• Title/Summary/Keyword: 연료 소모량

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An economic ship routing system based on a weather forecasting and a sailing cost prediction (기상예보와 운항비용예측 기반의 선박경제운항시스템)

  • Jang, Ho-Seop;Kwon, Yung-Keun
    • Proceedings of the Korea Information Processing Society Conference
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    • 2011.04a
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    • pp.1064-1067
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    • 2011
  • 선박경제운항이란 파도와 바람과 같은 해양 기상정보 예측을 바탕으로 선박의 운항방법에 따른 연료 소모량과 운항시간을 예상해보고, 가장 경제적인 운항을 하는 것을 말한다. 본 논문에서는 실용화할 수 있는 범용의 경제운항시스템 개발에 중점을 두었다. 기존의 시스템들을 살펴보면 임의의 정해진 경로를 대상으로 실험하는 경우가 많은데, 이를 개선하여 임의의 출발점과 도착점이 주어지면 A*알고리즘을 통해서 지리상 최단경로를 찾아내도록 하여 시스템을 자동화하였으며 적용범위를 세계 전역으로 확대 하였다. 그리고 기존의 엔진출력을 고정하거나 속력을 일정하게 운항한다는 가정에서 벗어나서 엔진출력을 탐색하여 보다 효율적인 운항 솔루션을 찾아내도록 하였다. 그리고 사용측면에서는 운항사들에게 보다 효용성 높은 시스템이 되기 위해서, 일방적인 권고보다는 연료소모량과 운항시간 별로 다양한 솔루션들을 제공하여 운항사의 판단을 존중함과 동시에 운항보조시스템으로서의 역할에 충실할 수 있도록 하였다.

The Reduction Rate of $CO_2$ with Fuel-cut Region Painting on the Road (퓨얼컷 구간 도로표시에 따른 $CO_2$ 배출 저감율)

  • Ko, Kwang-Ho;Yoo, In-Kyoon;Lee, Soo-Hyung;Kim, Je-Won
    • 한국방재학회:학술대회논문집
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    • 2010.02a
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    • pp.45.2-45.2
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    • 2010
  • 자동차 주행 시 엔진회전수가 1,500rpm 이상이고 주행속도가 50km/hr 이상의 조건에서 가속 페달을 밟지 않은 상태로 관성주행(타행주행)을 하면 연료분사량이 "0"이 되고 그에 따라 엔진 배출 $CO_2$ 배출량도 "0"이 된다. 본 연구에서는 고속도로 및 자동차 전용도로에서의 이러한 연료차단(퓨얼컷 fuel-cut) 주행 구간을 찾고 연료차단 기능을 활용하는 경우 그 효과를 평가하였다. 본 시험의 결과 퓨얼컷 주행을 활용하면 약 4~5% 정도의 $CO_2$ 배출량을 줄일 수 있음을 알 수 있었고, 감속의 정도를 도로 상황에 맞게 최적화하는 경우 감소율을 더욱 향상시킬 수 있을 것으로 판단된다. 추후 본 시험의 결과를 이용하여 도로 내리막 구간에서 연료소모량 및 $CO_2$ 배출량을 저감하면서도 과속으로 인한 사고를 예방하는 방안으로 활용할 수 있을 것으로 판단된다.

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Study on Power Distribution Algorithm in terms of Fuel Equivalent (등가 연료 관점에서의 동력 분배 알고리즘에 대한 연구)

  • Kim, Gyoungeun;Kim, Byeongwoo
    • Asia-pacific Journal of Multimedia Services Convergent with Art, Humanities, and Sociology
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    • v.5 no.6
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    • pp.583-591
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    • 2015
  • In order to evaluate the performance of TAS applied to the hybrid vehicle of the soft belt driven, acceleration performance and fuel consumption performance is to be superior to the existing vehicle. The key components of belt driven TAS(Torque Assist System), such as the engine, the motor and the battery, The key components of the driven belt TAS, such as the engine, the motor, and the battery, have a significant impact on fuel consumption performance of the vehicle. Therefore, in order to improve the efficiency at the point of view based on the overall system, the study of the power distribution algorithm for controlling the main source powers is necessary. In this paper, we propose the power distribution algorithm, applied the homogeneous analysis method in terms of fuel equivalent, for minimizing the fuel consumption. We have confirmed that the proposed algorithm is contribute to improving the fuel consumption performance satisfied the constraints considering the vehicle status information and the required power through the control parameters to minimize the fuel consumption of the engine. The optimization process of the proposed driving strategy can reduce the trial and error in the research and development process and monitor the characteristics of the control parameter quickly and accurately. Therefore, it can be utilized as a way to derive the operational strategy to minimize the fuel consumption.

