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Proposal for the use of the Z 143 Lsi aircraft for aerobatic operation
Hub, Pavel ; Juračka, Jaroslav (referee) ; Píštěk, Antonín (advisor)
This master thesis deals with the impact of given construction changes on the Zlín Aircraft Z 143 Lsi aircraft, the purpose of which is to enable the aircraft to operate in the aerobatic category in accordance with FAR-23 certification guidelines. An important part of the thesis is the definition of permitted flight configurations with respect to the aircrafts´ structural strength limits and flight performance. Furthermore, impact of these changes on flight within the normal and utility categories is investigated. An overview of neccessary certification procedures is provided as well. The goal of the thesis is to supply the company with relevant technical documentation to decide on adequacy of the concept.
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Turboprop powerplant installation into small twoseater airplane
Kövér, Ondřej ; Jebáček, Ivo (referee) ; Juračka, Jaroslav (advisor)
The diploma thesis deals with the problem of application of turboprop engine to a small 2-seater airplane. In the first part, reasons why the application is in considered are stated. Then, the air-plane is characterised, the choice of the most suitable engine, propeller and the weight analysis is made and the centres of gravity are calculated. For chosen engine and propeller, in chapter 6, the flight performance is calculated. In chapter 7 follows calculations of flight envelopes and the lim-it positive and negative load factor is stated. Flight envelopes calculations are followed by the calculation of engine mount loads of flight and ground cases. In chapter 9, the design of engine mount, inlet and outlet system and positioning of important elements are solved. The design part is followed by strength analysis of engine mount and its attachment into engine partition.
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Proposal for the use of the Z 143 Lsi aircraft for aerobatic operation
Hub, Pavel ; Juračka, Jaroslav (referee) ; Píštěk, Antonín (advisor)
This master thesis deals with the impact of given construction changes on the Zlín Aircraft Z 143 Lsi aircraft, the purpose of which is to enable the aircraft to operate in the aerobatic category in accordance with FAR-23 certification guidelines. An important part of the thesis is the definition of permitted flight configurations with respect to the aircrafts´ structural strength limits and flight performance. Furthermore, impact of these changes on flight within the normal and utility categories is investigated. An overview of neccessary certification procedures is provided as well. The goal of the thesis is to supply the company with relevant technical documentation to decide on adequacy of the concept.
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Turboprop powerplant installation into small twoseater airplane
Kövér, Ondřej ; Jebáček, Ivo (referee) ; Juračka, Jaroslav (advisor)
The diploma thesis deals with the problem of application of turboprop engine to a small 2-seater airplane. In the first part, reasons why the application is in considered are stated. Then, the air-plane is characterised, the choice of the most suitable engine, propeller and the weight analysis is made and the centres of gravity are calculated. For chosen engine and propeller, in chapter 6, the flight performance is calculated. In chapter 7 follows calculations of flight envelopes and the lim-it positive and negative load factor is stated. Flight envelopes calculations are followed by the calculation of engine mount loads of flight and ground cases. In chapter 9, the design of engine mount, inlet and outlet system and positioning of important elements are solved. The design part is followed by strength analysis of engine mount and its attachment into engine partition.
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