DESIGN AND CALCULATION OF TAKE-OFF AND LANDING GEAR FOR AIRPLANE WITH TAKE-OFF WEIGHT OF 2 000 KG

Abstract

The thesis describes the design of landing gear for aircraft weighing to 2,000 kg. Explaining basic terms related to the issue and concept of the chassis design for the proposed aircraft, classified according to regulation CS-23. A separate bonding calculation is carried out by Creo Parametric CAD program. For designed airplane was chosen as the best variant type of three-gear-wheel landing gear with the front landing gear.