Original title: Návrh podvozku pro letoun Rapid 600
Translated title: The Landing Gear design for RAPID 600 aircraft
Authors: Chren, Tibor ; Hlinka, Jiří (referee) ; Píštěk, Antonín (advisor)
Document type: Master’s theses
Year: 2010
Language: slo
Publisher: Vysoké učení technické v Brně. Fakulta strojního inženýrství
Abstract: [slo] [eng]
Táto práca sa zaoberá návrhom zaťahovacieho podvozku pre letún Rapid 600. Je v nej spracovaný rozbor a výber vhodných spôsobov zaťahovania pre predný aj hlavný podvozok. Práca sa ďalej zaoberá návrhom spôsobov ovládania zaťahovacieho podvozku, ktorá obsahuje aj návrh systému na automatické ovládanie podvozku, určuje funkcie a spôsob činnosti tohto systému. Jej súčasťou je aj analýza kritických režimov, ktoré systém dokáže odhaliť. This diploma thesis deals with design of retractable landing gear for Rapid 600 aircraft. The main purpose of this thesis is to analyze different retraction options for front and main landing gear and resulting selection of suitable variants. The thesis is consequently concerned with design of selected options including proposal of automatic landing gear control system and specifying the features and characteristics of this system. In the thesis there is also included the analysis of critical flight conditions which could be detected by this system.
Keywords: automatically controlled landing-gear; calculation of landing gear loading; critical flight conditions; engineering design; Rapid 600; retractable landing-gear; Ultra light aircraft

Institution: Brno University of Technology (web)
Document availability information: Fulltext is available in the Brno University of Technology Digital Library.
Original record: http://hdl.handle.net/11012/1578

Permalink: http://www.nusl.cz/ntk/nusl-578271


The record appears in these collections:
Universities and colleges > Public universities > Brno University of Technology
Academic theses (ETDs) > Master’s theses