Conceptual design analysis for a lightweight aircraft with a fuel cell hybrid propulsion system
Yazarlar (4)
Prof. Dr. Hüseyin Turan ARAT İskenderun Teknik Üniversitesi, Türkiye
Meryem Gizem Sürer
Iskenderun Technical University, Türkiye
Iskenderun Technical University, Türkiye
Semir Gökpınar
İskenderun Teknik Üniversitesi, Türkiye
İskenderun Teknik Üniversitesi, Türkiye
Kadir Aydın Çukurova Üniversitesi, Türkiye
| Makale Türü | Özgün Makale (SSCI, AHCI, SCI, SCI-Exp dergilerinde yayınlanan tam makale) | ||
| Dergi Adı | Energy Sources Part A Recovery Utilization and Environmental Effects (Q2) | ||
| Dergi ISSN | 1556-7036 Dergi Bilgileri (2020) | ||
| Dergi Tarandığı Indeksler | SCI-Expanded | ||
| Makale Dili | İngilizce | Basım Tarihi | 06-2020 |
| Cilt / Sayı / Sayfa | 45 / 1 / 46–60 | DOI | 10.1080/15567036.2020.1773966 |
| Makale Linki | http://dx.doi.org/10.1080/15567036.2020.1773966 | ||
| UAK Araştırma Alanları |
Enerji
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| Özet |
| With the ever-growing aviation industry, energy researches on aviation have turned to renewable energy sources providing electric propulsion. Fuel cells are one of the most popular sources of power for electric vehicles terms of being greener, more reliability, and higher efficiency. Among fuel cells, the most attractive option for flight is polymer electrolyte membrane fuel cells (PEMFC). This paper aims to compose of a hybrid propulsion system to a lightweight aircraft Cri-Cri for more electric aircraft concept. For this purpose, first, conceptual a hybrid propulsion system is designed for the prototype aircraft. The fuel-cell hybrid system proposed for this paper consists of electric motor, fuel cell system, battery, DC/AC converter, and DC/DC converter. Second, some analyses are done. These analyses contain required power, hydrogen consumption, energy consumption, etc.. As a result, Cri-cri needs 26 Kw during take-off … |
| Anahtar Kelimeler |
| aviation | battery | conceptual design | Cri Cri | hybridization | PEMFC |
BM Sürdürülebilir Kalkınma Amaçları
| Atıf Sayıları | |
| Web of Science | 35 |
| Scopus | 39 |
| Google Scholar | 62 |