A study on the greenhouse gas emission from ships with training ship HANBADA (실습선 한바다호를 이용한 선박부문 온실가스 배출량 산정에 관한 연구)

  • Lee, Sang Deuk;Koh, Dae Kwon;Jung, Suk Ho
    • Journal of Advanced Marine Engineering and Technology
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    • v.38 no.3
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    • pp.240-245
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    • 2014
  • As the seriousness of the global environment pollution is gaining our attention recently, researches on application of greenhouse gas emission of ship are being carried globally. However domestic study on greenhouse gas emission from ship was not carried out in various fields. In this study, quantitative data which was presented by greenhouse gas emission of training ship HANBADA and greenhouse gas emission was calculated by Tier 1 method based on total fuel consumption and amount of shore power. Actual voyage data for 1year in 2012 was used to analysis the greenhouse gas emission. This study showed how many weight of gases were exhausted per 1 gross tonnage and per 1trainee in the training ship. There is a need of further research to reduce pollutant and to respond to international environment regulation consistently.

A Study on the Fuel Saving Method through the Analysis of Fuel Consumption on Domestic Flight - Based on the Fuel Consumption of B737 Aircraft - (국내선 항공기 연료소모량 분석을 통한 연료절감 방안연구 - B737 항공기 연료소모량을 중심으로 -)

  • Choi, Jihun;Lee, Kyung-Han;Kim, Yong-og;Kim, Woong-Yi
    • Journal of the Korean Society for Aviation and Aeronautics
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    • v.30 no.2
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    • pp.24-33
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    • 2022
  • This study analyzed and derived a plan to reduce fuel consumption of domestic aircraft. Specifically, this study tested fuel consumption in the short-distance flights of B737. Fuel consumption was calculated by substituting the simulation variable values into Matlab. The strength of this study is that the actual operating environment was reflected by collecting the B737 flight data. As a result of the study, the domestic fuel consumption rate in the computed flight plan was less than the current fuel consumption rate. Existing limitations of this study is that it was difficult to reflect the various variables constituting the flight environment, and thus there can be errors in the measurement of the fuel consumption. There are two major expected applications from this study. First, applying the plans from this study will lead to a reduction in the amount of fuel and thus provide positive economic effects for commercial airlines. Second, the plan from this study will provide a basis for pilots to predict fuel consumption more accurately. In conclusion, this study proposes a fuel saving plan with useful applications for pilots and airlines.

A Case Study of Aircraft Taxi Fuel Consumption Prediction Model (A380 Case) (항공기 지상 활주 연료소모량 예측모델 사례연구 (A380 중심))

  • Jang, Sungwoo;Lee, Youngjae;Yoo, Kwang Eui
    • Journal of the Korean Society for Aviation and Aeronautics
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    • v.28 no.2
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    • pp.29-35
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    • 2020
  • In this paper, we established a prediction model of fuel consumption at the aircraft's taxi operation. To look for countermeasures to reduce fuel consumption and carbon emissions, Airbus A380's actual ground taxi data was used. As a result, the number of stops or turnings during the taxi operation was not related to fuel consumption. It was confirmed that the amount of fuel consumption in the taxi operation was the taxi time and the thrust change. It can be confirmed that ground control optimization, which is the result of close cooperation between the control organization and the airline, is absolutely necessary to reduce taxi time and minimize the occurrence of thrust change events.

