• 한국소성가공학회:학술대회논문집
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• 한국소성가공학회 2007년도 추계학술대회 논문집
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• pp.46-49
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• 2007

The purpose of this study is to develop the optimum shape of blank for the crank throw of large marine engine in order to reduce manufacturing cost and forging defects. The effects of the curvature radius and the height of wing part of blank selected as design variables on the defects and machining margin of final products after forging process were investigated using FEA. Based on the results, the optimum shape for the blank of the crank throw was proposed and verified by experiment.

• 한국게임학회 논문지
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• 제3권2호
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• pp.3-11
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• 2003

게임 기획은 초기 기획과 세부 기획으로 나뉘어진다. 초기 게임 기획에는 디자인적인 요소, 기술적인 요소, 마케팅적인 요소등이 효율적으로 고려되어야 한다. 특히 기술적인 요소 즉 플랫폼, 게임 엔진, 서버 구축 및 구성등은 개발 비용과 개발 기간에 영향을 줄 수 있다. 그러므로 게임을 기획할 때 해당 게임의 기획 의도에 적합한 기술 요소를 선택해야 한다. 본 논문에서는 게임을 초기 기획할 때 고려해야 할 기술적인 요소들을 플랫폼, 게임 엔진, 게임 서비스, 그리고 네트워크 인프라를 중심으로 연구하였다.

• 한국분무공학회지
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• 제25권1호
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• pp.8-14
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• 2020

Recently, 1-D model-based engine development using virtual engine system is getting more attention than experimental-based engine development due to the advantages in time and cost. Injection rate profile is the one of the main parameters that determine the start and end of combustion. Therefore, it is essential to set up a sophisticated model to accurately predict the injection rate as starting point of virtual engine system. In this research, procedure of 1-D model setup based on AMESim is introduced to predict the dynamic behavior and injection rate of diesel injector. As a first step, detailed 3D cross-sectional drawing of the injector was achieved, which can be done with help of precision measurement system. Then an approximate AMESim model was provided based on the 3D drawing, which is composed of three part such as solenoid part, control chamber part and needle and nozzle orifice part. However, validation results in terms of total injection quantity showed some errors over the acceptable level. Therefore, experimental work including needle movement visualization, solenoid part analysis and flow characteristics of injector part was performed together to provide more accuracy of 1-D model. Finally, 1-D model with the accuracy of less than 10% of error compared with experimental result in terms of injection quantity and injection rate shape under normal temperature and single injection condition was established. Further work considering fuel temperature and multiple injection will be performed.

• 한국추진공학회:학술대회논문집
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• 한국추진공학회 2010년도 제35회 추계학술대회논문집
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• pp.343-346
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• 2010

한국형발사체 추진기관 개발을 위한 연소기 연소시험설비, 터보펌프 실매질 시험설비, 엔진 지상 및 고공모사 연소시험설비, 추진기관시스템 시험설비 구축 계획에 대해 간략히 기술하였다. 연소기, 터보펌프, 엔진 시험설비에서는 75톤급 액체로켓엔진의 부품 및 엔진시스템의 개발 및 인증시험을 수행할 예정이고, 추진기관시스템시험설비에서는 한국형발사체 1/2/3단용 추진기관시스템의 개발 시험을 수행할 예정이다. 추진기관 시험설비는 나로우주센터에 건설될 예정이며 구축 일정, 예산, 안전거리, 효율성 등을 고려하여 구축하고자 한다.

• 한국소음진동공학회:학술대회논문집
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• 한국소음진동공학회 2009년도 추계학술대회 논문집
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• pp.328-329
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• 2009

Air-Damping Mount is proposed to compromise between performance and weight & cost. The design of Air-Damping Mount was based on the specification from the engine mounting system analysis of a small car. To verify it's feasibility, R&H test was done on the small car and it is proven that Air-Damping Mount shows the performance between hydraulic mount and rubber mount.

• 연구논문집
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• 통권28호
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• pp.49-58
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• 1998

포핏밸브형 2행정 기관의 소기 시스템 형상 변화에 따른 소기유동 및 소기효율의 개선 효과를 해석하기 위해, 각 흡기포트 형상별 소기 유동 가시화와 소기효율 정량화 연구를 수행하고자 한다. 소기시스템의 형상은 기계연구원에서 독자 개발한 RSSV(Rotatable Shrouded Scavenging Valve)의 슈라우드 각도를 변화시켰으며, 소기 효율 정량화를 위해 정상상태하에서 등유와 착색된 물을 사용한 single-cycle method. 동적모사장치(dynamic simulatior)에서 $CO_2$와 $O_2$가스를 사용한 가스추출법(gas sampling method)을 적용하였으며 실제 기관에서의 소기 효율을 측정하기 위해 압력 선도를 해석하였다. 위 실험들의 결과로부터 $90^circ$슈라우드 밸브가 가장 높은 효율을 가지는 것으로 판명되었으며, 특히 이들 실험방법들은 2행정 엔진 개발에 있어 시간과 비용을 절감하는데 아주 유용한 기법임을 알 수 있었다.

