• Title/Summary/Keyword: 7층 적층구조

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Design and Fabrication of Dual Linear Polarization Stack Antenna for 4.7GHz Frequency Band (4.7 GHz 대역에서 동작하는 이중 선형편파 적층 안테나의 설계 및 제작)

  • Joong-Han Yoon;Chan-Se Yu
    • The Journal of the Korea institute of electronic communication sciences
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    • v.18 no.2
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    • pp.251-258
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    • 2023
  • In this paper, we propose DLP(Dual Linear Polarization) stack antenna for private network. The proposed antenna has general stack structure and design airgap between two substrate to obtain the maximum gain. Also, to improve cross polarization isolation, two feeding port is designed to separate for each substrate. The size of each patch antenna is 17.80 mm(W1)×16.70 mm(L1) for lower patch and 18.56 mm(W2)×18.73 mm(L2) for upper patch, which is designed on the FR-4 substrate which thickness (h) is 1.6 mm, and the dielectric constant is 4.3, and which is 40.0 mm(W)×40.0 mm(L) for total size of substrate. From the fabrication and measurement results, bandwidths of 100 MHz (4.74 to 4.84 GHz) for feeding port 1, and 150 MHz (4.67 to 4.82 GHz) for feeding port 2 are obtained on the basis of -10 dB return loss and transmission coefficient S21 is got under the -20 dB. Also, cross polarization isolation between each feeding port obtained

Fabrication and Characterization of Red Organic Light-Emitting Diodes Using Red Fluorescent Material (도판트를 이용한 적색 유기 발광 다이오드의 제작 및 특성 연구)

  • Lee, Han-Seong
    • Proceedings of the KIEE Conference
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    • 2006.10b
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    • pp.171-174
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    • 2006
  • 본 연구에서 새로 합성한 적색 도판트 Red-1을 Physical vapor Deposition (PVD) 법을 이용하여 다층구조의 유기 발광 다이오드를 제작하였다. 적층된 유기물 층으로 정공주입층은 4,4',4"-tri [2-naphthyl(phenyl)amino]triphenylamine(2-TNATA) 정공 수송층으로4-4bis [N-(1-napthyl-N-phenyl-amino)biphenyl] (NPB)를 사용하였으며 전자 수송층은 tris (8-quinolinolato)-aluminum ($Alq_3$), 발광층에서의 host 재료로 사용한 물질은 $Alq_3$. 4,4'- N-N'-dicarba zole-biphenyl (CBP), 게스트재료는 Red-1, 정공저지층으로 2,9-dimethyl-4, 7-diphenyl -1 10-phen antroline (BCP), 전자 주입층으로는 lithiumquinolate (Liq)를 사용하여 보다 향상된 전기적, 발광특성을 보이는 소자를 제작하였다. 전하를 주입하는 전극으로 일함수가 큰 투명전극인 ITO (indium-tin-oxide)를 양전극으로, Al을 음전극으로 사용하였다. 그리하여, 발광층 내에서의 host재료 $Alq_3$와 CBP와의 energy transfer의 관점에서 그 특성을 연구하였다.

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BS/channeling studies on the epitaxially grown Pt(111) films on $Al_2O_3$(0001) (BS/Channeling을 이용한 Pt(111)/$Al_2O_3$(0001) 적층 생장 연구)

  • 이종철;김신철;김효배;정광호;김긍호;최원국;송종환
    • Journal of the Korean Vacuum Society
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    • v.7 no.4
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    • pp.300-305
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    • 1998
  • Crystallinity and structual properties of the epitaxially grown Pt films on $Al_2O_3$(0001) substrate by rf magnetron sputtering at a substrate temperature of $600^{\circ}C$ were studied by using backscattering spectrometry (BS)/channeling and transmission electron microscopy (TEM) measurements. $MeV^4$He ion BS/channeling results showed that the channeling minimum yield of Pt film with a thickness of 3500$\AA$ was 4%. This indicates an excellent crystallinity of Pt film. When the thickness of Pt film was less than 200 $\AA$, the channeling minimum yield of Pt film increased sharply with the decrease in film thickness. The Pt layer on $Al_2O_3$(0001) substrate grew epitaxially to the direction of (111) with six-fold symmetry. Cross-sectional TEM images also showed that Pt film on $Al_2O_3$(0001) substrate consist of twinned domains to release the strain induced by the lattice mismatch and the surface roughness of the film increased at the twin boundaries where the strain was contcentrated.

