Radial two-stage microturbine for pneumatic actuation
- Авторы: Kuznetsov Y.P.1, Khimich V.L.1, Khrunkov S.N.1, Krainov A.A.1
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Учреждения:
- R.E. Alekseev Nizhny Novgorod State Technical University
- Выпуск: Том 59, № 2 (2016)
- Страницы: 283-286
- Раздел: 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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Аннотация
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.
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Об авторах
Yu. Kuznetsov
R.E. Alekseev Nizhny Novgorod State Technical University
Email: tseu@nntu.nnov.ru
Россия, ul. Minina 24, Nizhny Novgorod, 603950
V. Khimich
R.E. Alekseev Nizhny Novgorod State Technical University
Email: tseu@nntu.nnov.ru
Россия, ul. Minina 24, Nizhny Novgorod, 603950
S. Khrunkov
R.E. Alekseev Nizhny Novgorod State Technical University
Email: tseu@nntu.nnov.ru
Россия, ul. Minina 24, Nizhny Novgorod, 603950
A. Krainov
R.E. Alekseev Nizhny Novgorod State Technical University
Автор, ответственный за переписку.
Email: tseu@nntu.nnov.ru
Россия, ul. Minina 24, Nizhny Novgorod, 603950
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