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Cockpit instruments for four-seater sport and leisure aircraft
Liberda, Jiří ; Janhuba, Luboš (referee) ; Hlinka, Jiří (advisor)
This master thesis includes a comprehensive review of four-seater sport and leisure aircraft with focus on their cockpit instruments. The description of the selected glass cockpits is listed. Thesis also includes design of instrument panel, which is designed according to the relevant regulations and standard configuration of existing aircrafts. There is also a brief overview of the regulations necessary for the installation of these systems in the aircrafts. At the end of the this work is failure mode and effects analysis, with calculation of probability malfunction for critical functions.
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Haptic Feedback System and its Reliability
Horpatzká, Michaela ; Hlinka, Jiří (referee) ; Janhuba, Luboš (advisor)
This master thesis covers conceptual design of haptic feedback system and safety and reliability assessment. System is developed for aircraft categories UL2, EASA CS-LSA, EASA CS-VLA and EASA-CS-23. Conceptual design is divided into three parts. First is aimed on haptic system test with simulator. Second is conceptual design of haptic system for in-flight test. Third part contains safety and reliability assessment and summarizes problems of haptic system installation in real aircraft.
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Airliners Passenger Cabins
Janhuba, Luboš ; Dvořák, Milan (referee) ; Šošovička, Róbert (advisor)
Modern air traffic creates difficult needs for all type of airliners. Because increasing market demand high capacity is necessary. Increase of passengers brings enhance of board organization, emergency provision and passenger service. Purpose of this work is to introduce summary of using board organization and basic requirements.
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Modern avionics system architecture for EASA CS-23 airplane
Vaňousová, Jana ; Hlinka, Jiří (referee) ; Janhuba, Luboš (advisor)
This master thesis covers with the modern architecture of avionics system for EASA CS-23 AIRPL. The thesis contains EASA CS-23 and EU-OPS analysis and market analysis of avionics systems for this category of aircrafts. The thesis also includes the design of avionics system architecture and its safety and reliability assessment – used tool is Failure Mode and Effect Analysis (FMEA). At the end of the thesis there is assesment of potential attack of the avionics system by third part.
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Flying drones rescue systems
Hájek, Tomáš ; Janhuba, Luboš (referee) ; Pejchar, Jan (advisor)
This paper addresses the issue of security and integration of UAVs in air traffic operations and analyses possible risks. This work defines methodology to demonstrate airworthiness of the parachute recovery system under extreme climatic conditions. The first part of the methodology deals with the compliance performance requirements in external environment and the second part verifies performance parachute canopy. Methodology developed herein is subsequently verified by practical tests on parachute recovery system Galaxy GBS 10.
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The meaning and essence of aeronautical information services in civil aviation
Dubnický, Lukáš ; Janhuba, Luboš (referee) ; Chlebek, Jiří (advisor)
The aim of this thesis is to produce an integrated overview and characteristic of practices and activities which are implemented to provide aeronautical information service in Czech Republic. The main information source is the Czech aeronautical law L15 which meets ICAO Annex 15 requirements. Due to high level of standardization, a great deal of information related to aeronautical information services in the Czech Republic can be understood as generally correct for ICAO based systems of other states. Where possible theoretical information are connected with practical applications.
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Safety and Security of the Air Transport
Daško, Matúš ; Janhuba, Luboš (referee) ; Obuch, Matej (advisor)
The bachelor’s thesis is focused on the Aviation Security and Safety. The aim is to describe diversity of areas, providing basic information and refer to current projects and new trends especially in passenger control. The attention is given to both areas (Security and Safety) by international organisations, legislative and technical support and in conclusion by international exhibitions. In each area are selected accidents related to deficiencies in these areas.
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Proposal of electro-hydraulic control system for the nose gear of small transport aircraft
Vodička, Petr ; Janhuba, Luboš (referee) ; Třetina, Karel (advisor)
The diploma thesis is focused on design of electrohydraulic system for nose gear control on small civil airliners. First part consists of brief review of small civil airliners, nose gears and CS 23 restrictions relevant for the design. In practical part a typical small civil airliner is defined and kinematic of landing gear mechanisms is designed. Then the electrohydraulic system itself is designed and parameters of some components are suggested. The wheel steering mechanism is simulated and, in conclusion, the whole system is evaluated.
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Micro UAV certification for CR airspace
Sobotka, Vojtěch ; Janhuba, Luboš (referee) ; Pejchar, Jan (advisor)
This bachelor‘s thesis maps the unmanned aircraft system operation legislation valid in the Czech Republic. It contains a summaries of design and operation restrictions of these systems and radio frequency bands suitable for operating them. It deals with the matter of legal responsibility for damage caused by unmanned aircraft system operation and the matter of possible violation of personal data protection. It includes a summary of common EU unmanned aircraft system legislation and its expected future development. The preparation of the documentation necessary for VUT 720 unmanned airrcaft system registration and certification is also part of this thesis.
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Fusalage and Tail of Competition Model Airplane
Kminiaková, Tatiana ; Hájek, Tomáš (referee) ; Janhuba, Luboš (advisor)
This bachelor’s thesis deals with empennage and fuselage design of new aircraft for design competition SAE Aero Design East 2020. The introduction is focused on regulations of this competiton and their subsequent analysis. The research part of the thesis takes in consideration possible configurations of the empennage and fuselage and their basic parameters. The most suitable configurations are compared and basic stability and load calculations are done. In the last part structural design is completed.
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