Results 111 to 120 of about 163 (134)
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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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(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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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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Vibration Analysis of a Micro Turbojet Engine under Two Impeller Structural Faults
Proceedings of Global Power & Propulsion SocietyDisk fracture and locking nut loosening of centrifugal impeller leads to severe vibration of micro turbojet engines, posing significant threats to engine stability and safety. In order to identify the engine vibration characteristics induced by the above two faults in a practical micro aero-engine, vibration acceleration of the engine casing is ...
Zhiming Yang +6 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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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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The Aeronautical Journal
AbstractIn this study, measurements and numerical analyses of the temperature distribution of exhaust gas passing through two types of mixers using a micro turbojet engine were performed to investigate the flow mixing performance based on the shape of the mixer, which mixes the bypass air and core air in a gas turbine turbofan engine.
C. Lee, S.M. Choi
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AbstractIn this study, measurements and numerical analyses of the temperature distribution of exhaust gas passing through two types of mixers using a micro turbojet engine were performed to investigate the flow mixing performance based on the shape of the mixer, which mixes the bypass air and core air in a gas turbine turbofan engine.
C. Lee, S.M. Choi
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