• Journal of Advanced Marine Engineering and Technology
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• 제29권8호
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• pp.891-898
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• 2005

Inertia welding is a solid-state welding process in which butt welds in materials are made in bar and in ring form at the joint race, and energy required lot welding is obtained from a rotating flywheel. The stored energy is converted to frictional heat at the interface under axial load. The quality of the welded joint depends on many parameters, including axial force, initial revolution speed and energy amount of upset. working time, and residual stresses in the joint. Inertia welding was conducted to make the large exhaust valve spindle for low speed marine diesel engine. superalloy Nimonic 80A for valve head of 540mm and high alloy SNCrW for valve stem of 115mm. Due to different material characteristics such as, thermal conductivity and flow stress. on the two sides of the weld interface, modeling is crucial in determining the optimal weld geometry and Parameters. FE simulation was performed by the commercial code DEFORM-2D. A good agreement between the Predicted and actual welded shape is observed. It is expected that modeling will significantly reduce the number of experimental trials needed to determine the weld parameters. especially for welds for which are very expensive materials or large shaft. Many kinds of tests, including macro and microstructure observation, chemical composition tensile , hardness and fatigue test , are conducted to evaluate the qualify of welded joints. Based on the results of the tests it can be concluded that the inertia welding joints of the superalloy exhaust valve spindle are better properties than the material specification of SNCrW.

• 대한기계학회:학술대회논문집
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• 대한기계학회 2004년도 추계학술대회
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• pp.1122-1127
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• 2004

an isolated droplet combustion exposed to pressure perturbations in stagnant gaseous environment is numerically conducted. Governing equations are solved for flow parameters at gas and liquid phases separately and thermodynamic parameters at the interfacial boundary are matched for problem closure. For high-pressure effects, vapor-liquid interfacial thermodynamics is rigorously treated. A series of parametric calculations in terms of mean pressure level and wave frequencies are carried out employing a n-pentane droplet in stagnant gaseous air. Results show that the operating pressure and driving frequency have an important role in determining the amplitude and phase lag of a combustion response. Mass evaporation rate responding to pressure waves is amplified with increase in pressure due to substantial reduction in latent heat of vaporization. Phase difference between pressure and evaporation rate decreases due to the reduced thermal inertia at high pressure. In addition to this, augmentation of perturbation frequency also enhances amplification of vaporization rate because the time period for the pressure oscillation is much smaller than the liquid thermal inertia time. The phase of evaporation rate shifts backward due to the elevated thermal inertia at high acoustic frequency.

• Tribology and Lubricants
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• 제13권1호
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• pp.14-20
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• 1997

This paper reports on theoretical study of the pressure overshoot in the delivery ports and pressure rising within balanced type vane pump. Pressure overshoot occur due to the accelerated fluid through the notch, so, result in pressure ripple, flow ripple, and noise. For calculating the pressure rising and fluctuations of pressure, we have modeled mathematically used continuity equation based on compressibility and momentum equation considered fluid inertia in the notch, and analyzed simultaneously. As a results of analysis, we have found oscillation of pressure and compression chamber pressure depend on the rotational speeds, notches. Using the model, notches have been shown to be important design factor in relaxing the rapid pressure rising and reducing the amplitudes of pressure overshoot.

• 한국기계가공학회지
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• 제18권11호
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• pp.47-56
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• 2019

A deep neural network (DNN) model was proposed to predict the upset in the inertia friction welding process using a database comprising results from a series of FEM analyses. For the database, the upset length, upset beginning time, and upset completion time were extracted from the results of the FEM analyses obtained with various of axial pressure and initial rotational speed. A total of 35 training sets were constructed to train the proposed DNN with 4 hidden layers and 512 neurons in each layer, which can relate the input parameters to the welding results. The mean of the summation of squared error between the predicted results and the true results can be constrained to within 1.0e-4 after the training. Further, the network model was tested with another 10 sets of welding input parameters and results for comparison with FEM. The test showed that the relative error of DNN was within 2.8% for the prediction of upset. The results of DNN application revealed that the model could effectively provide welding results with respect to the exactness and cost for each combination of the welding input parameters.

