• Title/Summary/Keyword: Aviation Fuel

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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.

A Case Study on Fuel Supply and Cooling Systems of High-Speed Vehicles (고속 비행체 연료공급 및 냉각계통 사례분석)

  • Choi, Seyoung;Park, Sooyong;Choi, Hyunkyung;Jun, Pilsun;Park, Jeongbae
    • Journal of the Korean Society for Aviation and Aeronautics
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    • v.21 no.2
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    • pp.1-6
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    • 2013
  • In high-speed vehicle, selection of fuel, configuration of components and cooling system are required to solve the heating issue by aerodynamic heating and inner combustion process. This subsystem consists of fuel tank, supply pump, various control valve, heat exchanger, including reactor, connecting line, adiabatic structures and insulations. In this paper, applicable fuel property is considered at flight characteristic of hypersonic vehicles. In this regard, current state of fuel/cooling system technology is identified.

The Status of Production and Usage of Bio-Jet Fuel (바이오항공유 생산 및 사용현황)

  • Young-Kwan, Lim;Jin-Woo Doe
    • Applied Chemistry for Engineering
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    • v.34 no.5
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    • pp.472-478
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    • 2023
  • The usage of jet fuel has been increasing with increasing passenger and logistics movements under globalization. CO2, which is the main global warming gas from aircraft, was charged about 3.5% of total global CO2 emissions and 12% of transportation fuel emissions. For these reasons, a lot of governments and the international civil aviation organization (ICAO) are trying to reduce CO2 emissions via the introduction of bio-jet fuel. In this paper, we showed the jet fuel properties, specifications, and presentative production methods of bio-jet fuel such as alcohol to jet (ATJ), oil to jet (OTJ), gas to jet (GTJ) and sugar to jet (STJ). Also, we described the status of global and domestic bio-jet fuel usage and the policy plan for efficient distribution.

Estimation of Flight Fuel Consumption Based on Flight Track Data and Its Accuracy Analysis (항적자료를 활용한 항공기 연료 소모량 추정 및 정확도 분석)

  • Park, Jang-Hoon;Ku, Sung-Kwan;Baik, Ho-Jong
    • Journal of the Korean Society for Aviation and Aeronautics
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    • v.22 no.4
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    • pp.25-33
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    • 2014
  • As global warming becoming an environmentally serious issue, more attention is drawn to fuel consumption which is the direct source of green house gas emission. The fuel consumption by aircraft operation is not an exception. Motivated by the societal and environmental context, this paper explains a method for estimation of aircraft fuel consumed during their flights as well as the computational process using real flight track data. Applying so-called 'Total Energy Model' along with aircraft specific parameters provided in EUROCONTROL's Base of Aircraft Data (BADA) to aircraft radar track data, we estimate fuel consumption of individual aircraft flown between Gimpo and Jeju airports. We then assess the estimation accuracy by comparing the estimated fuel consumption with the actual one collected from an airline. The computational results are quite encouraging in that the method is able to estimate the actual fuel consumption within ${\pm}6{\sim}11%$ of error margin. The limitations and possible enhancements of the method are also discussed.

Numerical Simulation of Orifice Injection Characteristics of High Temperature Aviation Fuel (고온 항공유의 오리피스 인젝터 분사특성 수치해석)

  • Sung-rok Hwang;Hyung Ju Lee
    • Journal of ILASS-Korea
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    • v.28 no.2
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    • pp.89-96
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    • 2023
  • This study presents a numerical simulation investigating hydrodynamic characteristics of high-temperature hydrocarbon aviation fuel injected through a plain orifice injector. The analysis encompassed the temperature range up to the critical point, and the obtained results were compared with prior experimental observations. The analysis unveiled that the injector's exit pressure remains equivalent to the ambient pressure when the fuel injection temperature is below the boiling point. However, when the fuel temperature surpasses the boiling point, the exit pressure of the injector transitions to the saturated vapor pressure corresponding to the fuel injection temperature. Consequently, the exit pressure of the injector increases in tandem with the rapid increase of the saturation vapor pressure due to escalating fuel temperatures. This rise in the exit pressure necessitates a proportional increase in fuel injection pressure to ensure a fixed fuel mass flow rate. Furthermore, the investigation revealed that the discharge coefficient obtained by applying the exit pressure instead of the ambient pressure did exhibit no decrease, but rather was maintained at a nearly constant value, comparable to its level below the boiling point.

Development of Test Simulator for Developing Fuel Quantity Measurement System for Supersonic Jet Trainer Conformal Fuel Tank (초음속항공기 보조연료탱크 연료량측정시스템 개발용 모사시험장치 개발)

  • Kim, Bong-Gyun;Park, Dae-Jin;Jeon, Hyeon-Wu;Lee, Sangchul
    • Journal of the Korean Society for Aviation and Aeronautics
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    • v.26 no.2
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    • pp.76-82
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    • 2018
  • A test simulator is needed to develop a fuel quantity measurement system that takes into account the roll and pitch motion of the aircraft. In this paper, we develop a test simulator that consists of attitude simulation equipment, fueling equipment, and data storage equipment. The attitude simulation equipment simulates the aircraft attitude. It is manufactured to operate pitch angle and roll angle movement. The fueling equipment supplies fuel to the supplementary fuel tank. The data storage equipment collects and stores the measured data. We also develop an automation software that operates the test simulator and collects data automatically. The test simulator has been automated to prevent testers from being exposed to toxic fuel. Through automation software, the collection period is reduced by one quarter compared to manual collection. The developed fuel quantity measurement system is verified through the test simulator.

