• 제목/요약/키워드: Non-dimensional Temperature

검색결과 263건 처리시간 0.03초

모터컨트롤센터의 BUS BAR 이상 감지를 위한 실험적 연구 (A study on sensing for abnormality of BUS BAR in motor control center)

  • 김성대
    • 한국산학기술학회논문지
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    • 제12권12호
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    • pp.5838-5842
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    • 2011
  • 본 연구는 고용량의 모터를 구동하기 위한 모터컨트롤센터(MCC)의 내부 구조 중 각 상(R,S,T)의 BUS BAR의 온도와 BUS BAR 볼트 체결부의 온도변화가 모터컨트롤센터의 노후화 및 진동에 따라 어떠한 차이가 있는지를 적외선 온도센서가 설치된 온도측정용 2차원 기구부를 설계 제작하고 모터컨트롤센터의 내부에 설치하여 BUS BAR의 온도 및 전류 변화량을 상시 모니터링 하였다. 실험을 통하여 부하에 따른 BUS BAR의 온도 변화를 BUS BAR 나사 체결부위를 중심으로 측정하였으며, BUS BAR의 온도변화와 소모 전류에 대한 비례관계를 확인할 수 있었다. 또한 이러한 비접촉식 2차원 온도측정 시스템을 모터컨트롤센터 내부에 장착하면 부하의 과전류로 인한 온도 상승이나 접촉 불량 등으로 발생될 수 있는 정전이나 화재 사고를 예방할 수 있을 것으로 기대된다.

레이저 유도 선해리 형광법과 래일레이 산란법에 의한 층류 비예혼합 수소/질소 화염의 온도 및 라디칼 특성에 관한 연구 (A Study on Characteristics of Temperature and Radicals in Laminar Non-premixed H2/N2 Flame Using LIPF and LRS)

  • 진성호;박경석;김군홍;김경수
    • 한국수소및신에너지학회논문집
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    • 제13권3호
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    • pp.169-180
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    • 2002
  • Rayleigh scattering and laser induced predissociative fluorescence are used to obtain two-dimensional images of temperature and species concentration in a laminar non-premixed flame of a diluted hydrogen jet. Rayleigh scattering cross-sections are experimentally obtained at 248nm. Planar images of OH and $O_2$ with tunable KrF excimer laser which has a) $0.5cm^{-1}$ linewidth, b) 0.5nm tuning range, c) 150mJ pulse energy, and d) 20ns pulse width are obtained to determine spatial distributions of OH and $O_2$. The technique is based on planar laser induced predissociative fluorescence (PLIPF) in which collisional quenching is almost avoided because of the fast predissociation. Dispersed LIPF spectra of OH and $O_2$ are also measured in a flame in order to confirm the excitation of single vibronic state of OH and $O_2$. OH and $O_2$ are excited on the $P_2$(8) and $Q_1$(11) line of the $A^2{\Sigma}^{+}({\nu}^{'}=3)-X^{2}{\Pi}({\nu}^{''}=o)$ band and R(17) line of the Schumann-Runge band $B^{3}{\Sigma}_{u}{^-}(\nu^{'}=0)-X^{3}{\Sigma}_{g}{^-}({\nu}^{''}=6)$, respectively. Fluorescence spectra of OH and Hot $O_2$ are captured and two-dimensional images of the hydrogen flame field are successfully visualized.

RBF Network 를 이용한 표면온도 역추정에 관한 연구 (Inverse Estimation of Surface Temperature Using the RBF Network)

  • 정법성;이우일
    • 대한기계학회:학술대회논문집
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    • 대한기계학회 2004년도 춘계학술대회
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    • pp.1183-1188
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    • 2004
  • The inverse heat conduction problem (IHCP) is a problem of estimating boundary condition from temperature measurement at one or more interior points. Neural networks are general information processing systems inspired by the connectionist theory of human brain. By properly training the network by the learning rule, the neural network method can handle many non-linear or other complex problems. In this work, neural network is applied to complicated inverse heat conduction problems. Efficiency of the procedure is enhanced by incorporating the radial basis functions (RBF). The RBF is trained faster than other neural network and can find smooth solution. In order to demonstrate the effectiveness of the current scheme, a typical one-dimensional IHCP is considered. At one surface, the temperature as well as the heat flux is known. The unknown temperature of interest is estimated on the other side of the slab. The results from the proposed method based on RBF neural network are compared with the conventional method.

