• Title/Summary/Keyword: 스프링장치

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Three dimensional analysis of tooth movement using different types of maxillary molar distalization appliances (간접골성 고정원을 이용한 상악 구치부 원심이동 장치 종류에 따른 치아 이동 양상 평가)

  • Kim, Su-Jin;Chun, Youn-Sic;Jung, Sang-Hyuk;Park, Sun-Hyung
    • The korean journal of orthodontics
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    • v.38 no.6
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    • pp.376-387
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    • 2008
  • Objective: The purpose of this study was to compare the three dimensional changes of tooth movement using four different types of maxillary molar distalization appliances; pendulum appliance (PD), mini-implant supported pendulum appliance (MPD), stainless steel open coil spring (SP) and mini-implant supported stainless steel open coil spring (MSP). Methods: These experiments were performed using the Calorific $machine^{(R)}$ which can simulate dynamic tooth movement. Computed tomography (CT) images of the experimental model were taken before and after tooth movement in 1 mm thicknesses and reconstructed into a three dimensional model using V-works $4.0^{TM}$. These reconstructed images were superimposed using Rapidform $2004^{TM}$ and the direction and amount of tooth movement were measured. Results: The mean reciprocal anchor loss ratio at the first premolar was 17 - 19% for the PD and SP groups. The appliances using mini-implants (MPD or MSP) resulted in less anchorage loss (7 - 8%). On application of a pendulum appliance or MPD, distalization was obtained by tipping rather than by bodily movement. Furthermore, the maxillary second molar tipped distally and bucally. But on application of MSP, distalization was achieved almost by bodily movement. Conclusions: Regarding tooth movement patterns during molar distalization, stainless steel open coil spring with indirect skeletal anchorage was relatively superior to other methods.

Shape Memory Alloy Actuator and Spiral Spring Based Separation Actuator for Small Satellite (형상기억합금구동기와 태엽스프링을 이용한 소형위성용 분리장치)

  • Lee, Min-Hyoung;Son, Jae-Hwang;Kim, Young-Woong;Kim, Byung-Kyu
    • Journal of the Korean Society for Aviation and Aeronautics
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    • v.19 no.3
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    • pp.10-15
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    • 2011
  • The separation actuator for the small satellite should fix satellite appendages with high clamping force. After operation, it has to be separated from the satellite body without any damage on satellite system and release the appendages such as a solar panel and an antenna successfully. Therefore, we invent a non-explosive separation actuator for the small satellite which generates low shock and is resettable. In order to confirm performance of the proposed separation actuator, we carried out experiments for separation time, maximum preload for activation, and shock level.

Development of Composite Tape-Springs for Deployable Structures (전개장치용 복합재료 테이프 스프링 개발)

  • Kim, Yeong-Bae;Jung, Geunsung;Kim, Do-won;Choi, Han-Sol;Lim, Jae Hyuk
    • Composites Research
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    • v.34 no.4
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    • pp.226-232
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    • 2021
  • In this paper, development of tape-springs made of composite materials was conducted for the deployment structures along with design, analysis, fabrication, and numerical and experimental investigation of mechanical behavior of the tape-springs. To this end, the tape-springs were manufactured according to three stacking patterns, and numerical and experimental investigation were conducted to determine whether or not they were damaged during bending with various selected composite materials. Finally, optimal stacking patterns that do not cause damage were selected during bending. With this information, the four-point bending test was conducted to obtain the moment-rotation curves. From results, it was confirmed that the nonlinear hysteresis phenomenon of the tape-springs was properly realized according to folding and unfolding. Therefore, it was confirmed that the composite material tape spring was properly developed.

Hybrid Damper of Steel Strip and Spring (강재 스트립과 스프링의 혼합형 댐퍼)

  • Kim, Dong-Baek;Lee, In-Duk;Lee, Jae-Won;Kim, Jong-Hoon
    • Proceedings of the Korean Society of Disaster Information Conference
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    • 2022.10a
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    • pp.299-300
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    • 2022
  • 구조물의 내진보강방법 중에서 가장 널리 이용되는 방법인 강재 이력형 감쇠장치는 수평하중에 대한 응력-변위 곡선을 이용하여 지진 에너지를 소산시키는 방법인데, 이 경우 편심하중 등에 의해서 부재가 면 외 방향으로 거동하여 응력-변위곡선이 불규칙하여 그 결과의 신뢰성이 떨어지는 경우가 있다. 이러한 형상을 방지하기 위해서는 별도의 채널(Channel)을 시공하는 불편함을 감수해야 하며, 또한 수평력이 반복적으로 작용할 때 그 효과를 장담할 수 없는 문제점이 있다. 본 연구에서는 강재 스트립과 스프링을 결합한 댐퍼를 고안하여 스프링은 탄성변형을, 강재 스트립은 소성변형을 받게 하는 혼합형 댐퍼를 개발하고자한다. 여기서, 스프링은 복원력으로 작용하여 반복하중에 대한 저항성을 키우고 강재 스트립의 하중변위 곡선을 규칙적으로 하는 역할을 수행하게 되며 에너지 소산량을 계산할 때 편리함과 정확도를 높이고자 한다. 강재 스트립의 폭과 길이는 일정하지만 두께를 변화시켜서 5종류를 선택하였으며, 댐퍼 1개당 3개의 스트립을 정삼각형 형태로 배치하고 그 중심에 상당한 강성을 갖는 스프링을 갖는 형태로 제작하였다. 댐퍼 시험체는 5개를 제작한 후, 이 댐퍼를 구조물에 배치하였을 때의 지진에 대한 에너지 소산량과 부재력을 검토하여 댐퍼의 안전성(Safety)를 검증하고자 한다.

