• International Journal of Aeronautical and Space Sciences
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• 제18권2호
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• pp.270-278
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• 2017

This paper describes development procedure and verification test results of a bi-propellant thruster using hydrogen peroxide and kerosene. The design thrust of the thruster is about 500 N and six swirl type coaxial injectors were used. The passage type manifolds were employed for the injector head to reduce the response time. The passage was designed to minimize stagnation points and recirculation region to ensure uniform flow distribution and sufficient cooling performance through flow analysis using Fluent. A catalytic igniter using hydrogen peroxide was installed at the center of the injector head. The propellant feeding and spray characteristics were confirmed by hydraulic tests. Combustion tests were performed on design and off-design points to analyze combustion characteristics under various mixture ratio conditions. The combustion test results show that combustion efficiency was over 95 % and chamber pressure fluctuation were less than 1.5 % under all test conditions.

• 한국CDE학회논문집
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• 제19권2호
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• pp.169-181
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• 2014

Recently ships and ocean platforms are becoming increasingly technological, unmanned, and huge. Maintenance and safety monitoring of these products is very important for safety reasons. Therefore, real-time monitoring of safety regions, such as the engine room, and hull structure, and environmental states, like fire and pressure of LNG tanks, is required for the sustainable ships. In this paper, a ZigBee-based wireless sensor network is suggested to monitor ships and ocean platforms effectively. However, this causes some telecommunication problems because these products are made of steel. To resolve this problem, we use the mesh networking of Zig-Bee that can monitor the regions and environmental states consistently. The telecommunication of such a monitoring system is tested on a real container ship and its performance is verified. The real-time monitoring results are displayed on the users' smart devices.

• Journal of Advanced Marine Engineering and Technology
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• 제28권7호
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• pp.1063-1071
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• 2004

Accurate heat release analysis of cylinder pressure data is important for evaluating performance in the development of diesel engine However, traditional single zone first law heat release model(SZM) has significant limitations due to the simplified assumption of uniform charge and neglecting local temperature inside cylinder during combustion process. In this study. heat release rate based on single zone heat release model has been evaluated by comparison with computational analysis results using Fire code which is based on multi-dimensional model(MDM). To overcome limitations due to simplicity of single zone assumption. especially the influence of specific heat ratio on gross heat release has been esteemed and newly suggested were the equation $\gamma$= $\gamma$(${T/T}_{max}$) which describes the variations of gases thermodynamic properties with mean temperature and maximum mean temperature inside cylinder Single zone heat release model applied with this equation is shown to give very good results over whole range of operating conditions when compared with computational analysis results based on multi-dimensional model.

• Computers and Concrete
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• 제1권3호
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• pp.303-324
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• 2004

The Component-Based Software Development (CBSD) has established itself as a sound paradigm in the software engineering discipline and has gained wide spread acceptance in the industry. The CBSD relies on the availability of standard software components for encapsulation of specific functionality. This paper presents the framework for the development of a software component for the design of general member cross-sections. The proposed component can be used in component-based structural engineering software or as a stand-alone program developed around the component. This paper describes the use-case scenarios for the component, its design patterns, object models, class hierarchy, the integrated and unified handling of cross-section behavior and implementation issue. It is expected that a component developed using the proposed patterns and model can be used in analysis, design and detailing packages to handle reinforced concrete, partially prestressed concrete, steel-concrete composite and steel sections. The component can provide the entire response parameters of the cross section including determination of geometric properties, elastic stresses, flexural capacity, moment-curvature, and ductility ratios. The component can also be used as the main computational engine for stand-alone section design software. The component can be further extended to handle the retrofitting and strengthening of cross-sections, shear and torsional response, determination of fire-damage parameters, etc.

• 대한인간공학회지
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• 제29권4호
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• pp.673-680
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• 2010

The effects of different auditory warnings on response time and accuracy were studied in a laboratory ship-bridge work environment. Subjective preference on the type of auditory warnings was also of a primary concern. Twenty five subjects were asked to select an appropriate button for the warning sound presented with three types of auditory warning (abstract sound, auditory icon, and voice alarm) and five levels of warning situation (fire, steering failure, collision, engine failure, and low power). Results showed that the response time and accuracy was significantly affected by the types of auditory warning. The voice alarm resulted in a higher accuracy and subjective preference, as compared to the auditory icon and abstract sound. Regarding the response time, auditory icons and voice alarms were equivalent and superior to abstract sounds. Actual or potential applications of this research include guidelines for the design of integrated ship bridge systems.

