Reliability Allocation Method for Electric Aircraft Lightweight Propulsion System
In order to solve the contradiction between lightweight and high reliability in the electric aircraft electric propulsion system, a reliability allocation method considering lightweight constraint is proposed for the first time. An analytical expression between weight and reliability is integrated i...
| الحاوية / القاعدة: | Shanghai Jiaotong Daxue xuebao |
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| المؤلف الرئيسي: | |
| التنسيق: | مقال |
| اللغة: | الصينية |
| منشور في: |
Editorial Office of Journal of Shanghai Jiao Tong University
2025-06-01
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| الموضوعات: | |
| الوصول للمادة أونلاين: | https://xuebao.sjtu.edu.cn/article/2025/1006-2467/1006-2467-59-6-867.shtml |