• Journal of the Korean Wood Science and Technology
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• 제28권2호
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• pp.10-18
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• 2000

초음파를 이용한 목재의 비파괴시험은 등급구분 수분 및 결점 탐지, 썩은 정도 평가 등의 용도에 적용되고 있다. 이와 같은 기술을 실제로 적용하기 위해서는 목재 내의 초음파 전달과 목재의 성질 사이의 관계에 대한 기본적인 연구가 선행되어야 한다. 이 연구에서는 함수율과 섬유경사각이 초음파 전달 속도에 미치는 영향을 분석하기 위하여 낙엽송과 소나무를 대상으로 초음파 비파괴시험을 실시하였다. 함수율에 대한 시험을 위한 시험편은 생재상태, 30%, 20%, 10% 및 전건상태의 함수율을 갖도록 준비하였고 섬유경사각에 대한 시험을 위해서는 접선방향으로 0, 15, 30, 45, 60, 75 및 90도의 섬유경사각을 갖는 시험편을 준비하였다. 초음파 전달 속도는 섬유포화점에 근사한 30% 이하의 낮은 함수율 범위에서는 함수율에 반비례하였으며 이보다 높은 함수율 범위에서는 함수율에 관계없이 일정한 경향을 나타내었다. 목재의 압축강도와 함수율 사이의 관계에서도 이와 유사한 경향이 관찰되었다. 목재의 섬유경사각도 초음파 전달 속도 및 압축강도와 반비례하는 경향을 나타내었다. 압축강도와 초음파 전달 속도 사이의 관계는 정비례하는 관계로서 하나의 직선식으로 나타낼 수 있었다.

• 한국해양학회지
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• 제18권2호
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• pp.149-160
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• 1983

해수면과 연안표층수온의 기록으로부터 바람에 의한 용승효과를 확인하기 위해서 1973년 부터 1979년까지의 자료들이 이용되었다. 하계에 남동해안에 평행한 바람이 우세하며 울기-감포 근해에서 용승을 일으키는 것으로 나타났는데 강한 남서풍이 3일 이상지속될 때 해수면과 표층수온이 감소하는 용승효과가 현저하게 나타났다. 평균적으로 한 번의 용승은 약10일동안 지속 되었고 그 동안에 해안에 평행안 성분의 평균풍속은 약 4.0m/sec였다.

• 대한전자공학회논문지SD
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• 제44권6호
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• pp.28-33
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• 2007

BD-R/RE/ROM을 2배속으로 기록하고 재생할 수 있는 전단 시스템을 개발하였다. 시스템의 재생능력은 PR(a,b,c,d,e)형 5탭 PRML을 채택함으로써 향상되었다. 제안된 PRML덕분에 2배속 25GB 디스크에서 ${\mp}0.6{\circ}$ 이상의 라디알 및 탄젠셜 틸드 마진을 가지고도 $2{\times}10^{-4}$이하의 BER을 얻을 수 있었다. 최적파워레벨이 다른 다양한 BD-R/RE의 안정적인 기록을 위해 OPC 방법에 대해서도 제안하였다. 개발한 시스템은 $0.18-{\mu}m$ CMOS공정으로 $60mm^2$ 면적에 1,400만 트랜지스터를 칩에 집적하였다.

• International Journal of Naval Architecture and Ocean Engineering
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• 제10권3호
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• pp.361-366
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• 2018

Ice crushing occurs in many situations that involve a sliding frictional component such as sports involving ice-contact, ice interaction with ship hulls, and ice-on-ice sliding/crushing within glaciers and between interacting sea ice floes. Ice crushing-friction tests were conducted in the lab at $-10^{\circ}C$ using a set of acrylic ice-crushing platens that included a flat smooth surface and a variety of high-roughness surfaces with regular arrays of small prominences. The experiments were part of Phase II tests of the Blade Runners technology for reducing ice-induced vibration. Ice was crushed against the platens where the ice movement had both a vertical and a horizontal component. High-speed imaging through the platens was used to observe the ice contact zone as it evolved during the tests. Vertical crushing rates were in the range 10-30 mm/s and the horizontal sliding rates were in the range 4.14-30 mm/s. Three types of freshwater ice were used. Friction coefficients were extraordinarily low and were proportional to the ratio of the tangential sliding rate and the normal crushing rate. For the rough surfaces all of the friction coefficient variation was determined by the fluid dynamics of a slurry that flowed through channels that developed between leeward-facing facets of the prominences and the moving ice. The slurry originated from a highly-lubricating self-generating squeeze film of ice particles and melt located between the encroaching intact ice and the surfaces.

• 대한기계학회논문집A
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• 제27권10호
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• pp.1720-1727
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• 2003

The object of this work is to develop the measurement method of the transmission error of the helical gears. For this purpose, experimental set up is designed by 3D CAD software. It consists of the motor, inverter, powdered brake equipment, torque sensor and helical gearbox. In this study, tangential linear accelerometers were used as the methods for the transmission error measurement. the acceleration signals are transmitted to the signal conditioners through the slip rings and the transmission errors are obtained by a specially designed circuit board. The transmission errors are analyzed in the frequency domain. As a result, The periodicity of the transmission error is confirmed in the mesh frequency and its harmonics. The magnitude of harmonic components is very dependent on the natural frequencies of the gear system. It usually increases with the rotational speed. However, it does not always increase with torque.

