This diploma thesis describes the design of retractable landing gear for the NG-4 ultralight aircraft. Its main part consists of general principle of gear retraction, kinematics analysis, load calculation and structural analysis, material selection and means of controlling by pilot. The thesis contents marginally the typology of aircraft landing gears and their evolution.
| Identifer | oai:union.ndltd.org:nusl.cz/oai:invenio.nusl.cz:229467 |
| Date | January 2011 |
| Creators | Bartoněk, Jaroslav |
| Contributors | Plhal, Martin, Matěják, Vladimír |
| Publisher | Vysoké učení technické v Brně. Fakulta strojního inženýrství |
| Source Sets | Czech ETDs |
| Language | Czech |
| Detected Language | English |
| Type | info:eu-repo/semantics/masterThesis |
| Rights | info:eu-repo/semantics/restrictedAccess |
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