• Title/Summary/Keyword: SAFE 선도

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Evaluation of Blades Vibration Reliabilities of KGT-74 Small Gas Turbine (KGT-74소형 가스터빈 블레이드의 진동 신뢰성 평가)

  • 김영철;이동환;이안성
    • Transactions of the Korean Society for Noise and Vibration Engineering
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    • v.14 no.5
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    • pp.410-415
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    • 2004
  • To ensure a safe operation of the prototype KGT-74 kW small gas turbine, vibrational reliabilities of the compressor 1st, 2nd, and 3rd stages and turbine blades have been estimated and reviewed. FE analyses have been carried out to obtain the natural vibration characteristics of the blades, and impact modal testings have been performed on every each one of the blades to measure their 1st natural frequencies. Then, the Campbell diagram analyses have been carried out to judge the safety of the blades from resonant failures up to 6k harmonics. Results show that the compressor 1st stage blade is exposed to a potential resonant failure with 3k harmonic around a rated speed of 30,000 rpm but that the other compressor 2nd and 3rd stages and turbine blades are safe from resonant failures. Finally, 27,900 rpm is selected as the safe operation limit for the KGT-74 ㎾ gas turbine relative to the blade vibrations.

Evaluation of Blades Vibration Reliabilities of KGT-74 Small Gas Turbine (KGT-74 소형 가스터빈 블레이드의 진동 신뢰성 평가)

  • 이안성;김영철;이동환;나언주
    • Proceedings of the Korean Society for Noise and Vibration Engineering Conference
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    • 2003.05a
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    • pp.297-302
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    • 2003
  • To ensure a safe operation of the prototype KGT-74 ㎾ small gas turbine, vibrational reliabilities of the compressor 1st, 2nd. and 3rd stages and turbine blades have been estimated and reviewed. FE analyses have been tarried out to obtain the natural vibration characteristics of the blades, and impact modal testings have been performed on every each one of the blades to measure their 1st natural frequencies. Then, the Campbell diagram analyses have been carried out to Judge the safety of the blades from resonant failures up to 6k harmonics. Results show that the compressor 1st stage blade is exposed to a potential resonant failure with 3k harmonic around a rated speed of 30,000rpm but that the other compressor 2nd and 3rd stages and turbine blades are safe from resonant failures. Finally. 27,900 rpm Is selected as the safe operation limit for the KGT-74 ㎾ gas turbine relative to the blade vibrations.

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A Study on the Ship Collision Avoidance Model considered Speed (속력을 고려한 선박충돌회피모델에 관한 연구)

  • Yang, Hyoung-Seon
    • Journal of Navigation and Port Research
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    • v.30 no.10 s.116
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    • pp.779-785
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    • 2006
  • From a point of view of suggesting the method to avoid ship's collision, the speed of ships has to be considered sufficiently according to encounter angle of ships. But the new safe-guard ring of ship's collision avoidance support model in the close quarters is established assuming that the ratio of own ship' speed to a target ship's speed is less than about 1.7. Therefore in this paper, as doing a study concerned with the establishment of safe-guard ring reflected the encounter angle and the speed of ships, we will propose the new model of ship collision avoidance for safe maneuver of ship's collision avoidance.

Load Carrying Capacity of Top Down Prefounded Columns on Different Excavation Schedule (굴착순서에 따른 Top Down 선기둥 지지력 산정)

  • Rhim, Hong-Chul;Hwang, Hee-Sun
    • Journal of the Korea Institute of Building Construction
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    • v.6 no.4 s.22
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    • pp.45-52
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    • 2006
  • Top Down method is more widely used in downtown construction, recently. As underground construction constitutes a significant portion of the total construction cost and time in Top Down construction, it is important to develop a construction method to reduce the time required in underground works. The purpose of this study is to analyze load carrying capacity of Top Down prefounded columns on different excavation schedule. When several floors are excavated, the valid buckling length of prefounded column is increased and allowable buckling stress is decreased. The result shows that all columns are safe in buckling down to B3 story whether 2 or 3 stories are excavated. However, several columns are not safe from B4 story when 2 or 3 stories are excavated straightly. With these results, a process can be designed that the first three stories in the basement are excavated, and then excavate B4 story after placing concrete on B1 and B2 floor.

