Radial two-stage microturbine for pneumatic actuation


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An innovative kinematic scheme of pneumatic turbine drive was proposed and the use of two-row centrifugal-centripetal turbine stage was justified. We proved the feasibility of the proposed kinematic scheme of the turbine drive in a variety of aircraft components by an example of the manual pneumatic grinding machine.

作者简介

Yu. Kuznetsov

R.E. Alekseev Nizhny Novgorod State Technical University

Email: tseu@nntu.nnov.ru
俄罗斯联邦, ul. Minina 24, Nizhny Novgorod, 603950

V. Khimich

R.E. Alekseev Nizhny Novgorod State Technical University

Email: tseu@nntu.nnov.ru
俄罗斯联邦, ul. Minina 24, Nizhny Novgorod, 603950

S. Khrunkov

R.E. Alekseev Nizhny Novgorod State Technical University

Email: tseu@nntu.nnov.ru
俄罗斯联邦, ul. Minina 24, Nizhny Novgorod, 603950

A. Krainov

R.E. Alekseev Nizhny Novgorod State Technical University

编辑信件的主要联系方式.
Email: tseu@nntu.nnov.ru
俄罗斯联邦, ul. Minina 24, Nizhny Novgorod, 603950

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