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Návrh podvozku pro letoun Rapid 600 / The Landing Gear design for RAPID 600 aircraft

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.

Identiferoai:union.ndltd.org:nusl.cz/oai:invenio.nusl.cz:229317
Date January 2010
CreatorsChren, Tibor
ContributorsHlinka, Jiří, Píštěk, Antonín
PublisherVysoké učení technické v Brně. Fakulta strojního inženýrství
Source SetsCzech ETDs
LanguageSlovak
Detected LanguageEnglish
Typeinfo:eu-repo/semantics/masterThesis
Rightsinfo:eu-repo/semantics/restrictedAccess

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