• Title/Summary/Keyword: Thruster efficiency

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Propulsive Performance Analysis of Ducted Marine Propulsors with Rotor-Stator Interaction

  • Jang, Jin-Ho;Yu, Hye-Ran;Jung, Young-Rae;Park, Warn-Gyu
    • Journal of Ship and Ocean Technology
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    • v.8 no.1
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    • pp.31-41
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    • 2004
  • A ducted marine propulsor has been widely used for the thruster of underwater vehicles for protecting collision damage, increasing propulsive efficiency, and reducing cavitation. Since a single-stage ducted propulsor contains a set of rotor and stator inside an annular duct, the numerical analysis becomes extremely complex and computationally expensive. However, the accurate prediction of viscous flow past a ducted marine propulsor is essential for determining hydrodynamic forces and the propulsive performances. To analyze a ducted propulsor having rotor-stator Interaction, the present work has solved 3D incompressible RANS equations on the sliding multiblocked grid. The flow of a single stage turbine flow was simulated for code validation and time averaged pressure coefficients were compared with experiments. Good agreement was obtained. The hydrodynamic performance coefficients were also computed.

A Study of Aero for Hovercraft (공기부양선의 추진기 고찰)

  • Kang, Dong-Woo;Lee, In-Sun
    • Special Issue of the Society of Naval Architects of Korea
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    • 2008.09a
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    • pp.62-67
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    • 2008
  • The hovercraft is the amphibious hovercraft. Design and manufacturing companies of the aero propeller exist rarely in the world. Hence the propeller has beef designed and manufactured by manufacturing companies which make aero propeller mainly. In this paper, the hovercraft propeller of similar, which is building and designing by HHIC, is considered the type of aero propeller, rotational speed, diameter, number of blades, Open air propeller efficiency. As the result of check, hovercraft which is necessary huge static thrust is needed the ducted propeller in order to improve climbing capacity. However, the number of blades and turning direction almost do not affect.

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Development Study of Mono-Propellant Micro Propulsion Using MEMS Technology

  • Dan, Yoichiro;Kishida, Masahiro;Ikuta, Tatsuya;Takahashi, Koji
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2004.03a
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    • pp.597-600
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    • 2004
  • Fabrication technique and performance test of catalytic micro propulsion are treated based on MEMS technology. This propulsion is designed to use hydrogen peroxide as liquid mono-propellant for attitude control of pica-satellite. The propellant is fed into the micro reactor channel and decomposed into hot gas yielding controllable thrust by catalyst. In order to increase the efficiency of the reaction that depends on the contact area of propellant and catalyst, porous surface formation on the channel accompanied by platinum particle deposition has been performed using H$_2$PtCl$_{6}$ solution as a precursor. Several thrusters were fabricated in different concentration of H$_2$PtCl$_{6}$ solution to determine the best quantity of Pt particles. For the comparison of the performance of each thruster, the volume of oxygen generated by the decomposition of hydrogen peroxide and the thrust were measured.red.

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Trajectory Optimization for Autonomous Berthing of a Twin-Propeller Twin-Rudder Ship

  • Changyu Lee;Jinwhan Kim
    • Journal of Ocean Engineering and Technology
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    • v.37 no.3
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    • pp.122-128
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    • 2023
  • Autonomous berthing is a crucial technology for autonomous ships, requiring optimal trajectory planning to prevent collisions and minimize time and control efforts. This paper presents a two-phase, two-point boundary value problem (TPBVP) strategy for creating an optimal berthing trajectory for a twin-propeller, twin-rudder ship with autonomous berthing capabilities. The process is divided into two phases: the approach and the terminal. Tunnel thruster use is limited during the approach but fully employed during the terminal phase. This strategy permits concurrent optimization of the total trajectory duration, individual phase trajectories, and phase transition time. The efficacy of the proposed method is validated through two simulations. The first explores a scenario with phase transition, and the second generates a trajectory relying solely on the approach phase. The results affirm our algorithm's effectiveness in deciding transition necessity, identifying optimal transition timing, and optimizing the trajectory accordingly. The proposed two-phase TPBVP approach holds significant implications for advancements in autonomous ship navigation, enhancing safety and efficiency in berthing operations.

A study on appropriate ship power system for pulse load combine with secondary battery (펄스부하에 적합한 이차전지 연동형 선박 전력시스템에 관한 연구)

  • Oh, Jin-Seok;Lee, Hun-Seok
    • Journal of Advanced Marine Engineering and Technology
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    • v.37 no.8
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    • pp.962-968
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    • 2013
  • Problem of greenhouse gases associated with global warming and the world rise in fuel oil prices due to the depletion of fossil fuel has attracted attention. For this reason, maritime transport business, has shown interest in green-ship technology to reduce the consumption of fuel and reduce greenhouse gas for environmental protection. Power system of the ship is one of the most important factors for safe operation. Therefore, at design of ship power system, most of existing vessel used comparative large capacity generator in order to respond peak load such as bow thruster, crane and etc. In the navigation of ship, marine generators most would be operated at low load operation. In the low load operation of the generation rate of 50% or less, the operation efficiency of the generator it deteriorated, to consume more fuel oil. It also, it means that adversely effect the life of the generator. In this paper, studied how to apply for a secondary battery in container ship that relatively frequent arrival and departure in port. As a result, in order to apply the secondary battery to increase the operating efficiency of the generator during the voyage, it was confirmed that it is possible to reduce fuel consumption.