A Research of Trends in Development of Bio-Diesel Aviation Fuel Technology using Microalgae (미세조류 이용 바이오디젤 항공유 기술개발 동향 연구)

  • Han-Young Yoon
    • Journal of the Korean Society for Aviation and Aeronautics
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    • v.32 no.2
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    • pp.151-158
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    • 2024
  • Microalgae are aquatic microorganisms capable of photosynthetic growth using water, carbon dioxide and sunlight, and can replace petroleum for transportation. It is receiving great attention as a potential next-generation biological resource. The microalgae biodiesel production process is largely based on the development of highly efficient strains and mass production. It consists of cultivation, harvesting, oil extraction, fuel conversion and by-product utilization. Currently, microalgae diesel is 3-5 times more expensive than petroleum diesel. However, with the optimization of each element technology and the development of integrated systems, not only biofuels, but also industrial materials, wastewater treatment, and greenhouse gases As application expands to various fields such as abatement, the timing of commercialization may be brought forward. Oil prices have recently fallen due to the influence of sail gas. Although there has been a significant drop, global warming is an urgent challenge for current and future generations. In particular, Korea, which does not have oil resources, We must always prepare for political environmental changes, high oil prices, and energy crises. In this paper, the need for eco-friendly biofuel for carbon dioxide conversion. In addition to research trends, domestic and international research trends, and economic prospects, the concept of microalgae and the element technologies of the biodiesel production process are briefly discussed introduced.

International Progress on the Impacts of Aviation on Climate Change and Study for an Advanced Carbon Calculation Methodology (국제항공 기후변화 관련 국제동향과 항공 배출가스 계산방법의 개선에 관한 연구)

  • Lee, Gun Young;Yoo, Kwang Eui;Hwang, Sung Youn
    • Journal of the Korean Society for Aviation and Aeronautics
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    • v.21 no.2
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    • pp.62-69
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    • 2013
  • The introduction of aviation into the EU-ETS has faced significant opposition from many ICAO member States. Accordingly a global solution through ICAO is in progress. This paper traces the progress of works done by the HGCC in the area of global aviation aspiration goals aiming for the submission to the 38th Session of the ICAO Assembly. Furthermore, devices for calculating the carbon dioxide emissions from flights have been developed by several agencies including international organizations, governments, airlines and nongovernmental organizations. These carbon calculators, however, introduce too many assumptions to simplify the calculation process. This study assesses carbon calculators for aviation emissions and suggests a modified calculation methodology using the pre-existing computer reservation system for better accuracy.

Design of Embedded System with Radio Control Method for Small Jet Engine Fuel Pump (소형제트엔진연료펌프의 무선제어방식을 적용한 임베디드시스템 고안)

  • Kyu-Jun Yu;Byeong-Gook Kwon;Gi Hun-Song;Jun-Hee Lee;Yoon-Suk Oh;Hyeong-Jun Jeon
    • Proceedings of the Korean Society of Computer Information Conference
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    • 2023.07a
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    • pp.105-106
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    • 2023
  • 소형제트엔진은 주로 연구, 실험, 교육 등의 목적으로 사용되고 있다. 이러한 소형제트엔진은 고도가 높고 고속으로 비행하는 드론에 추력 발생 장치로서의 중요한 역할을 수행할 수 있다. 그러나 엔진의 실질적인 활용을 위해서는 기존의 유선으로 구성된 컨트롤러를 무선으로 제어할 수 있는 방식으로 재구성하는 것이 필요하다. 이 중에서도 연료펌프의 무선제어시스템이 우선적으로 개발되어야만 다른 부분에 대한 무선제어개발이 가능해질 것이다. 본 논문에서는 소형 제트 엔진의 연료 펌프를 무선으로 제어할 수 있는 방식을 적용한 임베디드 시스템의 구성과 방식에 대해 제안하고 있다.

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Aircraft Fuel Efficiency Improvement and Effect through APMS (APMS 활용을 통한 항공기 연비향상 및 기대효과 )

  • Jae Leame Yoo
    • Journal of the Korean Society for Aviation and Aeronautics
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    • v.31 no.2
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    • pp.81-88
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    • 2023
  • SHM (Structural Health Monitoring) technique for monitoring aircraft structural health and damage, EHM (Engine Health Monitoring) for monitoring aircraft engine performance, and APM (Application Performance Management) is used for each function. APMS (Airplane Performance Monitoring System) is a program that comprehensively applies these techniques to identify the difference between the performance manual provided by the manufacturer and the actual fuel mileage of the aircraft and reflect it in the flight plan. The main purpose of using APMS is to understand the performance of each aircraft, to plan and execute flights in an optimal way, and consequently to reduce fuel consumption. First, it is to check the fuel efficiency trend of each aircraft, check the correlation between the maintenance work performed and the fuel mileage, find the cause of the fuel mileage increase/decrease, and take appropriate measures in response. Second, it is to find the cause of fuel mileage degradation in detail by checking the trends by engine performance and fuselage drag effect. Third, the APMS is to be used in making maintenance work decisions. Through APMS, aircraft with below average fuel mileage are identified, the cause of fuel mileage degradation is identified, and appropriate corrective actions are determined. Fourth, APMS data is used to analyze the economic analysis of equipment installation investment. The cost can be easily calculated as the equipment installation cost, but the benefit is fuel efficiency improvement, and the only way to check this is the manufacturer's theory. Therefore, verifying the effect after installation and verifying the economic analysis is to secure the appropriateness of the investment. Through this, proper investment in fuel efficiency improvement equipment will be made, and fuel efficiency will be improved.