• 제목/요약/키워드: In-Flight Apparatus

검색결과 6건 처리시간 0.023초

원심모형실험을 위한 시공단계모사장비개발 (Development of Construction Simulation Apparatus on Centrifugal Experiment)

  • 김유석;김경오;이종필;박진우
    • 한국지반공학회:학술대회논문집
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    • 한국지반공학회 2010년도 추계 학술발표회
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    • pp.979-990
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    • 2010
  • Although a centrifuge model test is performed with scaled models, it has a lot of advantages compared with usual scale model tests, for the reproduction of stress levels equal to a full scale test is possible. At the beginning of the Daewoo Institute of Construction Technology, a servo-motor-driven single axis actuator was introduced and has been in use with a geo-centrifuge. However, for variety of experiments and construction stage simulation, various apparatuses have been developed, such as a vacuum generator, a lateral actuator for tidal power simulation, a gravel hopper and a sand drainer for filled-up ground, and a water level controller. The apparatuses have been manufactured with enough strength and durability to be operated under specific g levels. This paper presents the properties of the apparatuses and the results of the tests performed with those.

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A new laser pulse atom-probe 제작 및 $H_2$ 가스와 He 가스의 time-of-flight mass spectrum (An extension of new laser pulse atom-probe construction and time-of-flight mass spectrum of $H_2$ and He gas)

  • 송순달;홍남관
    • 한국결정성장학회지
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    • 제7권3호
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    • pp.465-472
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    • 1997
  • 본 연구는 전기 장에서 광여기 탈착과 이온화에 근거한 표면연구의 새로운 장치를 개발하고 시험한 결과를 보고한다. 실험장치의 분해능을 테스트 하기 위해 텡스텐(110)면에서 흡착기체 $H_2$ 와 He 가스를 조사하였으며, 팁의 온도는 80 K이었다. 장세기가 10 V/nm에서 50 V/nm사이에서 사용한 파장은 193 nm이였으며, 텡스텐(110)면에 가스가 흡착되었을때 레이저빔의 전자적인 여기로 부터 흡착가스와 팁에서 여러종류의 이온들이 형성되었다($H_2^+, CO^+, H_2O^+, He^+, W^{3+}$ 그리고 $W^{2+}$). 전체 mass spectrum의 기록은 Transient recorder가 가능하게 한다.

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Accuracy Analysis of Magnetic Resonance Angiography and Computed Tomography Angiography Using a Flow Experimental Model

  • Heo, Yeong-Cheol;Lee, Hae-Kag;Park, Cheol-Soo;Cho, Jae-Hwan
    • Journal of Magnetics
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    • 제20권1호
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    • pp.40-46
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    • 2015
  • This study investigated the accuracy of magnetic resonance angiography (MRA) and computed tomography angiography (CTA) in terms of reflecting the actual vascular length. Three-dimensional time of flight (3D TOF) MRA, 3D contrast-enhanced (CE) MRA, volume-rendering after CTA and maximum intensity projection were investigated using a flow model phantom with a diameter of 2.11 mm and area of $0.26cm^2$. 1.5 and 3.0 Tesla devices were used for 3D TOF MRA and 3D CE MRA. CTA was investigated using 16 and 64 channel CT scanners, and the images were transmitted and reconstructed by volume-rendering and maximum intensity projection, followed by conduit length measurement as described above. The smallest 3D TOF MRA measure was $2.51{\pm}0.12mm$ with a flow velocity of 40 cm/s using the 3.0 Tesla apparatus, and $2.57{\pm}0.07mm$ with a velocity of 71.5 cm/s using the 1.5 Tesla apparatus; both images were magnified from the actual measurement of 2.11 mm. The measurement with the 16 channel CT scanner was smaller ($3.83{\pm}0.37mm$) than the reconstructed image on maximum intensity projection. The images from CTA from examination apparatus and reconstruction technique were all larger than the actual measurement.

평행봉 Basket with 1/2 Turn to Handstand 기술 분석 (Kinematical Analysis of Basket with 1/2 Turn to Handstand on Parallel Bars)

