• Title/Summary/Keyword: 흡열 반응

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A Technical Review of Endothermic Fuel Use on Supersonic Flight (고속비행체에서 흡열연료의 이용기술 동향)

  • Kim, Joong-Yeon;Park, Sun-Hee;Chun, Byung-Hee;Kim, Sung-Hyun;Jeong, Byung-Hun;Han, Jeong-Sik
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2009.11a
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    • pp.93-96
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    • 2009
  • Advances in high speed flight technologies and engine efficiencies increase heat load on the aircraft. As the temperature of air flow is too high to cool the structure at hypersonic flight speeds, it is necessary to utilize the aircraft fuel as the primary coolant. By undergoing endothermic reaction, such as thermal decomposition or catalytic decomposition, aircraft fuels have heat sink potential. These fuels are called endothermic fuels. The endothermic reaction can be improved by catalysts, but limited by coke deposition. In this study the essential technologies of endothermic fuels are described, and intended to be used for basic research.

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Study on the Deactivation Trends of Liquid Fuel According to the Types of Endothermic Catalyst in Flow Reactor (흐름형 반응기 내에서 액체연료의 흡열반응촉매 종류에 따른 비활성화 정도에 대한 연구)

  • Lee, Tae Ho;Jeon, Sunbin;Kim, Sung Hyun;Jeong, Byung Hun;Han, Jeong Sik
    • Journal of the Korean Society of Propulsion Engineers
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    • v.22 no.5
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    • pp.81-87
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    • 2018
  • In hypersonic aircraft, increase of aerodynamic and engine heat lead thermal load in airframe. It could lead structural change of aircraft's component and malfunctioning. Endothermic fuels are liquid hydrocarbon fuels which absorb the heat load by undergoing endothermic reactions. In this study, we investigated the relationship between product, coke formation and catalytic properites of endothermic catalysts by using exo-tetrahydrodicyclopentadiene as a fuel in a fixed bed flow reactor similar to the actual reaction conditions.

Study on the Method of Measurement the Heat Sink of the Endothermic Catalytic Reaction in the Flow Reactor (흐름형 반응기에서 흡열 촉매반응의 흡열량 측정 방법에 대한 연구)

  • Lee, Tae Ho;Hyeon, Dong Hun;Kim, Sung Hyun;Jeong, Byung Hun;Han, Jeong Sik
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2017.05a
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    • pp.991-994
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    • 2017
  • In hypersonic aircraft, increase of aerodynamic and engine heat lead thermal load in airframe. It could lead structural change of aircraft's component and malfunctioning. Endothermic fuels are liquid hydrocarbon fuels which are able to absorb the heat load by undergoing endothermic reactions. In this study, we investigated the method of measuring the heat sink of catalyst by using exo-tetrahydrodicyclopentadiene as a fuel in a packed bed flow reactor similar to the actual reaction conditions.

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The Development of Performance Test Equipment For Evaluating Endothermic Performance of Fuel Supply and Cooling System in High-Speed Vehicles (고속비행체 연료 공급 및 냉각 계통의 흡열성능 평가를 위한 성능시험 장치 개발)

  • Kim, Minsang;Choi, Won;Jun, Pilsun;Park, Jeongbae
    • Journal of Aerospace System Engineering
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    • v.13 no.4
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    • pp.43-49
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    • 2019
  • In this study, a test equipment which enables to feed endothermic fuel which is heated in the inside and outside environment of a high-speed vehicle and evaluate the heat exchangers' performance was designed and manufactured. For smooth operation of the test equipment, a test procedure that supplied endothermic fuel at high temperatures was established. The catalyst performance test was conducted based on the supply condition of the endothermic fuel and the amount of heat absorbed was analyzed. The validation of the test equipment was proved by comparing the results of catalytic reaction with the previous studies under similar reaction condition. This test equipment can be utilized in the endothermic reaction tests of catalyzed endothermic fuel under various conditions.

A Technical Review of Endothermic Fuel Use on High Speed Flight Cooling (흡열연료를 이용한 고속비행체 냉각기술 동향)

  • Kim, Joong-Yeon;Park, Sun-Hee;Chun, Byung-Hee;Kim, Sung-Hyun;Jeong, Byung-Hun;Han, Jeong-Sik
    • Journal of the Korean Society of Propulsion Engineers
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    • v.14 no.2
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    • pp.71-79
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    • 2010
  • As hypersonic flight speeds and engines efficiencies increase, heat loads on an aircraft and it's engine increase. Because the temperature of the air flow is too high to cool the aircraft structure at hypersonic flight speeds, it is essential to use the aircraft fuel as the primary coolant. Endothermic fuels are liquid hydrocarbon aircraft fuels which are able to absorb the heat loads by undergoing endothermic reactions, such as thermal and catalytic cracking. The endothermic reactions are improved by catalysts which change the extent of reaction and product distribution. At high temperature, liquid hydrocarbons would lead to coke formation that can reduce the effectiveness of heat exchanger and cause rapid degradation of the catalyst, thus endothermic capacity of endothermic fuels is limited to the temperature at which coke doesn't form. In this study, the essential cooling technologies by applying endothermic fuels and the properties of the endothermic fuels are described.