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Anti-Reflection Coating Application of SixOy-SixNy Stacked-Layer Fabricated by Reactive Sputtering (반응성 스퍼터링으로 제작된 SixOy-SixNy 적층구조의 반사방지 코팅 응용)

  • Gim, Tzang-Jo;Lee, Boong-Joo;Shina, Paik-Kyun
    • Journal of the Korean Vacuum Society
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    • v.19 no.5
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    • pp.341-346
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    • 2010
  • In this paper, anti-reflection coating was investigated for decreasing the reflection in visible range of 400~650 [nm] through four staked layers of $Si_xO_y$ and $Si_xN_y$ thin films prepared by reactive sputtering method. Si single crystal of 6 [inch] diameter was used as a sputtering target. Ar and $O_2$ gases were used as sputtering gases for reactive sputtering for the $Si_xO_y$ thin film, and Ar and $N_2$ gases were used for reactive sputtering for the $Si_xN_y$ thin film. DC pulse power of 1900 [W] was used for the reactive sputtering. Refractive index and deposition rate were 1.50 and 2.3 [nm/sec] for the $Si_xO_y$, and 1.94 and 1.8 [nm/sec] for the $Si_xN_y$ thin film, respectively. Considering the simulation of the four layer anti-reflection coating structure with the above mentioned films, the $Si_xO_y-Si_xN_y$ stacked four-layer structure was prepared. The reflection measurement result for that structure showed that a "W" shaped anti-reflection was obtained successfully with a reflection of 1.7 [%] at 550 [nm] region and a reflection of 1 [%] at 400~650 [nm] range.

Flexural Behavior of Layered RC Slabs, which Bio-Mimics the Interface of Shell Layers, Produced by Using 3D Printable Highly Ductile Cement Composite (3D 프린팅용 고연성 시멘트 복합체를 활용한 패류 껍질층 경계면 모방형 적층 RC 슬래브의 휨 거동)

  • Chang-Jin Hyun;Ki-Seong Kwon;Ji-Seok Seo;Yun-Yong Kim
    • Journal of the Korea institute for structural maintenance and inspection
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    • v.28 no.1
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    • pp.90-97
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    • 2024
  • In this study, we employed Highly Ductile Cement Composite (HDCC) to evaluate the flexural performance of a RC slab that simulates the laminating structure of a seashell. To evaluate flexural performance, we produced conventional RC slab specimens, HDCC slab specimens, and HDCC-M slab specimens which biomimics a seashell's layered structure by inserting PE mesh inside the slab made of HDCC. A series of 4-point bending tests were conducted. Experimental results shows the flexural strength of the HDCC-M slab specimen was 1.7 times and 1.2 times higher than that of the RC and HDCC slab specimens, respectively. Furthermore, the ductility was evaluated using the ratio of yield deflection to maximum deflection, and it was confirmed that the HDCC slab test specimen exhibited the best ductility. This is most likely due to the fact that the inserted PE mesh separates the layers and increases ductility, while the HDCC passing through the mesh prevents the loss of load carrying capacity due to layer separation.