  • 백진호;박종철;이용식
    • 한국운동역학회지
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    • 제17권1호
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    • pp.165-174
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    • 2007
  • The subject of this study was male apparatus gymnastics athlete who had scored high points doing basket with 1/2 turn on parallel bars. Then 3D motion analysis were used to calculate & analyse kinematic variables of Basket with 1/2 turn to Handstand. 1. The total average time spent for Basket with 1/2 turn took $2.16{\pm}.08sec$, at the downward upward phase took $.58{\pm}0.00sec$, $.23{\pm}.00sec$, at flight phase took $.28{\pm}.01sec$, at connected area phase took $.72{\pm}0.21sec$, at rotation area phase took $.35{\pm}.14sec$. To have a successful performance, there should be faster speed and velocity to rotate at the downward upward phase, then the upward velocity and height must be used adequately. Moreover, the speed must be faster at the flight connect phase to stabilize Center of Mass(CM) for the body, and must secure more time at the rotation area to have more stable performance. 2. After handstand on parallel bars while moving CM to right hand side, and It must be performed with big and magnificent performance with putting both hand's center to far away from the parallel bars. 3. Furthermore, CM must be moved fast from downwards to right hand side, and CM must be moved fast in vertical movement at upward and flight phase to avoid CM from moving back and forth, and left and right. 4. At downwards, the subject must rotate as bis as possible using hip-joint as wide as possible and at upwards, must put his body to vertical to have stable performance. While rotating or turning, it is better to do with bigger shoulder angle and have to make sure that trunk angle must be not scattered. To perform better and more positive in basket with 1/2 turn on parallel bars, the centrifugal force must be used big and fast at downward, and at upward and flight phase, downward movement must change to vertical movement as soon as possible while turning movement must happen at handstand position. Time spent must be shorten at connected area to stabilize CM and turning must be natural as possible while securing the necessary time of movement to well-balanced. Also, the body must be vertically closed from the ground.

광공진 현상을 이용한 입체 영상센서 및 신호처리 기법 (Optical Resonance-based Three Dimensional Sensing Device and its Signal Processing)

  • 박용화;유장우;박창영;윤희선
    • 한국소음진동공학회:학술대회논문집
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    • 한국소음진동공학회 2013년도 추계학술대회 논문집
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    • pp.763-764
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    • 2013
  • A three-dimensional image capturing device and its signal processing algorithm and apparatus are presented. Three dimensional information is one of emerging differentiators that provides consumers with more realistic and immersive experiences in user interface, game, 3D-virtual reality, and 3D display. It has the depth information of a scene together with conventional color image so that full-information of real life that human eyes experience can be captured, recorded and reproduced. 20 Mega-Hertz-switching high speed image shutter device for 3D image capturing and its application to system prototype are presented[1,2]. For 3D image capturing, the system utilizes Time-of-Flight (TOF) principle by means of 20MHz high-speed micro-optical image modulator, so called 'optical resonator'. The high speed image modulation is obtained using the electro-optic operation of the multi-layer stacked structure having diffractive mirrors and optical resonance cavity which maximizes the magnitude of optical modulation[3,4]. The optical resonator is specially designed and fabricated realizing low resistance-capacitance cell structures having small RC-time constant. The optical shutter is positioned in front of a standard high resolution CMOS image sensor and modulates the IR image reflected from the object to capture a depth image (Figure 1). Suggested novel optical resonator enables capturing of a full HD depth image with depth accuracy of mm-scale, which is the largest depth image resolution among the-state-of-the-arts, which have been limited up to VGA. The 3D camera prototype realizes color/depth concurrent sensing optical architecture to capture 14Mp color and full HD depth images, simultaneously (Figure 2,3). The resulting high definition color/depth image and its capturing device have crucial impact on 3D business eco-system in IT industry especially as 3D image sensing means in the fields of 3D camera, gesture recognition, user interface, and 3D display. This paper presents MEMS-based optical resonator design, fabrication, 3D camera system prototype and signal processing algorithms.

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열음향 피로 시험 장치를 이용한 티타늄 시편의 동적 거동에 관한 실험적 연구 (Experimental Study on Dynamic Behavior of a Titanium Specimen Using the Thermal-Acoustic Fatigue Apparatus)

  • 고은수;김문국;문영선;김인걸;박재상;김민성
    • 한국항공우주학회지
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    • 제48권2호
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    • pp.127-134
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    • 2020
  • 고초음속 항공기는 초음속 비행 중 공력 가열에 의하여 높은 온도 환경에 노출되기 때문에 동체 및 날개 구조물은 더블 패널 형태의 열 차폐 구조로 설계하여 기체 내부로 높은 온도의 열이 전달되는 것을 막는다. 얇은 두께의 더블 패널 외피는 초음속 항공기의 고출력 엔진 소음과 제트 유동에 의한 음향 하중에 노출되어 음향 피로 손상이 발생할 수 있다. 따라서 열음향 복합 하중을 받는 초음속 항공기 외피 구조의 거동 확인과 피로수명 예측이 필요하다. 본 논문에서는 열음향 복합 하중을 모사할 수 있는 열음향 시험 장치를 설계/제작하여 열음향 하중이 적용되는 티타늄 시편의 열음향 시험을 수행하였다. 열음향 복합 하중에 의한 구조물의 동적 거동을 확인하였으며, 시편 단위 열음향 시험 결과와 유한요소해석 결과를 비교하여 해석 모델을 검증하였다.