National Repository of Grey Literature 4 records found  Search took 0.01 seconds. 
Preparation of flight plan for cross-country flight from LKTB to ULLI by L-200A airplane
Hornych, Petr ; Imriš, Pavel (referee) ; Raudenský, Miroslav (advisor)
The objective of this study is the submission of entire IFR flight plans of chartered routes, including risk analysis and necessary equipment for flights in central and east Europe. The paper describes rules for IFR flights, which must be followed when flying into these areas and also focuses on the meteorological situation, legislation and general geographical characteristics of the mentioned states. The flight to Russia is divided into several legs. All the available information is according to the valid AIP.
Universal characteristics of piston engines with a propeller
Šafránek, Martin ; Matějů, Jiří (referee) ; Zikmund, Pavel (advisor)
Determining the characteristics of piston engines with a propeller is a complex task. Accurate calculations are based on engine and propeller characteristics from the manufacturers, which are, however, quite demanding. It is also possible to use simplified models that can predict the achievable values of propeller efficiency and fuel consumption. They are based on a simple propeller efficiency and maximum power. However, these models are often very inaccurate, which is a significant disadvantage. Therefore, it is possible to use the universal characteristics of propeller propulsion units, which offers a more accurate calculation of power and fuel consumption using a relatively simple model. The diploma thesis deals with a summary description of all characteristics of reciprocating internal combustion engines and propellers. A mathematical model was created here, which works according to a certain algorithm based on the joint work of the engine and the propeller. This model can predict the required power and fuel consumption in different flight modes much more accurately. The results were applied to the performance of ultralight aircraft, especially to the range, which was significantly increased.
Universal characteristics of piston engines with a propeller
Šafránek, Martin ; Matějů, Jiří (referee) ; Zikmund, Pavel (advisor)
Determining the characteristics of piston engines with a propeller is a complex task. Accurate calculations are based on engine and propeller characteristics from the manufacturers, which are, however, quite demanding. It is also possible to use simplified models that can predict the achievable values of propeller efficiency and fuel consumption. They are based on a simple propeller efficiency and maximum power. However, these models are often very inaccurate, which is a significant disadvantage. Therefore, it is possible to use the universal characteristics of propeller propulsion units, which offers a more accurate calculation of power and fuel consumption using a relatively simple model. The diploma thesis deals with a summary description of all characteristics of reciprocating internal combustion engines and propellers. A mathematical model was created here, which works according to a certain algorithm based on the joint work of the engine and the propeller. This model can predict the required power and fuel consumption in different flight modes much more accurately. The results were applied to the performance of ultralight aircraft, especially to the range, which was significantly increased.
Preparation of flight plan for cross-country flight from LKTB to ULLI by L-200A airplane
Hornych, Petr ; Imriš, Pavel (referee) ; Raudenský, Miroslav (advisor)
The objective of this study is the submission of entire IFR flight plans of chartered routes, including risk analysis and necessary equipment for flights in central and east Europe. The paper describes rules for IFR flights, which must be followed when flying into these areas and also focuses on the meteorological situation, legislation and general geographical characteristics of the mentioned states. The flight to Russia is divided into several legs. All the available information is according to the valid AIP.

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