• Title/Summary/Keyword: Engine Supply System

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Experimental Study of Tribological Properties According to Oil Grade (오일 등급에 따른 트라이볼로지 특성의 관한 실험적 고찰)

  • Lee, Jong-Ho;Seo, Kuk-Jin;Hwang, Youn-Hoo;Han, Jae-Ho;Kim, Dae-Eun
    • Tribology and Lubricants
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    • v.37 no.6
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    • pp.246-252
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    • 2021
  • Among the engine components of an internal combustion engine, the valve train is a series of systems that supply intake gas to the combustion chamber and operate intake and exhaust valves that discharge exhaust gas. If excessive wear occurs in the valve train system, the suction and exhaust valves do not open and close on time, which leads to abnormal combustion and exhaust gas. In this study, we conduct experiments and analyses on friction and wear characteristics of the valve train system. Moreover, we experimentally study the correlation between the pinball and pinball cap on engine oil lubrication, friction experiment, wear amount analysis, and surface analysis. Specifically, we experiment using Ball on reciprocating tribo-tester and apply commercial engine oil sold on the market engine oil. We construct the experimental conditions for each new oil and oil. Accordingly, the completed specimen was subjected to a confocal microscope to check the wear volume, observe the surface of the specimen, and confirm the elemental components using a scanning microscope (SEM) and an energy dispersion X-ray spectrometer (EDS). Through this experiment, we analyze the friction and wear characteristics of valve train components according to engine oil grade, and the obtained data serve as an effective engine oil management method.

A Performance Analysis of 60 Horsepower Vertical Mounted Gasoline Engine Applied to Multi-copter of Unmanned Aircraft Vehicle (무인 멀티콥터에 적용된 60마력급 직립형 가솔린 엔진의 성능 분석)

  • RYUNKYUNG KIM;KYUNGWAN KO;SUNGGI KWON;GYECHOON PARK
    • Transactions of the Korean hydrogen and new energy society
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    • v.34 no.6
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    • pp.758-766
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    • 2023
  • Multi-copter of unmanned aerial vehicle (UAV) was initially developed as strategic technology in the only military field, but it is developing into an industrial field with a wide range of applications in the civil sector based on the development and convergence of aviation technology and information and communication technology. Currently, the degree of utilization of multi-copter is increasing in various industries for the purpose of performing classic tactical missions, logistics transportation, farm management, internet supply, video filming, weather management, life-saving, etc, and active technology development responding to market demand. Existing commercial multi-copter mainly use an electric energy propulsion system consisting of an electric battery and a brushless direct current (BLDC) motor. It is the limitations for usage in the flying time (up to 20 minutes) and payload (less than 20 kg). this study aims to overcome these limitations and expand the commercialization of engine-powered multi-copter of UAV in various industries in the futures.

Experimental Research on the Performance of Air Turbine Starter for Gas Turbine Engines (가스터빈 엔진용 공기터빈 시동기 성능에 관한 실험적 연구)

  • Kim, Chun-Taek;Yang, In-Young;Cha, Bong-Jun
    • The KSFM Journal of Fluid Machinery
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    • v.15 no.4
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    • pp.27-32
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    • 2012
  • Gas turbines for an aircraft have the start and restart capabilities within their flight envelop. It is an important item for engine qualification and substantiated with the test. Experimental investigations were carried out to find the relation between the corrected torque and the corrected rotating speed of an air turbine starter in this study. A dedicated air supply system for the air turbine starter and a special device to measure the torque and the rotating speed of the air turbine starter were developed and installed at the altitude engine test facility in Korea Aerospace Research Institute. Experimental results show that the relations between the corrected torque and the corrected rotating speed of the air turbine starter are linear and the inlet temperature and pressure conditions for the air turbine starter were found out to provide minimum required torque for the engine qualification test at various altitude. The start and restart tests for the currently developing engine were successfully performed using this experimental results.