• 한국추진공학회지
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• 제8권4호
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• pp.84-90
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• 2004

추진제 주입압력 350 psia 에서 0.95 lbf 의 정상상태 공칭추력을 내는 단일액체추진제 하이드라진 추력기의 성능평가 결과를 추력, 임펄스 비트, 비추력 등을 통하여 제시한다. 연소시험 형상과 절차에 대한 간략한 묘사와 더불어 정상상태 연소모드로부터 얻어지는 추진제 공급압력. 질량유량, 추력기 작동환경 진공도, 그리고 추력 등의 변이거동에 대한 전형적인 결과를 검토한다. 제시된 추력기 성능은 1-lbf급 표준형 단일추진제 로켓엔진의 기준성능에 성공적으로 비교된다. 선별된 추력기군을 위성체 추진시스템의 비행모델로 채택하기 위한 추력기간 성능편차에 대해 부연한다.

• 한국추진공학회지
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• 제4권3호
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• pp.38-44
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• 2000

통상적으로 액체로켓의 노즐은 재생냉각에 의해 고온의 연소가스로부터 보호된다. 그러나 재생 냉각의 경우, 시스템에 상당한 투자가 요구되며, 잦은 엔진 결함의 원인을 제공하기도 한다. 최근들어 액체로켓에 재생냉각을 사용하지 않고, 연소실과 노즐 보호를 위해 삭마재료가 사용되고 있다. 노즐재료에 대한 삭마량과 삭마형상 연구를 위해 500회 이상의 연소실험이 수행되었다. 그러나 연소실험을 통한 삭마특성은 전혀 예측할 수 없는 방향으로 진행되고 있으며, 실험에 사용된 액체로켓의 작동범위가 실제 로켓과 거의 유사하다는 것을 감안한다면, 삭마재질을 로켓에 적용하기 위해서는 상당한 주의가 필요할 것으로 판단된다. 실험변수는 추진제의 공급 순서, 인젝터의 형상, 점화기의 위치, 그리고 액체산소의 공급온도이다.

• 대한조선학회논문집
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• 제55권3호
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• pp.274-280
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• 2018

This paper deals with the calculation of vulnerable areas of critical components required for the assessment of naval ship's vulnerability. Taking into account the effectiveness of threatening weapons, the probability density function of damage was used to assess vulnerable areas or vulnerabilities of critical components. It is shown that the vulnerable area of critical component can be simply computed from the damage function. Considering the weapon effectiveness of fragmentation and explosion on the target, both Carleton Damage Function and Rectangular Cookie Cutter Function representing the probability of damage are applied to the vulnerable area assessment. Carleton damage function is utilized to describe the weapon-target interaction in the vulnerability analyses. A problem of blast effect against an assumed naval ship is chosen as a case study. Vulnerability is evaluated by applying the suggested method to the equipments arranged in the engine room of the virtual ship.

• 한국항해항만학회:학술대회논문집
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• 한국항해항만학회 2019년도 추계학술대회
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• pp.266-266
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• 2019

해마다 증가하고 있는 해양사고는 기관고장, 충돌, 좌초, 화재 등 다양하게 발생하고 있다. 이러한 해양사고는 대형 인명사고의 위험이 있어 사전에 사고를 예방 하는 게 무엇보다 중요하다. 이를 위해서는 해양사고 발생을 사전에 예측하고 이에 대응할 수 있는 예측 체계가 요구된다. 본 연구에서는 과거에 발생한 데이터를 근거로 미래를 예측할 수 있는 마코프 체인 프로세스(Markov Chain Process)를 적용하여 해양사고 발생을 사전에 예측하기 위한 모델링을 제안한다. 제시된 모델링을 적용하여 미래 발생 가능한 해양사고 발생 확률을 산출하고 실제 발생한 빈도와 비교하였다. 또한 많이 사용되는 다른 예측 분석 방법과 비교하여 예측의 정확성을 측정하였다. 이를 통해 해양사고 발생에 관한 예측 체계를 마련하는데 하나의 확률 모형을 제안하였으며, 나아가 다양한 해양사고의 문제를 예측하는데 기여할 것으로 기대된다.

• 대한기계학회논문집B
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• 제37권3호
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• pp.275-283
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• 2013

차세대 로켓 엔진의 추진제중 하나로 부각되어지고 있는 메탄 엔진의 연소 특성을 파악하기 위하여 가스메탄과 액체산소를 추진제로 사용하는 로켓 엔진의 인젝터를 설계/제작 하였다. 동축 스월/전단형 인젝터를 채택하여 제작하였으며, 상용 해석 프로그램인 Fluent를 사용하여 유동해석을 수행한 결과를 바탕으로 인젝터의 주요 변수들을 선정하였다. 제작된 인젝터는 수류실험을 통하여 미립화와 분무특성을 파악하였고, 설계점에서의 연소실험을 수행하여 점화 및 연소 안정성을 확인하였다. 또한, 혼합비(O/F ratio)를 변화시켜가며 연소 실험을 수행하여 특성 속도($C^*$)와 연소실 압력 섭동 값을 이용하여 연소 특성 및 안정성을 평가하였다. 실험 결과 모든 혼합비 영역에서 평균적으로 90% 이상의 높은 연소 효율을 보였고, 압력 섭동 값이 2% 미만으로 연소안정성을 확인하였다.