Electrical properties of multilayer actuator and linear ultrasonic motor using low temperature PZW-PMN-PZT ceramics (저온소결 PZW-PMN-PZT 세라믹을 이용한 적층액츄에이터 및 선형초음파 모터의 전긱적 특성)

  • Lee, Il-Ha;Yoo, Ju-Hyun;Hong, Jae-Il;Jeong, Yeong-Ho;Yoon, Hyun-Sang
    • Proceedings of the Korean Institute of Electrical and Electronic Material Engineers Conference
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    • 2008.11a
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    • pp.206-206
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    • 2008
  • 압전소자를 이용한 초음파 모터는 전자기적 원리로 동작하는 기존의 모터에 비해 구조가 간단하고 소형, 경량화가 가능하며 저속에서 큰 토크가 가능하고 ${\mu}m$단위 까지 정밀제어가 가능하다는 장점 등으로 인해 그 응용분야가 점차 확대되고 있다. 초음파 모터의 원리는 수평과 수직방향에서 변위가 타원형 운동을 형성하는 것이다. 따라서 선택한 타원운동의 방식에 의해서 모터의 형상이 달라진다. 초음파 모터는 액츄에이터를 사용하여 만들기 때문에 액츄에이터의 특성은 모터의 타원변위나 토크에 영향을 미친다. 단판형 액츄에이터에 비하여 적층 액츄에이터는 입력 임피던스를 낮추어 낮은 구동전압에서 구동이 가능하며 큰 변위와 토크를 발생하기 때문에 진동자의 수명 향상과 구동전압을 낮추기에 적합하다. 적층 액츄에이터는 변위량이나 응력 등을 개선하기 위해서 전기기계 결합계수(kp) 및 압전 d상수가 큰 재료가 요구되며, 고전압에서 장시간 구동 시 마찰에 의한 열손실을 감소시키기 위해 높은 기계적 품질계수(Qm)를 가져야한다. 적층 시 내부전극으로 사용하는 Pd, Pt가 함유된 전극은 가격이 비싸 제조비용을 상승시킨다. 상대적으로 값싼 Ag전극을 사용하면 비용절감을 할 수 있지만 융점이 낮아서 저온소결이 불가피하다. 따라서, 특성이 우수한 적층 액츄에이터를 제조하기 위해서 저손실, 저온소결 할 수 있는 액츄에이터 재료가 필요한 실정이다. L1-B4 혈 선혈 초음파 모터는 L1모드와 B4모드의 공진 주파수가 일치하여야 큰 변위를 얻을 수 있는데 이전의 논문에서 Atila를 이용한 시뮬레이션 결과를 분석한 봐 있다. 적층 액츄에이터의 층수를 5,7,9,11,13,15층으로 하여 L1-B4모드에서의 공진주파수를 비교한 결과 13 층일 때 두 모드가 비슷한 공진주파수를 보였고, 티원변위궤적도 다른 층수에 비해 크게 나타났다. 본 연구에서는 시뮬레이션 결과 가장 좋은 특성을 보인 13층 액츄에이터로 선형 초음파 모터를 제작하였다. 또한, 액츄에이터는 압전 및 유전특성이 우수한 저온소결 PZW-PMN-PZT세라믹을 이용하여 제작하였고, 내부전극으로 Ag전극을 사용하였다. 제작된 13 층 선형초음파모터를 가지고 프리로드 및 전압에 따른 속도를 조사하였고, 시뮬레이션 결과와 비교해 보았다.

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A Study on Mechanical Properties of Strand/Particle Composites (II) - Measuring of Young's Moduli and Estimating of Anisotropy Using an Ultrasonic Method - (스트랜드/파티클 복합체의 기계적 성질에 관한 연구(II) - 탄성률 측정 및 초음파법에 의한 이방성의 예측 -)

  • Kim, Yu-Jung
    • Journal of the Korean Wood Science and Technology
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    • v.29 no.1
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    • pp.22-30
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    • 2001
  • Composites with various layer constructions involving the ratio of S/P were produced from wood strands(S) and particles(P) (Cryptomeria japonica D.Don) to measure various Young's moduli and anisotropy by ultrasonics. As a result, static Young's moduli of composites were almost same as dynamic Young's moduli obtained from natural frequency. However, these were smaller than those evaluated from ultrasonic wave propagation velocity. The differences between propagation velocity of the parallel(${\parallel}$) and perpendicular(${\bot}$) in-plane direction resulted in a tendency of anisotropy. The tendency of anisotropy was larger in three-layer constructions than in seven-layer constructions. The differences of strand surface layers showed larger values than those of particle surface layers. Also, composites with higher weight ratio of strand had a tendency to propagate rapidly in each direction. In contrast to these results, the propagation velocity in the thickness direction had a tendency to propagate rapidly in composites with particle surface layers and the lower weight ratio of strand.

