• Title/Summary/Keyword: 축방향 속도

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드럼식 세탁기의 진동/소음 저감 대책

  • 박정수;김형균
    • Journal of KSNVE
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    • v.7 no.6
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    • pp.881-887
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    • 1997
  • 우리가 일상생활에서 사용하는 가전제품 중에서 소음 진동이 발생하여 생활에 영향을 미치는 제품으로 세탁기를 들 수 있다. 세탁기의 종류는 회전하는 축의 방향에 의해 수직축(vertical axis)과 수평축 (horizontal axis) 방식으로 나누며 국내, 일본및 동남아시아 등에서 사용하는 펄세이터식(pulsator type) 세탁기와 미국을 비롯한 미주에서 사용하는 애지테이터식(agitator type)세탁기는 전자에 속하고 유럽에서 사용하는 드럼식(drum type) 세탁기는 후자에 속한다. 드럼 세탁기의 장점은 물을 적게 사용하고, 삶는 세탁이 가능하며, 건조 기능을 갖고 있으므로 별도의 건조기가 필요없어서 공간을 절약하는 것이다. 또 빨래가 펄세이터나 애지테이터 등의 교반체와 직접 접촉하지 않기 때문에 빨래의 마모가 적다. 드럼식 세탁기의 단점으로는 가격이 펄세이터식이나 애지테이터식에 비해서 비싸고, 무게가 무거우며, 탈수시에 소음과 진동이 심하다. 특히 탈수시 발생하는 소음과 진동은 이방식의 세탁기의 가장 큰 약점이다. 지금까지는 드럼식 세탁기의 진동 소음을 감소시키려는 적극적인 노력이 없었는데, 볼밸런스를 적용한 드럽 세탁기를 개발하여 소음과 진동을 획기적으로 감소시켰다.

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Reynolds Number Effects on the Near-Wake of an Oscillating Naca 4412 Airfoil, Part 1 : Mean Velocity Field (진동하는 NACA 4412 에어포일 근접후류에서의 레이놀즈수 효과 1: 평균속도장)

  • Jang,Jo-Won
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.31 no.7
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    • pp.15-25
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    • 2003
  • An experimental. study is carried out to investigate the near-wake characteristics of an airfoil oscillating in pitch. An NACA 4412 airfoil is sinusoidally pitched about the quarter chord point between the angle of attack -6$^{\circ}$ and +6$^{\circ}$. A hot-wire anemometer is used to measure the phase-averaged mean velocities in the near-wake region of an oscillating airfoil. The freestream velocities of present work are 3.4, 12.4, 26.2 m/s, and the corresponding Reynolds numbers are 5.3${\times}10^4$, 1.9${\times}10^5$, 4.l${\times}10^5$, and the reduced frequency is 0.1. Streamwise velocity profiles are presented to show the Reynolds number effects on the near-wake region behind an airfoil oscillating in pitch. All the cases in these measurements show that the velocity defects by the change of the Reynolds number are very large at the lowest Reynolds number $R_N$=5.3${\times}10^4$: and are small at the other Reynolds numbers ($R_N$=1.9${\times}10^5$ and 4.l${\times}10^5$) in the near-wake region. A significant difference of phase-averaged mean velocity between 5.3${\times}10^4$, and 1.9${\times}10^5$ is observed. The present study shows that a critical value of Reynolds number in the near-wake of an oscillating airfoil exists in the range between 5.3${\times}10^4$, and 1.9${\times}10^5$.

Non-linear Dynamic Analysis of Reinforced Concrete Slabs Subjected to Explosive Loading Using an Orthotropic Concrete Constitutive Model (이등방성 콘크리트 모델을 이용한 폭발하중을 받는 철근콘크리트 슬래브의 비선형 동적해석)

  • Lee, MinJoo;Kwak, Hyo-Gyoung
    • Journal of the Computational Structural Engineering Institute of Korea
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    • v.32 no.6
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    • pp.409-416
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    • 2019
  • An improved numerical model for non-linear analysis of reinforced concrete (RC) slabs subjected to blast loading is proposed. This approach considers a strain rate dependent orthotropic constitutive model that directly determines the stress state using the stress-strain relation acquired from the data obtained using the biaxial strength envelope. Moreover, the bond-slip between concrete and reinforcing steel is gradually enlarged after the occurrence of cracks and is concentrated in the plastic hinge region. The bond-slip model is introduced to consider the crack direction of the concrete under a biaxial stress state. Correlation studies between the numerical analysis and the experimental results were performed to evaluate the analytical model. The results show that the proposed model can effectively be used in dynamic analyses of reinforced concrete slab members subjected to explosive loading. Moreover, it was determined that it is important to consider biaxial behavior in the material model and the bond-slip effect.

