Automated Belt Grinding of Axial-Compressor Blades in Gas-Turbine Engines
- Авторлар: Poletaev V.A.1, Volkov D.I.1
-
Мекемелер:
- Solov’ev Rybinsk State Aviation-Engineering University
- Шығарылым: Том 39, № 7 (2019)
- Беттер: 594-597
- Бөлім: Article
- URL: https://journal-vniispk.ru/1068-798X/article/view/227753
- DOI: https://doi.org/10.3103/S1068798X19070177
- ID: 227753
Дәйексөз келтіру
Аннотация
The finishing of the flow sections of compressor blades is considered. A sequence of operations for this purpose in an automated cycle is proposed. The development of control programs for the grinding of flow sections of the blades is discussed, with allowance for the nonuniform distribution of the margin over the blade surface.
Авторлар туралы
V. Poletaev
Solov’ev Rybinsk State Aviation-Engineering University
Хат алмасуға жауапты Автор.
Email: poletaev@rsatu.ru
Ресей, Rybinsk
D. Volkov
Solov’ev Rybinsk State Aviation-Engineering University
Хат алмасуға жауапты Автор.
Email: prorectnir@rsatu.ru
Ресей, Rybinsk
Қосымша файлдар
