Radial two-stage microturbine for pneumatic actuation
- Авторлар: Kuznetsov Y.P.1, Khimich V.L.1, Khrunkov S.N.1, Krainov A.A.1
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Мекемелер:
- R.E. Alekseev Nizhny Novgorod State Technical University
- Шығарылым: Том 59, № 2 (2016)
- Беттер: 283-286
- Бөлім: Aircraft Production Technology
- URL: https://journals.rcsi.science/1068-7998/article/view/229714
- DOI: https://doi.org/10.3103/S1068799816020215
- ID: 229714
Дәйексөз келтіру
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.
Негізгі сөздер
Авторлар туралы
Yu. Kuznetsov
R.E. Alekseev Nizhny Novgorod State Technical University
Email: tseu@nntu.nnov.ru
Ресей, ul. Minina 24, Nizhny Novgorod, 603950
V. Khimich
R.E. Alekseev Nizhny Novgorod State Technical University
Email: tseu@nntu.nnov.ru
Ресей, ul. Minina 24, Nizhny Novgorod, 603950
S. Khrunkov
R.E. Alekseev Nizhny Novgorod State Technical University
Email: tseu@nntu.nnov.ru
Ресей, ul. Minina 24, Nizhny Novgorod, 603950
A. Krainov
R.E. Alekseev Nizhny Novgorod State Technical University
Хат алмасуға жауапты Автор.
Email: tseu@nntu.nnov.ru
Ресей, ul. Minina 24, Nizhny Novgorod, 603950
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