Development of an Air Electric Compressor for a No-Bleed Environmental Control System of an Advanced Regional Aircraft
- 作者: Tishchenko I.V.1,2, Chizhikov V.E.1, Tsarkov I.A.3, Likhachev I.V.4, Moroshkin Y.V.4, Ovdienko M.A.5, Merkulov V.I.1,2
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隶属关系:
- Research and Production Association “Nauka”
- Bauman Moscow State Technical University
- Nauka-Energotech
- State Research Institute of Aviation Systems
- Central Institute of Aviation Motors
- 期: 卷 111, 编号 2 (2022)
- 页面: 115-122
- 栏目: Original Study Articles
- URL: https://freezetech.ru/0023-124X/article/view/110694
- DOI: https://doi.org/10.17816/RF110694
- ID: 110694
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详细
BACKGROUND: Aircraft designers strive to increase the fuel efficiency of aircrafts, including increasing the efficiency of aviation environmental control systems (ECS) by introducing an autonomous source of compressed air with an electric drive as part of aircraft.
AIM: The present paper aimed to consideration of the results of research work (R&D) of the technologies demonstrator for the electric compressor of the aircraft electric ECS and estimation of the performance and compliance of the simulated and experimental characteristics of this electric compressor.
MATERIALS AND METHODS: Comparison of the simulated and experimental characteristics of the electric compressor of the electric ECS of the aircraft was carried out by confirming the compliance of the operating parameters of the technologies demonstrator for the electric compressor with those specified in the request for proposals (RFP), and by comparing the simulated and experimental values of the compression ratio of the compressor stage, isentropic coefficient of performance (COP), obtained during R&D study.
RESULTS: Information about the technical characteristics and design of the electric compressor is given and discussed. A comparative analysis of the presented simulated and experimental characteristics of the electric compressor has been carried out.
CONCLUSIONS: Conclusions are drawn on the compliance of the compressor characteristics with the characteristics specified in the RFP; on the achieved level of readiness of the technology of the electric compressor for the electric ECS of the aircraft, on the need for experimental design work on the electric compressor, taking account of external influencing factors typical for an application as part of aviation equipment.
全文:
作者简介
Igor Tishchenko
Research and Production Association “Nauka”; Bauman Moscow State Technical University
编辑信件的主要联系方式.
Email: iv.tishenko@npo-nauka.ru
ORCID iD: 0000-0001-6094-8723
SPIN 代码: 5630-4301
Cand. Sci. (Tech.)
俄罗斯联邦, Moscow; MoscowVladimir Chizhikov
Research and Production Association “Nauka”
Email: ve.chizhikov@npo-nauka.ru
ORCID iD: 0000-0002-2114-2986
SPIN 代码: 2325-9450
俄罗斯联邦, Moscow
Igor Tsarkov
Nauka-Energotech
Email: ia.tsarkov@evogress.com
ORCID iD: 0000-0002-1188-7466
SPIN 代码: 9963-3666
俄罗斯联邦, Moscow
Igor Likhachev
State Research Institute of Aviation Systems
Email: ivlihachev@gosniias.ru
ORCID iD: 0000-0003-2813-9138
SPIN 代码: 6033-8689
Cand. Sci. (Tech.), Associate Professor
俄罗斯联邦, MoscowYaroslav Moroshkin
State Research Institute of Aviation Systems
Email: yvmoroshkin@2100.gosniias.ru
ORCID iD: 0000-0002-6274-3454
SPIN 代码: 9593-3384
Cand. Sci. (Tech.)
俄罗斯联邦, MoscowMaxim Ovdienko
Central Institute of Aviation Motors
Email: maovdienko@ciam.ru
ORCID iD: 0000-0003-2255-9430
SPIN 代码: 2575-3726
俄罗斯联邦, Moscow
Vladislav Merkulov
Research and Production Association “Nauka”; Bauman Moscow State Technical University
Email: merkulov@bmstu.ru
ORCID iD: 0000-0002-3455-3709
SPIN 代码: 8409-8754
Dr. Sci. (Tech.), Professor
俄罗斯联邦, Moscow; Moscow参考
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