• 한국재료학회지
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• 제31권10호
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• pp.562-568
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• 2021

(Bi_1/2Na_1/2)TiO₃ (BNT)-based ceramics are considered promising candidates for actuator application owing to their excellent electromechanical strain properties However, to obtain large strain properties, there remain several issues such as thermal stability and high operating fields. Therefore, this study investigates a reduction of operating field in (0.98-x)Bi_1/2Na_1/2TiO₃-0.02 BiAlO₃-xSrTiO₃ (BNT-2BA-100xST, x = 0.20, 0.21, 0.22, 0.23, and 0.24) via analyses of the microstructure, crystal structure, dielectric, polarization, ferroelectric and electromechanical strain properties. The average grain size of BNT-${\underline{2}}$BA-100xST ceramics decreases with increasing ST content. Results of polarization and electromechanical strain properties indicate that a ferroelectric to relaxor state transition is induced by ST modification. As a consequence, a large electromechanical strain of 592 pm/V is obtained at a relatively low electric field of 4 kV/mm in 22 mol% ST-modified BNT-2BA ceramics. We believe that the materials synthesized in this study are promising candidates for actuator applications.

• 폴리머
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• 제27권3호
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• pp.195-200
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• 2003

알지네이트는 곁사슬에 강한 음이온을 가지고 있어 전기장 하에서 구동 특성을 발현할 수 있다. 본 연구에서는 가교제로 CaCl$_2$를 사용하여 가교 알지네이트 필름을 제조하였고, 제조된 필름의 열적 특성, 기계적 특성 및 전기적 구동 특성을 열중량 분석, 인장 강도 실험 및 전기응답 실험을 통하여 조사하였다. 가교제의 농도가 증가함에 따라 필름의 초기 분해 온도와 인장 강도가 증가하였다. 또한 팽윤비는 사슬 내 자유부피와 정전기적 반발력에 기인하여 가교제 농도의 감소와 pH가 증가함에 따라 증가하였다. 저기 자극에 의하여 알지네이트 필름은 유연한 물리적 거동을 발현하였다. 전기장에서 전압, 이온 강도 및 저해질 용액의 종류에 따라서 필름의 응답 속도 띤 거동에 영향을 주었다. 가교제의 농도가 5 wt%일 때 가장 좋은 굽힘 거동과 반복 회복성을 보였으며, NaCl과 KCl 전해질 용액의 이온 강도가 0.1 M일 때 가장 높은 전기 반응성을 나타냈다. 또한 전압이 증가됨에 따라 전하의 이동이 활발해지고 따라서 굽힘 거동이 증가하였다.

• Advances in aircraft and spacecraft science
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• 제4권5호
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• pp.503-514
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• 2017

The attitude control of an aircraft is usually fulfilled by means of thrusters at high altitudes. Therefore, the possibility of using also aerodynamic surfaces would produce the advantage of reducing the amount of fuel for the thrusters to be loaded on board. For this purpose, Zuppardi already considered some aerodynamic problems linked to the use of a wing flap in a previous paper. A NACA 0010 airfoil with a trailing edge flap of 35% of the chord, in the range of angle of attack 0-40 deg and flap deflections up to 30 deg was investigated. Computer tests were carried out in hypersonic, rarefied flow by a direct simulation Monte Carlo code at the altitudes of 65 and 85 km of Earth Atmosphere. The present work continues this subject, considering the same airfoil and free stream conditions but two flap extensions of 45% and 25% of the chord and two flap deflections of 15 and 30 deg. The main purpose is to compare the influence of the flap dimension with that of the flap deflection. The present analysis is carried out in terms of: 1) percentage variation of the global aerodynamic coefficients with respect to the no-flap configuration, 2) increment of pressure and heat flux on the airfoil lower surface due to the Shock Wave-Shock Wave Interaction (SWSWI) with respect to the same quantities with no SWSWI or in no-flap configuration, 3) flap hinge moment. Issues 2) and 3) are important for the design of the mechanical and thermal protection system and of the flap actuator, respectively. Under the above mentioned test and geometrical conditions, the flap deflection is aerodynamically more effective than the flap extension, because it involves higher variation of the aerodynamic coefficients. However, tests verify that a smaller deflection angle involves the advantage of a smaller increment of pressure and heat flux on the airfoil lower surface, due to SWSWI, as well as a smaller hinge moment.

