• 스마트미디어저널
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• 제4권4호
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• pp.64-69
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• 2015

본 논문에서는 UWB 통신 시스템의 테이퍼드 슬롯 안테나를 제안하였다. 테이퍼드 슬롯 안테나는 넓은 대역폭 특성과 진행파 안테나의 지향성 방사를 갖는다. 제안된 테이퍼드 슬롯 안테나는 Ansys사의 HFSS를 사용하여 설계하였으며, 반사손실 및 정재파비, 방사패턴 등을 분석하였다. 안테나의 동작 대역은 2.7 ~ 4.8 GHz 대역에서 -10 dB S11 및 $VSWR{\leq}2$(2.1 GHz)를 만족하였다. 안테나의 방사패턴은 E-평면(YZ plane)과 H-평면(XZ plane)에서 특정한 방향으로 신호를 전송하는 지향성 방사패턴을 보였으며, 이득은 4.5 GHz 대역에서 7.3 dBi의 높은 이득을 보였다. 따라서 제안된 테이퍼드 슬롯 안테나는 넓은 대역폭 특성과 위치인식에 적합한 지향성의 특성을 보인다.

• 대한전자공학회논문지TC
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• 제48권5호
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• pp.46-53
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• 2011

유한한 기판크기가 E-평면으로 배열된 선형 위상 배열 안테나의 방사 특성에 미치는 영향을 연구하였다. 여러 가지 기판 크기에 따른 active reflection coefficient 와 average active element pattern 으로부터 선형 배열안테나의 방사특성을 예측하였다. E-평면과 만나는 기판 가장자리까지의 거리 변화가 H-평면과 만나는 기판 가장자리까지의 거리 변화에 비해 위상 배열 안테나의 방사 패턴 특성에 미치는 영향이 큰 것을 알 수 있었다.

• 한국ITS학회 논문지
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• 제11권1호
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• pp.42-52
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• 2012

본 논문에서는 UWB (Ultra Wide Band) high 대역 (중심 주파수 : 9.5 GHz, -10 dB 대역폭 : 600 MHz, 6.4 %)의 차량 측후방 레이더 센서용 도파관 안테나를 설계 및 제작하였다. 안테나는 대역폭이 넓고 구조가 간단한 프로브 급전 구형도파관을 이용하였다. 본 연구의 차량 레이더 시스템에 있어서 송수신 안테나의 큰 격리도 특성을 얻는 것이 설계의 중요한 변수이다. 따라서 두 도파관 안테나를 E-면과 H-면 배열하였을 시 격리도 특성을 시뮬레이션 하였다. 그 결과 도파관 안테나의 $TE_{10}$ 모드에 의하여 E-면 배열 보다 H-면 배열의 격리도 특성이 우수한 것을 확인하였다. 따라서 H-면 배열된 송수신 도파관 안테나를 T-형 레이더 모듈에 장착하여 안테나의 특성을 검출하였다. T-형 모듈에 장착된 송수신 안테나의 -10 dB 대역폭은 각각 1000 MHz (10.52 %)와 1090 MHz (11.47 %)로 측정되었고 격리도 (S21)는 요구 대역 내에서 -50 dB 이하로 측정되었다. 송수신 안테나의 최대이득은 각각 7.65 dBi와 7.26 dBi로 나타났으며 H-면 빔폭은 $64^{\circ}$, $65^{\circ}$로 측정되어 차량 측후방 레이더 센서용 안테나로 적합함을 확인하였다.

• 대한전기학회논문지
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• 제43권4호
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• pp.666-672
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• 1994

An H-Plane waveguide component with arbitrary shape is analyzed using finite element method(FEM) Cooperated with boundary element method(BEM). For the application of BEM in the waveguide structure, a ray representation of the waveguide Green's function is used. This technique is applied to the analysis of the waveguide inductive junction. The results are compared with the results of the mode matching technique. The comparison shows good agreement.

• 전기학회논문지
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• 제56권1호
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• pp.161-166
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• 2007

In this paper, two 4$\times$4 rectangular patch array antennas operating at 20 GHz are implemented for the satellite communication. The sixteen patch antennas and microstrip feeding line are printed on a single-layered substrate. The design goal is to achieve high directivity and gain by optimizing design parameters through permutations in element spacing. The spacing between the array elements is chosen to be 0.736$\lambda$. Numerical simulation results indicate that the HPBW(Half-Power Beam Width) of the 4$\times$4 patch array antenna is 18.78 degrees in the E-plane and 18.48 degrees in the H-plane with a gain of 17.18 dBi. Numerical simulations of a 4$\times$4 recessed patch array antenna yield a HPBW of 18.71 degrees in the E-plane and 17.82 degrees in the H-plane with a gain of 19.43 dBi.

