• Title/Summary/Keyword: PROPULSION SPEED

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Experimental Equipment for Torsional Vibration of Marine Propulsion Shafting (선박용 추진축계 비틀림진동 실험장치의 소개)

  • Kim, S.H.;Kim, J.G.;Lee, D.C.;Park, S.H.
    • Proceedings of the Korean Society of Marine Engineers Conference
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    • 2005.06a
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    • pp.149-153
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    • 2005
  • Marine Propulsion shafting system coupled with medium diesel engine forms multi-degree torsional vibration system which consist of many inertia masses such as crank, flywheel, propeller and sometimes gear system is adopted additionally for the purpose of improving propeller's propulsion efficiency or connecting with PTO/PTI. The periodic excitation torques generated by combustion pressure in cylinder and reciprocating masses induce various kinds of vibrations in this shafting system. If the frequency of this excitation torques is equal to the natural frequency of the shafting, the amplitude of the torsional vibration increases steeply and the damage of crankshaft or gears may be occurred by that. This frequency is called critical speed. When making a plan for shafting system, it is important for this frequency to be expected exactly and not to be in commonly used speed. For this reason, this paper introduces the experimental equipment for torsional vibration of marine propulsion shafting system and describes the theoretic and the experimental methods to look for natural frequencies.

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Numerical Analysis on the Resistance and Propulsion Performances of High-Speed Amphibious Assault Vehicles (고속 상륙돌격장갑차의 저항 및 추진 성능에 관한 수치 분석)

  • Kim, Taehyung
    • Journal of the Korea Institute of Military Science and Technology
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    • v.24 no.1
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    • pp.84-98
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    • 2021
  • The hydrodynamic characteristics of amphibious assault vehicles are investigated using commercial CFD code, STAR-CCM+. Resistance performances of a displacement-type vehicle and a semi-planing type vehicle are analyzed in calm water. The self-propelled model is also computed for the semi-planing type vehicle. All computations are performed using an overset mesh system and a RANS based flow-solver coupled with a two-degree of freedom equations of motion. A moving reference frame is applied to simulate revolutions of impeller blades for a waterjet propulsion system. Grid dependency tests are performed to evaluate discretization errors for the mesh systems. The numerical analysis results are compared with the experimental results obtained from model tests. It is shown that RANS is capable of investigating the resistance and self-propulsion characteristics of high-speed amphibious assault vehicles. It is also found that a fully covered side skirt, which is covering tracks, reduces resistance and stern trim, besides increasing propulsive efficiency.

Mechanisms of microparticle propulsion by laser ablation

  • Gojani, A.B.;Menezes, V.;Yoh, J.J.;Takayama, K.
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2008.03a
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    • pp.837-841
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    • 2008
  • Propulsion of gene coated micro-particles is desired for non-intrusive drug delivery inside biological tissue. This has been achieved by the development of a device that uses high power laser pulses. The present paper looks at the mechanisms of micro-particle acceleration. Initially, a high power laser pulse is focused onto the front side of a thin aluminium foil leading to its ablation. The ablation front drives a compression wave inside the foil, thus leading to the formation of a shock wave, which will later reflect from the rear side of the foil, due to acoustic impedance mismatch. The reflected wave will induce an opposite motion of the foil, characterized by a very high speed, of the order of several millimeters per microsecond. Micro-particles, which are deposited on the rear side of the foil, thus get accelerated and ejected as micro-projectiles and are able to penetrate several hundreds of micrometers inside tissue-like material. These processes have been observed experimentally by using high-speed shadowgraphy and considered analytically.

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Ducted Rocket Propulsion System Development Proposal (Ducted Rocket의 현황과 추진기관 개발방안)

  • Lee Jun-Ho;Choi Sung-Han;Hwang Jong-Sun
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2005.11a
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    • pp.475-478
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    • 2005
  • Ducted rocket produces thrust by 2 steps, primary incomplete combustion in the gas generator, and secondary complete combustion reaction in combustion chamber mixed by air taken through duct. the range of a rocket is determined by the weight of propellant, especially the weight of fuel. So ducted rocket has more efficiency and high terminal speed compared to traditional solid rocket motor. This propulsion system expected to be applied to various kinds of missile for anti-aircraft, anti-ship

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Wind Tunnel Test on Propellers for Middle Size Electric Propulsion UAV (중형 전기추진 무인기용 프로펠러 풍동시험)

  • Park, Poo-Min;Hwang, Oh-Sik;Kim, Young-Mun;Kim, Chun-Taek;Kwon, Ki-Jung
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2011.11a
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    • pp.784-788
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    • 2011
  • Wind tunnel test on 20" class propellers are carried out at KARI's low speed wind tunnel (LSWT). The test was done to select most efficient propeller for middle size electric propulsion UAV of KARI. The propellers are commercially available 20" class folding type propellers made of carbon fiber composite material. As the result, 21"${\times}$15.5" propeller was selected whose efficiency is 66% at cruise condition.

