• Journal of the Korean Society of Fisheries and Ocean Technology
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• v.37 no.4
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• pp.275-284
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• 2001

The for this study, turning circle tests and maneuvering indices were conducted to study and evaluate the maneuverabilities of the fishery training ship M.S. A-RA(G/T : 990tons). The results obtained were summarized as follows : 1. The advances of the starboard and port of the turning circle were measured based on the dumb card test method were 198m, 192m, the size of tactical diameters of them were 194m, 188m, respectively. 2. The advances at the starboard and port of the turning circles were measured according to the DGPS positioning obtained 196m, 194m, the size of tactical diameters of them were 194m, 190m, respectively. 3. The results were compared which came from the sizes of turning circle measured up with the dumb card test method during the trial test and from the size of turning circle measured according to the DGPS positioning. The advance of the turning circle measured at the time of the starboard turning according to the DGPS positioning was 1m longer than that of the trial test. And it was 21m shorter at the time of the port turning. 4. The rudder was steered at $35^{\circ}$ of rudder angle each starboard and port while the ship M.S. A-RA was advancing at full speed of 13 k't. The velocity of the ship was reduced to 7.8 k't at $180^{\circ}$ of turning angle and 6.0 k't at $360^{\circ}$ of turning angle and mean values of turning angular velocity of the port and starboard were $2.4^{\circ}$/sec and $2.3^{\circ}$/sec, respectively. 5. The Z test at each $10^{\circ}$, $20^{\circ}$, and $30^{\circ}$ of rudder angle was carried out to have the maneuvering indices K and T measured. K for the each rudder angle were 1.24, 1.45, and 1.65 while T for the each rudder angle were 0.33, 0.20, and 0.14. That is, K at the Z test at $30^{\circ}$ was greater than at the Z test of $10^{\circ}$ and $20^{\circ}$ while T at the $30^{\circ}$ Z test was less than at the Z test of $10^{\circ}$ and 20.

• Proceedings of the Korean Institute of Navigation and Port Research Conference
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• 2018.11a
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• pp.9-11
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• 2018

선박의 파랑 중 조종성능 변화를 추정하기 위하여 선박해양플랜트연구소 공학수조에서 KCS 선형의 모형선으로 파랑 중 자유항주모형시험을 수행하였다. 파향, 파고, 파장 등이 변화는 규칙파 상태에서 KCS 선형의 35도 선회시험을 수행하여 파 중 선회궤적변화를 관찰하였고, 정상선회 상태에서 속도기반 궤적밀림 지수를 계산하였다. 계산된 속도기반 궤적지수를 정수 중 초기선회 상태에 외력으로 작용하여 그 시뮬레이션 결과를 보정하고 이를 파랑 중 초기선회 성능과 비교분석하였다. 그 결과 초기 선회 중 도출되는 선회성능인 전진거리, 전술선회직경은 선수파일 경우, 모형선의 전진방향 속도 변화를 추가적으로 고려해야함을 확인하였다.

• Proceedings of the Korean Society for Agricultural Machinery Conference
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• 2017.04a
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• pp.13-13
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• 2017

선회시스템의 수명을 정확히 예측하기 위해서는 굴삭기의 상부회전체 및 선회시스템의 모든 구성요소들의 질량관성모멘트를 고려하여 선회감속기의 수명 평가를 수행해야 한다. 선회감속기의 수명 평가방법은 주로 실험실 시험으로 수행이 되며, 시험 장비는 장비 구축 편의성과 비용 등의 이유로 증속기와 굴삭기 상부회전체의 등가 관성체 등으로 구성된다. 굴삭기 선회시스템의 정확한 등가 실험실 시험을 위해서는 시험에 사용되는 등가 관성체의 관성모멘트를 정확히 결정하는 것이 매우 중요하다. 본 연구는 굴삭기 선회시스템의 등가 실험실 시험을 위해 굴삭기 상부회전체의 관성모멘트를 결정하기 위하여 수행되었다. 굴삭기 선회 시험을 통하여 선회감속기 입력 속도 및 토크를 측정하였고, 반복계산법을 이용하여 굴삭기 상부 회전체의 등가관성모멘트를 계산하였다. 굴삭기 상부회전체의 시뮬레이션 모델을 개발하여 선회 시험 결과와 시뮬레이션 모델 비교 분석을 통해 굴삭기 시뮬레이션 모델을 검증하고, 검증된 모델을 이용하여 상부회전체의 관성모멘트가 반영된 등가 실험실 시험 시뮬레이션 모델을 개발하였다.

