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Performance and Emission of a Biofueled Micro Turbojet Engine
51st AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition, 2013The engine performance, fuel consumption and emission of a micro gas turbojet engine running B100 biodiesel fuel, kerosene, hydro processed renewable (HJ) fuel from dynamic fuels, and JP-8 fuel are reported in this paper. The data are recorded and analyzed in terms of the different fuels.
Ing Huang Tan, William Liou
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Thermo-dynamic cycle computation of a micro turbojet engine
2016 IEEE 17th International Symposium on Computational Intelligence and Informatics (CINTI), 2016Thermodynamic models are a perfect tool to describe heat engines. But such thermodynamic model must be extended to reflect reality as accurately as possible. Micro turbo compressor engines are a specific type of heat engines that are derived from normal turbo compressor engines. To compute their thermodynamic parameters we need to know their dimensions
Ladislav Fozo +2 more
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Second Law Analysis of an Experimental Micro Turbojet Engine
2018Mini class gas turbine engines are today used for small UAVs, cogeneration applications, and hybrid electric vehicle applications. In this paper, exergetic assessment of an indigenous mini class gas turbine engine is investigated. This engine is classified as mini class gas turbine where it differs from similar class engines in two ways, including ...
Kahraman, C. +3 more
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Analysis of energy and emission metrics for an experimental turbojet engine by regression approach
Energy Sources, Part A: Recovery, Utilization and Environmental EffectsThe common usage of micro turbojet engines has sparked attention on these systems due to their unique advantages, which enable insight into the characteristics of different scaled turbojet engines. In this study, 930 data points regarding an experimental
Mehmet Kirmizi +2 more
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Study on micro-turbojet engine with high thrust-to-weight ratio
Theoretical and Natural Science, 2023Micro-turbojet engine refers to a closed cycle gas turbine engine with thrust below 500kg and power below 100kW. The performance indicators of domestic products are relatively low, and the main problems of domestic products are low thrust-to-weight ratio, poor reliability, and low heat resistance.
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Thermodynamic and Mechanical Design Concept for Micro-Turbojet to Micro-Turboshaft Engine Conversion
Volume 8: Industrial and Cogeneration; Manufacturing Materials and Metallurgy; Marine; Microturbines, Turbochargers, and Small Turbomachines, 2020Abstract In this work, a design concept for micro-turbojet to micro-turboshaft engine conversion is presented. This is motivated by a lack of available micro-turboshaft engines which is shown in the market survey conducted. Thus, the presented concept deals with the conversion of an existing micro-turbojet engine to a micro-turboshaft ...
Christoph Öttl, Reinhard Willinger
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(INVESTIGATION OF A MICRO TURBOJET ENGINE VIA REVERSEENGINEERING)
2016Tersine mühendislik bir aygıt, nesne veya sistemin teknolojik çalışma prensiplerini keşfetme sürecidir. Bu çalışma, özellikle bir mikro turbojet motorun ters mühendisliği üzerine odaklanmaktadır. İlk olarak, gaz türbin motorunun bileşenleri üç eksenli bir optik tarayıcı kullanılarak taranmış ve dijital nokta bulutu formatına dönüştürülmüştür.
İÇKE, Ramiz Ömür, TUNÇER, Onur
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Development of a Hardware Simulator for a Micro Turbojet Engine
2022 IEEE 20th Jubilee World Symposium on Applied Machine Intelligence and Informatics (SAMI), 2022Roland Istenes-Nemeth +2 more
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Flow physics in a micro turbojet engine inter-shaft fuel supply system
Physics of FluidsInter-shaft fuel supply systems (ISFSSs) consisting of a shaft annulus and a fuel slinger are usually used in micro turbojet engines to pump the fuel to the combustor, aiming at reducing engine's size and weight. Differing from the configuration with stationary fuel pipework, the fast-rotating shaft in the annulus would induce significant drag ...
Zhixun Wang +4 more
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Modeling of Micro Turbojet Engine
AIAA Propulsion and Energy 2019 Forum, 2019Mahmoud M. Ashry +2 more
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