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1 lut 2021 · The aircraft landing gear and its associated systems represent a compelling design challenge: simultaneously a system, a structure, and a machine, it supports the aircraft on the ground,...
This paper describes the experience in designing the front main landing gear strut for a light multipurpose aircraft using up-to-date methods of numerical simulation. The main landing gear strut is one of the most critical and loaded aircraft components.
Learn more how to Design the Main Landing Gear Spring and select the proper Tire for the Light Airplane (regulated by FAR/CS 23). Energy Balance equation solution and non-linear deformations derivation procedure is described in details.
Abstract. Light aircrafts are designed to be used in both developed and undeveloped areas of a country. Hard landing conditions such as shocks and rebounds may occur. In this context, a good, efficient, robust and easy to maintain landing gear is vital.
Aircraft landing gears have three main functions: allow the aircraft to move on the ground, take off run, absorb the landing bump and braking. During cruise they have no function, so that they are often retraced or in some cases they are even dropped after take off. Landing gear design is ruled by a set or requirements.
Objective: Design the landing gear for a CESTOL type aircraft according to FAR 23 using: (i) the conceptual designs of the nose and main gear and (ii) evaluate the structural strength of the design …
22 sie 2012 · The book provides a vital link in landing gear design technology from historical practices to modern design trends, and it considers the necessary airfield interface with landing gear design. The text is backed up by calculations, specifications, references, working examples, and nearly 300 illustrations.