• 한국추진공학회:학술대회논문집
• /
• 한국추진공학회 2006년도 제26회 춘계학술대회논문집
• /
• pp.288-293
• /
• 2006

본 논문은 축소형 액체로켓엔진 연소기의 성능 및 연소특성에 관한 것이다. 축소형 연소기는 분사기 헤드부, 내열재 실린더부, 그리고 강제 물냉각 노즐부로 구성되어 있다. 분사기 헤드부는 18개의 주분사기와 한 개의 점화기용 분사기로 구성되어 있다. 분사기의 형태는 동축 와류형 분사기이며, 리세스 길이에 따른 4종류의 분사기를 적용한 각각의 축소형 연소기의 연소시험 결과, 성능 비교 및 정압, 동압 특성에 대해 기술하였다. 또한 설계점 및 탈설계점에서의 연소특성에 대해서도 기술하였다.

• 한국의상디자인학회지
• /
• 제10권1호
• /
• pp.99-116
• /
• 2008

This study reviewed pertinent literature and examined relics of manggon(a headband worn to hold a man's topknot hair in place), donggot(a topknot pin), and chigwan(a topknot cover). Before the modernized short hair style, wearing a gat was an important custom. Therefore, manggon, which was used to hold a man's hair in place under the gat, was considered an essential part of the man's official dress code. Donggot is a pin that held the topknot hair in place. It was a must have for a married man, like the binyeo, a lod-like hairpin, for a married woman. Unlike gwanja, it had nothing to do with official rank, but materials were of a variety of materials, including jade and gold. The structure of the donggot was studied in three parts-head, neck and body. Major forms for the head include the mushroom, bean and ball. Bullet and half-cut bullet forms were also found. Forms for the neck include straight-neck and curved-neck. A neck with a belt around a double chin was also found. Forms for the body include the tetrahedron, octahedron and cylinder. The most popular form for silver and white bronze donggot heads was the mushroom, followed by bean and pile forms. Chigwan is also called chipogwan, chichoal, choalgyesogwan, noingwan and sangtugwan. In poetry it was called chichoal, and it used to be called taegogwan in the past as well. Chigwan was so small that it managed to hold a topknot. According to confucian custom in the Joseon period, by wearing chigwan, men didn't display their bare topknot even when they didn't dress up. When they went out, they wore another official hat over the chigwan.

• 한국추진공학회:학술대회논문집
• /
• 한국추진공학회 2007년도 제29회 추계학술대회논문집
• /
• pp.114-118
• /
• 2007

본 연구는 30ton급 액체로켓엔진 지상연소시험용 연소기의 설계 및 제작에 관한 것이다. 본 연소기는 연소압력이 60 bar, 노즐 확대비가 12이며, 헤드부와 연소실부가 용접되는 일체형 재생냉각형 연소기이다. 헤드부는 저온에서 기계적 특성이 좋은 STS316L을 사용하였다. 연소실부는 실린더부, 노즐목부, 1차 노즐부, 2차 노즐부로 구성되어 있다. 연소실부의 내피 재질은 동합금 /STS319J1/STS316L, 외피 재질은 STS329J1을 사용하였다. 선반, 밀링, MCT, 롤링 및 프레싱 등의 기계적 가공을 통하여 단품들을 완성하였다. 이러한 각 단품들을 조립하여 일반 용접 및 전자빔 용접, 브레이징 등을 적용하여 일체형으로 접합하였다.

• 한국수소및신에너지학회논문집
• /
• 제5권2호
• /
• pp.111-119
• /
• 1994

Analysis of heat loss is needed to achieve the high performance and high efficiency in hydrogen engine. So, cooling losses at each part of the direct injection hydrogen fueled engine were measured to evaluate the behavior and distribution of heat loss. Unsteady instantaneous temperature and heat flux at cylinder head were measured by use of instantaneous temperature prove. And these results were compared with those of gasoline engine.

