• 한국항공우주학회지
• /
• 제38권3호
• /
• pp.249-257
• /
• 2010

가스터빈 엔진의 경우 디지털식 엔진제어장치 (FADEC)가 기존의 유압기계 및 전자식 제어기를 빠른 속도로 대체하고 있다. 하지만 헬리콥터 등 고성능 시스템을 대상으로 한 엔진 제어기의 경우 제어기를 설계하는 절차를 설정하는 과정이 잘 알려져 있지 않다. 본 논문에서는 충실도가 높은 헬리콥터 및 엔진 시뮬레이션 환경을 구성하고 이를 이용하여 시스템을 해석하고 설계자료를 추출할 수 있는 방안을 제시한다. 여기서는 이러한 방법을 기존의 헬리콥터 엔진을 대상으로 한 제어기의 선보상 스케줄을 작성하는데 사용하였으며, 그 결과 기존의 알고리듬과 동등하거나 우수한 조속 성능을 확인할 수 있었다.

• 한국항공우주학회지
• /
• 제47권7호
• /
• pp.517-524
• /
• 2019

진공추력 88톤급 다단연소 사이클 로켓엔진의 시스템 설계를 수행하였다. 엔진 구성품에 대한 성능 평가는 기존의 연구를 활용하였으며 수렴된 엔진 시스템 성능을 구할 수 있는 알고리즘을 제안하였다. 본 연구 방법은 RD-180에 대한 기존의 연구와 비교함으로써 검증하였다. 본 연구는 가격 경쟁력을 고려하면서 성능 개선을 달성하기 위하여 한국형발사체 75톤 엔진의 개발 이력을 최대한 승계하였다. 엔진의 제작 난이도, 비용 그리고 성능 개선을 고려하여 연소압력 12MPa을 적용하였고 결과로써 23.4s의 진공비추력 향상을 얻을 수 있었다.

• 한국자동차공학회논문집
• /
• 제19권4호
• /
• pp.99-106
• /
• 2011

This paper deals with engine room layout design optimization of fuel cell electric vehicle (FCEV), which has been proposed as a potential alternative to fossil fuel depletion. Investing the great R&D efforts, the global vehicle manufacturers, especially Honda motor corporate, have shown not prototype vehicle but commercial vehicle using fuel cell in the market recently. In this paper, we analyze cooling performance and flow characteristic in the engine room of newly FCEV, in addition we suggest the optimization process for engine room layout design optimization. The two radiators in the vehicle for fuel cell stack and electronic components cooling have been analyzed and their performance are obtained in terms of cooling performance ratio (CPR). The value of CPR should always be less than one and based on criteria, we have achieved the optimum cooling performance of radiators for stack and electronic components. Aerodynamic performance is evaluated in terms of drag coefficient, improved through underbody modification using air devices.

• 한국자동차공학회논문집
• /
• 제6권2호
• /
• pp.129-143
• /
• 1998

The vibrations of steering wheel are required to be reduced for convenient ride quality and good controllability. This phenomenon, vibration of steering wheel, is occured by interaction with suspension system, steering system, vehicle body, engine/transmission and tire complicately. But reviewing the current research activities, most researches are performed for the vibration analysis of steering wheel with a simple model, and mot easy to be applied to the variation of each component element connected with steering system as well as that of the steering system. In this study, suspension system and steering system are modelled by the T.L.H. coordinate system which is usually used by a passenger car maker. Also, rigid body motions of engine and elastic motions of vehicle body in the previous study are considered. Derive the equation of motion in 29 d.o.f. and the vibration of steering wheel is analyzed numerically and verify the midelling of steering system by comparison with test results for real car. And then, the optimal design values of the engine mount system obtained from the previous study are applied to the verified steering system model and investigate the effects of various engine mount design values on the vibration of steering wheel.