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Structural analysis of a thick composite rotor hub system by using equivalent properties (등가 물성을 이용한 두꺼운 복합재 로터 허브 시스템의 구조 해석)

  • ;Yanti Rachmadini
    • Composites Research
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    • v.16 no.5
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    • pp.7-14
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    • 2003
  • Modeling of thick composite structures for finite element analysis is relatively complicated. 2-D plane elements may cause inaccurate result since the plane stress condition cannot be applicable in these structures. Therefore a 3-D modeling should be used. However, the difficulty to model all the layers with different material properties and ply orientation arise in this case. In this paper, an equivalent modeling is proposed and numerically tested for analysis of thick composite structures. By grouping layers with same material and ply orientation, number of elements through the thickness is remarkably reduced and still the result is close enough to the one from a detail finite element model. MSC/NASTRAN and PATRAN are used for the analysis. The proposed modeling technique has been applied for analysis of composite rotor hub system designed by Korea Aerospace Research Institute(KARI). Using the proposed equivalent modeling technique, we could conduct stress analysis for the hub system and check the safety factor of each part.

Validation of Structural Safety on Multi-layered Blade-type Vibration Isolator for Cryocooler under Launch Vibration Environment (적층형 블레이드가 적용된 냉각기용 진동절연기의 발사환경에서의 구조건전성 검증)

  • Jeon, Young-Hyeon;Ko, Dai-Ho;Jo, Mun-Shin;Oh, Hyun-Ung
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.46 no.7
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    • pp.575-582
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    • 2018
  • The spaceborne cooler is applied to cool down of the focal plane of the infrared detector of the observation satellite. However, this cooler induces unnecessary micro-jitter which can degrade the image quality of the high-resolution observation satellite. In this study, we proposed a multi-layered blade type vibration isolator to attenuate micro-vibration generated from a spaceborne cooler, while assuring structural safety of the cooler under severe launch loads without an additional launch-lock device. The blade of the isolator is formed with multi-layers in order to obtain durability against fatigue failure and an adhesive is applied between each layers for granting high damping capability under launch vibration environment. In this study, the basic characteristics of the isolator were measured using the free-vibration test. The effectiveness of the isolator design was demonstrated by launch vibration test at qualification level.

Analytical and Experimental Study on the Damping of Vibrating Layered Plates Including the Effects of Shear and Thickness Deformation of the Adhesive Layer (접착제층의 전단과 법선변형 효과를 고려한 적층판의 진동감쇠특성 연구)

  • 김재호;박태학
    • Transactions of the Korean Society of Mechanical Engineers
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    • v.16 no.7
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    • pp.1244-1254
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    • 1992
  • This paper investigates the vibrational damping characteristics of laminated plates composed of elastic, viscoelastic and elastic layers by theoretical and experimental methods. Laminated plates are in cylindrical bending and visco-elastic adhesive layer is assumed as the visco-elastic spring which takes damping effect through both shear and normal deformations. Governing equations oof laminated plates are derived in the form of simultaneous first order differential equations, which account for the longitudinal displacements, rotary inertia and shear deformations of elastic base plate and elastic constraining plate. The numerical calculations of the equations are illustrated by the applications to the cantilever beam in transverse vibration. The results of the solutions agree well with the experimental measurements in general. The damping effects due to the shear and thickness deformations in the adhesives are analyzed and it is shown that for thicker adhesives, the damping effect due to thickness deformation becomes significant and for thinner adhesives, due to shear deformation.