Development, research and production of a centrifugal impeller

作者: Gureev V.¹, Salakhov R.¹, Falyakhov M.¹, Kudusov D.², Burlakov V.³
隶属关系:
1. Tupolev Kazan National Research Technical University
2. All-Russia Research Institute of Flow Metering (FGUP VNIIR)
3. OAO KAMAZ
期: 卷 59, 编号 1 (2016)
页面: 69-76
栏目: Aircraft and Rocket Engine Design and Development
URL: https://journals.rcsi.science/1068-7998/article/view/229569
DOI: https://doi.org/10.3103/S1068799816010116
ID: 229569

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The authors conducted a detailed study of possible options for geometry of blades with pressure and power characteristics of the impeller.

centrifugal impeller, blade, pump, pressure

Tupolev Kazan National Research Technical University

编辑信件的主要联系方式.
Email: viktor.gureev@kai.ru
俄罗斯联邦, ul. Karla Marksa 10, Kazan, 420111

Tupolev Kazan National Research Technical University

Email: viktor.gureev@kai.ru
俄罗斯联邦, ul. Karla Marksa 10, Kazan, 420111

Tupolev Kazan National Research Technical University

Email: viktor.gureev@kai.ru
俄罗斯联邦, ul. Karla Marksa 10, Kazan, 420111

All-Russia Research Institute of Flow Metering (FGUP VNIIR)

Email: viktor.gureev@kai.ru
俄罗斯联邦, ul. Vtoraya Azinskaya 7a, Kazan, 420088

OAO KAMAZ

Email: viktor.gureev@kai.ru
俄罗斯联邦, pr. Avtozavodskii 2, Naberezhnye Chelny, 423827