A Development of Robot Arm Direct Teaching System (로봇팔 직접 교시 시스템 개발)

  • Woong-Keun Hyun
    • The Journal of the Korea institute of electronic communication sciences
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    • v.19 no.1
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    • pp.85-92
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    • 2024
  • In this paper, we developed an intuitive teaching and control system that directly teaches a task by holding the tip of a robotic arm and moving it to a desired position. The developed system consists of a 6-axis force sensor that measures position and attitude forces at the tip of the robot arm, an algorithm for generating robot arm joint speed control commands based on the measured forces at the tip, and a self-made 6-axis robot arm and control system. The six-dimensional force/torque of the position posture of the robot arm operator steering the handler is detected by the force sensor attached to the handler at the leading edge and converted into velocity commands at the leading edge to control the 7-axis robot arm. The verification of the research method was carried out with a self-made 7-axis robot, and it was confirmed that the proposed force sensor-based robot end-of-arm control method operates successfully through experiments by teaching the operator to adjust the handler.

Experimental Study on Aerodynamic Performance and Wake Characteristics of the Small Ducted Fan for VTOL UAV (수직 이착륙 무인기용 소형 덕티드팬의 공력성능 및 후류특성에 관한 실험적 연구)

  • Shin, Soo-Hee;Lee, Seung-Hun;Kim, Yang-Won;Cho, Tae-Hwan
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.50 no.1
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    • pp.1-12
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    • 2022
  • Wind tunnel test for a small scale electric ducted fan with a 104mm diameter was conducted to analyze the aerodynamic characteristics when it was used as a propulsion system of tilt-propeller UAV. Experimental conditions were derived from flight conditions of a sub-scaled OPPAV. Forces and moments of the ducted fan model were measured by a 6-axis balance and 3-dimensional wake vectors which could induce an aerodynamic influence in the vehicle were measured by 5-hole probes. Thrust and torque on hover and cruise conditions were measured and analyzed to drive out the operating conditions when it was applied in the sub-scaled OPPAV. On transition conditions, thrust keep its value with tilt angle variation below 40° and increase after that. But, sideforce increase constantly until 75°. The maximum axial velocity in the wake on hover and cruise conditions was around 60m/s and tangential velocity was around 12m/s. The position of the maximum axial velocity and vortex center move off the fan rotation center line as the tilt angle increases.

Numerical Determination of Lateral Loss Coefficients for Subchannel Analysis in Nuclear Fuel Bundles (핵 연료집합체 부수로 해석을 위한 횡 방향 압력손실계수의 수치적 결정)

  • Kim, Sin;Park, Goon-Cherl
    • Nuclear Engineering and Technology
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    • v.27 no.4
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    • pp.491-502
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    • 1995
  • In accurate prediction of cross-flow based on detailed knowledge of the velocity field in subchannels of a nuclear fuel assembly is of importance in nuclear fuel performance analysis. In this study, the low-Reynolds number k-$\varepsilon$ turbulence model has been adopted in too adjacent subchannels with cross-flow. The secondary flow is accurately estimated by the anisotropic algebraic Reynolds stress model. This model was numerically calculated by the finite element method and has been verified successfully through comparison with existing experimental data. Finally, with the numerical analysis of the velocity Held in such subchannel domain, an analytical correlation of the lateral loss coefficient is obtained to predict the cross-flow rate in subchannel analysis codes. The correlation is expressed as a function of the ratio of the lateral How velocity to the donor subchannel axial velocity, recipient channel Reynolds number and pitch-to-diameter.

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Design and Performance Analysis of Steam Turbine for Variations of Degree of Reaction (반동도에 따른 증기터빈의 설계 및 성능해석)

  • Shin, Jung-Ha;Lee, Geun-Sik
    • Transactions of the Korean Society of Mechanical Engineers B
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    • v.35 no.12
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    • pp.1391-1398
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    • 2011
  • Design and performance analysis of a steam turbine for variations of degree of reaction were performed by computer simulation. Design parameters such as blade angles, exit areas, and heights of the nozzle and moving blade were represented as functions of the degree of reaction. The main performance factors such as turbine power, diagram efficiency, and axial thrust were also expressed in terms of the degree of reaction. For further information about the design and performance, the blade angles and main performance factors were investigated as functions of the flow coefficient. The turbine power and diagram efficiency reached a maximum value for a given degree of reaction and flow coefficient, and the symmetric shape of the moving blade showed distortion as the degree of reaction was increased.

