Experience with the design of ultralight airplane with unconventional powerplant
The result's identifiers
Result code in IS VaVaI
<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F68407700%3A21220%2F18%3A00327879" target="_blank" >RIV/68407700:21220/18:00327879 - isvavai.cz</a>
Result on the web
<a href="https://journals.sagepub.com/doi/full/10.1177/0954410018774117" target="_blank" >https://journals.sagepub.com/doi/full/10.1177/0954410018774117</a>
DOI - Digital Object Identifier
<a href="http://dx.doi.org/10.1177/0954410018774117" target="_blank" >10.1177/0954410018774117</a>
Alternative languages
Result language
angličtina
Original language name
Experience with the design of ultralight airplane with unconventional powerplant
Original language description
Ducted fan-powered ultralight (UL) aircraft UL-39 Albi has been developed at the Department of Aerospace Engineering at Faculty of Mechanical Engineering of the Czech Technical University in Prague. The aircraft was manufactured by the companies LA Composite, s.r.o. and JIHLAVAN Airplanes, s.r.o. The development was funded by the Ministry of Education and the Ministry of Industry and Trade of the Czech Republic. The airframe is fully made of composite materials, mainly carbon fibre/epoxy resin prepregs, and was cured in autoclave. The design contains many unconventional features. These were necessary to meet legal requirements (i.e. maximum take-off weight and maximum landing speed) and to achieve high flight performance. This puts extreme demands to both maximisation of propulsion efficiency and minimisation of airframe and powerplant weight. This paper presents more than fifteen years’ experience with design of ducted fan powered ultralight aircraft. Some solutions of design trade-offs are presented, namely integration of engine into the fuselage, carbon composite blade design and lightweight airframe design.
Czech name
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Czech description
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Classification
Type
J<sub>imp</sub> - Article in a specialist periodical, which is included in the Web of Science database
CEP classification
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OECD FORD branch
20304 - Aerospace engineering
Result continuities
Project
<a href="/en/project/EF16_019%2F0000826" target="_blank" >EF16_019/0000826: Center of Advanced Aerospace Technology</a><br>
Continuities
P - Projekt vyzkumu a vyvoje financovany z verejnych zdroju (s odkazem do CEP)
Others
Publication year
2018
Confidentiality
S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů
Data specific for result type
Name of the periodical
Proceedings of the Institution of Mechanical Engineers, Part G; Journal of Aerospace Engineering
ISSN
0954-4100
e-ISSN
2041-3025
Volume of the periodical
232
Issue of the periodical within the volume
14
Country of publishing house
GB - UNITED KINGDOM
Number of pages
13
Pages from-to
2721-2733
UT code for WoS article
000450355700012
EID of the result in the Scopus database
2-s2.0-85047386582