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열교환기 휜에서의 서리 성장 (Growth of frost formed on heat exchanger fins)

  • 안원준;김정수;이관수
    • 대한설비공학회:학술대회논문집
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    • 대한설비공학회 2008년도 동계학술발표대회 논문집
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    • pp.256-261
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    • 2008
  • In this study, frost behavior on two dimensional fins of a heat exchanger was experimentally investigated. Temperature distribution on a 2-D fin surface and frost properties were measured in the directions perpendicular to and parallel to airflow. The results indicated that the temperature gradient in the direction perpendicular to airflow was large because of fin heat conduction, while that in the direction parallel to airflow was very small. Frost thickness in the airflow direction decreased from the leading edge towards the trailing edge of the fin due to leading edge effect. The reduction rate of frost thickness in the airflow direction, however, was very small compared with that in the direction perpendicular to the airflow, as affected by the temperature distribution.

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Dynamic instability of functionally graded material plates subjected to aero-thermo-mechanical loads

  • Prakash, T.;Ganapathi, M.
    • Structural Engineering and Mechanics
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    • 제20권4호
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    • pp.435-450
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    • 2005
  • Here, the dynamic instability characteristics of aero-thermo-mechanically stressed functionally graded plates are investigated using finite element procedure. Temperature field is assumed to be a uniform distribution over the plate surface and varied in thickness direction only. Material properties are assumed to be temperature dependent and graded in the thickness direction according to simple power law distribution. For the numerical illustrations, silicon nitride/stainless steel is considered as functionally graded material. The aerodynamic pressure is evaluated based on first-order high Mach number approximation to the linear potential flow theory. The boundaries of the instability region are obtained using the principle of Bolotin's method and are conveniently represented in the non-dimensional excitation frequency-load amplitude plane. The variation dynamic instability width is highlighted considering various parameters such as gradient index, temperature, aerodynamic and mechanical loads, thickness and aspect ratios, and boundary condition.

A novel of rotating nonlocal thermoelastic half-space with temperature-dependent properties and inclined load using the dual model

  • Samia M. Said
    • Structural Engineering and Mechanics
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    • 제90권5호
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    • pp.459-466
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    • 2024
  • Eringen's nonlocal thermoelasticity theory is used to study wave propagations in a rotating two-temperature thermoelastic half-space with temperature-dependent properties. Using suitable non-dimensional variables, the harmonic wave analysis is used to convert the partial differential equations to ordinary differential equations solving the problem. The modulus of elasticity is given as a linear function of the reference temperature. MATLAB software is used for numerical calculations. Comparisons are carried out with the results in the context of the dual-phase lag model for different values of rotation, a nonlocal parameter, an inclined load, and an empirical material constant. The distributions of physical fields showed that the nonlocal parameter, rotation, and inclined load have great effects. When a nonlocal thermoelastic media is swapped out for a thermoelastic one, this approach still holds true.

상하면의 마찰이 틀린 비직각주 소재의 3차원 업셋팅에 관한 연구 (A study on the three-dimensional upsetting of non-prismatic blocks considering different frictional conditions at two flat dies)

  • 김종호;류민형;양동열
    • 대한기계학회논문집
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    • 제13권3호
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    • pp.345-352
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    • 1989
  • 본 연구에서는 3차원 변형형상을 갖는 소재에서 상하금형면의 마찰이 다른 경우에, 작각주 소재와 비직각주 소재(non-prismatic block)에 대해서 적용할 수 있는 동적 가용 속도장(kinematically admissible velocity field)을 유도해 내고자 한다.이론계산에 있어서 가공경화를 고려하기 위해 소성변형 영역을 유한개의 요소들로 나누고 이들 각 요소에 대해서 유효변형도, 유효응력을 계산하여 에너지 소비율을 계산하였다.

