Working out of pressure stabilizer for aircraft, test bench, and technical systems

Аuthors

Lalabekov V. I.^*, Pestunov V. A., Samsonovich S. L.^**

Moscow Aviation Institute (National Research University), 4, Volokolamskoe shosse, Moscow, А-80, GSP-3, 125993, Russia

*e-mail: Lalabekov.Valentin@yandex.ru
**e-mail: samsonovich40@mail.ru

Abstract

In the article the features of new type pressure stabilizer are considered, its operation principle, design realization, mathematic model, results of mathematic modeling and experimental researching the operation of the pressure stabilizer for aircraft, test bench and technical systems. The stabilizer is constructed on the base of using the energy of disturbance impulses itselves.

Keywords:

ppressure stabilizer, hydro blow, disturbance impulse, hydro (pneumatic) system, pressure self-stabilizer, pressure accumulater