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   The Methotodologies Of An Integrated Cad In The Design Of Mechanisms Of Electro-Actuators Used In Aircraft - Control Systems   [View] 
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 Author(s)   Alexander Urbah, Andrew Belovec, Amadou Coulibaly 
 Abstract   The peculiarities of Complex Mech-tronic Design of the aircraft control system on the basis of mechanisms with electro-actuators. The results of the design as well as the optimization of the structures by the means of CAD systems are targeted. The created 3-dimensions model of the actuator permitted to make number of analysis and optimization of its parts. Thus, static, dynamic, cinematic, equal-strength analysis have been done and optimization on the basic criteria of equalstrength, minimal weigh, rigidity and technology. 
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Filename:A82592
Filesize:181.1 KB
 Type   Members Only 
 Date   Last modified 2006-02-15 by System