• Proceedings of the Korean Institute of Navigation and Port Research Conference
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• 2011.06a
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• pp.346-348
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• 2011

해상에서 예부선이 항행시 부선의 선회운동으로 인하여 예부선의 안전운항에 많은 어려움을 겪고 있다. 본 연구에서는 안전한 예항업무를 위하여 실무에서 많이 사용되고 있는 2가지 부선 모델을 대상으로 skeg의 설치 유무 및 skeg의 설치 위치에 의한 부선의 선회운동과 이에 따른 예인장력을 알아보기 위해 정수중에서의 수조실험을 실행하였다. 실험결과 예인삭의 선회각도는 skeg을 설치하지 않았을 때 가장 크게 나타났고, center skeg을 설치했을 때부터 작아지기 시작하여 side skeg을 설치했을 때 예인삭의 선회각도가 급격히 작아지는 것으로 파악되었으며, 이러한 특성은 선수형상에 따라 조금씩 다르게 나타나고 있음을 확인하였다. 또한 예인삭의 선회각도가 커질수록 예인장력이 커지는 것을 알 수 있었다. 따라서 부선에 skeg을 설치하여 운항하는 것이 부선의 선회 운동을 감소시켜 최종적으로 예인장력이 작아지게 하여 안전예항업무에 도움이 될 것으로 판단된다.

• Journal of the korean Society of Automotive Engineers
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• v.9 no.5
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• pp.19-24
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• 1987

본 문에서는 선회의 정도를 나타내는 선회도가 크고 작은 대표적인 두가지 경우에 대하여 시간평균 구조와 난류혼합 특성을 나타내는 시간변동치의 상관관계를 실험적으로 구한 예를 제시함으로써 선회운동에 의한 난류혼합특성을 설명하고자 한다.

• Proceedings of the Korean Institute of Navigation and Port Research Conference
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• 2019.11a
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• pp.269-269
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• 2019

The ships are turning for the purpose of collision avoidence and change of course. It is possible that ships have capsizing accident when improper loading of cargo and excessive use rudder angle in turning. It is difficult for navigation officers to recognize the danger of heeling during a turn, because the dynamic state of the ship changes in real time. Thus, in this study, ship's heeling angle was predicted during turning using the maneuverability indices estimated from the ship's autopilot. The maneuverability indices estimated through the Kalman filter of Autopilot is real-time predictable. The turning radius was obtained from the estimated Index of turining ability and calculations of the heeling angle were possible in turning. It is intended to be used as a basic data on the prevention of danger heeling angle during turning.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.31 no.2
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• pp.63-71
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• 2003

This paper presents a robust slewing control of a flexible space structure based on sliding surface design. A sliding surface is designed for a single-axis rest-to-rest slewing in view of target angle, target angular velocity, and root monent of the flexible appendage. In comparison with the Lypunov control law, both controllers guarantee the stability and command tracking capabilities for nominal system. It is also shown that the designed control law provides further robustness to internal/external uncertainties. Extending the results of a single-axis maneuver, a sliding mode control law was sought for an arbitrary three-axis maneuver. Quaternion was used to determine the attitude of a space structure and sliding surfaces were designed for each axis, thereby a robust control law was derived considering the coupling effects between each rotational axis during the maneuver. Several numerical examples were demonstrated to show the effectiveness of the designed control law.

• Journal of the Korean Society of Propulsion Engineers
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• v.20 no.4
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• pp.40-49
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• 2016

This study aims to confirm the characteristics of low swirl combustion at our low swirl model combustor. To do it, it is experimentally conducted by evaluating the flame shape, stability region and emissions according to the swirl angle. The most significant feature of low swirl combustion is a occurrence of lifted flame. Such lifted flames happen to combine exquisitely propagating feature of premixed flame with diverging flow. This feature of lifted flame was confirmed through a velocity flow field and visualized the flame in this model combustor. The visualized flame was classified according to the thermal power and equivalence ratio. The variation study in swirl angles showed that the lean flammable limit could be extended only by swirl angles. Also, as the swirl angle increased, it was confirmed that the NOx and CO emissions were decreased due to the mixing enhancement and shorter resident time.

• Proceedings of the Korean Institute of Navigation and Port Research Conference
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• 2021.11a
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• pp.187-188
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• 2021

한국해양대학교 실습선 한나라호와 시뮬레이터 모델 선박의 제원에 따른 선회권을 비교하여 선박 제원에 따른 선회권을 분석하고, 시뮬레이터의 모델 선박을 사용하여 실제 선박의 선회 성능 및 조종 성능 평가 시 두 선박의 제원 확인에 대한 중요성을 제시한다.

• International Journal of Highway Engineering
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• v.9 no.4
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• pp.227-236
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• 2007

The design number of gyration is required in the process of asphalt mix design using gyratory compactor. The purpose of this study is to select the design number of gyration for asphalt mix design in the laboratory. Three types of methods were used to select the design number of gyration. The first method is to select the gyration number which gives the same density with the mixtures compacted with 75 blows of Marshall Compaction. The second method is to select the gyration number which gives the same deformation strength with the mixtures compacted with 75 blows of Marshall Compactor. The third method is to select the gyration number which meet the 4% air voids. Ten mixtures, one type of aggregate(granite), one type of asphalt binder(pen. 60-80), and 10 types of gradation, were prepared for the laboratory tests. As a result, 100 number of gyration was selected for the design number of gyration of the asphalt mix design. This result shows a similar trend with the design number of gyration used in the foreign countries. Thus, the design number of gyration selected in this study can be used for the asphalt mix design using the gyratory compactors.