• 한국정밀공학회지
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• 제11권5호
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• pp.134-142
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• 1994

An upper bound elemental technique (UBET) is applied to predict variations of neutral plane and optimal position of the initial billet for rib-wep shaped ring forging. In the analysis, the neutral plane position and velocity fields are determined by minimizing the total power consump- tion with respect to chosen parameters. The degree of die-cavity filling by initial billet-position and the variations of neutral plane by friction condition are investigated. Experiments have been carried out with pure plasticine billets at room temperature. The theoretical predictions of the forging load and the flow pattern are in good agrement with the experimental results.

• Geomechanics and Engineering
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• 제9권1호
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• pp.115-124
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• 2015

Determination of mobilized shear strength parameters (that identify stresses on the failure plane) is required for analyzing the stability by limit equilibrium method. Generalized Hoek-Brown (GHB) and Mohr-Coulomb (MC) failure criteria are usually used for obtaining stresses on the plane of failure. In the present paper, the applicability of these criteria for determining the stresses on failure plane is investigated. The comparison is based on stresses on the real failure plane which are obtained from the Mohr stress circle. To do so, 18 sets of data (consist of principal stresses and angle of failure plane) presented in the literature are used. In addition, the values account for (VAF) and the root mean square error (RMSE) indices were calculated to check the determination performance of the obtained results. Values of VAF and RMSE for the normal stresses on the failure plane evaluated from MC are 49% and 31.5 where for GHB are 55% and 30.5, respectively. Also, for the shear stresses on failure plane, they are 74% and 36 for MC, 76% and 34.5 for GHB. Results show that the obtained stresses and angles of failure plane for each criterion differ from real ones, but GHB results are closer to the empirical results. Also, it is inferred that results are affected by the failure envelope not real failure plane. Therefore, obtained shear strength parameters are not mobilized. Finally, a multivariable regressed relation is presented for determining the stresses on the failure plane.

• 한국소음진동공학회:학술대회논문집
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• 한국소음진동공학회 2002년도 추계학술대회논문초록집
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• pp.383.2-383
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• 2002

In this paper, an experimental technique using a reference accelerometer has been developed to measure the in-plane vibration intensity of a beam. It has the advantages of shortening measurement time and reducing accelerometer phase error comparing with the cross spectral Intensity measurement technique using an accelerometer array. The distribution of the in-plane vibration Intensity over the beam has been measured. (omitted)

• Journal of electromagnetic engineering and science
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• 제4권4호
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• pp.150-155
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• 2004

Universal design equations are presented for the H-plane T-junction power divider with a circular conducting post in a rectangular waveguide. For a given operating frequency and power split ratio, the post offset from the T-junction center line, the distance between the post and the waveguide wall, and the post diameter can be adjusted to obtain a minimum reflection at the input waveguide. Optimum values of the post offset are given in terms of the normalized frequency and the power split ratio. Corresponding values of the post diameter and the distance of the post from the waveguide wall are given in terms of the normalized frequency and the post offset.

• Journal of Magnetics
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• 제18권2호
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• pp.155-158
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• 2013

FeCoB films were being prepared on a Ru underlayer by using the oblique incidence of sputtered and back-scattered particles which have a high in-plane magnetic anisotropy field $H_k$ above 400 Oe. It is suitable to attain such deposition condition when facing targets sputtering system. The in-plane X-ray diffraction analysis clarified that there is anisotropic residual stress which is the origin of the high in-plane magnetic anisotropy. The directional crystalline alignment and inclination of crystallite growth were also observed. Such anisotropic crystalline structures may affect the anisotropic residual stress in the films. The B content of 5.6 at.% was appropriate to induce such anisotropic residual stress and $H_k$ of 410 Oe in this experiment. The film with B content of 6 at.% possessed large saturation magnetization of 22 kG and high $H_k$ of 500 Oe. The film exhibited high ferromagnetic resonance frequency of 9.2 GHz.