Email this article Radial two-stage microturbine for pneumatic actuation
- Authors: Kuznetsov Y.P.1, Khimich V.L.1, Khrunkov S.N.1, Krainov A.A.1
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Affiliations:
- R.E. Alekseev Nizhny Novgorod State Technical University
- Issue: Vol 59, No 2 (2016)
- Pages: 283-286
- Section: Aircraft Production Technology
- URL: https://journals.rcsi.science/1068-7998/article/view/229714
- DOI: https://doi.org/10.3103/S1068799816020215
- ID: 229714
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Abstract
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.
About the authors
Yu. P. Kuznetsov
R.E. Alekseev Nizhny Novgorod State Technical University
Email: tseu@nntu.nnov.ru
Russian Federation, ul. Minina 24, Nizhny Novgorod, 603950
V. L. Khimich
R.E. Alekseev Nizhny Novgorod State Technical University
Email: tseu@nntu.nnov.ru
Russian Federation, ul. Minina 24, Nizhny Novgorod, 603950
S. N. Khrunkov
R.E. Alekseev Nizhny Novgorod State Technical University
Email: tseu@nntu.nnov.ru
Russian Federation, ul. Minina 24, Nizhny Novgorod, 603950
A. A. Krainov
R.E. Alekseev Nizhny Novgorod State Technical University
Author for correspondence.
Email: tseu@nntu.nnov.ru
Russian Federation, ul. Minina 24, Nizhny Novgorod, 603950
