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Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering
Conventional research on compressor design often ignores the impact of the nose cone. This results in imprecise performance evaluations. By including the nose cone in the analysis, we can more accurately simulate operational conditions. This inclusion of
Saswat Kumar Panda +3 more
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Conventional research on compressor design often ignores the impact of the nose cone. This results in imprecise performance evaluations. By including the nose cone in the analysis, we can more accurately simulate operational conditions. This inclusion of
Saswat Kumar Panda +3 more
semanticscholar +1 more source
(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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Linear mathematical model of single-spool micro turbojet engine with fixed exhaust nozzle
2018 IEEE 16th World Symposium on Applied Machine Intelligence and Informatics (SAMI), 2018Main goal of this paper is to develop a linear state space representation of a micro turbojet engine based on physical laws describing the operation of the power plant. The importance of micro turbine engines is constantly rising; therefore it is essential to improve their reliability through advanced control systems.
Karoly Beneda +2 more
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Design of Two-Degree-of-Freedom Turbofan-Power-Ratio Control System for Micro Turbojet Engine
International Symposium on Applied Machine Intelligence and Informatics, 2019Control of gas turbine engines is a safety critical aspect of the industry, regardless of power turbines or aviation power plants. Moreover, modern turbine control systems implement additional features that allow efficient operation throughout the widest
K. Beneda, Khaoula Derbel
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optimization Design of High-Speed Generator for Micro Turbojet Engine Based on GDSFD-AL Method
IEEE Transportation Electrification Conference and Expo, Asia-Pacific, 2019Micro turbojet engine (MTE) uses generator to provide power for its accessory system and electronic equipment instead of fuel cell. In addition to high speed, the generator for MTE is required to have the smallest volume due to the limit of the ...
Jian Guo +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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Test Simulation and Control Law Optimization of Micro-Turbojet Engines
2023 14th International Conference on Mechanical and Aerospace Engineering (ICMAE), 2023Zhen Liu +5 more
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MACHINE LEARNING AND INFORMATION PROCESSING: PROCEEDINGS OF ICMLIP 2023, 2023
F. Z. Altair +3 more
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F. Z. Altair +3 more
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