|
|
Landing gear design for single-engine four-seat aircraft
Pauliny, Jozef ; Vaněk, František (oponent) ; Juračka, Jaroslav (vedoucí práce)
The purpose of this project is the design of a fixed tricycle landing gear for a single-engine, four-seat, all composite airplane adhering to the CS-23 Certification Specifications, by which it is intended to be certified. This includes the design of composite spring main landing gear struts, in combination with an oleo nose landing gear strut. The design process is divided into five specific phases; design requirements, preliminary design, detailed design, production planning, and prototype testing. Individual load condition are calculated in the preliminary design phase. The detailed design includes stress analysis of individual components. The prototype testing phase defines an acceptable method used to prove compliance with certification specifications. The study concludes with detailed technical documentation.
|
host ::
RSS.