• 제목/요약/키워드: Linear engine

검색결과 317건 처리시간 0.023초

액체로켓엔진 연소실에서의 상온 음향 시험 (Acoustic Tests on Atmospheric Condition in a Liquid Rocket Engine Chamber)

  • 고영성;이광진;김홍집
    • 대한기계학회논문집B
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    • 제28권1호
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    • pp.16-23
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    • 2004
  • Acoustic characteristics of unbaffled and baffled combustion chamber are experimentally investigated under atmospheric condition to preliminarily determine baffle for mitigation of combustion instability. To investigate the effect of the baffle which has several configurations such as radial baffles and hub/blade baffle, resonant-frequency shift and damping factors of the chamber were analyzed and compared quantitatively with those of the unbaffled combustion chamber. From a view of acoustic characteristics, radial baffles with several configurations have not much difference in resonant-frequency shift and damping factor ratio with each other. On the other hand, hub and blade baffle is very effective to suppress the first tangential mode which was found to be the most harmful acoustic mode in KSR(Korean Sounding Rocket)-III engine. But more study on design parameters such as hub size and axial length should be done for complete optimization of hub and blade baffle. The present study based on linear acoustic analysis is expected to be a useful confirming tool to predict acoustic field and design a passive control devices such as baffle and acoustic cavity.

로켓엔진 연소기에서 반파장 공명기의 음향감쇠에 관한 수치적 연구 (Acoustic-Damping Characteristics of Half-Wave Resonator in a Combustion Chamber of Liquid Rocket Engine)

  • 손채훈;박이선
    • 한국추진공학회지
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    • 제9권4호
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    • pp.9-15
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    • 2005
  • 고성능 연소기에서 주로 채택되는 기체-액체형 동축 분사기의 음향감쇠 효과를 선형 음향해석을 통해 조사하였다. 그러한 형태의 분사기는 반파장 공명기 역할을 수행할 수 있으므로 반파장 공명기와 1/4파장 공명기의 음향감쇠 특성을 비교/조사하였다. 공명기의 음향 감쇠 효과에 있어서 경계흡수계수의 영향과 공명기 길이 효과를 알아보았고, 연소실과 공명기내 유체의 음속 변화를 통해 반파장 공명기의 음향 감쇠 특성을 조사하였다. 계산 결과, 공명기의 최적 동조 길이가 짧고, 공명기내 유체의 음속이 낮은 조건에서 큰 감쇠효과가 나타남을 알 수 있었다. 또한, 경계흡수계수의 감소는 공명기의 동조 길이 범위를 좁게 하였다.

선박용 디젤엔진을 위한 지능적인 속도제어시스템의 설계 (Design of an Intelligent Speed Control System for Marine Diesel Engines)

  • J.S.Ha;S.J.Oh
    • Journal of Advanced Marine Engineering and Technology
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    • 제21권4호
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    • pp.414-420
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    • 1997
  • An intelligent speed control system for marine diesel engines is presented. The approach adopt¬ed is to use a conventional PID controller for normal operation and a feedforward controller for adaptive control. The feedforward controller is a neural network. The neural network is the inverse dynamics model of the plant, which is being trained on line. The parametric model of the diesel engine is represented in a linear second-order system, with a first-order combustion part and a revolution part each at a normal operating point. The time delay in the control of the com¬bustion part is approximated to the first-order system. The tuned PID parameters are set based on the model for normal operating point. To obtain the inverse dynamics of the diesel engine system, two neural networks are used, one for inverse, the other for forward dynamics. The former is posi¬tioned across the plant to learn its inverse dynamics during operation, and the latter is placed in series with the controlled plant. Simulation results are presented to illustrate the applicability of the proposed scheme to intelligent adaptive control of diesel engines.