• 제어로봇시스템학회:학술대회논문집
• /
• 제어로봇시스템학회 2004년도 ICCAS
• /
• pp.291-295
• /
• 2004

New valve driving system to control for the best volumetric efficiency at each load of an internal combustion engine within one engine cycle has been developed. The system needs to reduce pumping loss that cause by throttle valve during the intake valve is opened. In this system the intake valve is driven by a linear DC electromagnetic actuator which is controlled by personal computer. The result is compared both installed and uninstalled actuator into the cylinder head. By both of experimental and numerical calculation, the responsibility of the valve driving system to the engine speed was examined

• 대한기계학회논문집
• /
• 제8권1호
• /
• pp.71-78
• /
• 1984

본 논문은 왕복동 내연기관의 방열에 관한 연구의 하나로서 디이젤 기관 실린더 헤드와 흡 배기 밸브의 온도 분포와 열유속의 분포를 구한 것이다. 방열 해석은 기관의 정상 작동된 다음의 실린 더 헤드의 열부하가 일정하다고 생각하여 실린더 헤드의 밸드 시이트 양단의 온도와 연소 가스 배출 온도, 흡기 및 냉각수 온도를 측정하고 온도분포 및 열유속을 유한요소법을 적용하여 구하 였다. 본 연구의 결과 실린더 헤드 및 밸브의 과부하는 밸브의 경우에는 밸브 헤드 중심과 밸브 헤드 중심 부근에서 일어나며, 실린더 헤드의 경우에는 헤드 중심부 표면에서 발생하였다. 흡 배 기 밸브 및 물재킷부의 온도 분포 및 열유속의 분포를 주어진 냉각수 온도 조건에 대하여 구한 후 이들을 비교 검토 하였다.

• 유체기계공업학회:학술대회논문집
• /
• 유체기계공업학회 2002년도 유체기계 연구개발 발표회 논문집
• /
• pp.402-407
• /
• 2002

A commercial CFD code is applied to analyze the 3-D viscous flow field within vertical multi-stage centrifugal pimp including impeller with 6 blades and guide vane with 11 blades and is performed by changing flow rate from 10 to $26\;m^3/h$ at the constant 3500rpm. The purpose of this 3-D numerical simulation is to confirm how much the effect of blade inlet angle of guide vane has an influence on the performance of vertical multi-stage centrifugal pimp. these results performed by $20^{\circ},\;30^{\circ}$ inlet angle of guide vane are compared with grundfos performance data. The vertical multi-stage pump consist of the impeller, guide vane, and cylinder. The characteristics such as total pressure coefficient total heat shaft horse power, power efficiency, discharge coefficient are represented according to flow rate changing.

• 한국수소및신에너지학회논문집
• /
• 제4권1호
• /
• pp.1-9
• /
• 1993

To find performance and knock limit for compression ratio in hydrogen fueled engine, the variable compression ratio hydrogen fueled engine which was able to vary compression ratio during firing was manufactured and estimated. The characteristics of the variable compression ratio hydrogen fueled engine were as follows : 1) compression ratio variation by moving of cylinder head, 2) OHC which can be realized low S/V ratio, short flame propagation distance and unvariable configuration of combustion chamber for compression ratio variation, 3) direct injection of hydrogen gas to restrict back fire.

• 한국항공운항학회지
• /
• 제3권1호
• /
• pp.37-47
• /
• 1995

It is very important to determine the performance and operating envelope of engine for aircraft's flight. The basic performance is provided by manufacturer, but installed engine's operating envelop is only determined by flight test. First, this study was measured cylinder head temperature(CHT), exhaust gas temperature(EGT) and oil temperature. At pre-determined altitude and power rate, these temperatures were measured by change of mixture ratio and mixture ratio condition for economic operation and max. power were found. And secondly, with the measured temperatures, possible positions of mixture lever were determined by flight test for stable flight Chang-91 and Lycoming IO-360-A series four cylinders engine with 200 hp was used for this study.

• International Journal of Automotive Technology
• /
• 제5권4호
• /
• pp.297-302
• /
• 2004

This paper presents the low cycle thermal fatigue of the engine exhaust manifold subject to thermo-mechanical cyclic loading. As a failure of the exhaust manifold is mainly caused by geometric constraints of the less expanded inlet flange and cylinder head, the analysis is based on the exhaust system model with three-dimensional temperature distribution and temperature dependent material properties. The result show that large compressive plastic deformations are generated at an elevated temperature of the exhaust manifold and tensile stresses are remained in several critical zones at a cold condition. From the repetition of these thermal shock cycles, maximum plastic strain range (0.454%) could be estimated by the stabilized stress-strain hysteresis loops. It is used to predict the low cycle thermal fatigue life of the exhaust manifold for the thermal shock test.