원봉의 일방향 응고과정에 대한 수치해석

  • 김한상;김민수;노승탁;박용조;김학민
    • Transactions of the Korean Society of Mechanical Engineers
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    • v.14 no.4
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    • pp.1033-1041
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    • 1990
  • 본 연구에서는 금속의 응고과정에 수반되는 고체와 액체의 밀도차에 의한 체 적수축을 고려하여 원봉내에서의 일방향 응고과정에 대한 수치해석을 하였다. 상변 화면에서 체적수축에 의한 중력방향으로의 액상 전체운동(bulk motion)과 원봉의 인출 속도 및 주형벽면에서의 경계조건이 금속내부의 온도분포와 상경계면의 이동속도에 미 치는 영향에 대해 연구하였다.

Spectral Element Modeling for the Axially Moving Strings (축방향으로 이동하는 현에 대한 스펙트럴 요소 모델링)

  • Choi, Jung-Sik;Lee, U-Sik
    • Proceedings of the KSR Conference
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    • 2009.05a
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    • pp.1092-1096
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    • 2009
  • The spectral element modeling is known to provide very accurate structural dynamic characteristics, while reducing the number of degree-of-freedom to resolve the computational and cost problems. Thus, the spectral element model with variational method for an axially moving string subjected to axial tension is developed in the present paper. The high accuracy of the spectral element model is the verified by comparing its solutions with the conventional finite element solutions and exact analytical solutions. The effects of the moving speed and axial tension the vibration characteristics, wave characteristics, and the static and dynamic stabilities of a moving string are investigated.

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비정질 셀레니움 박막의 결정화 -결정의 형태와 그 변태속도-

  • 김기순
    • Journal of the Korean Ceramic Society
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    • v.11 no.2
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    • pp.38-49
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    • 1974
  • 운모기판에 증착한 비정형 셀레니움 박막의 결정성장의 형태와 그 변태속도에 대하여 연구하였다 열처리된 박막에서 비정질성분은 CS2에 용해되나 결정질은 아무 변화없이 남아 있으므로 쉽게 현미경을 이용하여 그 모양을 조사할 수 있다. 결정은 (30$^{\circ}$~10$0^{\circ}C$ 온도 범위에서) 박막과 운모기관의 경계면을 따라서 원형상(구상 결정의 이차원 적 모양) 중심으로 부터 일정 속도로 자란다. 또한 필라멘트 형태의 결정이 원형상 결정의 비 규칙적인 부분에서 박막을 뚫고 위로 자란다. 이들 필라멘트형 결정은 자유표면에 도달하여 새로이 자유표면을 따라서 원형상으로 자라게 된다. 경계에 있는 원형상 결정의 두께는 약 500$\AA$정도이고 이것이 비정질 세레니움 박막에서 보이는 "어두어 지는" 현상의 원인이 되고 있음이 밝혀졌다. 원형상 결정은 아주 조그마한 결정 "도메인"으로 구성되어 있으며 이들 "도메인"의 축 방향은 경계면과 나란하고 반경방향에 수직으로 되어 있다. 고온처리에서 얻어지는 규칙적인 결정은 이들 "도메인"이 모여서 "라멜라"를 형성하여 중심부에서부터 뻗어나가고 이들 "라멜라"간의 공간은 불규칙적으로 나열된 "도메인"으로 연결되어 있으며, 고분자 결정에 비하여 훨씬 두껍다. 반경 방향으로의 결정성장 속도는 아주 순도가 높은 박막에서는 시간에 따라 일정하고 주어진 온도에서 재현성이 아주 좋다. 이 실험에서 측정된 성장속도는 지금까지 발표된 어느 실험에서 관측된 것보다 빠르고 또 자유표면에서 자라는 속도에 비해서 약 백 여배나 빠르다. 결장 성장의 온도 의존은 u=6$\times$1015 exp[-32.7(kcal/mol)/RT] cm/sec로 표시할 수 있다.

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