• Title/Summary/Keyword: Waterjet

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Study on Performance Evaluation of Subsea Waterjet Trenching Machine Using Water Tank (수조실험을 통한 해저지반 굴삭용 워터젯 장비의 성능평가에 관한 연구)

  • Na, Kyoung-Won;Jo, Hyo-Jae;Baek, Dong-Il;Hwan, Jae-Hyuk;Han, Sung-Hoon;Jang, Min-Suk;Kim, Jae-Heui
    • Journal of Ocean Engineering and Technology
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    • v.29 no.6
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    • pp.470-474
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    • 2015
  • The demand for subsea cables and pipelines that transfer marine energy resources onshore has recently increased. Laying these underground after trenching is one engineering method to stabilize exposed subsea cables and pipelines. This experimental study found the optimum conditions for operating two types of waterjet arms mounted on an ROV trencher. A waterjet arm for trenching the seabed was scaled down at a ratio of 1:6, and a comparative analysis was conducted using diverse parameters. The results of this research provide a practical fundamental database to assist in making decisions about the ROV trencher performance in advance.

Effects of Operating Parameters on Tetrafluoromethane Destruction by a Waterjet Gliding Arc Plasma (워터젯 글라이딩 아크 플라즈마에 의한 사불화탄소 제거에 미치는 운전변수의 영향)

  • Lee, Chae Hong;Chun, Young Nam
    • Applied Chemistry for Engineering
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    • v.22 no.1
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    • pp.31-36
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    • 2011
  • Tetrafluoromethane ($CF_4$) has been used as the plasma etching and chemical vapor deposition (CVD) gas for semiconductor manufacturing processes. However, the gas need to be removed efficiently because of their strong absorption of infrared radiation and the long atmospheric lifetime which cause global warming effects. A waterjet gliding arc plasma system in which plasma is combined with the waterjet was developed to effectively produce OH radicals, resulting in efficient destruction of $CF_4$ gas. Design factors such as electrode shape, electrode angle, gas nozzle diameter, electrode gap, and electrode length were investigated. The highest $CF_4$ destruction of 93.4% was achieved at Arc 1 electrode shape, $20^{\circ}$ electrode angle, 3 mm gas nozzle diameter, 3 mm electrode gap and 120 mm electrode length.

Numerical Internal Flow Analysis of Intake Duct of Waterjet Propulsion (워터제트 추진기 유입관의 내부유동 전산해석)

  • Yun, Hyun-Suk;Park, Warn-Gyu;Chun, Ho-Hwan;Kim, Moon-Chan
    • Journal of the Society of Naval Architects of Korea
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    • v.42 no.1 s.139
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    • pp.1-9
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    • 2005
  • Waterjet propulsion is widely used to thrust high speed marine vessels in excess of 30-35 knots by virtue of the high propulsive efficiency, good maneuverability, and less cavitation. From the aspect of power loss, approximately $7-9\%$ of the total power is lost in intake duct due to the flow separation, nonuniformity, etc. Thus, detail understanding of flow phenomena occurring within intake duct is essential to reduce the power loss, as well as noise and vibration. The present work solved 30 incompressible RANS equations to provide complicated viscous flow features of intake duct. The numerical results were compared with experiments and good agreements were obtained for three jet velocity ratios.

Evaluation of Maneuverability in Still Water of an Unmanned Surface Vehicle through Sea Trials (실선 시운전을 통한 무인수상정 정수중 조종성능 평가)

  • Jeon, Myung-Jun;Yoon, Hyeon-Kyu;Ryu, Jea-Kwan;Lee, Won-Hee;Ku, Pyung-Mo
    • Journal of the Society of Naval Architects of Korea
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    • v.58 no.4
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    • pp.253-261
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    • 2021
  • This paper describes the process of evaluating maneuverability in still water of an unmanned surface vehicle based on data measured by performing sea trials. First, we set up a test scenario that is easy to analyze the maneuverability of the unmanned surface vehicle and to identify and verify the dynamics model. Since the attitude of hull varies according to the speed of the unmanned surface vehicle which has a planing hull shape, the relationship between waterjet RPM, speed and attitude is analyzed by performing straight forward tests at various speeds. The turning tests of the unmanned surface vehicle in which the waterjet angle rotates while turning are performed by changing the waterjet rotation angle under the condition of two representative speeds to analyze turning ability. The turning ability of the unmanned surface vehicle includes speed reduction, yaw rate, heel, and turing diameter at steady turning phase according to the speed and RPM.

Variation of abrasive feed rate with abrasive injection waterjet system process parameters (연마재 투입형 워터젯 시스템의 공정 변수에 따른 연마재 투입량 변화)

  • Joo, Gun-Wook;Oh, Tae-Min;Kim, Hak-Sung;Cho, Gye-Chun
    • Journal of Korean Tunnelling and Underground Space Association
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    • v.17 no.2
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    • pp.141-151
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    • 2015
  • A new rock excavation method using an abrasive injection waterjet system has been developed to enhance the efficiency and reduce the vibration of tunnel excavation. The abrasive feed rate is an important factor for the cutting performance and the economical efficiency of waterjet-based excavation. In this study, various experiments were performed to explore the effects of major process parameters for both the abrasive feed rate and the suction pressure occurring inside the mixing chamber when the abrasives are inhaled. Experimental results reveal that the abrasive feed rate is affected by geometry parameters (abrasive pipe height, length, and tortuosity), abrasive parameters (abrasive particle size), and jet energy parameters (water pressure and water flow rate). In addition, the relation between the cutting performance and the abrasive feed rate was discussed on the basis of the results of an experimental study. The cutting performance can be maximized when the abrasive feed rate is controlled appropriately via careful management of major process parameters.

