• Title/Summary/Keyword: High directivity

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Development of 4Hz Medical Ruby Laser System with Double Cavities using Multi-Resonant Converter (다중 공진형 컨버터를 이용한 이중 캐비티 구조의 4Hz 의료용 루비레이저 시스템 개발)

  • Lee, Jae-cheol;Zheng, Tao;Shengxu, Piao;Xu, Guo-Cheng;Kim, Hee-Je
    • The Transactions of The Korean Institute of Electrical Engineers
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    • v.64 no.8
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    • pp.1207-1211
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    • 2015
  • Various laser systems have been widely used in almost all industrial technologies because they have high energy density, directivity and coherence. Recently the clinical application is becoming wider in medical parts such as incurable disease, diagnosis and so on. Generally, ruby laser beam has the greatest efficacy for removing tattoos, freckle and other skin problem. But current medical ruby laser system has the maximum repetition rate of 2Hz and optical output beam energy of 1J. Many medical doctors really want to have a high repetition ruby laser system because that can reduce the operation time. We investigated a new ruby laser system with high repetition rate of 4Hz using double cavities. Furthermore, we develop a new power supply system adopting zero voltage switching(ZVS) to minimize switching loss by LLC resonant converter designed as 2kW class.

An Experimental Study on the Propagation Characteristics and Reduction of Impulse Noises from a High Voltage COS Fuse (고전압 COS 퓨즈로부터 방사된 충격성 소음의 전파특성과 저감에 관한 실험적 연구)

  • Song, Hwa-Young;Ju, Kyung-Min;Lee, Dong-Hoon;Kang, Rae-Goog;Jung, Nak-Hun
    • Proceedings of the Korean Society for Noise and Vibration Engineering Conference
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    • 2005.11a
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    • pp.71-74
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    • 2005
  • This experimental study describes the propagation characteristics and reduction of impulse noises emitted from a high voltage COS(Cut Out Switch) fuse of a transformer. When a high voltage COS fuse becomes a short circuit by the over current. The peak sound Pressure above 150dB(A) is generated. In this study, an impulse noise generator is designed for generating the impulse noises similar to the noise level of COS fuse, which is utilized to test the noise reduction of a reactive silencer. The reactive silencers have been tested for 10 different types with each different porosity, hole diameter and length. From the experimental results, it is found that the reactive silencer has an excellent performance to greatly suppress the impulse noise and that its performance is closely connected with the porosity and hole diameter.

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A Numerical Study on the Characteristic of Airflow and Aeroacoustic Noise in DVD Drive (DVD 드라이브 내에서의 유동 및 유동소음 특성에 관한 수치적 연구)

  • Yoo, Seung-Won;Lee, Jong-Soo;Min, Oak-Key;Kim, Soo-Kyung
    • Proceedings of the Korean Society for Noise and Vibration Engineering Conference
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    • 2000.11a
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    • pp.759-764
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    • 2000
  • The accurate prediction of aeroacoustic analysis is necessary for designers to control and reduce airflow-induced sound pressure levels in high speed rotating DVD drives. This paper focuses on the numerical prediction of airflow-induced sound in DVD drives. Computational fluid dynamics(CFD) is first conducted to evaluate flow field characteristics due to the high-speed disk rotation, and to support the acoustic analysis. The acoustic analogy based on Ffowcs Williams-Hawkings(FW-H) equation is adopted to predict aeroacoustic noise patterns. The integral solution for quadrupole volume source is included to identify the turbulence noise generated inside the DVD tray. The strength of sound pressure level with respect to rotating speed is discussed to meet upfront demand on the high fidelity product development. The present study also focuses on the noise directivity and examines how much the sound noise is sensitive to change in rotating speed. Near-field noise is strongly affected by the flow field characteristic, which is caused by the complex shape of the tray. For a mid-field, the quadrupole noise play as a counterpart of thickness noise or loading noise, so it generates different sound noise patterns compared with those in the near field.

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A Study on Design of Narrow Beamwidth Multimode Feed Horn Antenna for High Power Microwave Antenna System (초고출력 안테나 시스템 급전용 좁은 빔폭의 다중모드 혼 안테나 설계에 관한 연구)

  • Lee, Sang-Heun;Ahn, Ji-Hwan;Yoon, Young-Joong;So, Joon-Ho
    • Proceedings of the Korea Electromagnetic Engineering Society Conference
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    • 2005.11a
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    • pp.361-366
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    • 2005
  • In this paper, a modified multimode hem antenna is designed to have 142 mm horn aperture radius and 921 mm length in order to be safe under 100 MW peak pulse power at 3 cm wave length through breakdown phenomenon study that threshold field strengths for the air breakdown phenomena is decided to be 3.78 MV/m. The proposed antenna is measured gain over 27 dBi and the -25 dB beam width of 29$^{\circ}$ in vertical plane.

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An Analysis of Internal & External Duct Acoustic Fields by Using a Finite Element Method (유한요소법을 이용한 도관 내부 및 외부 음장해석)

  • 이재규;이덕주
    • Journal of KSNVE
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    • v.3 no.2
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    • pp.169-178
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    • 1993
  • Internal & External duct acoustic fields are calculated by using a finite element method. The geometry is assumed as an axisymmetric duct. External acoustic field; outside the duct, and combined internal & external acoustic fields are solved. For both cases a far field's nonreflecting boundary condition is enforced by using a wave envelope element, which is a kind of finite element. First, a pulsating sphere and an oscillating sphere problem are calculated to verify the external problems, and the results are compared with exact solutions. When the wave envelope element is applied at the far boundary, the calculated finite element solutions show good agreements with the exact solutions. Secondly, the combined internal & external duct acoustic fields are calculated and visualized when monopole sources are distributed inside the duct. It is observed that the directivity of sound intensity outside the duct is beaming toward the axis for high frequency sources.

