• 한국군사과학기술학회지
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• 제3권2호
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• pp.231-243
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• 2000

This paper describes a simulation of secondary motion of piston assemblies using PISDYN by Ricardo. Motions of the piston, pin, rod and skirt are separately calculated, by integrating equations of motion for individual components and dynamic degrees of freedom. The effects of engine speed at full load and pin offsets on the piston assembly secondary motions, forces and friction were investigated in parametric study for 4-cylinder gasoline engine. Results show that lateral displacement and friction loss of the piston increase as a function of engine speed. The lateral motion of the piston is affected by the change in pin offset. The minimum friction loss for the condition of 4800rpm WOT occurs at a pin offset of 1.6mm.

• 한국소음진동공학회논문집
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• 제22권11호
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• pp.1057-1063
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• 2012

A cycloid speed reducer is a type of the speed reducers. The cycloid speed reducer has a eccentric rotating motion and offset to avoid some problem of assembly, so it has a disadvantage for vibration. In this paper, a multi-body dynamic model is developed for a cycloid speed reducer and the dynamic behaviors of the reducer are investigated. The cycloid speed reducer consists of cycloidal plate gears, housing gear, input shaft, output pin and shaft, and eccentric bearings. Using a CAD program, each component of cycloid reducer is modeled based on the offset and multi-body simulations are performed using Recurdyn. As a result, the pin reaction force and the amplitude of bearing displacement are increased by the offset.

• 한국통신학회논문지
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• 제26권12C호
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• pp.268-272
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• 2001

본 논문에서는 24.42 GHz 전압제어 Hair-Pin 공진 발진기, 주파수 분주기, 완충 증폭기,-l0 dB 방향성 결합기, 위상 비교기를 이용하여 B-WLL용 PLVCO LO회로를 설계 및 제작하였다. 위상 고정된 발진기는 24.42GHz에서 16.5dBm의 출력을 나타내었으며 위상잡음은 중심주파수 24.42 GHz의 100kHz offset된 지점에서 -76.3 dBc/Hz, 10 kHz offset에서 -72.8 dBc/Hz를 얻었다.

• 한국통신학회논문지
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• 제27권5C호
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• pp.530-534
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• 2002

본 논문에서는 발진기의 안정도를 높이기 위해 2차 고조파를 병렬 궤환하는 새로운 구조로 자체 위상고정의 효과를 나타낼 수 있도록 제안하였다. 이 구조는 Hair-Pin 공진 발진기를 사용한 대역통과 여파기, 방향성 결합기, 기본주파수 발진기, 체배기, 그리고 출력전력의 궤환 및 격리를 위한 Wilkinson 전력분배기로 구성되었다. 제안된 발진기는 19.5GHz에서 2.5dBm의 출력을 나타내었으며 기본 주파수 억압 -25 dBc, 위상잡음은 중심주파수 19.5 GHz의 10 kHz offset 지점에서 -76.52 dBc/Hz의 안정된 특성을 얻었다.

• 한국자동차공학회논문집
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• 제1권3호
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• pp.22-33
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• 1993

A theoretical analysis of predicting the detailed motion of a piston-crank mechanism within piston-guide clearance is presented, and the analysis is applied to the piston motion in a gasoline engine. A piston movement program is developed to calculate the piston attitude relative to the bore, the piston to bore impact velocity and kinetic energy loss and the net transverse force acting on the piston. This paper presents the formulation of a set of differential equations governing the transverse and rotational motion of a piston. These equations of motion were solved by well established Runge-Kutta method. As a result of this study, it is possible to predict the effects of piston geometry and piston pin offset on a piston motion and kinetic energy loss.

• 대한기계학회논문집A
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• 제26권8호
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• pp.1591-1598
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• 2002

This paper reports on the effects of crankshaft offset on the engine friction. The effects of crank offset are investigated through the theoretical analysis. In this study, the mathematical models are presented fer evaluationg the friction level of each engine parts. Crank offset influences on the side force acted on the piston pin and sliding speed of piston. Crank offset is very effective to reduce the piston skirt friction. With application of crank offset, total engine friction decreases at low engine speed, but that increase as engine speed increases.

• 설비공학논문집
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• 제13권4호
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• pp.271-287
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• 2001

This paper has been made to investigate the thermal performance characteristics for the several types of layered aluminum heat sinks with offset-strip fin. Heat sinks with different fin height, fin length, number of fin layer and slanted fin are prepared and tested for natural convection as well as forced convection. The experimental results for layered heat sink(LHS) are compared to those for advanced pin fin heat sink (PHS) so that the appropriate heat sink can be designed or chosen according to the heating conditions. The overall heat transfer performances for LHS are almost comparable to those of PHS under natural convection, and become 1.2∼1.5 times as high as those of PHS under forced convection situation. This study shows that fin height and number of fin layer re important parameters, which have a serious influence on thermal performance for layered heat sinks.

• 한국정보통신학회논문지
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• 제5권7호
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• pp.1210-1218
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• 2001

본 논문에서는 이동식 레이더, 마이크로웨이브 통신 시스템의 송, 수신단에 사용되는 마이크로파 신호원이나 국부 발진기에 사용할 수 있는 발진기를 헤어핀 공진기를 이용하여 설계 및 제작 하였다. 이동식 레이더 시스템에 적용하기 위해서 비교적 충격에 강한 혜어핀 구조의 공진기를 이용하였고, 또한 위상잡음과 출력을 개선시키기 위하여 직렬 궤환 형식의 시스템을 이용하였다. 전체 모의 실험은 모의 실험 프로그램인 HP의 ADS로 했으며, 제작한 제품의 측정 결과 10.525 GHz에서 6.93dBm의 출력과 -23.9 dBc의 제2 고조파의 억압 효과, 그리고 100kHz offset에서 -57.74 dBc의 위상 잡음을 얻었다.

• 한국소음진동공학회논문집
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• 제23권3호
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• pp.234-239
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• 2013

There are many types of speed reducer for industrial uses. However the cycloid speed reducer is widely used in manipulators based on excellent performance of low backlash, high reduction ratio and compact size. It is essential to use precision speed reducer for accuracy of position controls on robot systems and electric vehicles. The cycloid speed reducer has a eccentric rotating motion and offset to avoid some problem of assembly, so it has a disadvantage for vibration. In this paper, a multi-body dynamic model is developed for a cycloid speed reducer and the dynamic behaviors of the reducer are investigated. The cycloid speed reducer consists of cycloidal plate gears, housing gear, input shaft, output pin and shaft, and eccentric bearings. Using a CAD program, each component of cycloid reducer is modeled based on the offset and eccentric. Multi-body simulations using Recurdyn and test using a rig tester are performed. As a result, the pin reaction force and the amplitude of housing displacement are increased by the larger offset and smaller eccentric value of cycloid reducer.

• KSTLE International Journal
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• 제3권2호
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• pp.84-89
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• 2002

Clearance movements of engine piston are very related to the piston impact to the engine block as well as many tribological problems. Some of the major parameters that influence these kinds of performances are piston profiles, piston offsets and clearance magnitudes. In our study, computational investigation is performed about the piston movements in the clearance between piston and cylinder liner by changing the skirt profiles and piston offsets. Our results show that curved profile and more offset magnitude to thrust side have better performance that has low side impact during the engine cycle.