• 한국전산유체공학회지
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• 제14권3호
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• pp.76-85
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• 2009

The shock wave is deformed and the vortex is elongated simultaneously during the shock-vortex interaction. More precisely, the shock wave is deformed to a S-shape, consisting of a leading shock and a lagging shock by which the corresponding local vortex flows are accelerated and decelerated, respectively: the vortex flow swept by the leading shock is locally expanded and the one behind the lagging shock is locally compressed. As the leading shock escapes the vortex in the order of microseconds, the expanded flow region is quickly changed to a compression region due to the implosion effect. An induced shock is developed here and propagated against the vortex flow. This happens for a strong vortex because the tangential flow velocity of the vortex core is high enough to make the induced-shock wave speed supersonic relative to the vortex flow. For a weak shock, the vortex is basically subsonic and the induced shock wave is absent. For a vortex of intermediate strength, an induced shock wave is developed in the supersonic region but dissipated prematurely in the subsonic region. We have expounded these three shock-vortex interaction patterns that depend on the vortex flow regime using a third-order ENO method and numerical shadowgraphs.

• 한국전자파학회지:전자파기술
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• 제11권4호
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• pp.39-52
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• 2000

A design of 2 stage S-DLVA(successive detector log video amplifier) was studied to detect wide dynamic radar pulse ranging from -70 ㏈m to 0㏈m. A basic design idea was focused on the linear detection in logarithmic scale of wide dynamic range radar pulses from nosie-like weak power of -70 ㏈m to relatively high power 0 ㏈m. It is highly formidable, since it requires high speed detection less than 10 nsec over the operating frequency ranges from 6 to 18 ㎓. A limiter diode, a tunnel diode and an L17-C were used as a protecting device, a detector diode and a log video amplifier in companion as a single stage detector to give voltage output proportional to the input power of about 35 ㏈ dynamic range. A protype of 2-stage DLVA having one more single stage detector was fabricated with a 32 ㏈ low noise amplifier and a 3 ㏈ hybrid coupler to provide total 70 ㏈ dynamic range detection. The logging characteristics were measured to have log slope of 25m.V/㏈ against 70 ㏈ logging range from -55 ㏈m to +15 ㏈m, the log linearity of within +/- 1.5 ㏈, and tangential sensitivity was at -63 ㏈m. The pulse dynamics of rise time and recovery time were measured as 50 nsec and 1.2 $\mu$sec, respectively. The reason might be due to the parasitic capacitances of packaged limiter, tunnel diode, and L17-C.

• 한국전기전자재료학회논문지
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• 제21권4호
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• pp.335-340
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• 2008

In this study, novel structured thin ultrasonic rotary motor has been proposed. Ultrasonic motors are based on an elliptical motion on the surface of elastic body. Thin brass plate was used as a cross shaped vibrator and eight ceramic plates were attached on upper side and bottom side of the brass plate. From the thin stator, elliptical displacements of the four contact tips were obtained. To find the optimal size of the stator, motions of the motors were simulated using ATILA by changing length, width and thickness of the ceramics. The stators had commonly three resonance peaks and contact tips of the stator moved on tangential or normal trajectories at these resonance peaks. The maximum displacements at the resonance peaks were compared. As results, maximum displacements of the contact tips were obtained at the length of 16 mm, width of 6 mm and thickness of 0.4 mm. Changes of the resonance frequencies were inversely proportional to the length of ceramic and proportional to the width of ceramic. The motor was fabricated by using the designed stator. And, the characteristics of the motor were compared with the simulated results. When the motor was fabricated with these results, speed fo 935 rpm was obtained by input voltage of 25 Vrms at 93.5 kHz.

• 한국기계가공학회지
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• 제16권6호
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• pp.41-46
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• 2017

Productivity improvement and cost reduction in the aircraft industry have become major industrial objectives, and improving productivity by reducing machining time has become a key focus. When numerical cutting code is created by CAM software, such as CATIA or UG-NX, it is impossible to control machining feed speed using cutting force changes depending on the machining tool path. However, machining an aircraft engine part from difficult material, such as Inconel 718, takes a long time, and tool chipping or breakage often occurs from forcing the machining path too quickly. This study investigated and verified the reliability of the AdvantEdge production module (PM)using cutting power tests. In particular, diffuser and diffuser case parts were considered, comparing cutting power and machining time using AdvantEdge PM and CATIA.

• Journal of Magnetics
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• 제20권2호
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• pp.186-192
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• 2015

This paper describes the electromagnetic and mechanical characteristics of coaxial magnetic gear (CMG) with a low gear ratio. The analysis models are restricted to a CMG with a gear ratio of less than 2. The electromagnetic characteristics including transmitted torque and iron losses are presented according to the variation of the gear ratio. The pole pairs of high speed rotor are chosen as 6, 8 and 10 by considering the torque capability. As the gear ratio approaches 1, both iron losses on the ferromagnetic materials and eddy current losses on the rotor permanent magnets are increased. The radial and tangential forces on the modulating pieces are calculated using the Maxwell stress tensor. When the maximum force is exerted on the modulating pieces, the mechanical characteristics including stress and deformation are derived by structural analysis. In CMG models with a low gear ratio, the maximum radial force acting on modulating pieces is larger than that in CMG models with a high gear ratio, and the normal stress and normal deformation are increased in a CMG with a low gear ratio. Therefore, modulating pieces should be designed to withstand larger radial forces in CMG with a low gear ratio compared to CMG with a high gear ratio.