• Journal of Advanced Marine Engineering and Technology
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• 제11권3호
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• pp.53-60
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• 1987

Steam ejector is a equipment which compresses the gases to desired discharge pressure. It is widely used for the evacuation systems because of its high working confidence. And recently it is used as the thermo-compressors in the various energy saving systems. Steam ejector is constructed of three basic parts; a suction chamber, a motive nozzle and a diffuser. The high velocity stream jet of steam emitted by the motive nozzle creats suction chamber, which draws the low pressure gases. The diffuser converts the kinetic energy of high velocity flow to pressure energy. It is not easy to determine the dimensions of a steam ejector met to the desired design condition, because that the expected suction rates must be obtained by reapeating the complicate calculation. And also such a calculation is concomitant with geometrical analysis for suction part and diffuser based on the stability of steam flow. Therefore, it is considered that the Computer-Aided Design (CAD) of steam ejector is a powerful design method. In this paper, computer program for steam ejector design is developed based on the theoretical research and the previous experimental results. And the determinating method of diffuser inlet angle and the velocity development profile of suction gas along to the diffuser are suggested. The validity of the development profile of suction gas along to the diffuser are suggested. The validity of the developed computer results with other's for the practical design calculation of a manufactured steam ejector.

• 한국소음진동공학회:학술대회논문집
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• 한국소음진동공학회 2001년도 춘계학술대회논문집
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• pp.1162-1167
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• 2001

Suction valve fluttering is generated by reciprocating motions of the piston inhaling and discharging process of gas in the hermetic compressor. A reactive type suction muffler, which produces high pressure-drop because of its complicated flow path, controls the impulsive noise radiated from the flutter of suction valve. The high-pressure drop in the muffler increases the transmission loss, but reduces the EER(Energy Efficiency Ratio) of the compressor. We consider how to design the high acoustic attenuation and low pressure-drop performance to take account of the acoustic and flow performances of the suction muffler. In this study, we identified the suction noise source of compressor from the measurement of the acoustic pulsation and flutter of suction valve. We analyzed the acoustic characteristics of muffler using the finite element method, and compared the experimental and analytical characteristics of flow path of suction muffler. Theoretical predictions and experimental results are compared from the viewpoint of the acoustic performance and energy efficiency of the compressor.

• 한국정밀공학회지
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• 제19권2호
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• pp.220-227
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• 2002

The design of suction muffler for compressor aims to achieve a maximum noise reduction and a minimum pressure loss. Until now, the design process has been performed experimentally rather than theoretically. In this paper, to achieve the maximum noise reduction and minimum pressure loss. we studied the effect of the shape and volume of the expansion tube of the muffler on TL and pressure drop. We made an extensive use of computer program such as SYSNOISE. FLUENT, and STAR-CD to calculate the TL and pressure distribution of suction muffler. The design of the muffler is optimized with respect to flow loss and TL. Experiments are performed to check the result of design change, which proves satisfactory results. It is expected that this process can reduce time to design a muffler in the fields.

• 대한토목학회논문집
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• 제39권2호
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• pp.317-325
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• 2019

석션 케이슨은 설치 수심제한이 적고, 비교적 단순한 설치공정과 빠른 시공이 가능하기 때문에 해양 구조물용 앵커 및 기초형식으로 활용되고 있으며 그 적용이 점차 확대되고 있다. 석션 케이슨 기초의 설계는 지반의 지지력 및 안정성 검토가 중심이 되며, 관련 설계기준에서 해석 방법을 제시하고 있다. 반면, 케이슨의 구조적 안전성 분석은 방법이 정형화되지 않았으며 특히 케이슨에 작용하는 하중 모델링에 대한 명확한 산정 방법이 정립되지 않아 석션 케이슨 단면 설계에 어려움이 있다. 이러한 이유로 본 연구에서는 이론 및 수치적 침투해석을 통해 석션압에 의해 발생되는 케이슨 내외부의 간극수압 크기 및 분포를 분석하고, 이를 바탕으로 구조해석에 적용할 수 있는 합리적인 하중 평가 방법을 제시하였다. 추가적으로 관입깊이, 투수계수의 이방성, 석션압 변화가 내외벽에 작용하는 간극수압에 미치는 영향을 분석하였다.

• 대한설비공학회:학술대회논문집
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• 대한설비공학회 2007년도 동계학술발표대회 논문집
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• pp.404-409
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• 2007

For a hermetic reciprocating compressor, it has been known that the gas pulsation in the suction line affects the compressor performance, and suction muffler design has been focused on both of noise reduction and minimum pressure drop across the muffler. Some studies have been carried out on the mutual interaction between the gas pulsation and the cylinder pressure to investigate some supercharging effects, but their efforts were limited on rather simple geometries. In this paper, interaction of the gas pulsation in the compressor suction line with cylinder pressure via suction valve motion has been calculated; for the gas pulsation analysis, modeling of Helmholtz resonators in series was used, and for cylinder pressure calculation, energy equations was set up for the gas inside the cylinder. For demonstration of this calculation method, four different types of suction line configurations for a hermetic reciprocating compressor were compared in terms of compressor performance and gas pulsation level.

