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Model identification and measurement of parameters of model turbine JetCAT
Tlustoš, Jiří ; Dolák, Petr (referee) ; Klusáček, Stanislav (advisor)
The bachelor's thesis deals with measurement of microturbine engine parameters. The first part of the thesis covers theory of microturbine parameters measurement, data analysis, interpretation and utilization for model identification, engine control, individual functional block charts and characteristics generation. All possible methods for engine parameters measurement, sensors selection and installation, data acquisition are analyzed here. The focus is on the engine air flow measurement. Selected method of the air flow measurement is described here in detail and verified for the specific case. The Calibration was carried out by means of measuring route with continuous air flow adjustment. In the final part is concept evaluation and recommendation for air flow measurement in the real application on the model turbine JetCAT.
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Fuel control unit system of jet turbine engines
Mašková, Šárka ; Bencalík, Karol (referee) ; Šplíchal, Miroslav (advisor)
This bachelor thesis describes fuel control unit systems of jet turbine engines, specifically historical development of these systems including current research, operating processes of different types of fuel control unit systems and important controling quantities. The last part of the thesis describes fuel control unit system produced by Jihostroj a.s. company for M601 engine.
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Single lever control system of piston engine with propeller
Gröger, Roman ; Cäsar, Tomáš (referee) ; Šplíchal, Miroslav (advisor)
This bachelor thesis deals with the description of the work of aircraft piston power plants and single-lever control systems. The first part describes the characteristics of piston engines and their indicators. The second part describes the work of piston engines with variable-pitch propeller. The third and fourth part deals with single-lever control systems of piston power plant, their comparison and possible problems of their control.
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Single lever control system of piston engine with propeller
Gröger, Roman ; Cäsar, Tomáš (referee) ; Šplíchal, Miroslav (advisor)
This bachelor thesis deals with the description of the work of aircraft piston power plants and single-lever control systems. The first part describes the characteristics of piston engines and their indicators. The second part describes the work of piston engines with variable-pitch propeller. The third and fourth part deals with single-lever control systems of piston power plant, their comparison and possible problems of their control.
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Fuel control unit system of jet turbine engines
Mašková, Šárka ; Bencalík, Karol (referee) ; Šplíchal, Miroslav (advisor)
This bachelor thesis describes fuel control unit systems of jet turbine engines, specifically historical development of these systems including current research, operating processes of different types of fuel control unit systems and important controling quantities. The last part of the thesis describes fuel control unit system produced by Jihostroj a.s. company for M601 engine.
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Model identification and measurement of parameters of model turbine JetCAT
Tlustoš, Jiří ; Dolák, Petr (referee) ; Klusáček, Stanislav (advisor)
The bachelor's thesis deals with measurement of microturbine engine parameters. The first part of the thesis covers theory of microturbine parameters measurement, data analysis, interpretation and utilization for model identification, engine control, individual functional block charts and characteristics generation. All possible methods for engine parameters measurement, sensors selection and installation, data acquisition are analyzed here. The focus is on the engine air flow measurement. Selected method of the air flow measurement is described here in detail and verified for the specific case. The Calibration was carried out by means of measuring route with continuous air flow adjustment. In the final part is concept evaluation and recommendation for air flow measurement in the real application on the model turbine JetCAT.
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