An Optimization of a Four-bar Linkage for control of trailing-edge flap

Result code in IS VaVaI
<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F68407700%3A21220%2F14%3A00226599" target="_blank" >RIV/68407700:21220/14:00226599 - isvavai.cz</a>
Result on the web
<a href="http://vx439500.server37.viwefix.cz/magazines/inbrowser.aspx?id=43" target="_blank" >http://vx439500.server37.viwefix.cz/magazines/inbrowser.aspx?id=43</a>
DOI - Digital Object Identifier
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Result language
angličtina
Original language name
An Optimization of a Four-bar Linkage for control of trailing-edge flap
Original language description
This paper deals with an option and use of evaluation criteria for design of a trailing-edge flap four bar linkage of an ultralight aircraft. A design procedure of individual mechanism variants is described briefly first. A description of chosen evaluation criteria and a simplified procedure of flap loading prediction, which is important for mechanism evaluation in view of actuation loads on rotary actuator, are described next. Survey of some designed variants of mechanisms, evaluated parameters and mention of next works course are described at the end of this paper.
Czech name
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Czech description
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Type
J<sub>x</sub> - Unclassified - Peer-reviewed scientific article (Jimp, Jsc and Jost)
CEP classification
JU - Aeronautics, aerodynamics, aeroplanes
OECD FORD branch
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Project
<a href="/en/project/FR-TI3%2F527" target="_blank" >FR-TI3/527: Ducted Fan Ultralight Aircraft</a><br>
Continuities
P - Projekt vyzkumu a vyvoje financovany z verejnych zdroju (s odkazem do CEP)

Publication year
2014
Confidentiality
S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů

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