mechanism is decided by the maximum displacement.

• 대한전기학회논문지
• /
• 제43권4호
• /
• pp.620-626
• /
• 1994

As the electrostrictive actuator for optic control, PZN-BT-PT ceramics were investigated for the influences of sintering conditions on the structural, electrostrictive properties and the optical properties of Fabry-perot Interferometer using eletrostrictive ceramics. The specimen SS15T, sintered 1hr at 1150$^{\circ}C$, is sutible for eletrostrictive actuator because its piezoelectric constants(dS131T) and strain(XS131T) at dc 10kV/cm had the higest value of 175${\times}$10S0-12TC/N, -255${\times}$10S0-6TΔl/l respectively. As the dc electric field increased, the interference effect of Fabry-Perot Interferometer was increased. The most intense interference fringe and the maximum power of 160${\mu}$W were observed at dc 6kV/cm. Thus it was considered that specimen SS15T could be used as the electrostrictive actuator for optic control.

• 한국통신학회논문지
• /
• 제17권10호
• /
• pp.1092-1099
• /
• 1992

본 논문은 광섬유 가속도기를 이용한 중력가속도$(0{\sim}1G)$의 감도를 보였다. 단일모드 광섬유 Mach-Zehnder 간섭계가 약 1 그람 정도의 probe mass를 이용하여 광섬유 내의 스트레인에 의해 발생된 광로정 변화를 감지하는데 이용 되었다. 본 시스템의 기준 통로내 PZT 원통의 위상 변환 이득은 0.88rad./v로 측정 되었다.

• Structural Engineering and Mechanics
• /
• 제67권2호
• /
• pp.143-153
• /
• 2018

Thermal buckling of nonlocal flexoelectric nanoplates incorporating surface effects is analyzed for the first time. Coupling of strain gradients and electrical polarizations is introduced by flexoelectricity. It is assumed that flexoelectric nanoplate is subjected to uniform and linear temperature distributions. Long range interaction between atoms of nanoplate is modeled via nonlocal elasticity theory. The residual surface stresses which are usually neglected in modeling of flexoelectric nanoplates are incorporated into nonlocal elasticity to provide better understanding of the physic of problem. A Galerkin-based approach is implemented to solve the governing equations derived from Hamilton's principle are solved. The verification of obtained results is performed by comparing buckling loads of flexoelectric nanoplate with previous data. It is shown that buckling loads of flexoelectric nanoplate are significantly affected by thermal loading type, temperature change, nonlocal parameter, surface effect, plate thickness and boundary conditions.