• 제목/요약/키워드: Lift-off

검색결과 417건 처리시간 0.029초

Fabrication of a Graphene Nanoribbon with Electron Beam Lithography Using a XR-1541/PMMA Lift-Off Process

  • Jeon, Sang-Chul;Kim, Young-Su;Lee, Dong-Kyu
    • Transactions on Electrical and Electronic Materials
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    • 제11권4호
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    • pp.190-193
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    • 2010
  • This report covers an effective fabrication method of graphene nanoribbon for top-gated field effect transistors (FETs) utilizing electron beam lithography with a bi-layer resists (XR-1541/poly methtyl methacrylate) process. To improve the variation of the gating properties of FETs, the residues of an e beam resist on the graphene channel are successfully taken off through the combination of reactive ion etching and a lift-off process for the XR-1541 bi-layer. In order to identify the presence of graphene structures, atomic force microscopy measurement and Raman spectrum analysis are performed. We believe that the lift-off process with bi-layer resists could be a good solution to increase gate dielectric properties toward the high quality of graphene FETs.

농도구배와 평균속도가 삼지화염의 부상 특성에 미치는 영향에 관한 실험적 연구 (An Experimental Study on the Effects of Concentration Gradient and Mean Velocity on the Liftoff Characteristics of the Triple Flame)

  • 서정일;김남일;오광철;신현동
    • 대한기계학회논문집B
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    • 제27권8호
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    • pp.1061-1070
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    • 2003
  • A triple flame in a mixing layer was studied experimentally with concentration gradient and mean velocity by using a multi-slot burner, which can stabilize the lift-off flame. Flame stabilization condition, lift-off heights, and some other characteristics were examined for methane and propane flame within a range of very low concentration gradient. Pitot-tube and LDV(Laser Doppler Velocimetry) were used for velocity. Mass spectroscopy and Rayleigh scattering signal were used for concentration gradients. Thermo-couples and SiC TFP(Thin Filament Pyrometer) were used for temperature. It was found that minimum values of the lift-off heights exist at a certain concentration gradient for constant mean velocity and this means that the propagation velocity has a maximum value. The scales of flame to the burner nozzle and intensity variation of the diffusion flame were suspected as the cause.

언로드 성능 향상을 위한 딤플 포인트의 최적설계 (Optimal Dimple Point of SFF HDD Suspension for Improving the Unloading Performance)

  • 김기훈;이용현;이형준;박노철;박영필
    • 한국소음진동공학회:학술대회논문집
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    • 한국소음진동공학회 2007년도 춘계학술대회논문집
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    • pp.609-612
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    • 2007
  • The HDD (hard disk drive) using Load/Unload (L/UL) technology includes the benefits which are increased areal density, reduced power consumption and improved shock resistance than those of contact-start-stop (CSS). Dynamic L/UL has been widely used in portable hard disk drive and will become the key technology for developing the small form factor hard disk drive. The main design objectives of the L/UL mechanisms are no slider-disk contact or no media damage even with contact during L/UL, and a smooth and short unloading process. In this paper, we focus on lift-off force, pitch static attitude (PSA), roll static attitude (RSA) and dimple point. The "lift-off" force, defined as the minimum air bearing force, is another very important indicator of unloading performance. A large amplitude of lift-off force increases the ramp force, the unloading time, the slider oscillation and contact-possibility. PSA and RSA are also very important parameters in L/UL system and stability of slider is mainly determined by PSA and RSA. Dimple point by PSA and RSA is also important indicator. Therefore we find the optimal dimple point of SFF HDD suspension for improving the unloading performance.

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Dynamic response of a Timoshenko beam on a tensionless Pasternak foundation

  • Coskun, Irfan;Engin, Hasan;Tekin, Ayfer
    • Structural Engineering and Mechanics
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    • 제37권5호
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    • pp.489-507
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    • 2011
  • The dynamic response of a Timoshenko beam on a tensionless Pasternak foundation is investigated by assuming that the beam is subjected to a concentrated harmonic load at its middle. This action results in the creation of lift-off regions between the beam and the foundation that effect the character of the response. Although small displacements for the beam and the foundation are assumed, the problem becomes nonlinear since the contact/lift-off regions are not known at the outset. The governing equations of the beam, which are coupled in deflection and rotation, are obtained in both the contact and lift-off regions. After removing the coupling, the essentials of the problem (the contact regions) are determined by using an analytical-numerical method. The results are presented in figures to demonstrate the effects of some parameters on the extent of the contact lengths and displacements. The results are also compared with those of Bernoulli-Euler, shear, and Rayleigh beams. It is observed that the solution is not unique; for a fixed value of the frequency parameter, more than one solution (contact length) exists. The contact length of the beam increases with the increase of the frequency and rotary-inertia parameters, whereas it decreases with increasing shear foundation parameter.

