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Centrifugal Compressor and Bell mouth Air Intake Preliminary Design for Micro Turbojet Engine

Journal of Karary University for Engineering and Science, 2021
This paper presents a design of centrifugal compressor and air intake for micro turbojet engine of 200 N thrust. Because of the small size of the micro turbine engines the air intake is designed in the form of bellmouth air intake in order to capture the needed amount of mass flow rate (0.45 kg/s).
Hamed Mohamed Ahmed Ali   +4 more
openaire   +1 more source

(INVESTIGATION OF A MICRO TURBOJET ENGINE VIA REVERSEENGINEERING)

2016
Tersine 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
openaire   +1 more source

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), 2018
Main 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
openaire   +1 more source

Flow physics in a micro turbojet engine inter-shaft fuel supply system

Physics of Fluids
Inter-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
openaire   +1 more source

Vibration Analysis of a Micro Turbojet Engine under Two Impeller Structural Faults

Proceedings of Global Power & Propulsion Society
Disk 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
openaire   +1 more source

Development of a Hardware Simulator for a Micro Turbojet Engine

2022 IEEE 20th Jubilee World Symposium on Applied Machine Intelligence and Informatics (SAMI), 2022
Roland Istenes-Nemeth   +2 more
openaire   +1 more source

Modeling of Micro Turbojet Engine

AIAA Propulsion and Energy 2019 Forum, 2019
Mahmoud M. Ashry   +2 more
openaire   +1 more source

Test Simulation and Control Law Optimization of Micro-Turbojet Engines

2023 14th International Conference on Mechanical and Aerospace Engineering (ICMAE), 2023
Zhen Liu   +5 more
openaire   +1 more source

Energy, exergy, environmental and sustainability assessments of jet and hydrogen fueled military turbojet engine

International Journal of Hydrogen Energy, 2022
Ozgur Balli, Hakan ÇaliŞkan
exaly  

Trends of Micro Turbojet Engines within Thrust Range up to 1,000N

The KSFM Journal of Fluid Machinery, 2020
Dong-Ho Rhee   +2 more
openaire   +1 more source

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