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Summary of unconventional aircraft concepts
Nečas, David ; Šošovička, Róbert (referee) ; Lajza, Ondřej (advisor)
This bachelor´s thesis deals with civil aircrafts of unconventional conceptions, which got into serial production. The thesis will be divided according to categories of aircrafts, whereas in every category with the exception of large transport aircrafts one conventional and two unconventional aircrafts will be specified for comparing various properties. Military aircraft will be mentioned only marginally because of the representative of significant unconventional conception.
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Aerospace - Futuristic Aircraft Cockpit Design
Bílek, Jan ; Bartoň, Radek (referee) ; Chudý, Peter (advisor)
This work describes the visualization design of the flight related quantities in a cockpit of a modern light sport aircraft. It focuses on the utilization of the state of the art trends in flight data displays and introduces the innovative implementation of the aircraft's energy state smart clues that reduce pilots' workload. The initial part of the work presents a research into the flight, engine and navigation data presentation on analog instruments, followed by their illustrative depiction in glass cockpits. Within the framework of this thesis, Microsoft Flight Simulator has been used as a source of the flight related data. Final advances in the display design were introduced through the implementation of the synthetic vision system and a visualization of the virtual tunnel in the sky.
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Electrically powered plane conceptual design
Ševčík, Igor ; Sklenář, Filip (referee) ; Popela, Robert (advisor)
The master’s thesis deals with conceptual design of a new electrically powered aircraft as assignment for Evektor, s.r.o. company. In the first part of thesis there is more detailed elaboration of small aircraft statistics and their comparison. Thesis then concentrates on assigned parameters and requirements for design. Next section continues with the most important part of thesis, which is optimization of wing used for aircraft design and also analysis of its characteristics. The problematics of preliminary verification of flight performances as well as aircraft dimension design and follow-up weight analysis with consideration of power cells placement is described thereafter. A few different flight configurations is taken into consideration within weight analysis. Final part contains evaluation of optimization and design process.
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Front landing gear design of PS-28 Cruiser aircraft
Marcinko, Peter ; Šplíchal, Jan (referee) ; Katrňák, Tomáš (advisor)
This diploma thesis deals with the design of the front landing gear with steering nose leg and hydropneumatic shock absorber, designed for aircraft PS - 28 Cruiser. In the thesis there was created design of basic types of front landing gear and the best option was selected. The work is further elaborated design of hydropneumatic shock absorber and comparise with the measured load. At the end of the work it was created the structural design of the front landing gear.
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Electrically powered plane conceptual design
Ševčík, Igor ; Sklenář, Filip (referee) ; Popela, Robert (advisor)
The master’s thesis deals with conceptual design of a new electrically powered aircraft as assignment for Evektor, s.r.o. company. In the first part of thesis there is more detailed elaboration of small aircraft statistics and their comparison. Thesis then concentrates on assigned parameters and requirements for design. Next section continues with the most important part of thesis, which is optimization of wing used for aircraft design and also analysis of its characteristics. The problematics of preliminary verification of flight performances as well as aircraft dimension design and follow-up weight analysis with consideration of power cells placement is described thereafter. A few different flight configurations is taken into consideration within weight analysis. Final part contains evaluation of optimization and design process.
|
|
|
Front landing gear design of PS-28 Cruiser aircraft
Marcinko, Peter ; Šplíchal, Jan (referee) ; Katrňák, Tomáš (advisor)
This diploma thesis deals with the design of the front landing gear with steering nose leg and hydropneumatic shock absorber, designed for aircraft PS - 28 Cruiser. In the thesis there was created design of basic types of front landing gear and the best option was selected. The work is further elaborated design of hydropneumatic shock absorber and comparise with the measured load. At the end of the work it was created the structural design of the front landing gear.
|
|
|
Aerospace - Futuristic Aircraft Cockpit Design
Bílek, Jan ; Bartoň, Radek (referee) ; Chudý, Peter (advisor)
This work describes the visualization design of the flight related quantities in a cockpit of a modern light sport aircraft. It focuses on the utilization of the state of the art trends in flight data displays and introduces the innovative implementation of the aircraft's energy state smart clues that reduce pilots' workload. The initial part of the work presents a research into the flight, engine and navigation data presentation on analog instruments, followed by their illustrative depiction in glass cockpits. Within the framework of this thesis, Microsoft Flight Simulator has been used as a source of the flight related data. Final advances in the display design were introduced through the implementation of the synthetic vision system and a visualization of the virtual tunnel in the sky.
|
|
|
Summary of unconventional aircraft concepts
Nečas, David ; Šošovička, Róbert (referee) ; Lajza, Ondřej (advisor)
This bachelor´s thesis deals with civil aircrafts of unconventional conceptions, which got into serial production. The thesis will be divided according to categories of aircrafts, whereas in every category with the exception of large transport aircrafts one conventional and two unconventional aircrafts will be specified for comparing various properties. Military aircraft will be mentioned only marginally because of the representative of significant unconventional conception.
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Export strategy of a company Aerospool s.r.o.
Mečiarová, Jana ; Halík, Jaroslav (advisor) ; Fridrich, Jan (referee)
The first part of this paper analyses basic principles of light aircraft industry and an export strategy of the company Aerospool with the aim to identify key aspects of this industry. The second part covers specifically the market of the USA. It contains competition analysis and PEST analysis which identifies key specifics of this market. SWOT analysis discover strengths and weaknesses of the company in the context of US market and threats and opportunities, which company can meet at this market. In the end there is a proposition of possible way of bigger penetration of the company Aerospool.
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