Safe Navigation Plan for Dredging Operations to build Sunken Tunnel for Access Road between Busan-Geoje (부산-거제간 연결도로 침매터널공사의 준설작업에 따른 안전통항방안)

  • Kim, Jung-Hoon;Gug, Seung-Gi
    • Journal of Navigation and Port Research
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    • v.30 no.10 s.116
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    • pp.825-831
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    • 2006
  • This research does by purpose that present safe navigation plan for ships during doing dredging construction with dredger crossing waterway of Gadeok Dredging operations need to build sunken tunnel that cross the bottom of the sea under waterway of Gadeok for access road construction between Busan- Geoje. Accordingly, dredger must cross and dredge waterway of Gadeok fatally. There is possibility of marine accident of collision for latent danger situation of ships to navigate waterway of Gadeok relatively. Therefore, safe navigation plan of ship is groped in reply and its countermeasure is presented. Firstly, navigating traffic in daytime was forecasted less than 20% of its maximum capacity through estimating the traffic volume and traffic congestion The proposal was presented to execute dredging operations in three-step and to establish temporary waterway after reviewing waterway design principles. The role of VTS center was emphasized in the new Busan Port, lastly.

Performance Analysis of Landing Point Designation Technique Based on Relative Distance to Hazard for Lunar Lander (달 착륙선의 위험 상대거리 기반 착륙지 선정기법 성능 분석)

  • Lee, Choong-Min;Park, Young-Bum;Park, Chan-Gook
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.44 no.1
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    • pp.12-22
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    • 2016
  • Lidar-based hazard avoidance landing system for lunar lander calculates hazard cost with respect to the desired local landing area in order to identify hazard and designate safe landing point where the cost is minimum basically using slope and roughness of the landing area. In this case, if the parameters are only considered, chosen landing target can be designated near hazard threatening the lander. In order to solve this problem and select optimal safe landing point, hazard cost based on relative distance to hazard should not be considered as well as cost based on terrain parameters. In this paper, the effect of hazard cost based on relative distance to hazard on safe landing performance was analyzed and it was confirmed that landing site designation with two relative distances to hazard results in the best safe landing performance by an experiment using three-dimensional depth camera.

The Reconstruction and the Circuit Translation of An Extended Mark Flow Graph (확장된 마크흐름선도의 재구성과 회로변환)

  • 여정모;하재목
    • Proceedings of the Korea Multimedia Society Conference
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    • 1998.04a
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    • pp.423-431
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    • 1998
  • 이진값을 가지는 이진 시스템을 모델화하고 설계하여 구현할 수 있도록 Petri Net의 한 부류인 박스의 마크수가 최대 1인 안전(safe)한 확장된 마크흐름선도(EMFG : Extended Mark Flow Graph)를 재구성하였다. 레벨박스와 펄스박스 및 게이트박스를 하나의 박스로 통일하였으며, 보존아크를 제거하고 서로 상반되는 개념을 가지는 일반아크와 역아크만을 사용하였고, 특히 트랜지션의 출력아크로 새로이 역아크를 도입함으로써 EMFG의 표현을 명확하게 하였다. 또한 EMFG에서 자기루프를 정의하였다. 그리고 이진 시스템을 모델링한 EMFG를 실제회로로 구현하는 방법이 새로이 제시되었다.

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A Study on the Application of Variable Safe-Guard Ring for the Ship Collision Avoidance in Shallow Water (천수역에서 충돌회피를 위한 가변안전경계영역 적용에 관한 연구)

  • Yang, Hyoung-Seon;Ahn, Young-Sup
    • Journal of the Korean Society of Marine Environment & Safety
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    • v.14 no.2
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    • pp.157-162
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    • 2008
  • The ship's maneuverability is the important factor to avoid ship's collisions. The ship's maneuverability is usually measured in a deep water, and the turning ability is decreased and the course stability is improved in a shallow water. The variation of the turning ability could cause the risk of collision. In this paper, we proposes application technique of Variable Safe-Guard Ring to consider the shallow water effect and to be simple to estimate the grade of collision risk simultaneously. Through the mathematical simulation, the availability of new method was varified. Therefore this method is expected enough to support a maneuver for collision avoidance.

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A Case Study of Unmanned Lunar Lander Design (무인 달 착륙선 설계 사례 분석)

  • Rew, Dong-Young;Ju, Gwang-Hyeok;Kim, Sung-Hoon;Lee, Sang-Ryool
    • Current Industrial and Technological Trends in Aerospace
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    • v.8 no.1
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    • pp.62-76
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    • 2010
  • In this paper, recent researches about the unmanned lunar lander development are studied. Objectives of this study are to derive research trends and to identify key design activities especially in early design phase of unmanned lunar lander. Case study covers SELENE-2 of Japan, LEDA and MoonNEXT of ESA, and small and modular spacecraft approach of NASA. Lunar lander concepts proposed for the International Lunar Network Anchor Nodes are also studied. For each lunar lander program, mission requirements are summarized and mission design results are reviewed. Approaches of safe lunar landing including design of navigation, guidance and control, combination of sensors, derived sensor and propulsion performance requirements are also analyzed.

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