• 제어로봇시스템학회:학술대회논문집
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• 제어로봇시스템학회 2005년도 ICCAS
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• pp.1048-1053
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• 2005

This paper presents design and integration of the ROBHAZ-DT3, which is a newly developed mobile robot system with chained double-track mechanisms. A passive adaptation mechanism equipped between the front and rear body enables the ROBHAZ-DT3 to have good adaptability to uneven terrains including stairs. The passive adaptation mechanism reduces energy consumption when moving on uneven terrain as well as its simplicity in design and remote control, since no actuator is necessary for adaptation. Based on this novel mobile platform, a rescue version of the ROBHAZ-DT3 with appropriate sensors and a semi-autonomous mapping and localization algorithm is developed to participate in the RoboCup2004 US-Open: Urban Search and Rescue Competition. From the various experiments in the realistic rescue arena, we can verify that the ROBHAZ-DT3 is reliable in traveling rugged terrain and the proposed mapping and localization algorithm are effective in the unstructured environment with uneven ground. The another application is an military robot for an EOD(Explosive Ordnance Disposal) and reconnaissance mission. The military version of the ROBHAZ-DT3 with a water disrupter, a thermal scope and a long distance wireless communication device is developed and sent to the area of military tactics in Iraq. Consequently, the feasibility of the military version of ROBHAZ-DT3 is verified.

• 한국항공우주학회지
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• 제38권8호
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• pp.767-773
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• 2010

본 논문에서는 위성 본체에 장착된 탑제체를 위성으로부터 분리하기 위한 비폭발식 분리 메커니즘을 제안하였다. 작동기로서 경제적이고 신뢰성 있는 유성기어가 통합된 소형 직류모터를 채택하였다. 제안된 분리장치는 별도의 지그나 구조물 없이도 재장전이 용이 하도록 하였으며, 단순한 구조로 제작이 수월한 장점이 있다. 완성된 분리장치는 분리반응속도 측정시험, 최대분리가능하중 측정 시험, 최대발생충격 측정 시험을 통하여 그 성능을 입증하였고, 진동시험, 열진공 시험을 통하여 우주 환경에서 사용 가능함을 보여주었다. 개발된 인공위성용 비폭발식 분리장치를 통하여 그동안 사용되었던 폭발식 분리장치 등의 해외위성용 분리장치를 대체 할 수 있을 것으로 기대된다.

• Smart Structures and Systems
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• 제18권1호
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• pp.139-154
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• 2016

This paper is concerned with the dynamics of hyperelastic solids and structures. We seek for a smart control actuation that produces a desired (prescribed) displacement field in the presence of transient imposed forces. In the literature, this problem is denoted as displacement tracking, or also as shape morphing problem. One talks about shape control, when the displacements to be tracked do vanish. In the present paper, it is assumed that the control actuation is provided by imposed eigenstrains, e.g., by the electric field in piezoelectric actuators, or by thermal actuators, or via analogous physical effects, such as magneto-striction or pre-stress. Structures with a controlled eigenstrain-type actuation belong to the class of smart structures. The action of the eigenstrains can be conveniently characterized by actuation stresses. Our theoretical derivations are performed in the framework of the theory of small incremental dynamic deformations superimposed upon a statically pre-deformed configuration of a hyperelastic solid or structure. We particularly ask for a distribution of incremental actuation stresses, such that the incremental displacements follow exactly a prescribed trajectory field, despite the imposed incremental forces are present. An exact solution of this problem is presented under the assumption that the actuation stresses can be tailored freely and applied everywhere within the body. Extending a Neumann-type solution strategy, it is shown that the actuation stresses due to the distributed control eigenstrains must satisfy certain quasi-static equilibrium conditions, where auxiliary body-forces and auxiliary surface tractions are to be taken into account. The latter auxiliary loading can be directly computed from the imposed forces and from the desired displacement field to be tracked. Hence, despite the problem is a dynamic one, a straightforward computation of proper actuator distributions can be obtained in the framework of quasi-static equilibrium conditions. Necessary conditions for the functioning of this concept are presented. Particularly, it must be required that the intermediate configuration is infinitesimally superstable. Previous results of our group for the case of shape control and displacement tracking in linear elastic structures are included as special cases. The high potential of the solution is demonstrated via Finite Element computations for an irregularly shaped four-corner plate in a state of plain strain.

• 한국전기전자재료학회논문지
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• 제29권12호
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• pp.769-775
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• 2016

Characteristics of a wireless sensor powered by the IDE (interdigitated electrode) embedded piezoelectric cantilever generator were analyzed in order to evaluate its potential for use in wireless sensor applications. The IDE embedded piezoelectric cantilever was designed and fabricated to have a self-resonance frequency of 126 Hz and acceleration of 1.57 G, respectively, for the mechanical resonance with a practical conveyor system in a thermal-power plant. It produced maximum output power of 2.81 mW under the resistive load of $160{\Omega}$ at 126 Hz. The wireless sensor module is electrically connected to a rectifier capacitor with capacity of 0.68 farad and 3.8 V for power supply by the piezoelectric cantilever generator. The unloaded capacitor could be charged as a rate of approximately $365{\mu}V/s$ while the capacitor exhibited that of 0.997 mV/min. during communication under low duty cycle of 0.2%. Therefore, it is considered that the fabricated IDE embedded piezoelectric cantilever generator can be used for wireless sensor applications.

