• 월간 기계설비
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• no.spc85
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• pp.88-94
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• 1997

• The Journal of the Acoustical Society of Korea
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• v.26 no.6
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• pp.286-292
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• 2007

The dominant source of noise in a sea-connected piping system is usually due to a seawater cooling pump which circulates seawater to operate onboard equipments normally, and so its water-borne noise with some tonal frequencies should be reduced using proper silencers. In order to obtain the transmission loss of water-borne noise silencers experimentally the present paper suggests a transfer function technique that acoustic wave in the piping system is decomposed into its incident and transmitted components when the reflection at the termination of the system exists. Good agreement in the interested frequency range with theory and the proposed technique shows the validity of the technique.

• Journal of the Korean Society of Marine Environment & Safety
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• v.30 no.2
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• pp.233-238
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• 2024

The pipe cleaning process is a crucial step in the shipbuilding process of a shipyard. It involves removing foreign substances from the inside of the pipes before moving on to the stage of testing equipment after installing the pipes. If there are foreign substances inside the pipes and the equipment is tested, the foreign substances can enter the high-priced equipment and become a factor in the breakdown of pumps, gears, bearings, and other components. Especially in the case of pumps or hydraulic valves, even small foreign substances can lead to major accidents if they enter the equipment, and such equipment accidents can be a potential cause of major disasters, leading to accidents involving workers operating the equipment in the vicinity. Therefore, it is a process that shipyard customers, who are shipowners, also focus on and manage very intensively. To solve these problems, this study developed a system that can increase the cleaning effect of the cleaning fluid inside the pipes by increasing the flow of the cleaning fluid inside the pipes in the existing pipe cleaning method.

• Proceedings of the Korean Nuclear Society Conference
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• 1998.05a
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• pp.617-622
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• 1998

일체형원자로인 SMART에서는 증기발생기와 주순환펌프가 배관으로 연결되어 있지 않고 주순환펌프를 통과한 냉각수가 압력헤더를 통하여 12개의 증기발생기 카세트로 흐르게 된다. 각 증기발생기 카세트를 통과하는 냉각수 유량분포의 비균일도를 운전모드에 따라 계산하여 이 압력헤더가 각 증기발생기 카세트로 흐르는 냉각수 유동분포에 미치는 영향을 분석하고 SMART 주순환펌프 압력헤더의 설계가 설계기준을 만족시키는 지를 검증하였다. 검증계산 결과 비균일도가 정상운전시는 0.8%. 비정상 운전시는 7.1%로 설계기준을 만족시키는 것을 확인하였다.

• Aerospace Engineering and Technology
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• v.4 no.1
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• pp.171-178
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• 2005

An acoustic analysis of a fuel-rich gas generator for the drive of a turbopump in a liquid rocket engine has been performed and the length of a simulating duct has been determined by comparing the resonant frequency of unstable acoustic modes to simulate an actual flight model gas generator. To simulate more realistically, a realistic short-length simulating duct has been determined by considering 1 or 2 wavelength of the unstable modes. Duct-length adjustment to turbopump can be a method to suppress a combustion instability problem by decoupling of acoustic mode and combustion characteristics. This method has been set up and validated with acoustic analysis and hot firing tests.

• Proceedings of the Korean Society for Noise and Vibration Engineering Conference
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• 1995.04a
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• pp.318-321
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• 1995

원자력 발전소의 안전성 보장 및 신뢰성 향상을 위하여 시운전 단계에서 원자력 발전소내 안전등급에 해당하는 배관계통의 상태 확인을 위하여 각종시험을 하도록 되어있다. 특히 새로운 설계기념, 크기 또는 용량을 갖는 원자로 모델에 대해서는 필수적으로 건전성 평가를 하게 되었다. 이를 위해 발전소 건설기간에 시행하는 고온 기능시험 중에 원자로 주변 주요 시스템인 원자로 냉각재 루프 계통에 대한 건전성 확인을 위해 압전형 고온 가속도 센서를 이용하여 정상운전상태의 진동을 측정하여 시스템 진동거동을 규명하였다. 배관시스템의 일상운전상태는 유체의 흐름과 기기운전이 일정한 정상상태와 펌프의 기동 또는 정지 및 밸브의 급격한 개폐등으로 발생하는 과도상태로 나눌 수 있다. 따라서 두 가지 상태의 진동을 측정해야 한다. 배관계통은 정상운전 상태로 설계수명을 유지할 수 있어야 하므로 정상진도잉 최소화 되어야 한다. 진동 평가기준은 배관재질의 응력(S/N 커브) 곡선을 참조하여 설계수명내에 손상이 일어나지 않도록 재료의 허용응력을 산정하고 이를 진동변위로 환산하여 정한 것이며 이 값에 측정 데이타를 비교하여 1차계통 배관의 건전성을 확인하였다.

• Journal of the Korean Society of Propulsion Engineers
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• v.21 no.4
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• pp.1-11
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• 2017

TPTF (Turbopump Real Propellant Test Facility) at Naro Space Center has used alcohol burner system to simulate the gas flow of gas generator of liquid rocket engine. During the test at TPTF, the temperature and pressure at turbine inlet were smoothly increased while those of the gas generator of engine were constant. Present research developed a simulation code for the burner and the piping system and applied to the system. The calculation results were in good agreement with the test, and confirmed quantitatively that the non-steadiness is due to the heat transfer of the pipe. While the insulation of the pipe is ineffective, the length has a large impact on the turbine inlet condition. The present research clarified the empirically estimation of test condition, and can be applied to determination of the following test conditions.

• Journal of the Korean Society of Propulsion Engineers
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• v.22 no.4
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• pp.61-67
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• 2018

High-frequency signals are analyzed at the inlet/outlet pipeline and pump casing during cavitation tests of the LOx pump for liquid rocket engines. Root-mean square values of all data are investigated with respect to cavitation number. The values of synchronous, harmonic, and cavitation instability frequencies are also calculated. Pressure pulsations of the inlet and outlet pipelines are affected by cavitation instabilities. The 3x component (i.e., the blade-passing frequency of the inducer) is predominant in the outlet pulsation sensor. This seems to be related to the fact that the number of impeller blades is a multiple of the number of the inducer blades. The cavitation instability is also measured at the accelerometer of the pump casing.

• The Magazine of the Society of Air-Conditioning and Refrigerating Engineers of Korea
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• v.29 no.9
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• pp.27-37
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• 2000

설비시스템 설계에 있어 물과 공기를 반송하는 펌프와 송풍기는 배관 및 덕트 설비의 동력원으로써 건물에너지 소비량의 대단히 큰 비중을 차지할 뿐 아니라, 시스템 계획상 중요한 요소이면서도 시스템 계획에 부적합하게 선정되어 효율적인 시스템 구성에 실패하는 사례가 종종 있다. 설비시스템 설계에 있어 펌프나 송풍기의 선정과 적용에 필요한 기본적인 내용들을 정리하여 효율적인 시스템 설계에 도움이 되고자 한다.

• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 2007.04a
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• pp.322-325
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• 2007

This paper shows the development procedure of the low pressure LOX feed system which is used in the liquid rocket with a turbopump. Korean Air has cooperated with KARI in developing the LOX feed system to turbopump. The LOX feed system is characterized with cryogenic temperature and the thin-thickness tube for weight saving. The system in this project is composed with a main feed line and a recirculation line for the LOX temperature conditioning. Each piping system has many components, namely, bellows, filter, orifice, valves, flange and support. In this paper, system design & manufacturing, structural & thermal analyses, and component tests are explained. Finally, the system was assembled to the KARI's PTF test facility and functioned well to meet its required performance.