The adjustment of discharge and spray in fuel injectors of aircraft engines
- Authors: Smolentsev V.P.1, Safonov S.V.1, Koptev I.I.1
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Affiliations:
- Voronezh State Technical University
- Issue: Vol 59, No 4 (2016)
- Pages: 571-578
- Section: Aircraft and Rocket Engine Design and Development
- URL: https://journals.rcsi.science/1068-7998/article/view/229920
- DOI: https://doi.org/10.3103/S1068799816040218
- ID: 229920
Cite item
Abstract
The paper deals with the technology of adjusting the parameters of injectors operating jointly in fuel supply units of jet and rocket engines. We present the new techniques and devices that are used for adjusting the discharge and spray of components. We developed the technology of combined processing of the flow duct that, for the first time, allowed reducing the area of small-size injector openings and shape the channels with a propelling nozzle configuration.
About the authors
V. P. Smolentsev
Voronezh State Technical University
Author for correspondence.
Email: vsmolen@inbox.ru
Russian Federation, prospekt Moskovskii 14, Voronezh, 394026
S. V. Safonov
Voronezh State Technical University
Email: vsmolen@inbox.ru
Russian Federation, prospekt Moskovskii 14, Voronezh, 394026
I. I. Koptev
Voronezh State Technical University
Email: vsmolen@inbox.ru
Russian Federation, prospekt Moskovskii 14, Voronezh, 394026