• 항공우주시스템공학회지
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• 제16권6호
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• pp.123-128
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• 2022

본 연구는 전개형 SAR 안테나에 적용하기 위한 비폭발 분리장치를 제안하였다. Ni-Cr 와이어를 감아 제작된 분리장치를 이용하여 SAR 안테나의 벨트가 전개되지 않도록 구속한다. 분리 장치를 구속하는 Ni-Cr 와이어는 발열을 통해 절단함으로써 벨트 전개 시 충격량을 최소화한다. 분리장치의 설계를 위해 설계하중(99g)과 preload를 고려하여 AL과 Ti을 대상으로 유한요소 해석을 수행하였다. AL을 이용 시 해석결과, 최대 변형량이 0.256 mm 발생하였고, 안전마진은 +0.09로 확인되었다. 또한 궤도상 열분석을 수행하여 온도분포를 확인한 결과, 최저온 궤도와 최고온 궤도에서 -50~+2℃의 온도분포와 -10~+90℃의 온도분포를 각각 나타내어 우주환경에서도 구속분리장치가 안정적임을 입증하였다.

• 한국화재소방학회논문지
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• 제31권3호
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• pp.63-72
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• 2017

본 논문에서는 저압용 10회로 분전반을 전기공업협동조합(KEMC) 2102-610 규정에 근거하여 제작하였다. 또한, 개발된 10회로 분전반의 특성 평가를 실시하여 안전성을 확보하고자 한다. 개발된 10회로 분전반은 내식성, 절연 재료의 특성, 자외선 복사의 내성, 기계적 충격 등에 적합하도록 설계되었다. 개발된 분전반은 외함의 보호 등급, 감전방지와 보호회로, 개폐 장치와 구성품, 내부 전기 회로와 연결부, 외부 도체의 단자, 절연 특성, 온도 상승 시험, 열저항 등이 적합하도록 제작하였다. 개발된 10회로 분전반은 단상 회로와 3상 회로 등으로 구분되어 있다. 분기된 각각의 차단기 부하측에 센서 모듈을 설치하여 부하의 전선로에서 발생되는 누설전류의 크기를 실시간 측정할 수 있다. 그리고 부하의 용도 및 목적 등에 따라 회로를 증설할 수 있고, 각각의 부하 상태 역시 실시간 부하 관리 및 점검이 가능하다. 개발된 10회로 분전반의 온도 상승 시험을 실시한 곳은 인입 접속부, 주회로 및 분기회로 모선, 모선지지물 등 18 개소이다. 온도가 가장 높게 측정된 곳은 분기회로 모선용 MCCB 전원측 접속부의 R-phase으로 $65.3^{\circ}C$, 부하측은 T-phase으로 $61.6^{\circ}C$로 기록되었다. 그리고 내열 실험 장치를 이용하여 MCCB를 $180^{\circ}C$에서 6시간 동안 열적 스트레스를 인가하였을 때 작동 손잡이의 변형이 확인되었고, 트립 상태로 이동한 것이 확인되었다.

• 한국정밀공학회:학술대회논문집
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• 한국정밀공학회 2005년도 춘계학술대회 논문집
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• pp.1883-1886
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• 2005

In this paper, a decoupled dual servo (DDS) stage for ultra-precision scanning system with large working range is introduced. In general, dual servo systems consist of a fine stage for short range and a coarse stage for long range. The proposed DDS also consists of a $XY\theta$ fine stage for handling and carrying workpieces and one axis coarse stage. Its coarse stage consists of air bearing guide system and a coreless linear motor with force ripple. The fine has four voice coil motors(VCM) as its actuator. According to a VCM's nature, there are no mechanical connections between coils and magnetic circuits. Moreover, VCM doesn't have force ripples due to imperfections of commutation components of linear motor systems - currents and flux densities. However, due to the VCM's mechanical constraints the working range of the fine is about $25mm^2$. To break that hurdle, the coarse stage with linear motors is used to move the fine about 500mm. Because of the above reasons, the proposed DDS can achieve higher precision scanning than other stages with only one servo. With MATLAB's Sequential Quadratic Programming (SQP), the VCMs are optimally designed for the highest force under conditions and constraints such as thermal dissipations due to its coil, its size, and so on. And for their movements without any frictions, guide systems of the DDS are composed of air bearings. To get precisely their positions, a linear scale with 5nm resolution are used for the coarse stage's motion and three plane mirror laser interferometers with 5nm for the fine's $XY\theta$ motions. With them, on scanning the two stages have same trajectories. The control algorithm is named Parallel method. The embodied ultra-precision scanning system has sub 100nm following error and in-positioning stability.