• Transactions of the Korean Society of Automotive Engineers
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• v.10 no.4
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• pp.1-6
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• 2002

Engine lubrication system is generally affected by vehicle driving conditions, which are composed of acceleration, braking deceleration and accelerating during cornering. The major reason is due to the oil pan system in which oil is directly influenced by inertia farce caused by vehicle driving conditions. Therefore, to confirm safety of engine lubrication system inertia farce effects are also considered in the developing state. For the purpose, we have carried the engine tilting tests using ourselves made test rig. Verifying the test results we also measured the inertia effects on the engine lubrication system using the circular tuning and slalom test with vehicle. Through the comparison study between two kinds of results we obtained that the engine tilting test rig was very useful to confirm the safety evaluation of engine lubrication system.

• Proceedings of the KWS Conference
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• 2001.10a
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• pp.140-142
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• 2001

항공기의 제트 엔진을 비롯하여 육상용 발전기, 선박용 엔진, 로켓 엔진 등에 널리 사용되는 터빈 블레이드를 포함한 고온용 가스터빈 부품은 최대 온도 120$0^{\circ}C$ 이상의 고온에 노출되어 가혹한 기계적 응력을 받는 동시에 고온에서의 표면 안정성이 요구되므로 초내열 니켈 합금(superalloy), 티타늄 합금, 내열강 등의 고온강도가 우수한 합금이 사용된다. 그런데 합금성분이 많이 첨가된 내열 합금을 용접하는 경우, 미세균열, 용접부의 기계적 성질의 저하, 용접열영향부의 내식성과 내산화성의 저하, 용접외부 결함에 의한 피로강도 저하 등의 문제가 발생하므로 이를 해결해야 한다. 본고에서는 생산성과 용접품질이 우수한 고밀도 에너지빔 용접의 적용 현황에 관하여 고찰코자 한다.

• Proceedings of the Korea Information Processing Society Conference
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• 2017.04a
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• pp.242-245
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• 2017

기존의 엔진제어기(ECU)는 주요 mapping data(ECU에 대응되는 값)들에 대해서 기밀성과 무결성을 제공하는 보호 기법의 부재로 인해 임의적인 튜닝이 가능하다는 특징이 존재하였다. 이로 인해 자칫 잘못된 튜닝이나 악의적인 조작이 발생할 수 있는 여지가 있으며, 이는 차량 엔진 및 조작의 안정성을 떨어뜨림과 동시에 운전자 및 보행자들의 안전을 위협할 수 있다는 문제가 있다. 이에 본 논문에서는 ECU에 적용되는 Firmware의 주요 mapping data를 안전하게 암호화하는 방식을 제안하며, 이 과정에서는 차량의 식별 및 ECU에 mapping 되는 data의 무결성 검증을 위해 인증서를 사용하는 방식을 제안한다. 본 논문의 제안을 통해 주요 mapping data를 안전하게 보호하는 기술을 통해 차량의 안전성을 유지할 수 있다.

• Journal of Aerospace System Engineering
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• v.15 no.3
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• pp.93-98
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• 2021

In Europe, it is necessary to fulfil the type certification criteria by the European Aviation Safety Agency (EASA) when developing an aircraft engine. According to type certification criteria, a 150 hours endurance test should be performed to verify the stability of the engine structure under the engine's operating limit conditions. The type certification criteria for the 150 hour endurance test are specified in JAR-E, which is the EASA type certification. Currently, the Arriel 2L2 engine is being developed in cooperation with a foreign manufacturer, and a 150 hours endurance test was performed. In this study, a 150 hours endurance test procedure is conducted in consideration of the operation characteristics of the currently developed engine.

• Journal of Korea Ship Safrty Technology Authority
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• v.15
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• pp.17-30
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• 2004

중, 소형 선박의 추진시스템은 주 동력원인 4행정 디젤엔진, 프로펠러의 추진 효율을 증대시키기 위한 감속장치, 진동 및 충격토크를 절연시키는 탄성커플링, 동력을 전후방향의 추력으로 전환하는 추진기로 구성되어 있다.<중략>

• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 2009.05a
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• pp.395-399
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• 2009

Advanced afterburner used in the most modernized gas turbine has new designing paradigm to cope with reinforced power density. The most distinct change is the designing trend to integrate fuel injectors and flame holder in order to manage higher temperature of inlet air. F414 and F110-GE-132 engine adopted this methodology and installed a variable nozzle utilizing CMC(Ceramic Matric Composite) material and active cooling of nozzle flap with ejector nozzle in order to enhance the life cycle of engine components and an economical aspect. These technological trends can be utilized for an advanced ramjet engine and combined cycle engine like TBCC.

• Journal of the Korean Society of Propulsion Engineers
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• v.14 no.4
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• pp.71-80
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• 2010

The KSLV-II(Korea Space Launch Vehicle-II) which being a successor of the KSLV-I is a space launch vehicle capable of delivering 1.5 ton-class satellite into a low earth orbit. The development of a 75 tonf-class liquid rocket engine(LRE) is planned on the basis of the technologies mastered through the preceded research of a 30 tonf-class LRE. The thrust chamber of the LRE is required to have higher combustion stability, structural integrity and thermal durability. This paper deals with the design requirements of the 75-tonf thrust chamber and a variety of technical considerations which have been conducted analytically in the course of the design for the realization of the requirements.

• Journal of the Korean Society of Propulsion Engineers
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• v.24 no.5
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• pp.77-83
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• 2020

The operating characteristics of a main oxidizer shut-off valve have been examined by life-cycle tests in which the valve operates as many times as is required at room and cryogenic temperatures. It is shown that there is no significant change of the operating characteristics in the course of the life-cycle tests. The critical pressures and principal forces, which represent the operating characteristics, differ at each operating time by less than about 3%. These qualified operating characteristics of the valve are expected to play an indispensible role in the stable startup and shutdown of a liquid rocket engine.

• Journal of Advanced Marine Engineering and Technology
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• v.38 no.6
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• pp.744-750
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• 2014

The monitoring and abnormality warning of marine diesel engine are important to take appropriate responses for safety navigation. If maintenance engineers do not take appropriate response because of diagnosis mistakes, it will occur a nasty accident. Therefore, we need integrated monitoring and diagnosis system for supporting a diagnosis objectively. In this paper, we analyze time-series data which measured by real-time, monitor the changing of conditions and trends of the analyzed data. Furthermore, we design and implement a monitoring and diagnosis system for objective supporting of real-time diagnosis. When the integrated monitoring and diagnosis system is adopted, it can help to improve stability of marine diesel engine by providing abnormality warning alarm with appropriate responses.

• Proceedings of the Korea Information Processing Society Conference
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• 2005.11a
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• pp.1359-1362
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• 2005

본 논문은 차량 및 공장 자동화 분야에서 널리 쓰이고 있는 Controller Area Network 의 안정성 보장을 위한 Fault-Tolerant 프로토콜을 제안한다. 제안된 Fault-Tolerant 프로토콜은 실시간 Fault-Tolerant 시스템을 대상으로 한 Time-Triggered 프로토콜의 중복 메커니즘을 이용하며 event-triggered 방식인 CAN 에 알맞게 변형하여 이용한다. 본 논문의 프로토콜은 Atmel 사의 AT89C51CC03 을 이용하여 구현하여 가능성을 검증 하였다. 제시한 프로토콜을 이용하여 엔진과 X-by-Wire, ABS 분야와 같은 안정성-중시 시스템에 좀더 높은 안정성을 부여할 수 있을 것이다.