Effects of Hydrogen-enriched LPG Fuelled Engine on Exhaust Emission and Thermal Efficiency [II] (LPG엔진에서 수소첨가가 배기 성능과 열효율에 미치는 영향 [II])

  • Kwon, T.Y.;Kim, J.H.;Choi, G.H.;Chung, Y.J.
    • Transactions of the Korean hydrogen and new energy society
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    • v.13 no.4
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    • pp.297-303
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    • 2002
  • The purpose of study is obtaining low-emission and high-efficiency in LPi engine with hydrogen enrichment. The test engine was named variable compression ratio single cylinder engine (VACRE). The fuel supply system provides LPG/hydrogen mixtures based on same heating value. A varied sensors such as crank shaft position sensor (CPS) and hall sensor supplies spark timing data to ignition controller. Displacement of VACRE is $1858.2cm^3$. VACRE was runned 1400rpm with compression ratio 8. Spark timing was set MBT without knocking. Relative air-fuel ratio($\lambda$) of this work was varied between 0,8 and 1.5.

Automobile Engine Diagnostic System by Current Monitoring to Self Motor (시동모터 전류 관찰에 의한 자동차엔진 압축압력 검사장치)

  • Hyun, Woong-Keun
    • The Journal of the Korea institute of electronic communication sciences
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    • v.12 no.1
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    • pp.93-100
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    • 2017
  • Four-stroke cycles in an automobile engine are suction stroke, compression stroke, combustion stroke and exhaustion stroke. A normal operation of engine in compression and power stroke must be processed in optimal fuel-air pressure. In this paper we describe a development of measuring equipment for engine cylinder pressure with observing supply current to self motor(start motor). By comparing the current wave on pressure of the 4 or 6 cylinder in engine, a abnormal cylinder state will be found. The validity of the proposed measuring equipment was shown by experiment for real automobile.

Risk Assessment of Marine LPG Engine Using Fuzzy Multicriteria HAZOP Technique (퍼지 다기준 HAZOP 기법을 이용한 해상용 LPG 엔진의 위험성 평가)

  • Siljung Yeo
    • Journal of the Korean Society of Marine Environment & Safety
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    • v.29 no.2
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    • pp.238-247
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    • 2023
  • Liquefied petroleum gas (LPG) is an attractive fuel for ships considering its current technology and economic viability. However, safety guidelines for LPG-fueled ships are still under development, and there have been no cases of applying LPG propulsion systems to small and medium-sized ships in Korea. The purpose of this study was to perform an objective risk assessment for the first marine LPG engine system and propose safe operational standards. First, hazard and operability (HAZOP) analysis was used to divide the engine system into five nodes, and 58 hazards were identified. To compensate for the subjectivity of qualitative evaluation using HAZOP analysis, fuzzy set theory was used, and additional risk factors, such as detectability and sensitivity, were included to compare the relative weights of the risk factors using a fuzzy analytical hierarchy process. As a result, among the five risk factors, those with a major impact on risk were determined to be the frequency and severity. Finally, the fuzzy technique for order of preference by similarity to ideal solution (TOPSIS) was applied to select the risk rank more precisely by considering the weights of the risk factors. The risk level was divided into 47 groups, and the major hazard during the operation of the engine system was found through the analysis to be gas leakage during maintenance of the LPG supply line. The technique proposed can be applied to various facilities, such as LPG supply systems, and can be utilized as a standard procedure for risk assessment in developing safety standards for LPG-powered ships.

Gas Leakage Condition and CFD analysis on Gas Fuelled ship FGS system (Gas Fuelled Ship FGS 시스템에 대한 가스누출 조건 검토 및 CFD 해석)

  • Kim, Ki-Pyoung;Kang, Ho-Keun;Park, Jae-Hong;Choung, Choung-Ho
    • Proceedings of the Korean Society of Marine Engineers Conference
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    • 2011.06a
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    • pp.7-10
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    • 2011
  • According to the requirement of Res.MSC.285(86) for natural gas-fueled engine installations in ships, pump and compressor rooms should be fitted with effective mechanical ventilation system of the under pressure type, providing a ventilation capacity of at least 30 air changes per hour. It generally considered that gas leakage is more likely from a Fueled Gas Supply System(FGS) room as compared to other places, where installed in many kind of machinery or equipments like gas supply high-pressure pipes, valves, flanges and etc. Furthermore, leaked gas may be dispersed in a short time in an enclosed space, especially a FGS room, due to high pressure. However, the present requirement in Res.MSC.285(86) just considers the ventilating capacity of air changes per hour but the capacity of leaked gas. Hence, the current requirements may not meet effectively when enforcing the new propulsion systems as marine fuel. This study is conducted for the purpose of safety evaluation about the dispersion and ventilation efficiency with estimated leakage scenario. Numerical analysis predictions as the result of this paper are explained to know the features of flow pattern and the diffusion of natural gas concentration.

