• Journal of Advanced Marine Engineering and Technology
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• 제29권7호
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• pp.713-721
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• 2005

A marine diesel engine should realize optimal operation efficiency while reducing NOx, PM (Particulate Matters) and other emissions. Fuel injection systems that use electronic control can become an effective means of achieving that objective. However. it still needs some accurate and instant information in order to bring its ability into full potential while sailing on the sea. The important information of them are a shaft torque and continuous combustion pressures of all cylinders. The shaft torque and the propeller thrust described in this paper are measured at an intermediate shaft by using a unique principle that one of two electromagnet coils oscillates a vibrating strip which the length changes with force and the other coil picks up the change of the frequency of the vibrating strip. For further reference, the shaft power meter multiplied the torque by the shaft revolution has already had about 750 sets of sales performance. The research presented in this paper started about ten years ago and is concerned with the development of a combustion pressure sensor that uses the same principle. Recently, the pressure sensor which bears continuous operation has been developed after a hard struggle, that is, the system that consists of a shaft horsepower meter, a propeller thrust meter and a combustion pressure sensor has been completed and has been shown to be reliable. This paper describes the configuration of this system, the material of the combustion pressure sensor, the principle of that, and the improving point of the sensor, and, we finally consider the use of this system.

• 한국항공우주학회지
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• 제42권10호
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• pp.823-832
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• 2014

변위 비케플러 궤도란 질량중심이 궤도면에 대하여 변위를 갖는 궤도인데, 일반적인 궤도에 비해 다양한 임무를 수행할 수 있다는 장점이 있다. 비케플러 궤도를 유지하기 위해서는 지속적인 추력이 필요한데, 태양돛 우주선은 연료 소모 없이 지속적으로 추력을 얻을 수 있기 때문에 비케플러 궤도 운용에 적합하다. 본 논문에서는 소모성 추진제와 태양돛에 모두 적용할 수 있는 비케플러 궤도 이론을 소개하고, 태양돛 우주선에 적용시 차이점을 분석하였다. 비케플러 궤도를 4가지 유형으로 분류하고 궤도 유지를 위한 요구가속도를 계산하였다. 각 유형별 궤도안정성 식을 분석하고 시뮬레이션을 통해 검증하였다. 불안정 영역에서 궤도를 제어하기 위해 실시간 LQR을 적용한 제어기법을 개발하여 이에 대한 시뮬레이션을 수행하였다.

• 조명전기설비학회논문지
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• 제18권1호
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• pp.122-128
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• 2004

본 논문에서는 가동자의 이동방향에 따른 진동과 고정자에 대하여 수직으로 작용하는 진동을 동시에 고려할 수 있는 이론을 제시함에 있어서, LSM의 구조를 기초로 자기등가회로를 구성하였으며, 자기등가회로에 대한 방정식을 이용하여 LSM의 전기적인 등가회로를 유도하였다. 그리고, LSM의 변위에 따른 수직력 분포를 유한요소법(Flux2D)으로 계산하였으며 이를 방정식으로 나타내었다. 최종적으로 1상 여자방식에 의한 가동자의 이동방향에 따른 진동과 고정자에 대하여 수직으로 작용하는 진동을 전압방정식, 추력 및 수직력 방정식, 운동방정식을 사용하여 ACSL(Advanced Continuous Simulation Language)에 의하여 시뮬레이션 하였다.

• 자원환경지질
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• 제9권1호
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• pp.13-26
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• 1976

The basic rocks distributed in the Okchon paleogeosynclinal zone have been previously considered as intrusive in majority, but as sedimentary parensis in few variety. The present study is to find out some clues to conclude otherwise, if any, by clarifying 1) the nature and characteristics of the rocks, 2) type of the associated sedimentary rocks if any, and 3) their occurrence in related to regional geologic structure. The finding are as follows: 1) The basic rocks are identified and classified to hornblende gabbro, amphibolite, basalt and andesite (in part metamorphosed to meta-volcanics), green schist and peridotite(which appears in separate locality from the others). 2) Associated sedimentary rocks which appear to overlie the basic rocks are known as Kunjasan and Baekwhasan formations. The two formations are probably same, but been used differently by different authers at different localities. The rocks is exclusively consisted of cherty looking siliceous quartzite and some localitis it shows very calcarious nature. The formation seems to indicate a sort of pelagic siliceous sediments although it contain some pebbles. 3) The basic rock suites are always underlain by the same continuous, great thrust, which separates the Okchon paleogeosyncline zone from the neogeosynclinal zone in the area studied. The comparison of Okchon basic rocks suite to the ophiolite suites in other parts of the world indicates some similarity with which the writers suggested the probalility of Okchon basic rocks being ophiolites that occur along ancient geosuture line now represented by the great thrust.

