Tests of the low emission combustion chambers compartment with pressure and pressure–air assist atomizers
- Authors: Maslov V.P.1, Mashinistova N.P.1, Sviridenkov A.A.1, Jagodkin V.I.1
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Affiliations:
- Central Institute of aviation engine production named after P. I. Baranov, Moscow
- Issue: Vol 10, No 5 (2011)
- Pages: 162-167
- Section: ISSUE WITHOUT SECTION
- URL: https://journals.ssau.ru/vestnik/article/view/2756
- DOI: https://doi.org/10.18287/2541-7533-2011-0-5(29)-162-167
- ID: 2756
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Abstract
For the purpose of improvement of ecological and resource characteristics of the existing civil aircraft a front module of a combustion chamber with a combined centrifugal air-atomizing burner is developed. High completeness of fuel combustion, satisfactory range of steady burning, low emission of unburned hydrocarbons, carbon oxide and reduced emission of nitric oxide in the modified version of a combustion chamber with a combined atomizer is experimentally confirmed.
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About the authors
V. P. Maslov
Central Institute of aviation engine production named after P. I. Baranov, Moscow
Author for correspondence.
Email: vorobeev@ciam.ru
Chief of Sector
Russian FederationN. P. Mashinistova
Central Institute of aviation engine production named after P. I. Baranov, Moscow
Email: sviriden@ciam.ru
Leading Engineer
Russian FederationA. A. Sviridenkov
Central Institute of aviation engine production named after P. I. Baranov, Moscow
Email: sviriden@ciam.ru
Leading Engineer
Russian FederationV. I. Jagodkin
Central Institute of aviation engine production named after P. I. Baranov, Moscow
Email: yagodkin@ciam.ru
Candidate of Technical Sciences
Chief of Sector
Russian Federation