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Introduction of Thrust Vector Control System and Control Valve Development for Space Launch Vehicles (우주발사체용 추력벡터제어 시스템 및 제어밸브류 개발 현황 소개)

  • Lee, Je-Dong;Park, Bong-Kyo;Park, Ho-Youl;Kim, Sang-Beom;Jun, Pil-Sun;Jang, Ki-Won
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2009.11a
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    • pp.613-615
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    • 2009
  • This paper is to introduce Hanwha Aerospace R&D Center's development status of TVC(Thrust Vector Control) system and control valves for Korean space launch vehicles. With the successful development of KSR-III TVC system, Hanwha have developed TVC system and RCS control valves for KSLV-I. Also, in the advance research area of KSLV-II, Hanwha have participated in LOx and fuel flow control valves and LOx shut-off valve development in the engine supply system. Based on the accumulated experiences and technologies in the aerospace key components and system development, Hanwha will make an important contribution to KSLV-II development in the future.

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Improvement of Broadband Radiated Emission Noise in Military Tactical Vehicle by Using Additional Alternator in Engine (엔진 발전기 추가 적용을 통한 군(軍) 지휘·지원차량의 광대역 전자파 방사 노이즈 개선)

  • Seo, Suk Ho;Ku, Ki Beom;Kim, Ji Hoon;Oh, Dae San
    • Journal of the Korea Academia-Industrial cooperation Society
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    • v.21 no.9
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    • pp.397-404
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    • 2020
  • The military tactical vehicle currently being operated is manufactured by improving the parts of commercial vehicles. In addition, the power supply system is applied by installing a separate converter inside the communication room to secure the operating environment of communication equipment. On the other hand, due to electromagnetic radiation noise, there are problems in frequent noise and deterioration in communication sensitivity during wireless communication in vehicles. To improve these, an advanced power supply system is applied, which is also equipped with an alternator to receive power required for communication equipment reducing broadband electromagnetic radiation noise. An additionally installed alternator, which is located in the engine room, is separated from the communication room where communication equipment is operated and is expected to reduce the effect of electromagnetic radiation noise generated from the power supply system. To verify these, a broadband radiation test was performed on a previous and advanced one. As a result, the broadband radiation noise of vehicles with an applied advanced power supply system satisfied all of the domestic vehicle safety standards and reduced in most of the sections except for some frequencies compared to previous typed vehicles. In particular, broadband radiation noise was decreased by up to 10.751 dB𝜇V/m in the vertical sections in 170 to 200 MHz on the right side of the vehicle.

Dynamic Performance of Natural Gas Injection Valve for Heavy-Duty CNG Dual Fuel Engine (대형 CNG 혼소 엔진용 천연가스 분사밸브 동특성 연구)

  • Kim, Yong-Rae;Choi, Young
    • Journal of the Korean Institute of Gas
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    • v.21 no.5
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    • pp.9-15
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    • 2017
  • Natural gas fuel has known to be very promising in terms of abundancy and economic value. Therefore it is widely treated as research topics in a variety field of production, storage and utilization. Natural gas has become one of the major sources for the power generation by using internal combustion engines(ICE). Development of natural gas fuel injection device should be preceded to realize a reliable natural gas fuel supply system for a MW class power generation reciprocating ICE. In this research, an injection valve which consists of solenoid and body part with a moving plate was designed and its dynamic performance was experimented in the engine-like environment. Displacement length and diameter of an armature and diameter of a solenoid coil were tested at former study. In this research the effect of materials of solenoid core, size of main housing inlet and supply gas pressure are examined.