Koncepční návrh letounu general aviation na elektrický pohon
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Date
Authors
ORCID
Advisor
Referee
Mark
C
Journal Title
Journal ISSN
Volume Title
Publisher
Vysoké učení technické v Brně. Fakulta strojního inženýrství
Abstract
The design of electric aircraft represents an opportunity in the aviation field by offering promising advancements in terms of efficiency and sustainability. This project aims to explore the feasibility of designing a purely electric aircraft at a time when electric mobility is widespread in the automotive sector but not yet in the aviation industry. It will encompass the study of marketing and the market field, as well as the performance characteristics of the model, including the calculation of aircraft surfaces, with the goal of achieving the most realistic project possible.
The design of electric aircraft represents an opportunity in the aviation field by offering promising advancements in terms of efficiency and sustainability. This project aims to explore the feasibility of designing a purely electric aircraft at a time when electric mobility is widespread in the automotive sector but not yet in the aviation industry. It will encompass the study of marketing and the market field, as well as the performance characteristics of the model, including the calculation of aircraft surfaces, with the goal of achieving the most realistic project possible.
The design of electric aircraft represents an opportunity in the aviation field by offering promising advancements in terms of efficiency and sustainability. This project aims to explore the feasibility of designing a purely electric aircraft at a time when electric mobility is widespread in the automotive sector but not yet in the aviation industry. It will encompass the study of marketing and the market field, as well as the performance characteristics of the model, including the calculation of aircraft surfaces, with the goal of achieving the most realistic project possible.
Description
Citation
CERVERA, I. Koncepční návrh letounu general aviation na elektrický pohon [online]. Brno: Vysoké učení technické v Brně. Fakulta strojního inženýrství. 2023.
Document type
Document version
Date of access to the full text
Language of document
en
Study field
bez specializace
Comittee
doc. Ing. Jaroslav Juračka, Ph.D. (předseda)
doc. Ing. Jiří Hlinka, Ph.D. (místopředseda)
doc. Ing. Ivo Jebáček, Ph.D. (člen)
Ing. Robert Popela, Ph.D. (člen)
Ing. Miroslav Šplíchal, Ph.D. (člen)
Ing. Pavel Zikmund, Ph.D. (člen)
Date of acceptance
2023-06-19
Defence
The student first presented the results he achieved in his work. The committee then got to know the assessment of the supervisor and reviewer. The student then answered the reviewer's questions and other questions from the committee.
Q1: What is the reason to use the negative swept angle on the wing and the swept back angle on the horizontal tail?
A1: It is used to reduce drag. It wasn't planned on the wing. Inspiration by Shark.
Q2: How is the maximum revolution for the propeller defined?
A2: Not to overcome the supersonic speed at the tip of the propeller. No propeller was defined.
Q3: Pros and cons of the two-seater configuration.
A3: Advantage is to decrease the frontal cross-section area. Disadvantage to control the aerodynamic center.
Q4: How to manage the fire of a battery? What is the weight of the battery?
A4: Protection by non-flammable materials. Battery has 330 kilograms.
Based on the opinion of the reviewer´s and the supervisor's assessment, the presentation and the student's answers to the questions, the committee decided to rate the work with a grade of C, good.
Result of defence
práce byla úspěšně obhájena
Document licence
Standardní licenční smlouva - přístup k plnému textu bez omezení