• 한국추진공학회:학술대회논문집
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• 한국추진공학회 2011년도 제36회 춘계학술대회논문집
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• pp.465-465
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• 2011

Rolls-Royce is a global company producing advanced power systems for use on land, at sea and in the air. In order to develop competitive products and services, Rolls-Royce invests in technology, infrastructure and capability with much of the research carried out in a global network of University Technology Centres, such as the UTC in Thermal management at Pusan National University. Heat exchangers and thermal management play a critical role in today's gas turbine engines, maintaining the fuel and oil temperatures within the correct operational range. Future products are likely to place an increased duty on the thermal management system and thus require advances in heat exchanger design, installation and manufacturing. Heat exchangers further have the potential to play a vital role in Advanced Cycle Gas Turbine products. The Intercooled and recuperated WR21 marine gas turbine engine recently entered service with the Royal Navy and is delivering very attractive fuel burn in service. The development of an advanced cycle aero-engine is a significantly greater challenge, requiring better understanding of compact and light weight heat exchanger surfaces, novel installations and ducting systems and may required novel manufacturing techniques to achieve the volume, weight and cost necessary to realise a viable advanced cycle gas turbine aero-engine.

• 한국산학기술학회논문지
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• 제19권11호
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• pp.529-535
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• 2018

레인지 익스텐더 전기자동차는 소형의 발전용 엔진이 가장 효율이 좋은 특정 운전영역에서 기동하여 배터리를 충전시키며 주행거리를 연장하는 메커니즘으로 주행한다. 본 연구에서는 저가이면서 제어 로직이 간단한 시스템을 개발하기 위하여 기존 쓰로틀바디시스템을 대체하는 스텝모터방식 흡입공기량 공급시스템을 개발하여 기존 base 엔진에 적용하고, 흡입공기량 증대를 통한 성능 개선을 위해 흡 배기다기관의 길이 변경 효과를 실험적으로 살펴보았다. 실험결과, 하나의 스텝모터로 작동하는 Type B의 흡입공기량조절장치가 Type A보다 전 운전영역에서 성능이 높았으나 유동저항의 증가로 base 엔진보다는 성능이 낮았다. 이를 개선하기 위해 흡기매니폴드에 140mm 어댑터를 장착한 경우와 새로 설계된 70mm 길이의 배기 매니폴드를 적용한 경우 2200rpm과 4300rpm 두 속도조건에서 엔진성능이 향상됨을 확인할 수 있었다. 최적 설계된 엔진을 대상으로 레인지 익스텐더 전기자동차에 적용 가능하도록 발전기 부하를 연결하여 2단 속도로 고정밀 운전제어를 구현하였으며 그 결과, 1단 2200rpm과 2단 4300rpm 운전조건에서 ${\pm}2.5%$ 이내의 속도변화율을 나타내었고, 1단 속도에서 2단 속도로 상승 시 610rpm/s의 목표속도 추종성 결과를 얻었다.

• 한국자동차공학회논문집
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• 제15권3호
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• pp.99-105
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• 2007

Currently, BLDC fuel pump was applied on LPi vehicle using 3rd fuel supply system as liquified phase LPG injection method had already shown better performance than others. Its cost, however, is rather expensive because of drawbacks such as complicated structure, a fault of localization of system. In this work, demonstration system for a developed turbine type fuel pump to replace BLDC system was setup and investigated. This study results that fuel mass flow rate of turbine type pump and injection performance of injector were better compared to BLDC type. Comparing flow rate of summer LPG with that of winter LPG, the flow rate decreased about 25% using winter LPG. Performance applying turbine type LPi fuel pump to engine is confirmed.

• 한국생산제조학회지
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• 제18권6호
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• pp.642-651
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• 2009

The history of excavator design is not long enough which still causes most of the design considerations to be focused on static analysis or simple functional improvement based on static analysis. However, the real forces experiencing on each component of excavator are highly transient and impulsive. Therefore, the prediction and the evaluation of the movement of the excavator by dynamic load in the early design stage through the dynamic transient analysis of the excavator and ensuring of design technique plays an importance role to reduce development-cost, shorten product-deliver, decrease vehicle-weight and optimize the system design. In this paper, Commercial software DADS and ANSYS help to develop the track model of the crawler type excavator, and to evaluate the performance and the dynamic characteristics of excavator with various simulations. For that reason, the track of crawler type excavator is modelled with DADS Track Vehicle Superelement, and the reaction forces on the track rollers were predicted through the driving simulation. Also, the upper frame and cabin vibration characteristics, at the low RPM idle state, were evaluated with engine rigid body modelling. And flexibility body effects were considered to determine the more accurate joint reaction forces and accelerations under the upper frame swing motion.