• 대한조선학회논문집
• /
• 제30권2호
• /
• pp.155-160
• /
• 1993

본 논문은 선박 기관실의 특설늑골에 대한 치수결정 방법으로써 하나의 접근방법을 서술하였다. 특설늑골의 치수결정 인자는 실적선의 데이터를 중심으로 조사 연구되었으며, 그 구성인자로는 주로 갑판간 거리, 주기 및 프로펠러 기진 주파수, 만재흘수선, 특설늑골 배치간격, 갑판수 그리고 주기마력 등이다. 이러한 주요인자를 기초로 정하중 및 동하중이 고려된 특설 늑골 치수를 결정할 수 있는 설계식을 유도하였다. 본 논문은 기관실구조의 특설늑골의 치수를 검토할 수 있는 한 방법으로써 설계단계에서 정하중 및 동하중을 고려한 합리적인 설계가 될 수 있을 것으로 판단된다.

• 한국소성가공학회:학술대회논문집
• /
• 한국소성가공학회 2003년도 추계학술대회논문집
• /
• pp.25-28
• /
• 2003

The articulated piston that was used to more powerful diesel engine was composed by Al casted skirt part and steel forged crown part. this paper has the target to design the forging process of crown part. The parameters of piston design and forging process design were gotten based on work experience, experimental data, approximately calculated data and finite element analysis. Preform design parameter decided using the Taguchi method. Through this research, could design optimal shape of preform and produce prototype of the articulated piston

• 한국정밀공학회:학술대회논문집
• /
• 한국정밀공학회 2005년도 춘계학술대회 논문집
• /
• pp.139-142
• /
• 2005

The Digital Meister is an advisory system to help the designer using the knowledge obtained from design and analysis data. In this paper, Taguchi method was applied to analyze the design parameters of automotive engine pulley. As a finite element method (FEM), ALGOR Multi-physics was used for analyzing the static analysis. As a result, two bending positions and material thickness were highly related to the maximum stress. These correlations between design parameters and analysis result will be used for supporting the design process of Digital Meister.

• 한국소음진동공학회:학술대회논문집
• /
• 한국소음진동공학회 2006년도 춘계학술대회논문집
• /
• pp.314-319
• /
• 2006

Main focus on balance shaft module is to reduce the vibration triggered from engine block and compensate it from unbalance mass in balance shaft. Since the performance of balance shaft module is controlled by rotor shape including unbalance mass, a design strategy on rotor is key issue on determine the quality of balance shaft system. Even the design result on balance shaft mostly affect the lay-out of housing and other related components, its issue on balance shaft should be considered in advance throughout the total design procedure. In this paper, optimal design strategy focused on balance shaft is presented to make a design process efficiently with ensuring its high performance. And its method is verified with field design process of balance shaft in commonly adapted vehicle with 3-cylinder and 4-cylinder engine.

• 한국자동차공학회논문집
• /
• 제3권5호
• /
• pp.10-16
• /
• 1995

In this study, the optimum design is carried out upon the crankshaft of in-line 6-cylinder internal combustion diesel engine with the mechanical analysis for the layout design, which is standard calculation whose process contains quadratic curve fitting method and quasi newton method about cost function, design variables and constraint conditions, Without finite element analysis, this process in wich mechanical analysis is performed upon the most critical part in crankshaft gives necessary and satisfied output in layout design and saves time and cost in developing a new diesel engine. In this study, also, the 3-dimensional finite element method is used in confirming the standard calculation for the optimization of crankshaft and the shape optimization in crankweb is obtained.

• 항공우주시스템공학회지
• /
• 제1권3호
• /
• pp.13-20
• /
• 2007

The objective of this study is to investigate endurance test of localization part for T-50 aircraft engine. Major localization parts of the engine (F404-STW-102) was performed using Accelerated Simulated Mission Engine Test. The purpose of this test is to evaluate of quality demonstration capability, to verify design of engine localization parts, and to improvement safety and operation rate of T-50 advanced trainer by finding out operational problems in production phase and fixing it.