Study on the Biofouling Management of International Ships Entering South Korea (국내입항 국제운항선의 선체부착생물 관리에 대한 연구)

  • Park, JeongKyeong;Hoe, ChulHoi;Kim, HanPil;Cho, YuKyeong
    • Journal of the Korean Society of Marine Environment & Safety
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    • v.28 no.1
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    • pp.10-18
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    • 2022
  • With the increase in world trade through ships, the destruction of the marine ecosystem and socioeconomic damage due to invasive alien species (IAS) are continuously increasing. In particular, marine organisms attached on the hull surface and niche area increase the friction resistance of ships as well as the invasion of non-indigenous species, and causes a decrease in operational efficiency and an increase in GHG (Green House Gas) emissions. The International Maritime Organization (IMO) has recently begun revising guidelines for the control and management of ship's biofouling, and New Zealand and California in the United States are already regulating biofouling management under their own laws. This study investigated the management status of the submerged surface of ships and marine organisms attachments on five international ships entering South Korea, and analyzed species group and coverage (%) of biofouling communities to evaluate the LoF (Level of Fouling) rank. Macroflouling was observed on all ships surveyed, and specially, the adhesion of macro organisms in niche areas such as bow thruster, bilge keels and sea-chest gratings appeared to be at a serious level. This study proposed the management direction our country should take with regard to ship's biofouling and the improvement measures for evaluation of LoF rank and inspection methods of hull and niche ares.

Study of Knudsen Pump using Vacuum Chamber and It's Upgrade Plan to Thermal Vacuum Chamber (고고도 우주환경 모사용 진공챔버를 이용한 누센펌프의 연구와 열진공챔버로의 개선 방향)

  • Kim, Hye-Hwan;Huh, Hwan-Il
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2009.05a
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    • pp.361-364
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    • 2009
  • Vacuum facility is required for high altitude space environment test to develop small thruster to be applied for micro-satellite. After selecting vacuum equipment and integrating the chamber to simulate 100-120km attitude with max, $10^{-5}\;torr$. We tested the performance of high vacuum chamber. We designed, fabricated the knudsen pump and analyzed pressure gradient efficiency of membrane according to Knudsen number under vacuum conditions. We described the upgrade plan to a thermal vacuum chamber.

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Data Sharing Architecture for an Effective Implementation of Underwater Robot S/W Framework (효과적인 수중로봇 S/W 프레임웍 구현을 위한 데이터 공유구조)

  • Jeong, Soon-Yong;Choi, Hyun-Taek
    • Journal of the Institute of Electronics Engineers of Korea SC
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    • v.48 no.2
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    • pp.1-8
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    • 2011
  • An underwater robot S/W framework consists of various sub-modules such as sensory data processing module, thruster control module, cognition module and behavior control module. Performance of a robot is determined by not only the efficiency of algorithms used but also effectiveness of their implementations. One most important factor of the effective implementation is the efficiency of data sharing module, as it transmits signals and data between the sub-modules and thus is directly related to the cycles of sensing and control The ideal data sharing module enables immediate access to any data source irrespective of system configurations. In reality, however, there are lots of obstacles including limitation of processing capacity of source modules, delay over network, and scheduling latency of operating systems. The paper proposes a new data sharing architecture and programming models to effectively handle such obstacles in implementation of underwater S/W framework on a small scale distributed computing system.

Numerical Study on Thrust Characteristics of an E-D Nozzle for Altitude Compensation (고도 보정용 E-D 노즐의 추력 특성에 대한 수치해석 연구)

  • Hwang, Heuiseong;Huh, Hwanil
    • Journal of the Korean Society of Propulsion Engineers
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    • v.20 no.3
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    • pp.87-95
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    • 2016
  • A study on the effect of altitude-compensation and the possibility of throttling is performed by designing an E-D nozzle that is a type of altitude-compensation nozzles. In order to examine the effect of the altitude-compensation, a CFD analysis is conducted by using three kinds (sea level, altitude at 10 km and 16 km) of the atmosphere condition while maintaining the chamber pressure. Results show that the effective nozzle exit area is also gradually increased when the altitude get increased. Understanding the possibility of throttling, a CFD analysis is conducted by moving the location of the pintle. Just as same as a general pintle thruster, the chamber pressure and thrust are increased when the nozzle throat area get decreased.

Development of Sub-200 W Laboratory Model Hall Thrusters for Small and Micro Satellites (소형 및 초소형위성 활용을 위한 200 W 이하 저전력 홀 전기추력기 랩모델 연구개발)

  • Lee, Dongho;Kim, Holak;Doh, Guentae;Kim, Youngho;Park, Jaehong;Lee, Jaejun;Choe, Wonho
    • Journal of the Korean Society of Propulsion Engineers
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    • v.26 no.2
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    • pp.40-46
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    • 2022
  • Hall thrusters are one of the electric propulsion, where ions are accelerated to generate thrust and are widely utilized in space missions due to their high specific impulses. Recently, as the utilization of small and micro satellites with the mass of similar or less than 100 kg is highly increasing, the importance of research and development of the low-power electric propulsion is also raised. In this study, we developed two sub-200 W or less class, laboratory model Hall thrusters and measured the thrust and analyzed the discharge characteristics. Consequently, we obtained 2.5-9.0 mN of thrust, 600-1,150 s of specific impulse, and 15-28% of anode efficiency at 50-175 W of anode power.