• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.45 no.11
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• pp.951-966
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• 2017

In this work, numerical analyses are carried out and the behaviors are investigated for three types of double-acting oleo-pneumatic shock absorbers along with the mathematical models proposed in the part I of this work. After presenting each numerical algorithm corresponding to each model, the numerical algorithms are implemented as user-subroutines in MSC/ADAMS commercial multi-body dynamic software. By using the developed user-subroutines, numerical studies are carried out for compression/stretch test as well as drop test. From the comparative studies, we investigated the salient feature of each double-acting oleo-pneumatic shock absorber. Results identifies that it is possible to increase the absorbing efficiency in accordance with the requirements for aircraft landing conditions.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.45 no.11
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• pp.939-950
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• 2017

In this work, mathematical models are newly presented for three types of double-acting oleo-pneumatic shock absorbers as the first part of a comparative study on the several types of double-acting oleo-pneumatic shock absorbers. After a typical single-acting shock absorber model is presented for the sake of completeness, mathematical models of three types of double-acting shock absorbers are proposed. To derive the models, Bernoulli equation and orifice discharge coefficient are utilized along with the assumptions of incompressibility and poly-tropic process. The proposed models are expected to be used for investigation of the salient features of several types of double-acting oleo-pneumatic shock absorbers.

• Journal of the Korea Academia-Industrial cooperation Society
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• v.12 no.7
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• pp.2919-2924
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• 2011

The automatic drawer is used to absorb the movement shock and adjust its velocity when it opens and closes. The tube in shock-absorber is the cylindrical case which surrounds its parts and is made of acetal. The purpose of this study is to determine the quality stability of the tube in the shock-absorber in injection molding process. The tube which had been manufactured in the process with 4 cavity cooling unit was used. In this study, the analysis and test are carried out to determine its quality stability. Which are the quality analysis with numerical simulation and performance tests of the tube compared with one of foreign make. It is calculated that the injection press is 87.6 MPa and the deflections in X, Y, Z directions are ranged in 0.07~1.00 mm. When the researched tube is compared with the foreign made tube, the maximum bending compressive load is 231 kgf higher, average axial compressive load is 0.05 kgf higher, and the roughness(Ra) on the inner surface is $0.02\;{\mu}m$. lower. In the result, it is known that the quality of researched tube in injection mold process is stable and its performance is superior.

• Proceedings of the KIEE Conference
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• 1997.07d
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• pp.1298-1300
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• 1997

금속기판상 초전도 $YBa_2CU_3O_{7-{\delta}}$ (YBCO) 박막을 yttria-stabilized zirconia (YSZ) 완충막을 이용하여 in situ 펄스 레이저 증착법에 의해 증착하였다. YBCO 박막을 직접 금속기판에 증착하게 되면 YBCO 박막과 금속기판 사이의 계면에서 상호확산현상이 발생하기 때문에 이를 방지하기 위해 YSZ 완충막이 사용되었다. YSZ 완충막의 증착온도가 박막의 결정성과 전기적 특성에 미치는 영향을 알아보기 위해 YSZ 완충막은 여러 가지 온도로 증착되었다. YBCO 박막의 증착온도와 같은 온도로 YSZ 완충막을 증착했을 때보다 YBCO 박막의 증착온도보다 높은 온도로 YSZ 완충막을 증착했을 경우, 증착된 YBCO 박막은 x선 회절에 의해 c 축 방향으로 성장하였음을 알 수 있었고, 저항이 0이 되는 임계온도가 83K가 되는 실험 결과를 얻었다.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.35 no.7
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• pp.612-618
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• 2007

The dynamic behaviors of a KT-1 family aircraft nose landing gear have been analyzed and the optimal design of an aircraft shock absorber has been conducted to improve efficiency of shock energy absorption. The nose landing gear is modeled as a 2 DOF system using ADAMS and various operational and environmental landing conditions were considered. The results of dynamic simulation for various landing conditions agree well with experiments. Also the effect of parameters of a shock strut on the dynamic behaviors and on shock energy absorption of the nose landing gear has been evaluated for optimal design to define design variables. It has been found that the parameters of a shock strut such as oil-density and orifice area have more effects on dynamic behaviors than those of operation conditions. Optimal design is performed to maximize the efficiency of shock energy absorption using Feasible Direction Method. As a result the design values of the shock strut for maximum efficiency of shock energy absorption are derived and it turns out that efficiency and dynamic behaviors of the nose landing gear were improved by the optimal design.