Heat Sink Measurement of Liquid Fuel for High Speed Aircraft Cooling (고속 비행체 냉각을 위해 사용되는 액체연료의 흡열량 측정연구)

  • Kim, Joongyeon;Park, Sun Hee;Hyeon, Dong Hun;Chun, Byung-Hee;Kim, Sung Hyun;Jeong, Byung-Hun;Han, Jeong-Sik
    • Journal of the Korean Society of Propulsion Engineers
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    • v.18 no.2
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    • pp.10-15
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    • 2014
  • For hypersonic aircraft, increase of flight speeds causes heat loads that are from aerodynamic heat and engine heat. The heat loads could lead structural change of aircraft's component and malfunctioning. Endothermic fuels are liquid hydrocarbon fuels which are able to absorb the heat loads by undergoing endothermic reactions, such as thermal and catalytic cracking. In this study, methylcyclohexane was selected as a model endothermic fuel and experiments on endothermic properties were implemented. To improve heat of endothermic reaction, we applied zeolites and confirmed that HZSM-5 was the best catalyst for the catalytic performance. The objective is to investigate catalytic effects for heat sink improvement. The catalyst could be applied to system that use kerosene fuel as endothermic fuel.

Study on the Aging Behaviors of a Rapidly Solidified Al-Li-Zr Alloy by Differential Scanning Calorimetry (열분석 방법에 의한 급냉응고 Al-Li-Zr 합금의 시효거동 연구)

  • Hong, Yeong-Jun;Gang, Jeong-Yun;Kim, In-Bae;Lee, Sang-Rae
    • Korean Journal of Materials Research
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    • v.5 no.4
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    • pp.405-411
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    • 1995
  • 급냉응고된 Al-3.51wt%Li-0.34wt%Zr 합금의 시효거동을 시차주사열량계(DSC)에 의한 열분석 방법으로 조사하였다. DSC에 의한 비열측정 결과 $\delta$’의 석출에 의한 발열반응과 $\delta$, $\beta$ 및 복합석출상의 석출에 의한 발열반응을 확인하였으며 $\delta$’ 및 $\delta$의 재고용에 의한 2개의 흡열반응을 확인하였다. 7$0^{\circ}C$ 저온시효시 $\delta$’의 석출에 의한 발열반응 이전에 흡열반응이 나타났으며 이것은 $\delta$’ 석출 이전에 $\delta$’ 전구생성물이 형성되었음을 의미한다. DSC 곡선상에 나타난 발열과 흡열곡선을 해석하여 얻은 $\delta$’상 석출과 재고용의 활성화에너지값은 각각 83KJ/mol과 98KJ/mol로서 Al-Li 2원계 및 Al-Li-Mg에 비해 높은 값을 나타내엇으며, 시효에 의한 강화가 일어나 DSC에 의한 비열변화 조사결과 나타난 $\delta$’상 석출 완료 시효조건점 (21$0^{\circ}C$, 1시간)에서 최고경도값(Hv 160)을 나타내었다.

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Thermal Decomposition of High Speed Aircraft Fuel in Supercritical Phase (고속비행체 연료의 초임계조건에서 열분해반응 연구)

  • Kim, Joong-Yeon;Park, Sun-Hee;Chun, Byung-Hee;Kim, Sung-Hyun;Jeong, Byung-Hun;Han, Jeong-Sik
    • Journal of the Korean Society of Propulsion Engineers
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    • v.15 no.5
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    • pp.1-9
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    • 2011
  • Researches on hypersonic aircraft technologies have been carried out to increase flight speeds. However, increase in flight speeds causes heat loads that could lead structural change of aircraft's component. Researches on cooling technologies using endothermic fuels are progressing in the USA, France and Russia to treat the heat loads. Endothermic fuels are liquid hydrocarbon aircraft fuels which are able to absorb the heat loads by undergoing endothermic reactions, such as thermal and catalytic cracking. In this study, methylcyclohexane, n-octane, and n-dodecane were selected as model endothermic fuels and experiments in endothermic properties were implemented. Experimental conditions were supercritical condition of each model fuels in which actual endothermic fuels were exposed. The object of this study is to identify endothermic properties of the model endothermic fuels and to predict endothermic properties of actual fuels such as kerosene fuels.

Thermal Decomposition of High Speed Aircraft Fuel in Supercritical Phase (고속비행체 연료의 초임계조건에서 열분해반응 연구)

  • Kim, Joong-Yeon;Park, Sun-Hee;Chun, Byung-Hee;Kim, Sung-Hyun;Jeong, Byung-Hun;Han, Jeong-Sik
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2010.11a
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    • pp.279-286
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    • 2010
  • Hypersonic aircraft technologies have been developed with increase in flight speeds. As hypersonic flight speeds increase, heat loads on an aircraft and it's engine increase. Researches on cooling technologies using endothermic fuels are progressing in the USA, France, and Russia to treat the heat loads. Endothermic fuels are liquid hydrocarbon aircraft fuels which are able to absorb the heat loads by undergoing endothermic reactions, such as thermal and catalytic cracking. In this study, methylcyclohexane, n-octane, and n-dodecane were selected as model endothermic fuels and experiments in endothermic properties were implemented. Experimental conditions were supercritical phase of each model fuels in which actual endothermic fuels were exposed. The object of this study is to identify endothermic properties of the model endothermic fuels and to predict endothermic properties of actual fuels such as kerosene fuels.

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Research Activities about Characteristics of Fuel Injection and Combustion Using Endothermic Fuel (흡열연료를 이용한 연료분사 및 연소 특성 연구동향)

  • Choi, Hojin;Lee, Hyungju;Hwang, Kiyoung
    • Journal of the Korean Society of Propulsion Engineers
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    • v.17 no.4
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    • pp.73-80
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    • 2013
  • Endothermic fuel utilizing technology is considered as a unique practical method of hypersonic vehicle for long distance flight. Research activities about characteristics of fuel injection and combustion using cracked by endothermic reaction are reviewed. Studies on characterization of supercritical fuel injection and mixing within supersonic flow field are surveyed. Researches on combustion characteristics such as ignition delay time, laminar burning velocity and combustion efficiency at supersonic model combustor are reviewed. In addition, domestic research activities on endothermic fuel are surveyed.