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Effects of the Design Parameters of Suspension Systems on the Bounce of Electric Trains (전동차 상하진동에 대한 현가장치 설계변수의 영향)

  • Park, Ki-Soo;Choi, Yeon-Sun
    • Journal of the Korean Society for Railway
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    • v.11 no.1
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    • pp.39-44
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    • 2008
  • A two degree-of-freedom model for the bogie and car body of an EMU(Electrical Multiple Unit) was implemented on the basis of the experimental data which was actually measured during the running test of an EMU. The air spring of the EMU was modeled using Nishimura's air spring model to accommodate viscoelastic characteristics. Numerical simulation for the variation of th e design parameters of the suspension system shows that reduction of the stiffness of the air spring by decreasing the internal pressure of the air tank or increasing the size of the auxiliary tank can reduce the bounce of the car body within the stability range of the suspension system.

신자재: 방진 및 내진용 배관 고정장치 개발 - 주헌건설(주)

  • 대한설비건설협회
    • 월간 기계설비
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    • s.247
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    • pp.58-59
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    • 2011
  • 주헌건설(주)은 지난해 6월 자체 개발한 내진 스프링가대가 특허(제10-0962993호)를 획득함에 따라 본격생산에 들어갔다. 내진 스프링가대는 펌프 등 실비기기의 자체진동을 방지하고 지진 발생시 충격을 흡수해 산재사고 예방 및 내진 안전성을 확보하는 장치이다. 이 제품은 지난 2010년 10월 "제4차 UN 재해위험 경감을 위한 아시아 각료회의"의 부대행사로 열린 재해경감 방재산업전에 출품해 호평을 받았다. 또한 배관의 신축 팽창을 자체 흡수하고 각종 슈 대신 절연 유볼트로 시공하므로 원가절감 효과가 있으며 타 공정과의 간섭 없이 시공할 수 있는 장점이 있다.

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Study on Damping Coefficient of Shock Absorber with Magnetic Effects (자기효과를 이용한 충격흡수장치의 감쇠계수에 관한 연구)

  • Yi, Mi-Seon;Bae, Jae-Sung;Hwang, Jae-Hyuk;Hwang, Do-Sun
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.39 no.9
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    • pp.832-838
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    • 2011
  • The shock absorber with magnetic effect is suggested for a lunar lander. The shock absorber consists of a metal tube, a piston rod, and several permanent magnets moved by a piston rod in the tube, and the shock energy can be dispersed and dissipated by magnetic effects such as the magnetic force existed between a metal and magnets and the eddy current effect generated by a relative motion with a conductor and magnets. Besides, the shock-absorbing effect similar to that of a coil spring can be obtained by arranging the magnets in line, which are facing the same polar each other. The device has a very simple structure and is usable in space due to the unnecessariness of any oil or gas. The shock absorber was designed and manufactured for experiments and its spring and damping characteristics were studied by the theoretical, analytical and experimental methods.

A Study on Design Method of the Cylindrical-Taper Section Coil Spring (등반경-테이퍼 소재 비선형 특성의 코일 스프링 설계 방법 연구)

  • 권혁홍;최선준
    • Journal of the Korean Society for Precision Engineering
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    • v.15 no.9
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    • pp.175-181
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    • 1998
  • The coil spring is used in the suspension of automotive vehicles and small omnibus. Recently, it can be adopted hardening type spring which spring constant is accompanied by increasing displacement to increase passenger comfortability. One of methods which assert this characteristic is cylindrical-taper section coil spring. In this paper we calculate ideal spring characteristic curve from the given vehicle conditions, and show the design method of the cylindrical-taper section coil spring.

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Analysis of rear suspension using airspring (공기스프링 현가장치 성능해석)

  • Tak, tae-oh;Kim, kum-Chul
    • Journal of Industrial Technology
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    • v.19
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    • pp.31-42
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    • 1999
  • This paper presents a method for evaluating the performance of a leaf spring suspension and an air spring suspension systems for trucks in terms of ride and handling. Leaf springs, which generally have non-linear progressive force-deflection characteristics, are modeled using beam and contact elements. The leaf spring analysis model shows good correlation with experimental results. Each component of an air spring suspension system, which is a single leaf, air spring, height control valve, compressor and linkages, is modeled appropriately. Non-linear characteristics of air spring are accounted for using the measured data, and pressure and volume relations for height control system is also considered. The wheel rate of the air suspension is taken lower but roll stiffness is taken higher than those of leaf springs to improve ride and handling performance, which is verified through driving simulations.

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