• 한국가스학회지
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• 제2권3호
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• pp.88-95
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• 1998

회전기계의 진동해석은 기계의 이상을 미리 판정하여 적절한 유지 보수를 수행하기 위한 지표로 팔용이 가능하다 현재 평택기지에 설치된 고장진단시스템은 LNG펌프의 진동수치가 위험수준에 도달시 기계적 결함부위 진단을 할 수 있다. 본 연구는 Windows NT환경에서 DSP보드를 사용한 자동진단시스템 개발에 대한 것이다. 펌프의 상태진단을 위해 2개의 가속도센서로부터의 속도신호를 해석하고 펌프의 상태에 대한 다양한 그래프를 보여주며 특정 진동값을 일정시간 간격마다 저장하여 펌프의 결함 발생시 운전자가 컴퓨터 모니터에서 전문가 시스템을 활용하여 자동으로 진단하고 경향을 감시함으로써 펌프의 상태를 점검할 수 있다.

• 한국기계가공학회지
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• 제11권1호
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• pp.113-118
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• 2012

Mulching vinyl is used on field crops to reduce herbicides and this causes multiple effects. The mulching vinyl must be collected for the next crop season, but was left alone due to a shortage of labor. The used mulching vinyl that was left alone acted as one of the main sources of environmental pollution on farms. In order to solve these problems, a self-propelling vinyl remover was developed. The self-propelling vinyl remover consists of a travelling part and rotating of remover wheel. Each output device has a 1.5ps engine and a 2.5ps engine. The vinyl was twisted 17~47cm/times length. The bobbin's diameter was 160mm and it's stable travelling speed was 0.5m/s. The revolution of the remover wheel bobbin was 60rpm to maintain the wheel's linear velocity. As seen at performance test at the field which had 950mm ridge intervals and 10a area, the average working speed was 0.56m/s and the turning time was 15seconds. Therefore, the working performance was 40.1min/10a.

• 한국기계가공학회지
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• 제19권2호
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• pp.38-46
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• 2020

The purpose is to evaluate the structural characteristics of 750 mm diameter injection spiral blades under various operating conditions. A fiber-glass reinforced polypropylene material was employed to the injection blades, and mechanical tests on two kinds of glass-reinforced polypropylene were performed to evaluate the mechanical properties and to select a suitable candidate material. Also, three kinds of spiral blade geometries were studied to observe the influence of fixing rods between blades. For this, structural analyses were conducted to understand the role of fixing rods under a range of rotating speed. In addition, modal analysis was performed to confirm the resonance in the operating speed range. One-way fluid-structure interaction (FSI) analysis was carried out to know its mechanical integrity under dangerous wind speed conditions. Through this work, the structural characteristics of the proposed spiral blade geometries were studied under various operating conditions, and the requirements of mechanical properties of blades were determined.

• 한국추진공학회:학술대회논문집
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• 한국추진공학회 2007년도 제29회 추계학술대회논문집
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• pp.354-358
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• 2007

초소형 터보제트엔진에 적용되는 슬링거 인젝터 시스템의 분무특성을 파악하기 위한 연구를 수행 하였다. 이 연료 분사시스템은 엔진의 회전축으로부터 발생된 원심력에 의하여 연료가 연소기 내부로 공급되고, 액체연료의 미립화를 초래한다. 시험장치는 고속으로 회전하는 Spindle, 슬링거 인젝터, 가압식 물탱크, 아크릴 케이스로 구성하였다. 분무입자의 크기 및 속도를 측정하기 위해 PDPA(Phase Doppler Particle Analyzer) 시스템을 사용하였고, Nd-Yag Laser를 광원으로 사용하여 분무를 가시화 하였다. 시험결과 SMD(Sauter Mean Diameter)는 회전수, 유량, Injection Orifice 수에 큰 영향을 받는 것으로 나타났다. 이러한 실험적 연구로부터 이 시스템의 분무특성을 이해할 수 있었고, 초소형 터보제트엔진에 적합한 슬링거 인젝터의 형성을 도출할 수 있었다.

• 한국해양공학회지
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• 제19권6호통권67호
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• pp.78-85
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• 2005

Initial alignment and localization are important topics in inertial navigation systems, since misalignment and initial position error wholly propagate into the navigation systems and deteriorate the performance of the systems. This paper presents the error convergence characteristics of the hybrid navigation system for underwater vehicles initial position, which is based on an inertial measurement unit (IMU) accompanying a range sensor. This paper demonstrates the improvement on the navigational performance oj the hybrid system with the range information, especially focused on the convergence of the estimation of underwater vehicles initial position error. Simulations are performed with experimental data obtained from a rotating ann test with a fish model. The convergence speed and condition of the initial error removal for random initial position errors are examined with Monte Carlo simulation. In addition, numerical simulation is conducted with an AUV model in lawn-mowing survey mode to illustrate the error convergence of the hybrid navigation System for initial position error.