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Development of the Computer Program for Predicting the Aero-acoustic Performance in the Design Process of Axial Flow Fan (축류형 송풍기 설계 과정에서 공력-음향학적 성능 예측을 위한 전산 프로그램의 개발)

  • Chung, Dong-Kyu;Hong, Soon-Seong;Lee, Chan
    • 유체기계공업학회:학술대회논문집
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    • 2000.12a
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    • pp.91-98
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    • 2000
  • Developed is a computer program for the prediction of the aero-acoustic performance characteristics such as discharge pressure, efficiency, power and noise level in the basic design step of axial flow fan. The flow field and the aerodynamic performance of fan are analyzed by using the streamline curvature computing scheme with total pressure loss and flow deviation models. Fan noise is assumed to be generated due to the pressure fluctuations induced by wake vortices of fan blades and to radiate via dipole distribution. The vortex-induced fluctuating pressure on blade surface is calculated by combining thin airfoil theory and the predicted flow field data. The predicted aerodynamic performances, sound pressure level and noise directivity patterns of fan by the present computer program are favorably compared with the test data of actual fan. Furthermore, the present computer program is shown to be very useful in optimizing design variables of fan with high efficiency and low noise level and in analyzing their design sensitivities.

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3-Dimensional Computations of the Weak Shock Wave Discharged from the Exit of Duct (관출구로부터 방출되는 약한 충격파에 관한 3 차원 수치해석)

  • Kweon, Yong-Hun;Shin, Hyun-Dong;Kim, Heuy-Dong;Lee, Dong-Hoon
    • Proceedings of the KSME Conference
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    • 2003.04a
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    • pp.1742-1747
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    • 2003
  • When a shock wave is discharged from the exit of a duct, complicated flow is formed near the duct exit. The flow field is much more complicated under the ground effects or any other objects near the exit of a duct, such as the circumstance near the exit of the high-speed railway tunnel. The resulting flow is essentially three-dimensional unsteady with the effects of strong compressibility. In the current study, three-dimensional flow fields of the weak shock wave which is discharged from the exit of a duct are numerically investigated using a CFD method. Computations are performed for the weak shock wave in the range below 1.5. The results obtained show that the directivity and magnitude of the weak shock discharged strongly depend upon the Mach number of initial shock wave and are significantly influenced by the ground effects.

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Sweet spot search using Genetic Algorithm (Genetic Algorithm을 이용한 sweet spot search)

  • ;;;Sosuke Onodera;Yoichi Sato
    • Proceedings of the IEEK Conference
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    • 2003.07a
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    • pp.274-277
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    • 2003
  • Millimeter-wave networking is composed of narrow beam link. High directivity of the beam provides either advantage or disadvantage in comparison with conventional wide-lobe microwave communications. In such networks, it is very substantial that beam connecting point to point is fixed in right direction. It is major requirement in the beam network to keep the beam in best direction. In this paper, We propose the method to find a best suited direction of the antenna's beam using the Genetic Algorithm in point-to-point link. Proposed method presume that each station knows his direction $\theta$$_1$,$\theta$$_2$ at every step of Genetic Algorithm, then it can be expected that GA is possible to search the ideal solution. Intensity of the received signal is evaluated by the multiplication of lengths to the point which the lobe meets with the horizontal line.

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A Study on the Aerodynamic Noise of a Supersonic Exhaust Nozzle of Perforated Tube (다공관형 초음속 배기노즐의 공력소음에 관한 연구)

  • 이동훈
    • Journal of KSNVE
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    • v.9 no.1
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    • pp.113-120
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    • 1999
  • A perforated tube nozzle as an exhaust noise suppressor of a high-speed civil transport(HSCT) is proposed. The experimental results for the near and far field sound. the visualization of jet structures and the static pressure distributions in the jet passing through a perforated tube are presented and discussed in comparison with those for a simple tube. It is shown that the perforated tube has an excellent performance to greatly reduce the shock-associated noise and that also the turbulent mixing noise is reduced in the range of a limited jet pressure ratio. This considerable noise reduction is due to the pressure relief caused by the through-flow through the perforated holes. Such a pressure relief results in the transformation of normal shock waves into weak Mach waves of X -type and increases the thrust force of the perforated tube nozzle.

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Microstrip directional coupler with the high directivity (높은 지향성을 갖는 마이크로스트립 방향성 결합기 설계)

  • Kim, Chul-Soo;Lim, Jong-Sik;Kim, Jong-Hwa;Ahn, Dal
    • Proceedings of the Korea Electromagnetic Engineering Society Conference
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    • 2003.11a
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    • pp.318-321
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    • 2003
  • 마이크로스트립 구조의 방향성 결합기는 이방성 유전체로 인하여 지향성 특성이 저하된다. 즉 우, 기모드의 위상차에 의해 격리특성이 저하된다. 이러한 문제점을 개선하고자 결합선로간의 대칭형으로 입출력단에 위상 보상용 커패시터를 구현해주어 격리특성을 개선하였다. 보상용 캐패시터는 평면형으로 구현하여 제작의 편리하고, 우, 기모드 위상차를 줄여주어 높은 지향성 특성을 얻을 수 있었다. 부가적으로 결합선로의 길이를 약 10%를 줄 일수 있다. 제시된 방법의 타당성을 입증하기 위하여 12dB, 20dB와 30dB의 마이크로스트립 방향성 결합기를 제작하여 30dB의 높은 지향성 특성을 얻었다.

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