• Title/Summary/Keyword: SMA 형상기억합금

Search Result 175, Processing Time 0.025 seconds

Micro-vibration Isolation Performance Verification for the Passive Vibration Isolator using SMA Mesh Washer (SMA 메쉬 와셔를 적용한 수동형 진동절연기의 미소진동 절연성능 검증)

  • Kwon, Sung-Cheol;Jeon, Su-Hyeon;Oh, Hyun-Ung
    • Proceedings of the Korean Society for Noise and Vibration Engineering Conference
    • /
    • 2014.10a
    • /
    • pp.900-903
    • /
    • 2014
  • Fly-wheel, Gimbal antenna, CMG, Spaceborne cyrocooler generate micro-vibration during their on-orbit operation as well as implementing their own function. To comply with the mission requirement of high resolution observation satellite, additional technical efforts have been required to isolate the micro-vibration derived from such payloads by applying the vibration isolator. In this study, we proposed a passive isolator using SMA mesh washer, which guarantees the structural safety of both micro-vibration disturbance source and itself under harsh launch vibration loads without an additional holding mechanism and the micro-vibration isolation performance on orbit environment. To verify the micro-vibration isolation performance of the proposed vibration isolator, we performed the micro-vibration isolation measurement test using the dedicated micro-vibration measurement device proposed in this study.

  • PDF

Design of HDD Load/Unload Suspension Using Shape Memory Alloy (형상기억합금을 이용한 HDD Load/Unload 서스펜션의 설계)

  • Lim S. C.;Park Y. P.;Park N, C.;Choi S, B.
    • 정보저장시스템학회:학술대회논문집
    • /
    • 2005.10a
    • /
    • pp.163-170
    • /
    • 2005
  • In this work, we propose a new type of HDD Load/unload (L/UL) suspension featuring shape memory alloy (SMA). The mechanical and thermal properties of the SMA film with respect to the material phase states are experimentally estimated and the SMA film is carefully integrated to the suspension. In order to obtain the desirable dynamic characteristics of the suspension during L/UL process, the design parameters of the SMA film such as geometric properties are determined by considering the vibration modes of the suspension related to the L/UL performance. After analyzing the modal characteristics of the proposed suspension, L/UL performance is evaluated through L/UL simulation by observing the vibration motion and minimum flying height of the slider during L/UL process.

  • PDF

Grain Size Refinement in CuAlNi Shape Memory Alloy using Melt-spun Ribbon (급냉응고된 Ribbon을 이용한 CuAINi 형상기억합금의 결정미세화)

  • Choe, Yeong-Taek
    • 연구논문집
    • /
    • s.22
    • /
    • pp.127-139
    • /
    • 1992
  • The mechnial properties such as fracture strength, ductility and fatigue strength of Cu shape memory alloy are lower than those of Ti-Ni SMA, because of their high elastic anisotropy and large grain size. And in order to improve the mechanical property of Cu SMA, some techniques such as casting method by addition of refining element, powder metallurgy and rapid solidification process have been studied on the refinement of the grain size of Cu SMA. This study was carried out to refine the grain size of CuAlNi SMA by applying the melt spinning method. According to this study, the conclusions are as follows; - grain size of the melt-spun ribbon was about $1\mum$ - there was not change in grain size, although increasing of hot pressing temperature -grain size of the hot-extruded specimen was about $30-40\mum$, it is more refiner than that of castings

  • PDF

Design of HDD Load/Unload Suspension Using Shape Memory Alloy (형상기억합금을 이용한 HDD Load/Unload 서스펜션의 설계)

  • Lim, Soo-Cheol;Park, Young-Pil;Park, No-Cheol;Choi, Seung-Bok
    • Transactions of the Society of Information Storage Systems
    • /
    • v.2 no.1
    • /
    • pp.71-78
    • /
    • 2006
  • In this work, we propose a new type of HDD Load/Unload(L/UL) suspension featuring shape memory alloy(SMA). The mechanical and thermal properties of the SMA film with respect to the material phase states are experimentally estimated and the SMA film is carefully integrated to the suspension. In order to obtain the desirable dynamic characteristics of the suspension during L/UL process, the design parameters of the SMA film such as geometric properties are determined by considering the vibration modes of the suspension related to the L/UL performance. After analyzing the modal characteristics of the proposed suspension, L/UL performance is evaluated through L/UL simulation by observing the vibration motion and minimum flying height of the slider during L/UL process.