ELECTRON TEMPERATURE ESTIMATION OF NON-THERMAL ATMOSPHERIC-PRESSURE NEON AND OXYGEN ADMIXTURE PLASMA JET BY CONVECTIVE WAVE PACKET MODEL

  • SORNSAKDANUPHAP, Jirapong;SUANPOOT, Pradoong;Hong, Young June;Ghimire, Bhagirath;CHO, Guangsup;CHOI, EunHa
    • 한국진공학회:학술대회논문집
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    • 한국진공학회 2016년도 제50회 동계 정기학술대회 초록집
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    • pp.207-207
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    • 2016
  • plasma group velocities of neon with oxygen admixture (ug) are obtained by intensified charge coupled device (ICCD) camera images at fixed gate width time of 5 ns. The propagation velocities outside interelectrode region are in the order of 104 m/s.The plasma ambipolar diffusion velocities are calculated to be in the order of 102 m/s. Plasma jet is generated by all fixed sinusoidal power supply, total gas flow and repetition frequency at 3 kV, 800 sccm and 40 kHz, respectively. The amount of oxygen admixture is varied from 0 to 2.75 %. By employing one dimensional convective wave packet model, the electron temperatures in non-thermal atmospheric-pressure plasma jet are estimated to be in a range from 1.65 to 1.95 eV.

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ELECTRON TEMPERATURE ESTIMATION OF NON-THERMAL ATMOSPHERIC-PRESSURE NEON AND ARGON PLASMA JET BY CONVECTIVE WAVE PACKET MODEL

  • SORNSAKDANUPHAP, Jirapong;SUANPOOT, Pradoong;Hong, Young June;Ghimire, Bhagirath;CHO, Guangsup;CHOI, Eun Ha
    • 한국진공학회:학술대회논문집
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    • 한국진공학회 2015년도 제49회 하계 정기학술대회 초록집
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    • pp.156.1-156.1
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    • 2015
  • Neon and argon plasma group velocities (ug) are obtained by intensified charge coupled device (ICCD) camera images at fixed gate width time of 5 ns. The propagation velocities in upstream and downstream region are in the order of 104-105 m/s. The plasma ambipolar diffusion velocities are calculated to be in the order of 101-102 m/s. Plasma jet is generated by sinusoidal power supply in varying voltages from 1 to 4 kV at repetition frequency of 40 kHz. By employing one dimensional convective wave packet model, the neon and argon electron temperatures in non-thermal atmospheric-pressure plasma jet are estimated to be 1.95 and 1.18 eV, respectively.

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Performance analysis of a 746 W HTS generator equipped with 70 A class contactless superconducting field exciter

  • Chae, Yoon Seok;Kim, Ho Min
    • 한국초전도ㆍ저온공학회논문지
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    • 제22권3호
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    • pp.1-6
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    • 2020
  • This paper presents the analysis results on the electrical output performance characteristics of a 746 W high temperature superconducting generator (HTSG). The HTS field winding is charged by non-contact excitation method, i.e., contactless superconducting field exciter (CSFE) which is originated by rotary flux pump based on permanent magnet. In this paper, the preliminary current charging test was carried out using a 70 A CSFE to evaluate the performance of field exciter and analyze its non-contact excitation characteristics for the full-scale HTS field winding of the 746 W HTSG. First, the various contactless current-charging tests were conducted using assembly with HTS field winding and CSFE. Then, in order to estimate the output power performance characteristics of the 746 W HTSG, finite element analysis was conducted based on field excitation information which is experimentally measured under various operating conditions. Finally, the electrical output characteristics in no-load and load models were simulated by two-dimensional transient solver in ANSYS electromagnetics 19.0 release.