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베어링 캡 유한 요소 해석 설계 방법 (Design Methodology of Main Bearing Cap by a Finite Element Analysis)

  • 양철호;한문식
    • 한국자동차공학회논문집
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    • 제17권1호
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    • pp.80-86
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    • 2009
  • Main bearing cap is one of the essential structural elements in internal combustion engine. Main bearing cap guides and holds the crankshaft, withstanding the full combustion and inertia loads of the engine. A seamless design methodology using FEA has been proposed to produce a reliable design of main bearing cap. A Levy's thick cylinder model was applied to calculate the contact pressure between bearing shell and housing bore. A calculated contact pressure at housing bore is within the allowed limit comparing with that from bearing shell model. An adequate FEA model was suggested to obtain reliable solutions for the durability of main bearing cap. 3D global model consists of engine bulkhead, main bearing cap, and bolts. Sub-model consisting of cap and part of bolts is used to get detailed solution of main bearing cap. A very careful contact modeling practice is needed to resolve the convergence problems frequently encountering during combined geometric and material non-linear problems. A proposed methodology has been applied to the main bearing cap model successfully and obtained reliable stress results and fatigue safety factors.

PSD322-Axle형 지게차 자동변속기의 변속제어 (Shifting Control Method for Automatic Transmission of PSD-Axle Forklift)

  • 권순기;최시영;권기령;한승우
    • 한국생산제조학회지
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    • 제18권6호
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    • pp.565-575
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    • 2009
  • A forklift (also called a lift truck) is a powered industrial truck that is used to lift and transport materials. It has become an indispensable piece of equipment in manufacturing and warehousing operations. The modem forklift is equipped with automatic transmission to meet the requirement of loading and easy operation of the vehicle. This paper proposes the design of TECU(Transmission Electronic Control Unit) which is applied to PSD322-Axle transmission. Garofalo's control technique is generally used to the automatic transmission. We consider the work quality and market requirement that does not want to control engine throttle. This paper proposes new controller system which guarantees efficient speed changes with simple system. This new system does not control the engine throttle spontaneously. But it has the load of engine and vehicle as a maximum disturbance. The scope of the disturbance is limited to the stoll area of the torque converter. This paper proposes a ideal control commander that converges relative velocity of the input and ouput of a clutch into a zero. We design linear controller to execute the idea control commander. We applied the control algorithm to the forklift of PSD322-Axle type and the performance of this controller was verified.

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액체추진제 로켓엔진 연소기 저주파 동특성 (Low Frequency Dynamic Characteristics of Liquid-Propellant Rocket Engine Combustor)

  • 하성업;정영석;김희태;한상엽;조광래
    • 한국추진공학회지
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    • 제8권4호
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    • pp.91-101
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    • 2004
  • 분사기와 연소실만을 가지는 연소기의 수학적 선형모델을 가지고, 액체추진제 로켓엔진 연소기에 대한 저주파 동특성 분석을 수행하였다. 연소실의 압력변화가 추진제 유량변화로 되먹임되는 구조를 가짐에 따라 저주파 섭동을 나타냈으며. 연소실의 시정수가 증가할수록, 분사기의 차압이 증가할수록, 연소시간지연이 짧을수록 시스템은 안정하였다. 분사기 시정수 변화가 안정성에 미치는 영향은 크지 않았다. 연소시간지연이 없는 경우의 시스템은 항상 안정하였으며, 지연시간이 증가할수록 섭동 주파수 및 감쇠율은 줄어들며, 결국 시스템은 불안정하게 되었다.

다중 엔진모델을 이용한 센서 고장허용 가스터빈 엔진제어기 설계 (Sensor Fault-tolerant Controller Design on Gas Turbine Engine using Multiple Engine Models)

  • 김중회;이상정
    • 한국추진공학회지
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    • 제20권2호
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    • pp.56-66
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    • 2016
  • 모델기반 FDI 과정에서 모델오차와 센서잡음은 피할 수 없으므로 견실성은 모델기반 FDI에서 매우 중요하다. 본 연구에서는 이러한 선형모델 오차 및 신호잡음으로 인하여 고장진단 과정에서 발생하는 결함판단 오류들을 비선형 NARX (Nonlinear Auto Regressive eXogenous) 모델과 칼만추정기를 적용하여 개선하는 방법을 제안하였다. 최종 고장판단은 퍼지로직을 이용하여 발생하는 오차의 추이에 대한 확률로 결정하여 순간적인 신호잡음에 강인하도록 설계하였다. 시뮬레이션을 통하여 운용 환경조건에서 엔진제어기의 고장허용에 따른 성능을 확인하였다.

