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The Methotodologies Of An Integrated Cad In The Design Of Mechanisms Of Electro-Actuators Used In Aircraft - Control Systems
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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 |
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Type |
Members Only |
Date |
Last modified 2006-02-15 by System |
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