عنوان المقالة: Assembly/disassembly of a high-pressure line of a modern aero-engine
طيار مهندس/ محمد الشعلان | Capt. Mehmed asch-Schaalan | 5318
Publication Type
Standard
Arabic Authors
طيار مهندس/ محمد الشعلان، نويليا نونيز، ساشين ناجاراجا، فرانسيسكو لوبيز
English Authors
Mehmed asch-Schaalan, Noelia Nunez, Sachin Nagaraja, Francisco Lopez
Abstract
This measurement will deep dive into two elements of the high pressure body of the DGEN 380, the centrifugal compressor and the axial turbine, as well as in other fundamental components such as bearings and the lubrication system. Further reasoning with regards to energy transfer, temperature evolution, entropy and degree of reaction will be issued. Finally, the material selection for the compressor and turbine will explored.
Publication Date
6/16/2021
Publisher
جامعة بروكسل الحرة "BRUFACE"
Volume No
Issue No
DOI
10.13140/RG.2.2.18204.82560
File Link
تحميل (1 مرات التحميل)
External Link
https://www.researchgate.net/publication/352786800_Assemblydisassembly_of_a_high-pressure_line_of_a_modern_aero-engine
Keywords
Aero engine, engine, aeronautics, modern, compressor, turbine, energy, system, temperature
رجوع