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Design and Analysis of Load Shedding for the Electric Propulsion System (전기추진시스템의 부하저감 설계 및 해석)

  • Kim, Kyung-Hwa;Kim, Dae-Heon;Lee, Seok-Hyun
    • The Transactions of The Korean Institute of Electrical Engineers
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    • v.64 no.7
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    • pp.971-977
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    • 2015
  • The electric propulsion system requires more reliability and safety than the conventional propulsion system because any sudden changes of electric system would bring tremendous effects on the ship's safety and propulsion. So it is very important to consider the potential transient effects. This paper discusses one of the worst electric accident. That is, one or two of generators are out of service in normal seagoing condition. And the appropriate measures are simulated in order to prevent the frequency decline that can bring the other generator's tripping. In addition, the relation between the transient effects and the major factors(inertia of generator/motors, governor's drooping characteristic and response speed) are also identified using the ETAP software.

A Study on the Coupled Forced Lateral Vibration of Multi-Supported Shafting by the Transfer Matrix Method (전달매트릭스법에 의한 다지점지지계의 연성강제감쇠 횡진동 계산에 관한 연구)

  • 이돈출;박병학;전효중
    • Journal of Advanced Marine Engineering and Technology
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    • v.14 no.2
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    • pp.35-47
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    • 1990
  • The natural frequency of lateral vibration for ship's propulsion shafting tends to become lower as the relative stiffness of supproted system of the propulsion shafting decreases and the weight of shafting increases. Especially, the propulsion shafting of high-power ships such as car ferries, roll-on/roll-off, and container ships are susceptible to lateral vibration for their resonant speeds are happened to be in ordinary operating speed ranges. So far, many papers on the lateral vibration of ship's propulsion shaftings are published but they treated mainly special cases and not explained explicitly the calculation process. In this paper, the calculation processes of undamped and also forced damped lateral vibration by the transfer matrix method are presented and the calculation programs are developed. With the developed computer programs, a ship's propulsion shafting which was introduced on the published paper is analyzed for its lateral vibration and also the lateral vibration of the main drive shaft for a lathe is calculated to show the availiability of developed computer programs.

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Overview on Hypersonic Scramjet Engine Developments (극초음속 스크램제트 엔진 개발의 개관)

  • Won Su-Hee;Jeung In-Seuck;Choi Jeong-Yeol
    • Journal of the Korean Society of Propulsion Engineers
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    • v.9 no.1
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    • pp.67-83
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    • 2005
  • The evolution of hypersonic scramjet engines was reviewed from the 1960s to the present. Concepts of hypersonic air-breathing propulsion systems based on scramjet engine, such as combined-cycle engine, were described and compared with other high-speed propulsion systems. The development history of scramjet engines over the past 40 years odd was introduced with priority given to the efforts in the United States, and the current status of scramjet technology was reviewed through the recent development programs in several developed countries.

High Speed Propulsion System Test Research Using a Shock Tunnel (충격파 터널을 이용한 고속추진기관 시험 연구)

  • Park, Gisu;Byun, Jongryul;Choi, Hojin;Jin, Yuin;Park, Chul;Hwang, Kiyoung
    • Journal of the Korean Society of Propulsion Engineers
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    • v.18 no.5
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    • pp.43-53
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    • 2014
  • Shock tunnels are known to be capable of simulating flow-field environments of supersonic and hypersonic flights. They have been operated successfully world-wide for almost half a century. As a consequence of the strong interest in hypersonic vehicles in Korea, attention has been given on this type of facility and so an intermediate-sized shock tunnel has lately been built at KAIST. In the light of this, this paper presents our tunnel performance and some of the model scramjet test data. The freestream flow used in this work replicates a supersonic combustor environment for a Mach 5.7 flight speed.

Dynamic Characteristics Analysis on the Power Factor Correction (PFC) System for Propulsion System of KTX High Speed Train (KTX 고속전철 추진제어시스템의 역률제어장치(PFC) 동작특성 분석)

  • Lee, Eul-Jae;Lee, Eun-Gyu;Yoon, Cha-Jung
    • Proceedings of the KSR Conference
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    • 2011.05a
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    • pp.82-92
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    • 2011
  • This paper presents a PFC(Power Factor Correction) system to control the power factor of input current of the converter system which is working in the propulsion system of KTX high speed train. In the KTX train system, initially introduced from ALSTOM, the thyristor converter with phase controlling technique is adopted in the current fed type powering system. The input current induces harmonic losses highly because the waveform becomes rectangular shapes according to the filter inductor current increased as the train speed increasing gradually. Especially the interference with the signalling systems is severe concerned due to high current harmonics on the catenary line. To protect this problem, a frequency trap filter(notch filter) is operating with the input converter system. In this paper, an analysis work and PC simulation have been done on the PFC system to upgrade its performance and maintenance efficiency.

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