Prediction of Performance of Waterjet Propulsors by Surface Panel Method (패널법에 의한 물 분사 추진장치의 성능해석)

  • Moon, II-Sung;Lee, Chang-Sup;Song, In-Haeng;Kim, Ki-Sup
    • Journal of the Society of Naval Architects of Korea
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    • v.34 no.4
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    • pp.31-41
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    • 1997
  • This paper describes a potential-based panel method formulated for the prediction of the steady performance of a waterjet propulsor. The method employs normal dipoles and sources distributed on the solid surfaces such as the impeller/stator blades, hub and duct, and normal dipoles in the shed wakes trailing the impeller and stator to represent the potential flow around the waterjet propulsor. To define a closed boundary surface, the inlet and outlet open boundary surfaces are introduced where the sources and dipoles are distributed. The kinematic boundary condition on the solid boundary surface is satisfied by requiring that the normal component of the total velocity should vanish. On the inlet surface, the total inflow flux into the duct is specified, and on the outlet surface the conservation of mass principle is applied to evaluate the source strength. The solid surfaces are discretized into a set of quadrilateral panel elements and the strengths of sources and dipoles are assumed constant at each panel. Applying this approximation to the boundary conditions leads to a set of simultaneous equations. Systematic numerical tests show that the present numerical method is fast and stable. In order to validate the present method, sample computations are carried out first for the case of a conventional axial flow fan which has a similar geometry as the waterjet propulsor, and then for the case of a waterjet propulsor on which experiments are carried out at KRISO(Korea Research Institute of Ships and Ocean Engineering).

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A Study on the Configuration of Two-Dimensional Waterjet Inlet (이차원 물분사 추진장치 입구면 형상에 관한 연구)

  • J.M. Lew;S.K. Hong;Y.G. Kim
    • Journal of the Society of Naval Architects of Korea
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    • v.36 no.2
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    • pp.9-21
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    • 1999
  • The waterjet is very widely used today in propulsion system of high speed vessel but manufacturer is limited because of an efficiency and a difficulty of a manufacture on the inlet configuration of the waterjet. The importancy in designing the inlet configuration of the waterjet lies on the minimization of the cavitation which is largely affecting the efficiency. In this paper, the configuration analysis is carried out to find a optimum shape which is minimizing the cavitation using a two dimensional potential-based panel method with an inlet configuration of a flush type. Also, it is developed a direct design method finding an inlet configuration by a given pressure distributions. The numerically obtained optimum shape using this configuration analysis method show a good agreement compared to the Kashiwadani's results. It is carried out a direct design method over a lip and a ramp of an inlet configuration wish pressure distributions obtained a result of the configuration analysis and the results show a good agreement compared to original configuration.

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A Fundamental Study to Estimate Construction Performance of Subsea Waterjet Trenching Machine (해저지반 굴삭용 워터젯 장비의 시공성능 추정에 관한 기초적 연구)

  • Na, Kyoung-Won;Beak, Dong-Il;Hwang, Jae-Hyuk;Han, Sung-Hoon;Jang, Min-Suk;Kim, Jae-Heui;Jo, Hyo-Jae
    • Journal of Navigation and Port Research
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    • v.39 no.6
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    • pp.539-544
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    • 2015
  • There is drift toward moving offshore structures operating sites to deep water that brings subsea systems and types of apparatus to meet more severe environment than onshore. At this moment, climatic condition and seabed state affect trenching efficiency so trenching process is need to make steady progress in a short time. This paper is research on estimation about construction performance of waterjet trenching machine mounted on ROV trencher. Optimal number of nozzles that can maximize trenching efficiency is selected by considering clearance and angle of nozzles through CFD. Then verified effectiveness of waterjet apparatus on the result of trenching depth and velocity by model test analogized performance for construction work of waterjet trenching machine.

Analysis of drilling performance and shape for granite according to operating parameters of waterjet nozzles (복수의 워터젯 노즐 운용변수에 따른 화강암 천공성능 및 형상 분석)

  • Park, Jun-Sik;Cha, Hyun-Jong;Hong, Eun-Soo;Jun, Hyung-Woo;Oh, Tae-Min
    • Journal of Korean Tunnelling and Underground Space Association
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    • v.23 no.6
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    • pp.589-604
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    • 2021
  • Waterjets for rocks have various advantages of the non-contact and eco-friendly excavation using only water and abrasive. To overcome the problems (e.g., dust and noise occurrence) of the conventional drilling methods, waterjet excavation methods are broadly used. It is advantageous to operate a couple of nozzles in order to increase the waterjet excavation efficiency. When multiple nozzles are used, it is essential to analyze the excavation performance and shape according to the nozzle operation method. In this study, nozzle angle, horizontal distance between nozzles, and standoff distance were defined as nozzle operating parameters and the excavation performance and shape were analyzed. As a result of the experiment, when the nozzle angle and standoff distance are increased, the excavation depth is decreased and the effective depth tends to be increased. In addition, based on the experimental results, the excavation shape criteria required for nozzle insertion were proposed and optimal nozzle operating parameters were derived according to the criteria. This study result is expected to be used as useful basic research in the future development of multiple waterjet nozzles for rock drilling.