75톤급 액체로켓엔진의 가상적 고장 상황에서의 칼만 필터 잔차 생성 (Kalman Filter Residual Calculation of a 75-ton Liquid Rocket Engine under an Artificial Fault)

  • 이계림;차지형;고상호;박순영;정은환
    • 한국추진공학회:학술대회논문집
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    • 한국추진공학회 2017년도 제48회 춘계학술대회논문집
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    • pp.218-223
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    • 2017
  • 본 논문은 75톤급 액체로켓엔진의 상태진단을 위해 칼만 필터를 이용한 고장진단 연구를 수행하였다. 칼만 필터 설계를 위해 75톤급 액체로켓엔진 비선형 시뮬레이션 모델을 공칭 작동점에서 선형화하였으며, 정상 모델의 상태량 변수 4가지를 이용하여 측정값과 추정값 비교를 통해 칼만 필터의 성능을 확인하였다. 이를 이용한 고장진단 알고리즘의 성능을 확인하기 위하여 터보펌프 고장을 모사하였으며 정상 모델의 잔차 변화를 비교하여 칼만 필터를 이용한 고장진단이 가능함을 확인하였다.

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TRANSIENT PERFORMANCE OF AN SI ENGINE BY TRANSIENT RESPONSE SPECIFICATIONS

  • Kwark, J.H.;Jeon, C.H.;Chang, Y.J.
    • International Journal of Automotive Technology
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    • 제4권3호
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    • pp.109-117
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    • 2003
  • The analysis and evaluation of the transient performance by the transient response specifications under various acceleration speeds and types based on driver's typical acceleration habit are implemented by the experimental study to provide the appropriate direction for the transient control in a gasoline engine. The concept of the transient response specifications which consist of delay time, rising time, maximum overshoot and settling time, and the analysis method using them are introduced to evaluate the characteristics of the transient performance quantitatively. Furthermore four acceleration speeds and four acceleration types are set respectively to realize the various transient states which are similar to the real drive. Several performance parameters in terms of engine speed, manifold absolute pressure, fuel injection duration and air excess ratio are measured simultaneously during the various acceleration using a throttle actuator controlled by a PC. The transient response specifications characterized well the transient performance for the various acceleration speed and types quantitatively. Delay and rising time with increment of the acceleration speed became shorter, but settling time did longer. Intensified acceleration type appeared to be the most economical in view of fuel consumption, and linear acceleration type was found to have the least harmful emission concentration.

초내열합금 링제품의 형상링 압연 제조 기술 (Profile Ring Rolling Manufacturing Technology of Alloy 718)

  • 김태옥;김국주;김남용;이진모;염종택
    • 한국소성가공학회:학술대회논문집
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    • 한국소성가공학회 2009년도 추계학술대회 논문집
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    • pp.425-428
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    • 2009
  • Aerospace engine application needs to stand high temperature and pressure. Because of its mechanical properties such as high strength at high temperature, Alloy 718 is used aerospace engine application about 80%. But alloy 718's mechanical properties cause some problem to manufacturing profile ring like damage of material and mold. In this study, alloy 718's mechanical properties investigated for knowing its formability and using FE-Simulation for designing profile ring roll process and mold shape. Profile ring rolling processing is designed with "Initial material$\rightarrow$Blank$\rightarrow$Linear Ring$\rightarrow$Profilering". Blank's heating temperature is setting $1100^{\circ}C$ for manufacturing a trial profile ring on the basis of FE-Simulation. As a result of manufacturing alloy 718 profile ring, it is possible to make near target profile shape ring with all of the processing condition which gives in this study.

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