Masterarbeit, 2019
83 Seiten, Note: 1,5
1. Introduction
2. Electrical Vertical Take-Off and Landing Concepts
2.1 Vertical Take-Off and Landing Overview
2.2 Methodology to Concept Analysis
2.3 The Lilium Jet
2.3.1 Technological Concept
2.3.2 Safety
2.3.3 Critical Analysis
2.4 Airbus A³ Vahana
2.4.1 Technological Concept
2.4.2 Safety
2.4.3 Critical Analysis
2.5 Aurora Flight Sciences Passenger Air Vehicle
2.5.1 Technological Concept
2.5.2 Safety
2.5.3 Critical Analysis
2.6 Kitty Hawk Cora
2.6.1 Technological Concept
2.6.2 Safety
2.6.3 Critical Analysis
2.7 Comparison of the Different Concepts
3. Key Technology Challenges
3.1 Batteries
3.2 Noise Pollution
3.3 Autonomous flying
4. Key Legislative Challenges
4.1 Organization of Aviation Law
4.2 Amendments to enable eVTOL Aircraft Operations
5. Conclusion
6. Outlook
This Master's Thesis evaluates whether flying cars—specifically electrical Vertical Take-Off and Landing (eVTOL) aircraft—possess a realistic potential to alleviate overloaded ground transportation infrastructure within a mid-term ten-year timeframe.
2.3.1 Technological Concept
The Lilium Jet should be created as a five-seater eVTOL aircraft without the disadvantages of existing VTOL alternatives like helicopters which are comparably slow but at the same time have a high fuel consumption (15). So Liliums objective was clear – they wanted to ‘define a transition aircraft concept with better performance in safety, noise, speed, range and payload than existing concepts’ (16). Simultaneously they aim to reduce the complexity to one third compared to VTOL alternatives.
The jet generally consists of a fuselage with two rigid wings, one in the front of the aircraft and a longer one at the back (16). The wings include 12 moveable flaps, four on the smaller one in the front and eight on the bigger one in the back. Each flap then again consists of three electric jet engines. This functionality enables the Lilium Jet to adjust the flaps and thus also the engines depending on the respective flight mode. In order to take-off the flaps are tilted vertically to lift the jet. Once the required flight altitude is reached, the flaps gradually tilt into a horizontal position and the aircraft gathers speed. In cruise mode, i. e. in a full horizontal position of the flaps and engines, all lift which is necessary to keep the jet airborne, is provided by the pair of wings. Lilium calls that ‘high-lift system’. Its objective is to increase the lift even at lower speed. This will be supported by the engines which are designed in an aerodynamic manner to ensure a very low drag coefficient during cruise flight.
1. Introduction: Introduces the rising problem of urban traffic congestion and proposes eVTOL aircraft as a potential solution, outlining the research objective and scope.
2. Electrical Vertical Take-Off and Landing Concepts: Provides an overview of various VTOL groups and conducts a detailed, structured analysis of the four most mature concepts (Lilium, Vahana, Aurora PAV, Cora).
3. Key Technology Challenges: Analyzes the fundamental technical obstacles for widespread eVTOL adoption, specifically focusing on energy density in batteries, noise pollution, and the hurdles of autonomous flight.
4. Key Legislative Challenges: Examines the regulatory landscape and the necessary amendments to aviation law in Europe, the US, and New Zealand to facilitate eVTOL operations.
5. Conclusion: Summarizes the findings, confirming the potential of eVTOL aircraft while noting the significant technical and regulatory challenges that remain.
6. Outlook: Discusses the necessity for continued stakeholder management, manufacturing scalability, and future research to ensure the successful integration of air taxis into urban environments.
eVTOL, Urban Air Mobility, Flying Cars, Battery Technology, Noise Pollution, Autonomous Flight, Aviation Law, EASA, FAA, Lilium Jet, Airbus Vahana, Aurora PAV, Kitty Hawk Cora, Infrastructure, Transportation
The thesis evaluates the potential of electrical Vertical Take-Off and Landing (eVTOL) aircraft to act as a viable alternative for urban ground transportation infrastructure within the next ten years.
The work identifies three major hurdles: battery technology limitations (energy density), noise pollution levels, and the complexities regarding autonomous flight certification.
The main objective is to analyze whether flying cars can realistically improve overloaded ground transportation systems on a mid-term, ten-year basis.
The author conducted qualitative research, including database analysis, a comparative content analysis of the four most mature aircraft concepts, and a review of relevant legal texts and aviation regulations.
The main section covers an overview of VTOL groups, detailed technical and safety analysis of four specific aircraft models (Lilium, Vahana, Aurora, Cora), and an evaluation of key technology and legislative barriers.
Key terms include eVTOL, Urban Air Mobility, battery density, aircraft noise, autonomous systems, and aviation certification frameworks.
The Lilium Jet is ranked first, primarily because its piloted approach is seen as a major advantage for gaining public trust and satisfying regulatory requirements compared to concepts focusing solely on autonomy.
The legislative framework is a critical bottleneck. The author highlights that while agencies like EASA are making progress with specific conditions, harmonized global regulations are still in the early stages and required to enable safe urban operations.
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