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