• Agricultural and Biosystems Engineering
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• 제4권1호
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• pp.34-38
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• 2003

A mathematical model was developed for estimating the mechanical interrelation between characteristics of soil and main design factors of a tracked vehicle, and predicting the tractive performance of the tracked vehicle. Based on the mathematical model, a computer simulation program (TPPMTV) was developed in the study. The model considered the continuous change in tension for the whole track of a tracked vehicle, the analysis of shape and tension of the track segment between sprocket and first roadwheel, and the side thrust on both sides of grouser by the active earth pressure theory in predicting the tractive performance of a tracked vehicle. Also, the model contained not only sinkage depth of the track but the pressure distribution under the track in analyzing the side thrust. The effectiveness of the developed model was verified by performing the draw bar pull tests with a tracked vehicle reconstructed for test in loam soil with moisture content of 18.92％. The predicted drawbar pulls by the model were well matched to the measured ones. Such results implied that the model developed in the study could estimate the drawbar pulls well at various soil conditions, and would be very useful as a simulation tool for designing a tracked vehicle and predicting its tractive performance.

• 한국추진공학회:학술대회논문집
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• 한국추진공학회 2004년도 제22회 춘계학술대회논문집
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• pp.306-313
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• 2004

The microwave discharge ion engine generates plasmas of both the main ion source and the neutralizer using 4㎓ microwave without discharge electrodes and hollow cathodes, so that long life and durability against oxygen and air are expected. The MUSES-C “HAYABUSA” asteroid explorer installing four microwave discharge ion engines “$\mu$10s” was launched into deep space by M-V rocket No.5 on May 9, 2003. After vacuum exposure and several runs of baking for reduction of residual gas the ion engine system established the continuous acceleration of the spacecraft toward the asteroid “ITOKAWA”. The Doppler shift measurement of the communication microwave revealed the performance of ion engines, which is 8mN thrust force for a single unit with 3,200sec specific impulse at 23mN/㎾ thrust power ratio. At the end of 2003 the accumulated operational time exceeded 8,000 hour and unit. HAYABUSA will execute the Earth swing-by on June 2004 and arrive at the asteroid in 2005 and return to Earth in 2007.

• 한국항공우주학회지
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• 제33권1호
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• pp.1-10
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• 2005

비정렬 격자계에서 continuous adjoint 방정식을 사용하여 제자리 비행을 하는 헬리콥터 로터 블레이드에 대한 공력 형상 최적설계 기법을 개발하였다. 효율적인 민감도 계산을 위해 회전좌표계에서 continuous adjoint 민감도 해석 기법을 유도하였다. 설계과정의 반복적인 수치계산의 효율을 높이기 위해서 영역 분할 기법에 기반을 둔 병렬처리 기법을 도입하였다. 끝단 와류의 정확한 포착을 위해서 끝단와류를 따른 격자적응을 수행하였다. 이러한 방법은 Caradonna와 Tung의 실험형상 및 UH60 헬리콥터 로터 블레이드의 공력 최적설계에 적용되었으며, 본 연구에서 사용된 최적설계 기법을 이용하면 일정한 추력을 유지하면서 요구동력을 현저하게 줄일 수 있음을 보였다.

• 한국항공우주학회지
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• 제47권9호
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• pp.658-664
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• 2019

핀틀 인젝터를 사용하는 액체로켓개발에 있어서 분무특성인 분무각도, 액적크기, 액적의 분포정도는 중요한 요소이다. 세 종류의 다중 홀형 핀틀 팁과 연속형 핀틀 팁을 설계하여 분무실험을 수행하였다. 다중 홀형 인젝터에서 홀 개수에 따른 액적크기는 크게 차이가 없었으며, 홀 개수가 많을수록 액적이 균일하게 분포하였다. 연속형 핀틀은 다중 홀형 핀틀보다 액적의 미립화가 잘 이루어 지고 공간내로 더 고르게 분산되는 것을 확인하였다. 핀틀의 액체분사면적조절을 통한 추력제어는 다중 홀형보다는 면 접촉 닫힘(face-shutoff)이 용이한 연속형 핀틀이 적합하다. 각 핀틀 팁의 TMR에 따른 분무각을 측정하여 특정한 경향성과 그에 해당하는 경험식을 도출하였다.

• 제어로봇시스템학회:학술대회논문집
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• 제어로봇시스템학회 2003년도 ICCAS
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• pp.7-12
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• 2003

In this paper, S(stochastic)-eigenvalue concept and its S-eigenvector for linear continuous-time systems with probabilistic uncertainties are proposed. The proposed concept is concerned with the perturbation of eigenvalues due to the probabilistic variable parameters in the dynamic model of a plant. S-eigenstructure assignment scheme via the Sylvester equation approach based on the S-eigenvalue concept is also proposed. The proposed design scheme is applied to the longitudinal dynamics of open-loop-unstable aircraft with possible uncertainties in aerodynamic and thrust effects as well as separate dynamic pressure.

• Journal of Mechanical Science and Technology
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• 제18권6호
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• pp.933-945
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• 2004

In this paper, S (stochastic)-eigenvalue concept and its S-eigenvector for linear continuous-time systems with probabilistic uncertainties is proposed. The proposed concept is concerned with the perturbation of eigenvalues due to the probabilistic variable parameters in the dynamic model of a plant. S-eigenstructure assignment scheme via the Sylvester equation approach based on the S-eigenvalue concept is also proposed. The proposed design schemes are illustrated by numerical examples, and applied to the longitudinal dynamics of open-loop-unstable aircraft with possible uncertainties in aerodynamic and thrust effects as well as separate dynamic pressure. These results explicitly characterize how S-eigenvalues in the complex plane may impose stability on S-eigenstructure assignment.