Response of a finite beam on a tensionless Pasternak foundation under symmetric and asymmetric loading

  • Coskun, Irfan;Engin, Hasan;Ozmutlu, Aydin
    • Structural Engineering and Mechanics
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    • 제30권1호
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    • pp.21-36
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    • 2008
  • The static response of a finite beam resting on a tensionless Pasternak foundation and subjected to a concentrated vertical load is assessed in this study. The concentrated vertical load may be applied at the center of the beam, or it may be offset from the center. The tensionless character of the foundation results in the creation of lift-off regions between the beam and the foundation. An analytical/ numerical solution is obtained from the governing equations of the contact and lift-off regions to determine the extent of the contact region. Although there is no nonlinear term in the equations, the problem shows a nonlinear character since the contact region is not known in advance. Due to that nonlinearity, the essentials of the problem (the coordinates of the lift-off points) are calculated numerically using the Newton-Raphson technique. The numerical results are presented in figures to illustrate the behaviours of the free-free and pinned-pinned beams under symmetric or asymmetric loading. The figures illustrate the effects of the shear foundation parameter and the symmetric and asymmetric loading options on the variation of the contact lengths and the displacement of the beam.

DLC-coated Si-tip FEA 제조에 있어서 기판 상에 경사-회전 증착된 Al 희생층을 이용한 Gate누설 전류의 감소 (Decrease of Gate Leakage Current by Employing Al Sacrificial Layer Deposited on a Tilted and Rotated Substrate in the DLC-coated Si-tip FEA Fabrication)

  • 주병권;김영조
    • 마이크로전자및패키징학회지
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    • 제7권3호
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    • pp.27-29
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    • 2000
  • Lift-off를 이용한 DLC-coated Si-tip FEA 제조에 있어서 gate 절연막의 측면에 DLC가 coating되는 것을 방지하기 위해 기판 상에 Al 희생층을 경사-회전 증착한 뒤 DLC를 coating하고, 다음으로 희생층을 식각하여 tip 이외의 DLC를 제거하는 방법을 제안하였다. 이러한 Al희생층을 이용한 lift-off공정에 의해 제조된 DLC-coated Si-tip FEA의 전류전압 특성과 전류 표동 특성을 조사하였으며, gate 누설 전류의 감소와 방출 전류의 안정성을 확인하였다.

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스쿠터 승하차를 위한 밴승합차용 윈치 리프트 설계 (Design of a Winch Lift for a Scooter to Get On and Off a Coach Van)

  • 이덕영;윤재웅;이수철;임구
    • 한국정밀공학회지
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    • 제22권5호
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    • pp.189-196
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    • 2005
  • The numbers of the elder are rapidly growing who wants to enhance social activities, because Korea is already an aging society since 2000. The mobility and accessibility are the key issues to enhance them. The electric motor scooter and the power wheel chair are efficient movable means at a short range. It would be needed to get on and off them if the elder wants use them after arriving a long distant destination. But the electric scooter is too heavy for a man to get on and off a coach van. The motor winch lift is developed for the elder and the handicapped to get on and off a van easily. The lift consists of 3-linkage which can be installed in a trunk of a van with a small space. The clearance and stress of each component are checked by a computer simulation. The prototype was made. and the performances of safety and comfortableness were verified by operational ability test and durability test.

프로펠러와 고양력 장치와의 공력간섭에 대한 수치해석 연구 (NUMERICAL STUDY OF PROPELLER AND HIGH LIFT DEVICE AERODYNAMIC INTERFERENCES)

  • 박영민;김철완;정진덕;이해창
    • 한국전산유체공학회지
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    • 제16권4호
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    • pp.47-54
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    • 2011
  • A rotating propeller of turboprop aircraft gives much effect on the aerodynamic characteristics of wing such as lift, moment and stall. Specially propeller effect on the wing surface is much more dominant when aircrafts are in landing or take-off conditions. In the present paper, three dimensional Navier-Stokes simulations for the interaction of propeller and wing were carried out for medium sized turboprop aircraft. For rotating propeller, unsteady sliding mesh method was used to simulate a relative motion between moving and static bodies. For the power effect analysis in landing and take off configurations, double slotted flap was also considered and the aerodynamic characteristics were investigated. It was shown that the propeller slipstream enhanced the lift slope including maximum lift by eliminating local flow separation region and this enhancement was more dominant with high lift device.