• Journal of the Korea Academia-Industrial cooperation Society
• /
• v.16 no.11
• /
• pp.7250-7255
• /
• 2015

The objective of this study is to experimentally investigate the heating performances of the portable air combustion heater using diesel fuel for auxiliary cabin heating of the battery electric vehicle. In order to evaluate the heating performances of the air combustion heater, the heating capacity was calculated by the temperature at inlet and outlet parts of the considered heater and the inner temperature distribution characteristics of the vehicle were measured during 1600 seconds with an interval of 1 second. The theoretical efficiency of the tested heater was calculated by temperature data of the air of supplying and exhausting to the cabin. As the air passed the heat-sink, the air temperature at the end of heat-sink reached to $101.3^{\circ}C$ and the difference of temperature on heat-sink was 67.8%. The average heating capacity of the air combustion heater showed 2.0 kW. After 1800 seconds, the inner temperature of the vehicle cabin was continuously increased. The temperatures of the top side and the bottom side of the car cabin under consideration were increased upto $42.5^{\circ}C$ and $24.3^{\circ}C$, respectively, and the theoretical efficiency of the tested heater was on average 63.7%.

• Fire Science and Engineering
• /
• v.26 no.6
• /
• pp.92-98
• /
• 2012

In this sturdy, large experimental (ISO 13785-2) was performed to analyze the building materials used in fire retardant materials for aluminum composite panel and in general properties. As a results, maximum temperature in the case of the general materials was measured in 210 seconds $1,021^{\circ}C$, the retardant materials was measured in 1,200 seconds early $1,190^{\circ}C$. The retardant material of aluminum composite panel, Fire behavior if the ignition is slow and the general materials in aluminum composite panel, fire ignition and combustion at the same time was growing rapidly. The general materials and flame-retardant material of aluminum composite panel was an obvious difference to the combustion ignition but after ignition combustion mode showed a similar pattern of the rapidly vertical spread of flame. The results of this study, in order to reduce the risk of aluminum composite panels for fire and the retardant materials used for ignition the slow should be actively encouraging. Also after the ignition, there is an urgent need to put out a fire in exterior materials for extinguishing facilities.

• Transactions of the Korean Society of Mechanical Engineers B
• /
• v.36 no.3
• /
• pp.335-342
• /
• 2012

Nowadays, automobile manufacturers are focusing on the reduction of exhaust-gas emissions because of the harmful effects on humans and the environment, such as global warming by greenhouse gases. Gasoline direct injection (GDI) combustion is a promising technology that can improve fuel economy significantly compared to conventional port fuel injection (PFI) gasoline engines. In the present study, ultra-lean combustion with an excess air ratio of over 2.0 is realized with a spray-guided-type GDI combustion system, so that the fuel consumption is improved by about 13%. The level of exhaust-gas emissions and the operation performance with the multiple injection strategy and exhaust-gas recirculation (EGR) are examined in comparison with the emission regulations and from the point of view of commercialization.

• Journal of the Korean Society of Propulsion Engineers
• /
• v.19 no.5
• /
• pp.62-70
• /
• 2015

A liquid rocket engine system can cause rapid pressure and temperature variations during the startup period. Thus the startup analysis is required to reduce time and expense for successful development of liquid rocket engine through the startup prediction. In this study, a startup analysis simulator is developed for a staged combustion cycle engine powerpack. This simulator calculates propellant flow rates using pressure and flow rate balances. In addition, a rotational speed of turbopump is obtained as a function of time by mathematical modeling. A startup analysis result shows that the time to reach a steady-state and a rotational speed at the steady-state are 1.3 sec and 27,500 rpm, respectively. Moreover it can indicate proper startup sequences for stable operation.

• Transactions of the Korean Society of Mechanical Engineers A
• /
• v.34 no.12
• /
• pp.1909-1915
• /
• 2010

The material properties of gas turbine components change during the daily start/stop thermal cycle because of exposure to the hot combustion gas. Recently, single-crystal Ni-based superalloys have been used to manufacture many hot-gas components for gas turbines. However, the user needs to depend on the manufacturer for maintenance issues because of the lack of data required for predicting blade life and material degradation. In this study, we investigate the time-dependent degradation of first-stage blades at various operating facilities to collect the basic data for life assessment and damage analysis. The blade material is a single-crystal Ni-based superalloy, CMSX-4, and the EOH (equivalent operating hours) are 25,000 and 52,000, respectively. We prepared the test specimen directly from used blades and carried out mechanical tests and microstructural observations.

• Fire Science and Engineering
• /
• v.26 no.2
• /
• pp.90-96
• /
• 2012

Since vertical flame spread speed on exterior materials is much faster than horizontal fire, analysis of its fire characteristic is required. For the study of vertical fire pattern created by penetrating windows or openings from the exterior wall of buildings, the research is based on the fire simulation for an aluminum-complex-panel with which is commonly used as exterior materials and consists of polyethylene core material. As a result, the flame reaches the 2nd floor after 135 seconds in the early stage of fire, the 10the floor after 470 seconds and the 30th floor, the highest floor, after 711 seconds. The result shows that fire spread abruptly expands on upper floor due to stack effect of a turbulent flow or exterior materials. In consequence, we can confirm a serious problem that a conflagration of a building through an opening that is equipped with the exterior-materials spreads into interior of building at that same time.