Effect of Passenger Car Fuel Consumptions and Fuel Cost Savings by Hi-Pass System (하이패스 이용시 승용차 연료소모 및 연료비용 절감효과)

  • Kwak, Jin-Ho;Kim, Dong-Nyong;Jeong, Ae-Ra
    • The Journal of The Korea Institute of Intelligent Transport Systems
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    • v.14 no.1
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    • pp.94-102
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    • 2015
  • The high-pass(brand name of Electronic Toll Collection System) utilization trend on the highway continues to grow as 59.4% (by the end of 2013). In this study, we applied the carbon balance method using a fuel chassis dynamometer with the four passenger car classes in order to measure the fuel consumption of the car using the expressway tollgate. We experimented 18 driving mode at general tollgate and high-pass tollgate. As a result, in case of entry/exit toll there were 21.0~56.4ml/veh fuel consumption savings, in case of open toll fuel consumption savings was analyzed as 10.5~28.1ml/veh. In addition, the annual fuel cost savings by virtue of high-pass was 28.2~57.3 billion won at 70% utilization rate, 32.2~65.5 billion won at 80%, 36.2~73.7 billion won at 90% and 40.3~81.9 billion won at 100%.

Weak Stability Boundary를 이용한 지구-달 천이궤적 연구

  • Gang, Sang-Uk;Choe, Gi-Hyeok;Sim, Eun-Seop
    • The Bulletin of The Korean Astronomical Society
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    • v.37 no.2
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    • pp.162.2-162.2
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    • 2012
  • 한국형 발사체 KSLV-2의 발사능력을 고려하면 달 탐사선의 총 무게는 약 550kg이 된다. 따라서 달 탐사선에 탑재할 수 있는 탑재체 무게를 최대화하기 위해서는 지구에서 달로 가는 천이궤적을 가장 효율적으로 설계하여 연료 소모량을 최소화하여야 한다. 본 연구에서는 최근에 달 탐사 천이궤적으로 가장 많이 사용되고 있는 Weak Stability Boundary 천이궤적에 관해 연구를 수행하였다. Weak Stability Boundary 천이궤적은 지구로부터 출발한 후 원지점 약 1.4 km(지구-태양의 L1 점 근처)까지 비행한 후 태양풍을 통해 에너지를 얻어 근지점 거리를 지구-달 거리만큼 증가시켜 LOI(Lunar Orbit Injection)시 ${\Delta}V$를 최소화하여 달 궤도에 들어가는 방법이다. Weak Stability Boundary 천이방법의 TLI(Trans Lunar Injection) 값은 직접천이 방법의 TLI 값보다 더 크지만 달 궤도 진입에 필요한 LOI ${\Delta}V$값은 25% 정도 덜 든다는 장점이 있다. 이 방법은 일본의 Hiten 탐사선이 최초로 사용하였으며, 달에 도착하기까지 수개월이 걸리는 단점이 있다. Weak Stability Boundary 천이궤적 시뮬레이션을 통해 최대로 절약할 수 있는 연료 소모량을 확인할 수 있었으며, 다른 천이방법들과의 장단점 비교를 통해 한국형 달 탐사선의 지구-달 천이궤적 후보로 사용 될 수 있음을 확인하였다.

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A Study on the Performance Comparison of Energy Saving Devices for Handy-size Bulk Carrier (산적화물선의 에너지 저감 장치들의 성능 비교에 관한 연구)

  • Kim, Eok-Kyu;Lee, Kang-Ki;Cho, Kwon-Hae
    • Journal of Advanced Marine Engineering and Technology
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    • v.39 no.1
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    • pp.1-7
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    • 2015
  • The environmental regulations for CO2 emissions from the ship have been established recently, and fuel oil price has been increased continuously. In order to overcome these circumstances, Energy Saving Devices (ESDs) have been developed continuously to reduce the fuel oil consumption and improve the propulsive efficiency. This paper describes the trial performance of PBCF (Propeller Boss Cap Fins), SCHNEEKLUTH duct, Asymmetric rudder bulb and Mewis duct applied to handy-size bulk carriers. As a result, SCHNEEKLUTH duct is more effective than other energy saving devices at the reducing the fuel oil consumption and the improvement of the propulsive efficiency. In addition, it is confirmed that SCHNEEKLUTH duct is really effective in the vibration of the deck house. And the fuel oil consumption can also be reduced through main engine de-rating.