• 한국지반공학회논문집
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• 제36권12호
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• pp.35-43
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• 2020

현재 국내에서 하천/해상 교량 공사시 교량기초 설치를 위한 가시설로서 원형 단면의 가물막이(cofferdam)를 많이 적용하고 있다. 기존 케이슨(caisson), 시트파일(sheet pile), 셀(cell) 식 등의 가물막이 공법이 많이 활용되고 있으나 이러한 공법은 설치 및 해체시 많은 시간과 비용이 소요된다. 해상공사에서 가장 보편적으로 사용되고 있는 시트파일 공법의 경우 지반 관입에 의한 시트파일 손상과 요소 부재 연결 작업의 어려움으로 내적 및 외적 안정성 확보를 위해 주의가 필요하다. 본 연구에서는 서해안 연약지반을 대상으로 원형강관의 석션관입성 설계를 수행하였고, 현장실험을 통하여 원형강관 석션관입 시공이 가능한 것을 확인하였다. 그리고 표준관입시험(N치) 결과보다 콘관입시험(CPTu)을 이용한 지반 분석 결과를 설계에 적용하는 것이 현장 실험 결과와 보다 유사한 결과를 나타내는 것을 확인하였다. 또한 실트질 사질토 지반에서 상한석션압 이상의 석션압을 적용시 가물막이 내부의 국부적인 파괴(piping 현상)를 유발하는 것을 확인하였다.

• 대한기계학회논문집B
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• 제28권4호
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• pp.406-414
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• 2004

In Gerotor pump, the pressure pulsations which occur due to the pump geometry result in vibration and noise of pump elements as well as cavitation in hydraulic system when the chambers of gerotor enter the delivery port and leave the suction port. Therefore it is important to study on the pressure pulsations before design and analysis of characteristics in Gerotor pump. In this paper, to reduce the unnecessary pressure pulsations, the port plate of Gerotor pump is designed based on the notch of the vane pumps and the relief grove of the piston pumps. The theoretical analysis of the pressure pulsations is performed in consideration of design parameters of the port plate which include each port positions and groove width and operating conditions which include rotational velocity and delivery pressure.

• 한국산학기술학회논문지
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• 제22권2호
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• pp.1-10
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• 2021

본 연구에서는 해상(수상) 교량기초 시공 시 석션압으로 간편하게 설치될 수 있는 원형관 공법을 개발하고자, 실내 모형실험을 통하여 저수심 모래지반에 원형관 관입 시 설치 석션압을 평가하였다. 포화된 사질토의 반복실험을 위해 3개의 진동발생기를 활용한 진동다짐 토조 시스템을 구축하였고, 지반강도 확인을 위하여 소형 콘관입 장비를 활용하였다. 진동다짐 토조 시스템은 내부의 모래지반에 반복적으로 진동을 가하여 효율적으로 균질한 모래지반을 확보할 수 있었다. 다양한 지름과 두께를 가지는 원형관 모형체를 제작하고, 다양한 수심조건에 대하여 석션관입 실험을 수행하였다. 실험을 통한 석션압 분석결과 원형관의 관입깊이가 커짐에 따라 석션압은 커지고 지름이 클수록 원형관을 관입시키는데 필요한 석션압은 작아지는 것을 확인하였다. 특히, 수위가 낮을수록 석션관입을 위해 원형관 내부에서 끌어 올려야 하는 수두가 커지는 반면, 높아진 수두에 의한 물의 무게는 원형관의 전체 자중을 증가시켜 관입에 필요한 석션압은 작아짐을 알 수 있었다. 따라서, 저수심 조건에서 석션압을 이용하여 원형관을 설치할 경우 수심의 영향을 고려하여 설계 석션압을 결정해야 할 것으로 판단된다.

• 한국추진공학회:학술대회논문집
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• 한국추진공학회 2004년도 제22회 춘계학술대회논문집
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• pp.192-197
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• 2004

Recently, fluidic thrust vectoring methods have been preferably employed to control the movement of propulsive systems due to relatively simpler design and lower cost than mechanical thrust vectoring methods. For An application of the thrust vectoring to flight bodies, it is necessary to understand very complicated exhaust flows which are often subject to shock waves and boundary layer separation. But researches for the thrust vector control using counterflow have been few. In the present study, experiments have been performed to investigate the characteristics of supersonic jets controlled by a thrust vectoring method using counterflow. The primary jet is expanded through a two-dimensional primary nozzle shrouded by collars, and is deflected by the suction of the air near nozzle into an upper slot placed between the primary nozzle and the upper collar. A shadowgraph method is used to visualize the supersonic jet flowfields. Primary nozzle pressure ratios and suction nozzle pressure ratios are varied from 3.0 to 5.0, and from 0.2 to 1.0 respectively. The present experimental results showed that, for a given primary nozzle pressure ratio, a decrease in the suction nozzle pressure ratio produced an increased thrust vector angle. As the suction nozzle pressure ratios were increased and decreased, the hysteresis of the thrust vectoring was observed through the wall pressure distributions

• 대한기계학회:학술대회논문집
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• 대한기계학회 2003년도 추계학술대회
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• pp.592-597
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• 2003

Thrust vector control using a coflow-counterflow concept is achieved by suction and blowing through a slot adjacent to a primary jet which is shrouded by a suction collar. In the present study, the flow characteristics of thrust vectoring is investigated using a numerical method. The nozzle has a design Mach number of 2.0, and the operation pressure ratio is varied to obtain various flow features of the nozzle flow. Test conditions are in the range of the nozzle pressure ratio from 6.0 to 10.0, and a suction pressure from 90kPa to 35kPa. Two-dimensional, compressible Navier-Stokes computations are conducted with RNG ${\kappa}-{\varepsilon}$ turbulence model. The computational results provide an understanding of the detailed physics of the thrust vectoring process. It is found that an increase in the nozzle pressure ratio leads to increased thrust efficiency but reduces the thrust vector angle.