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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

  • Czech description

Classification

  • Type

    J<sub>imp</sub> - Article in a specialist periodical, which is included in the Web of Science database

  • CEP classification

  • 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