• 대한기계학회논문집A
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• 제41권3호
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• pp.205-211
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• 2017

차량제어의 고도화에 의해, 자동 대열 주행 제어와 같은 정밀한 제어의 필요성이 더욱 높아지고 있다. 정밀 제어를 수행하기 위해서는 차량제어에 필요한 차량 파라미터를 항상 파악하는 것이 중요하다. 특히 화물 운송용 트럭의 경우, 화물 적재 상태에 따라 차량 질량과 차량 관성모멘트 등의 차량 파라미터가 크게 변화한다. 따라서 미지의 파라미터가 있을 경우, 실시간으로 파라미터 추정하여 제어시스템에의 반영이 요구된다. 본 연구에서는 차량이 곡선 주행할 때에 차량의 조향제어에 중요한 차량 파라미터 중 하나인 요관성모멘트에 대하여 Dual Kalman filter알고리즘과 GPS센서를 이용하여 차량이 주행 중에 미지의 요관성모멘트 값을 실시간으로 추정할 수 있는 방법을 제안하고, 차량동역학 상용 프로그램을 이용한 시뮬레이션을 통해 추정방법의 타당성을 검토한다.

• 한국산학기술학회논문지
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• 제17권9호
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• pp.688-693
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• 2016

본 논문에서는 현재 고고도 이탈 및 저고도 개산강하(HALO, High Altitude Low Opening)용으로 사용하고 있는 군용 낙하산의 훈련 시뮬레이터 개발을 위해 필요한 낙하산 모델링 및 시뮬레이션 결과를 정리하였다. 대상인 군용 낙하산은 파라포일(Parafoil) 형태의 사각 낙하산으로 원형 낙하산과는 달리 강하자가 조종을 통해 원하는 위치로 유도할 수 있는 기동성이 뛰어나 공수부대원들의 적진 침투시에 주로 이용된다. 실재 낙하산의 형상자료를 이용하여 파라포일과 낙하물의 질점 모델을 기반으로 9-자유도 비선형 운동방정식을 유도하고, 각각의 관성모멘트와 공력 미계수를 산출하여 MATLAB/Simulink 기반의 비선형 시뮬레이션을 수행하여 그 결과를 나타내었다. 특히 낙하산과 같은 공기부양(LTA, Lighter-Than-Air) 비행체는 일반적인 항공기 비선형 운동과 달리 부가질량(Added Mass) 및 부가 관성모멘트(Added Moment of Inertia)의 효과가 크기 때문에 이에 대한 경험수식을 바탕으로 동역학 모델링에 포함하여 고려하였다. 수행된 낙하산 운동 모델링의 검증을 위해 비대칭 조종입력을 통한 나선형 강하 비행조건을 시뮬레이션하여 대상 군용 낙하산에서 제시된 실재 성능값과 시뮬레이션 결과치를 비교하여 유도된 운동모델이 타당함을 검증하고 그 결과를 나타내었다.

• 전력전자학회:학술대회논문집
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• 전력전자학회 2000년도 전력전자학술대회 논문집
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• pp.232-236
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• 2000

In this paper a novel estimation algorithm of mechanical parameters in two-mass system is proposed. The inertia of a load and a motor and the stiffness are estimated by using RLS (Recursive Least Square) algorithm and acceleration information of motor. The effectiveness of the proposed scheme is verified with simulation and experiments results.

• Journal of Mechanical Science and Technology
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• 제14권6호
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• pp.590-596
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• 2000

Cause of excessive vibration with twice the rotational speed of a two-pole generator rotor for the fossil power plants was investigated. The two-pole generator rotor, treated as a typically asymmetric rotor in vibration analysis, produces asynchronous vibration with twice the rotational speed, sub-harmonic critical speeds, and potentially unstable operating zones due to its own inertia and/or stiffness asymmetry. This paper introduces a practical balancing procedure, and presents the results of the investigation on sources of the excessive vibration based on the experimental vibration data of the asymmetric two-pole rotor in balancing.

• Tribology and Lubricants
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• 제2권1호
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• pp.30-38
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• 1986

In the paper, static characteristics of spiral grooved seal is theoretically obtained by Using Navier-Stokes equation. In the analysis, inertia term of fluid is considered and the flow and pressure in the steady state are obtained for the groove direction and vertical to the groove direction. As the journal rotating frequency increases, the leakage flow decreases. Therefore, zero net leakage flow is possible at the region of some rotating frequency.

• 대한기계학회논문집
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• 제19권3호
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• pp.605-614
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• 1995

In the automatic transmission using planetary gear there exists nonlinearities due to the finite difference between gear ratios, which yield torque hole during shift and influence on the ride quality and life of clutch. Based on the reaction carrier and converter turbine speed sliding functions are defined. Nonlinear closed-loop control laws are derived using them. Computer simulation shows that the closed loop design is better than the open loop design and semi-closed loop design.