• 한국항공우주학회지
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• 제46권3호
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• pp.189-196
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• 2018

고고도 무인기용 프로펠러의 추력 및 토크를 측정하기 위한 시험장치를 고안하였으며, 직경 1 m급 2개의 모델에 대해 성능시험을 수행하였다. 기계적인 동력을 측정하기 위해 프로펠러 회전축에 토크센서를 설치하였으며, 작은 추력을 정밀하게 측정하기 위해 프로펠러 및 구동부 전체를 지지하는 가이드레일 시스템을 적용하였다. 반복성시험 분석 및 불확도 분석을 통해 프로펠러 성능시험에 영향을 미치는 인자들을 고찰하였다. 불확도 분석결과는 추력 로드셀의 정밀도와 시험부 풍속을 결정하는 측정인자의 정밀도가 유사한 정도로 프로펠러 성능시험에 영향을 주고 있음을 나타내고 있다. 특정 RPM 조건에서 풍속을 변경시켜가며 프로펠러의 성능을 측정한 후, 5개의 서로 다른 RPM 조건에 대한 측정결과를 프로펠러 성능계수로 나타내었다.

• 대한기계학회논문집
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• 제13권1호
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• pp.178-189
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• 1989

본 연구에서는 우선 승용차의 1/10 모형의 형상을 더욱 단순화시킨 2차원 자동차형 물체를 대상으로 하여 그 주위의 압력, 속도 및 난류량의 분포를 측정하고, 또한 울터프트(wool tuft)를 이용한 유동가시화법으로 후류구조를 파악함으로써 향후 계속될 실험적 및 수치해석적 연구의 기초를 마련하고자 한다.

• 한국자동차공학회논문집
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• 제7권8호
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• pp.91-98
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• 1999

This paper describes the air flow characteristics inside the throttle valve. Tow-dimensional steady incompressible Navier-Strokes equation are solved numerically with embedding the conceopt of the artificial compressibility and adopting the Baldwin-Lomax turbulence model. With varying the valve opening angles(the Reynolds number )such as 15$^{\circ}$(5000) , 45$^{\circ}$(3000) , 75$^{\circ}$(7000) and 90$^{\circ}$(10000), respectively. tow cases, with a valve shaft and without one, are analysed. The pressure loss between the entrance and exit is severe at 15$^{\circ}$, 100 times as larger as that of 90$^{\circ}$ case, which also depends much on the existece of the valve shaft. The counter rotating vortices are formed over the valve plate with the shaft at only 75$^{\circ}$. They are smally and very large scale in front and back of the valve shaft , respectively. The velocity profiles of 15$^{\circ}$ and 90$^{\circ}$ at the exit are almost symmetric to the horizontal center line, however, the symmetricity is no longer maintained at 45$^{\circ}$ and 75$^{\circ}$ , and in addition, the flow at 75$^{\circ}$ is enforced a lot below center line. The pressure distribution on the walls is largely changed near the valve shaft, and its magnitude becomes great as the valve angle decreases.

• 정보저장시스템학회논문집
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• 제5권1호
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• pp.47-52
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• 2009

Most hard disk drives that apply the ramp load/unload technology unload the heads at the outer edge of the disk while the disk is rotating. The load/unload includes the benefits as like an increased areal density, a reduced power consumption and an improved shock resistance. A lot of papers investigating the effects of the various load/unload parameters such as a suspension tab, a limiter, a ramp and air-bearing surface designs have been published. However, in previous researches, an effect of the suspension is not considered at each load/unload step. In this paper, we focus that a variation of the state matrix affects the load/unload performance on based on a state matrix that is a stiffness matrix of the suspension. Because the state matrix is related to the suspension at each load/unload step, to change the state matrix means the structural change of the suspension. Therefore, we investigated a range of a pitch static attitude(PSA) and a roll static attitude(RSA) for load/unload performance. We also analyzed an effect of the variation of the state matrix a range of load/unload velocity occurred a slider-disk contact. We determined the variation of the state matrix to improve the load/unload performance through comparison of each factor of state matrix.

• 유체기계공업학회:학술대회논문집
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• 유체기계공업학회 2004년도 유체기계 연구개발 발표회 논문집
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• pp.396-401
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• 2004

In this paper, a 1MW HAWT(FIL-1000) rotor blade has been designed by BEMT(Blade Element Momentum Theory) with Prandtl's tip loss. Also, a 3-D flow and performance analysis on the FIL-1000 rotor blade has been carried out by using the 3-D Navier-Stokes commercial solver (CFX-5.7) to provide more efficient design techniques to the large-scale HAWT engineers. The rated power and itsapproaching wind velocity at design point (TSR=7.5) are 1MW and 9.99m/s respectively. The rotor diameter is 54.5m and the rotating speed is 26.28rpm. Airfoils such as FFA W-301, DU91-W-250, DU93-W-210, NACA 63418, NACA 63415 consist of the rotor blade from hub to tip. Recent CFX version, 5.7 was adopted to simulate 3-D flow field and to analyze the performance characteristics of the rotor blade. Entire mesh node number is about 730,000 and it is generated by ICEM-CFD to achieve better mesh quality The predicted maximum power occurringat the design tip speed ratio is 931.45kW. Approaching to the root, the inflow angle becomes large, which causesthe blade to be stalled in the region. Therefore, k-$\omega$ SST turbulence model was used to predict the quantitative flow information more accurately. Application of commercial CFD code to optimum blade design and performance analysis was proved to be more effective environment to HAWT blade designers.