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Controller Design for Micro Turbojet Engine
2020 12th International Conference on Electrical Engineering (ICEENG), 2020Modern turbojet engines are controlled using digital controllers. First of all, the micro turbojet engine discrete model is identified. System identification technique utilized real data obtained from jet cat P200sx engine running experiments. Digital PID controllers are mostly used for controlling these engines.
Ahmed M. shehata +2 more
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Turbojet and Turboprop Engine Controls
SAE Technical Paper Series, 1951<div class="section abstract"><div class="htmlview paragraph">THE gas turbine fuel control situation is in a state of confusion, the author feels, because of such factors as the newness of gas turbine development, the lack of comparative evaluation tests on controls, and the lack of time for the results of field experience to become ...
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Production Problems of Turbojet Engines
SAE Technical Paper Series, 1949<div class="htmlview paragraph">THE production problems associated with turbojet engines are not more complex than those encountered with reciprocating engines, according to the author, but they are of a surprisingly different nature.</div> <div class="htmlview paragraph">For instance, he points out that, whereas reciprocating engine ...
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Development study of a precooled turbojet engine
Acta Astronautica, 2010Abstract A precooled turbojet engine has been developed by JAXA used for the hypersonic airplane and spaceplane. The subscale engine named “S-engine” whose thrust and weight are about 1.2 kN and 100 kg was designed, fabricated and tested. The components and the system firing tests under the sea-level-static condition were successfully conducted.In ...
Tetsuya Sato +8 more
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Performance Evaluation of an Experimental Turbojet Engine
International Journal of Turbo & Jet-Engines, 2017Abstract An exergy analysis is presented including design parameters and performance assessment, by identifying the losses and efficiency of a gas turbine engine. The aim of this paper is to determine the performance of a small turbojet engine with an exergetic analysis based on test data.
Ekici, Selcuk +4 more
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Reduction of Turbojet Engine Noise
2004The urgency of the problem of jet noise reduction has been rising again at the present stage of aircraft technology development. The main reasons are the following. The studies of attenuation of turbo-machine noise have demonstrated that the jet is one of the main noise sources even in engines with high by-pass ratios.
A. S. Ginevsky +2 more
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Automatic Control of Turbojet Engines
Journal of Fluids Engineering, 1949Abstract This paper presents the requirements for automatic control of a turbojet engine in order to meet the needs of military aviation and to realize the full operational performance of the engine. The author describes how these requirements were established, and outlines the recommended approach to the design of an optimum engine ...
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Variable Structure Control of a Turbojet Engine
1986 American Control Conference, 1986We study the fuel control problem of a single-spool turbojet engine. A transfer function approximation method is utilized to identify linear models about operating points. Then, a sliding mode control is developed to regulate the fuel flow so that the engine speed and temperature are within their physical constraints, based on the identified linear ...
Chin-Yu Chao +2 more
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Large Lightweight Turbojet Engines
SAE Technical Paper Series, 1958<div class="section abstract"><div class="htmlview paragraph">THIS paper deals with the general performance of turbojet engines in both subsonic and supersonic flight in relation to aircraft requirements.</div><div class="htmlview paragraph">The advantages and disadvantages of the bypass engine and small turbojet in relation to ...
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Availability Analysis of a Military Turbojet Engine
Journal of Failure Analysis and Prevention, 2019Availability analysis has been performed on a military turbojet engine using commercially available reliability software. Failure data of the engine over a period of 7 years are considered. The failures/defects are categorized, and then analysis is performed for the major defects.
R. Ragupathy, R. K. Mishra
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