• Journal of Nuclear Fuel Cycle and Waste Technology(JNFCWT)
• /
• v.9 no.3
• /
• pp.191-198
• /
• 2011

In general, conventional criticality analyses for spent fuel transport/dry storage systems have been performed based on assumption of fresh fuel concerning the potential uncertainties from number density calculation of Transuranic and Fission Products in spent fuel. However, because of economic loss due to the excessive criticality margin, recently the design of transport/dry storage systems with Burnup Credit(BUC) application has been actively developed. The uncertainties in criticality analyses on transport/storage systems with BUC technique show strong dependance upon initial enrichment and burnup rate, whereas those in the conventional criticality evaluation based on fresh fuel assumption do not show such a dependance. In this study, regulatory-required uncertainties of the criticality analyses for BK 26 Cask, which is conceptually designed spent fuel transport cask with BUC corresponding to the limiting circumstances on nuclear power plants in Korea, are evaluated as a function of initial enrichment and burnup rate. Results of this study will be used as basic data for spent fuel loading curve of BK 26 Cask.

• Transactions of the Korean Society of Automotive Engineers
• /
• v.6 no.1
• /
• pp.213-221
• /
• 1998

The investigation regarding the ignition system of a plasma jet explored by using a constant volume vessel. The purpose of this study is to elucidate relation between the characteristics of the configuration and jet ejection of plasma jet plug, when the sub energy were supplied at plasma jet ignition system. From the results of a visualization by the schlieren system, the jut ejection for plasma jet ignition are depended on the jet plug configuration and sub energy, but the configuration of plasma jet plug is more influenced than the sub energy on the plasma jet ejection. And the plasma jet ignition strongly influences upon the combustion enhancement than the conventional spark ignition.

• Proceedings of the Korean Society of Propulsion Engineers Conference
• /
• 1998.10a
• /
• pp.31-31
• /
• 1998

제트베인을 이용한 추력방향 제어장치를 개발하여 평균추력 2950 lbf, 평균 압력 714 psig, 연소시간 4.8초, 노즐 출구직경 약 100mm인 추진기관에 장착하고 이를 시험하고 분석하였다. 재질에 따른 제트베인의 삭마성을 알아보기 위하여 텅스텐과 구리(W/Cu), 지르코늄산화물과 텅스텐(ZrO$_2$/W), 지르코늄 산화물과 몰리브덴(ZrO$_2$/Mo)의 3가지 재질의 베인을 사용하였다 시험된 제트베인 재질 중 지르코늄 산화물과 몰리브덴(ZrO$_2$/Mo)의 합금을 사용한 베인이 내열성 및 삭마성에서 가장 우수하였으며(삭마량 27.65% 삭마율 5.7mm/sec), 지르코늄 산화물과 텅스텐(ZrO$_2$/W), 텅스텐과 구리(W/Cu)의 순서이었다.

• 한국전산유체공학회:학술대회논문집
• /
• 2010.05a
• /
• pp.446-447
• /
• 2010

최근 개발된 니켈 초합금 금속폼은 기존의 매연저감장치 신소재로 여겨지고 있다. 금속폼은 세가지 두드러진 특징을 갖고 있다. 첫째, 금속폼은 큰 기공의 다공성 매질로써 매연을 포집하여 축적할 수 있는 용량이 기존 필터에 비해 상대적으로 크며 그로인하여 재생 시 연소 안전성이 두드러진다. 둘째, 복잡하고 굴곡있는 기공 구조와 큰 비표면적은 물질전달 특성을 향상시켜 촉매 적용 시 촉매의 전환성능을 향상시키고 그로 인하여 귀금속 촉매량을 줄일 수 있는 장점이 있다. 셋째, 금속폼은 다양한 기공크기를 가지며, 다양한 조합의 금속폼을 개발할 수 있어 요구 성능에 따른 최적의 필터 설계를 가능케 한다. 이번연구에서는, 금속폼의 필터 성능을 다양한 실험을 통하여 측정 평가하며, 이런 이해를 기반으로 필터로 제작하여 엔진실험벤치에서 그 성능을 검증하였다. 필터의 성능은 수트 포집효율과 그에 따른 필터의 압력강하와 촉매 활성 능력으로 평가되었다. 이러한 실험과 병행하여 금속폼에서의 수트 포집과정을 모델링하고 이를 상용 프로그램인 CFD-ACE+에 추가하여 설계전용 프로그램을 개발하였으며, 엔진실험결과와 비교 검증하였다. 본 논문에서는 금속폼의 높은 매연축적용량과 향상된 물질전달 특성이 어떻게 필터의 귀금속 촉매와 체적을 줄일 수 있는지 제시하고 있다.