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Installation of the LYCOMING power unit into the Bristel UL aircraft
Kročil, Petr ; Juračka, Jaroslav (referee) ; Píštěk, Antonín (advisor)
This diploma thesis focuses on Lycoming drive unit mounting used in two-seater plane of VLA category (the very light aircraft). In the beginning characteristics of currently produced Bristell aircrafts are described. Following chapters aim at research selection of new drive unit mounting based on multi-criteria decision analysis. For selected unit, the weight, center of mass and flight performance are calculated. Additionally, the construction of engine mount is proposed. According to CS-VLA and CS-23 stress level of mounting is defined followed by strength verification. Later in this thesis, a suitable engine cover for engine and cockpit cooling is proposed. A complete fuel system is described in following chapter. Last chapter deals with financial costs of re-engining as well as aircraft operational costs.
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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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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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|
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Installation of the LYCOMING power unit into the Bristel UL aircraft
Kročil, Petr ; Juračka, Jaroslav (referee) ; Píštěk, Antonín (advisor)
This diploma thesis focuses on Lycoming drive unit mounting used in two-seater plane of VLA category (the very light aircraft). In the beginning characteristics of currently produced Bristell aircrafts are described. Following chapters aim at research selection of new drive unit mounting based on multi-criteria decision analysis. For selected unit, the weight, center of mass and flight performance are calculated. Additionally, the construction of engine mount is proposed. According to CS-VLA and CS-23 stress level of mounting is defined followed by strength verification. Later in this thesis, a suitable engine cover for engine and cockpit cooling is proposed. A complete fuel system is described in following chapter. Last chapter deals with financial costs of re-engining as well as aircraft operational costs.
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