  • PDF

AE Characteristics on the Damage Behavior of TiNi/A16061 Shape Memory Alloy Composites at High Temperature (TiNi/A16061 형상기억복합재료의 고온에서의 손상거동에 대한 AE 특성)

  • Lee, Jin-Kyung;Park, Young-Chul;Ku, Hoo-Taek
    • Journal of the Korean Society for Nondestructive Testing
    • /
    • v.22 no.1
    • /
    • pp.45-52
    • /
    • 2002
  • It has been known that tensile residual stresses occurring by the thermal expansion coefficient mismatch between fiber and matrix is a cause of the weak strength of metal matrix composites(MMCs). In order to solve this problem, TiNi alloy fiber was used as a reinforced material in TiNi/A16001 shape memory alloy composite in this study. TiNi alloy fiber improves the tensile strength of the composite by causing compressive residual stress in matrix on the basis of its shape memory effect. Pre-strain was imposed to generate the compressive residual stresses inside the TiNi/A16001 shape memory alloy composites. AE technique was used to quantify the microscopic damage behavior of the composite at high temperature. The effect of applied pre-strains on the AE behavior was also evaluated.

The Evaluation of Mechanical Properties of TiNi/Al 6061 Shape Memory Composites by Using Experimental and Finite Element Analysis (TiNi/Al 6061 형상기억복합재료의 기계적특성에 관한 실험 및 해석적 평가)

  • 박동성;박영철;이동화;이규창
    • Proceedings of the Korean Society of Precision Engineering Conference
    • /
    • 2001.04a
    • /
    • pp.687-691
    • /
    • 2001
  • Al alloy matrix composite with TiNi shape memory fiber as reinforcement has been fabricated by hot pressing to investigate mechanical properties. The stress-strain behavior of the composites was evaluated at temperatures between 363K and room temperature as a function of pre-strain by using experimental and finite element analysis, and both cases showed that the tensile stress at 363K was higher than that of the room temperature. Especially, the tensile stress of this composite increases with increasing the amount of pre-strain, and it also depends on the volume fraction of fiber and heat treatment. The smartness of the composite is given due to the shape memory effect of the TiNi fiber which generates compressive residual stress in the matrix material when heated after being pre-strained.

  • PDF

Motion Control of Non-Contact Start/stop Hard Disk Drive Using Shape Memory Alloy Actuator (형상기억합금 작동기를 이용한 비접촉 시동 및 정지형 하드디스크 드라이브의 운동제어)

  • Im, Su-Cheol;Park, Jong-Seong;Choe, Seung-Bok;Park, Yeong-Pil
    • Transactions of the Korean Society of Mechanical Engineers A
    • /
    • v.26 no.1
    • /
    • pp.196-202
    • /
    • 2002
  • In this work, we propose a new type of HDD suspension featuring shape memory alloy (SMA) actuator in order to prevent the contact between the slider and disk. The principal design parameters are obtained from the modal analysis using finite element analysis, and then the dynamic model is established to formulate the control scheme for Non-Contact Start/stop mode drive. Subsequently, a robust H$\_$$\infty$/ control algorithm is designed by integrating experimentally-Obtained SMA actuator dynamics to the proposed HDD suspension system. The controller is empirically realized and control results for the load/unload profiles are presented in time domain. In addition, the contact signal between the slider and disk is measured by the electrical resistance method.

