• 한국추진공학회지
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• 제17권6호
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• pp.120-130
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• 2013

최근 들어 차세대 추진제로서 각광을 받고 있는 메탄의 성능특성을 분석하고, 메탄/산소 로켓엔진의 기술개발 동향을 조사하였다. 로켓연료로서의 액체메탄은 무독성, 경제성, 우수한 재생냉각성능, 그리고 행성의 현지자원활용(ISRU) 가능성 등과 같은 여러 유리한 특성을 가지며, 액체산소와의 조합시 높은 비추력 확보 및 시스템 경량화가 가능하다. 이러한 이유로, 메탄/산소 엔진에 대한 연구가 활발하게 진행되고 있기는 하지만 그 기술성숙도가 아직은 그리 높지 않은 것으로 확인되는 바, 메탄 로켓엔진 개발을 통하여 우주기술 선진국과의 기술격차 해소가 필요한 시점이라고 판단된다.

• 대한기계학회:학술대회논문집
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• 대한기계학회 2007년도 춘계학술대회B
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• pp.3323-3328
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• 2007

Conventional LPG pump for Liquified Petroleum injection(LPi) engine has been adopted vane type. But the BLDC type fuel pump for LPi system has complicated structure and its price is high. Therefore, as a alternative, this study has mainly focused on the development of turbine type LPG pump which has lower cost and simple structure than conventional BLDC type. To verify the possibility of substitute the performance tests were performed for each fuel pump. The comparative items were pressure settling time, variation of fuel outlet temperature and engine performance of hot restart ability. As a result, performances of turbine type LPG pump were equivalent or high comparing to the BLDC type all over the tests for different fuel composition.

• International Journal of Automotive Technology
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• 제7권7호
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• pp.841-846
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• 2006

This paper presents a numerical approach to optimizing vehicle fuel economy in a higway bus. The method described is based on using a commercial software vehicle simulation to identify the relative efficiency of each of the vehicle systems, such as the engine hardware, engine software calibration, transmission, cooling system and ancillary drives. The simulation-based approach offers a detailed understanding of which vehicle systems are underperforming and by how much the vehicle fuel economy can be improved if those systems are brought up to best-in-class performance. In this way, the optimum vehicle fuel economy can be provided to the vehicle customer. A further benefit is that the simulation requires only a minimum number of vehicle testing for initial validation, with all subsequent field test cycles performed in software, thereby reducing development time and cost for the manufacturer.

• 한국소음진동공학회:학술대회논문집
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• 한국소음진동공학회 2008년도 춘계학술대회논문집
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• pp.540-545
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• 2008

The design on balance shaft module is performed based on the target specification of engine module as well as the its own dynamic nature under a high speed rotation. However, the specific information for engine module is not always available for non-motor companies even though a reliable analytical result should be attached in the conceptual design process or more detail works. In this paper, the analysis on balance shaft module, both each parts or module itself, is suggested to estimate the performance on the target component with respect to durability and NVH without any consideration of a engine module. This methodology could modify the nominal balance shaft model before the production of prototype such that cost reduction as well as time saving can be expected during design process of balance shaft module.

• 한국소음진동공학회:학술대회논문집
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• 한국소음진동공학회 2000년도 춘계학술대회논문집
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• pp.1643-1647
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• 2000

The intake noise of an automobile induced by firing of an engine accompanies acoustic resonances of ducts of an intake system. Conventionally, the adoption of the Helmholtz type resonator was one of possible ways to eliminate the booming noise due to acoustic resonances of air ducts. Although the Helmholtz type resonator is convenient to attenuate the intake noise of an automobile, the usage of the Helmholtz type resonator requires cost increase or big engine room space. Therefore, reduction of the number of the resonators or the volume of the resonators is essential to increase the value of an automobile. To meet these requirements, other types of resonator are suggested instead of the Helmholtz type resonator. The effectiveness of the suggested resonators is compared considering noise reduction ability, effect to the engine performance and size of each resonator.

• 한국추진공학회:학술대회논문집
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• 한국추진공학회 2011년도 제36회 춘계학술대회논문집
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• pp.12-15
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• 2011

현재 가장 널리 쓰이고 있는 케로신-액체산소 액체로켓엔진은 신뢰도와 개발 비용의 문제로 이전의 설계에서 크게 벗어나지 않은 스킴을 사용하고 있다. 하지만 냉각 방법, 엔진 싸이클 및 냉각유로 형상의 변경, 추진제가 아닌 추가의 냉각제 이용 등의 여러 방법으로 효율을 향상시킬 수 있다. 여기에서는 그 중 냉각제를 케로신에서 액체산소로 변경하여 효율이 높아진 사례에 대하여 기술한다.

• 한국정밀공학회:학술대회논문집
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• 한국정밀공학회 1997년도 춘계학술대회 논문집
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• pp.410-415
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• 1997

Recently, The manufacturing companies are introducing the CAD/CAM systems to solve problems for the lack of experts, the higher cost of manufacturing and the difficulties of process. Knowledge engineering approach makes it possible to change a know-how of experts to computerized information effectivly. The proposal of this paper is the development of an interactive knowledge-based CAM system to disign and manufacture the mold with non-expert engineers used easily. This system is composed of two functional parts. One is the geometric modeler that used the technique of a feature modeling. The other is the expert system module that composed inference engine and databas which contains characteristics of materials and cutting tools setc.

• 한국자동차공학회논문집
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• 제6권6호
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• pp.195-201
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• 1998

This study aims at the optimal design of rotors and the development of screw type Supercharger of CNG-fueled engine for commercial vehicle. Based on the new rotor profile, an advanced oil free type Supercharger has been developed, which can achieve higher adiabatic efficiency and lower manufacturing cost. The performance test of screw type Supercharger has achieved high volumetric efficiency and the durability on the bench of performance test has also been established in the compact body.

• 대한기계학회논문집B
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• 제22권11호
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• pp.1547-1554
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• 1998

The object of this study was to develop an economic assessment program for the optimal design of the cogeneration systems composed of combining engine, generator, waste heat recovery exchanger, absorption chiller, and boiler, etc. The energy demand categorized by electric power, heating, cooling and water supply was determined by statistical data of the existing cogeneration systems. An economic assessment was performed by comparing the total cost of cogeneration system with that of non-cogeneration system. The total cost was evaluated by adding initial investment to operational cost considering efficiency of equipment, cost of equipment, fuel and electricity. To confirm the validity of the developed program, a hotel building with an area of $127,960m^2$ was selected, and the simulated results were compared with the measured data. The difference between the simulated and the measured values for the selected hotel building was approximately 12% for annual electric consumption.

• 한국항공우주학회지
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• 제44권2호
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• pp.139-155
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• 2016

본 논문에서는 최근의 우주발사체 기술 발전에 대한 소개가 이루질 것이다. 민간 분야에서의 우주개발 사업들의 사업 모델 및 핵심 기술에 대하여 간단한 정리하고, 핵심 기술의 발전 사항들에 대하여 좀 더 구체적으로 살펴볼 것이다. 특히 Rocketlab 사가 개발 중인 저가 고성능 경량 우주발사체 Electron 에 사용될 예정인 전기펌프 사이클 엔진에 대하여 좀 더 구체적으로 살펴보고, 이들이 로켓 과학자들에게 주는 시사점에 대하여 살펴볼 것이다.