Abstract

In the work the structural scheme of nano piezoengine with lumped parameters is determined for aerospace. The PZT nano engines have small dimensions, high accuracy, simple design. Calculation of structural scheme nano piezoengine with lumped parameters was made at voltage and current control for aerospace. Method mathematical physics is used for calculation of structural scheme nano piezoengine. Schemes nano piezoengines with lumped parameters at voltage and current control for aerospace are determined.

Keywords

nano piezoengine, structural scheme, aerospace