Seismic Behavior and Estimation for Base Isolator Bearings with Self-centering and Reinforcing Systems (자동복원 및 보강 시스템과 결합된 면진받침의 지진거동과 평가)

  • Hu, Jong Wan
    • KSCE Journal of Civil and Environmental Engineering Research
    • /
    • v.35 no.5
    • /
    • pp.1025-1037
    • /
    • 2015
  • Flexible base isolation bearings that separate superstructure from ground have been widely used in the construction field because they make a significant contribution to increasing the fundamental period of the structure, thereby decreasing response acceleration transmitted into the superstructure. However, the established bearing devices installed to uphold the whole building give rise to some problems involved with failure and collapse due to lack of the capacity as modern structures are getting more massive and higher. Therefore, this study suggests new isolation bearings assembled with additional restrainers enabled to reinforcing and recentering, and then evaluates their performance to withstand the seismic load. The superelastic shape memory alloy (SMA) bars are installed into the conventional lead-rubber bearing (LRB) devices in order to provide recentering forces. These new systems are modeled as component spring models for the purpose of conducting nonlinear dynamic analyses with near fault ground motion data. The LRB devices with steel bars are also designed and analyzed to compare their responses with those of new systems. After numerical analyses, ultimate strength, maximum displacement, permanent deformation, and recentering ratio are compared to each model with an aim to investigate which base isolation models are superior. It can be shown that LRB models with superelastic SMA bars are superior to other models compared to each other in terms of seismic resistance and recentering effect.

On-orbit Thermal Characteristic for Multilayered High Damping Yoke Structure Based on Superelastic Shape Memory Alloy for Passive Vibration Control of Solar Panels (태양전지판의 수동형 제진을 위한 초탄성 형상기억합금 기반 적층형 고댐핑 요크 구조의 궤도상 열적 특성 분석)

  • Min-Young Son;Jae-Hyeon Park;Bong-Geon Chae;Sung-Woo Park;Hyun-Ung Oh
    • Journal of Aerospace System Engineering
    • /
    • v.18 no.1
    • /
    • pp.1-10
    • /
    • 2024
  • In a previous study, a structure of a superplastic yoke consisting of a thin FR4 layer laminated with viscoelastic tape on both sides of a shape memory alloy (SMA) was proposed to reduce residual vibration generated by a deployable solar panel during high motion of a satellite. Damping properties of viscoelastic tapes will change with temperature, which can directly affect vibration reduction performance of the yoke. To check damping performance of the yoke at different temperatures, free damping tests were performed under various temperature conditions to identify the temperature range where the damping performance was maximized. Based on above temperature test results, this paper predicts temperature of the yoke through orbital thermal analysis so that the yoke can have effective damping performance even if it is exposed to an orbital thermal environment. In addition, the thermal design method was described so that the yoke could have optimal vibration reduction performance.

Fatigue Characterization of NiTiCu Shape Memory Alloys (NiTiCu 형상기억합금의 피로특성)

  • Han, Ji-Won;Park, Sung Bum
    • Journal of the Korean Society of Safety
    • /
    • v.29 no.4
    • /
    • pp.28-33
    • /
    • 2014
  • Recently, the actuator worked by the driving recovery-force of the thermo elastic martensitic transformation of shape memory alloys(SMA) has been studied. This paper presents a study on the fatigue life of shape memory alloy (SMA) actuators undergoing thermally induced martensitic phase transformation under various stress levels. shape memory recoverable stress and strain of Ti-44.5at.%Ni-8at.%Cu alloys were by means of constant temperature tensile tests. Differential scanning calorimetry (DSC) was employed in order to investigate the transformation characteristics of the alloy before the tests. the results were summarized as follows. The martensite inducing stress incerased with the increasing of the Cu-contents. The fatigue life decreased with the increasing of the test load and the Cu-content. The data acquired will be very useful during the design process of an SMA NiTiCu element as a functional part of an actuator.