• Journal of the Korea Society for Simulation
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• v.32 no.4
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• pp.1-10
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• 2023

This study examines the response when the shock by underwater explosion is transmitted to a vertical launch air-vehicle mounted on a ship using modeling and simulation, and is about a plan to increase method shock resistance to protect the air vehicle. In order to obtain an accurate mathematical model, a dynamic characteristic test was performed on similar equipment, and through this, the mathematical model could be supplemented. And, using the supplemented mathematical model, the air vehicle simulated the shock response by the underwater explosion specified in the BV043 standard. As a result of the first simulation, it was confirmed that air vehicle could not withstand shock, and air vehicle protection method using a ring spring type shock absorber was studied. In addition to the basic shape of abosber, it was confirmed that the ring spring absober can be used to increase the impact resistance of a shipborn vertical launch vehicle by performing simulations for each case by changing deseign varables.

• Proceedings of the KSME Conference
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• 2008.11a
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• pp.932-937
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• 2008

The pulsation of a reciprocating type hydrogen compressor is occurred from the mechanism and this pulsation makes much noise and vibration. To reduce this pulsation, snubber is usually installed on that. To maintain the efficiency in the reciprocating type hydrogen compressor, the pulsation and vibration should be reduced. so it is necessary to research about the characteristic of pulsation and vibration. Therefore in this paper, the vibration characteristic of the snubber is analyzed in the base of optimized modeling condition through the flowing analysis of existing snubber. The prototype of reciprocating type hydrogen compressor is analyzed with numerical analysis. And making sure the present condition of hydrogen compressor through measurement of vibration and noise, and then it is established that the vibration characteristic data base on numerical analysis which will be develope.

• Journal of Biosystems Engineering
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• v.28 no.2
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• pp.143-150
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• 2003

전분 완충재의 물리적, 기계적 특성을 개선하기 위한 노력들이 많이 이루어지고 있지만 기존의 플라스틱 완충재와 비교하면 더 많은 노력이 요구되어진다. 그래서 본 연구에서는 전분 완충재의 물리적 기계적 특성에 대한 유연제(plasticizers)와 첨가제(additives)의 영향을 규명하였다. 전분과 합성수지 그리고 여러 유연제 또는 첨가제를 혼합한 뒤 Brabender사의 일축 압출기를 이용하여 여러 축속도(60~120 rpm)에서 압출 가공한 후 물리적, 기계적 특성을 조사하였다. 전분 완충재의 밀도(bulk density)와 압축성(bulk compressibility)은 혼합물에서 물의 비율이 증가함에 따라 증가하였지만, 복원성(bulk resiliency)은 조금 감소하였다. 측정되어진 전분 완충재의 특성은 변형전분(hydroxypropylated starch)의 사용으로 향상되었다. 또한, glycerol, glycerol monostearate 그리고 alkylglucosides의 첨가도 전분 완충재의 밀도와 압축성을 증가시켰다. 염화철(II) 0.5%을 포함한 전분 완충재는 첨가제를 포함하지 않은 전분 완충재에 비하여 밀도 42%와 압축성 58%가 각각 감소한 반면, 복원성은 13%포인트 증가하였다. 변형전분과 염화철(II)이 첨가된 전분 완충재는 기존의 플라스틱 완충재에 비하여 밀도와 압축성은 떨어지지만, 대체 사용되어질 수 있는 것으로 판단되었다.

• Journal of Advanced Marine Engineering and Technology
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• v.32 no.8
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• pp.1116-1122
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• 2008

The reciprocating type hydrogen compressor has a pulsation due to the reciprocative characteristics which results in noise and vibration. Snubber is installed for the relaxation of pulsation, but it causes reduction of compressor efficiency because of pressure loss. Five types of snubber were modeled for the numerical investigation of the effect of the relative position of inlet and outlet and buffer angle on the pulsation amplitude and pressure loss. MSC/NASTRAN is used as a numerical tool to identify the vibration characteristic of each type. Frequency responses in forced vibration mode are compared for various cases and buffer angles.

• Korean Journal of Cognitive Science
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• v.23 no.4
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• pp.425-455
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• 2012

Multi-dimensional verbal short-term memory mechanisms are largely divided into the phonological channel and the lexical-semantic channel. The former is called phonological short-term memory and the latter is called semantic short-term memory. Phonological short-term memory is further segmented into the phonological input buffer and the phonological output buffer. In this study, the language performance of each of three patients with similar levels of conduction aphasia was analyzed in terms of multi-dimensional verbal short-term memory. To this end, three patients with conduction aphasia were instructed to perform four different aspects of language tasks that are spontaneous speaking, repetition, spontaneous writing, and dictation in both word and sentence level. Moreover, the patients' phonological memories and semantic short-term memories were evaluated using digit span tests and verbal learning tests. As a result, the three subjects exhibited various types of performances and error responses in the four aspects of language tests, and the short-term memory tests also did not produce identical results. The language performance of three patients with conduction aphasia can be explained according to whether the defects occurred in the semantic short-term memory, phonological input buffer and/or phonological output buffer. In this study, the relations between language and multi-dimensional verbal short-term memory were discussed based on the results of language tests and short-term memory tests in patients with conduction aphasia.