Open hydrostatic drive for gyroplane rotor starting

Aviation technics and technology


Аuthors

Mishchenko V. Y.

,

e-mail: vicl03@mai.ru

Abstract

The article suggests a method of defining design and hydrodynamic parameters of hydrostatic drive, occasionally operating in conditions of significant inertia and positional load. As a simulation case there has been chosen the process of gyroplane rotor starting, there have been defined main parameters of the drive. There has been obtained existence domain of hydrostatic drive project.

Keywords:

gyroplane; pump; relief valve; hydromotor; return valve; delivery pressure; reservoir pressure; heat liberation.


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