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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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THE EFFECT OF PRIMARY FLIGHT INFORMATION FAILURE ON SAFETY AND RELIABILITY OF AIRCRAFT
Sklenář, Filip ; Badánik, Benedikt (referee) ; Juračka, Jaroslav (referee) ; Hlinka, Jiří (advisor)
It is necessary to have certain flight information available to control the airplane. This information is usually displayed on flight instruments, which are located on the dashboard of the aircraft. In case of loss of indication or misleading indication of certain devices, control of the aircraft can be very complicated or even impossible. The dissertation deals with the issue of loss of information indication from aerometric instruments (especially from the airspeed indicator). The work contains research on the course of degradation of total pressure measurements using a Pitot tube. Based on this research, it is possible to design a new system for detecting blockage of the Pitot tube, which will increase aviation safety. The phenomenon described was investigated in a wind tunnel and in real conditions. Furthermore, the work defines instructions for the compilation of an emergency procedure, which the pilot could use in the event of a fault condition with aerometric instruments. The real possibilities of use were demonstrated on a Cessna 172SP aircraft during the validation experiment. The validation experiment proved the possibilities of the safe usage of the emergency procedure during flight. The final part of the work is focused on the evaluation of possible changes in the creation of reliability and safety analyzes with regard to the application of new knowledge based on this work.
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Civil aviation security and protection against illegal acts
Srba, Matěj ; Sklenář, Filip (referee) ; Chlebek, Jiří (advisor)
This bachelor's thesis is focused on protection of civil aviation or rather on legal documents that provide this protection. In addition, the thesis describes two basic directions that aviation security deals with. The aim of this thesis is to compile a comprehensive overview of the basic documents with the special focus to L 17 (Annex 17). Along with this, provide answers to the ATPL sample questions specifically addressed to this regulation. In addition, the thesis describes several major accidents that have significantly affected the development of regulations as a starting point for creating legal documents. This is also linked to the history of these laws and agreements, which is also described.
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Role and tasks of air traffic services of the civil aviation
Panáček, Jiří ; Sklenář, Filip (referee) ; Chlebek, Jiří (advisor)
This bachelor thesis deals with rols and tasks of air traffic services of the civil aviation. Its aim is to compile a comprehensive overview of air traffic services, including the characteristics of their significance and definition of their activities. There is also emphasis on the submission of information in more readable form than what can be found in official documents describing the issue.
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Design of UL aircraft for physically handicapped pilots
Hejkalová, Anna ; Sklenář, Filip (referee) ; Bartoněk, Jaroslav (advisor)
The diploma thesis deals with the issue of operating aircrafts by people with physical disabi-lities. Firstly, it formulates medical eligibility requirements for pilots with mobility restricti-ons. Because there is a large number of movement restrictions and each of them is very indi-vidual, an adaptation for only one of these categories was chosen for the conceptual design of the aircraft in this diploma thesis: limitation of the lower half of the body. The aircraft is designed to best meet the needs of pilots with this limitation of movement, with emphasis on ergonomics, the possibility of independent use without any help of other people and espe-cially on the safety of the user. Furthermore, the work examines possibilities of adjusting the control of aircraft for the disabled, tries to choose the most suitable one which is then desci-bed. In the end, an examination of the UL2 regulation requirements for the designed aircraft is done.
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Technology of aircraft automatic flight control along an approach trajectory
Kočiš, Martin ; Sklenář, Filip (referee) ; Vosecký, Slavomír (advisor)
This diploma thesis is focused to systems used for automatic control of civil aircraft along an precision approach trajectory. It describes precision approach systems used in the past and their evolutional steps leading to their current and future configuration. The thesis does not put the goal to be a detailed study but to be a publication providing to pilots and students of Aeronautical traffic the introduction to the field of precision approach systems in context to another fields of aeronautical traffic, describing its current status and infer its further development.
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Planning of optimal VFR routes from the Czech Republic to the Republic of Croatia
Klačan, Matej ; Raudenský, Miroslav (referee) ; Sklenář, Filip (advisor)
The aim of this bachelor thesis is to create a detailed ground preparation of three different VFR flights from Czech Republic to the Republic of Croatia for a full occupied Cessna 172SP. The first reserch part is general introduction to the issue and acquaintance with the aircraft and its equipment. Special emphasis is placed on the fact that all planed flights are in accordance with aviation legislation, which is dealt with in the second part of the research part of the thesis work. The practical part of the thesis work deals with the issue of ground preparation itself, with the fact that it deals in more detail with navigation preparation of individual flights. Finally, the financial demands for our flights are given.
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Analysis of the operational risks of newly introduced aircraft types
Sklenář, Filip ; Janhuba, Luboš (referee) ; Chlebek, Jiří (advisor)
This thesis examines the process of introducing a new aircraft into the service, in particular by the steps from initial vision of a new aircraft until after the aircraft. The content of the thesis consists of seven parts. In the first four sections, I describe the organizations involved in aviation and reliability, physical principles of aircraft systems, accident statistics, regulatory requirements. The fifth section focuses on reliability and describes the procedures for the analysis of reliability. The sixth part is focused on the procedure for introducing new aircraft into service and also includes the methodology for eliminating the element of lack of confidence, which was one of the main objectives of this work. The seventh part is a demonstration of the procedure for the introduction of aircraft into operation.
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Certification of flight simulator training devices according to EASA requirements
Dittel, Daniel ; Šplíchal, Miroslav (referee) ; Sklenář, Filip (advisor)
The aim of this bachelor thesis is to compile a flight simulator certification procedure according to EASA requirements. The thesis contains a basic division of simulators according to the requirements for simulation fidelity and deals with the certification process of a specific Boeing 737 MAX simulator, where the aim is to certify the simulator to the FNPT II/MCC level. The thesis analyzes the certification from a general point of view, as well as from the point of view of the requirements for the visual system and the sound system and also contains the requirements for the extension from the FNPT II level to the FNPT II/MCC level. The thesis also contains an overview of regulations according to which the certification of flight simulators is done. The thesis also contains a chapter where the possibilities of using the Boeing 737 MAX simulator of the FNPT II/MCC level are described.
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