Abstract
Power electronics are an enabling technology for the electrification of aircraft power and propulsion systems. The higher integration of power electronics will lead to new fault modes, including cascading faults. To facilitate the design of resilient electrified systems with appropriate electrical fault management and limit future aircraft accidents, identification of the probability and severity of cascading faults linked to the implementation of necessary and effective fault management methods is required. This paper proposes a framework for the prioritisation of fault management methods to address cascading faults in state-of-the-art and future aircraft. Air accident investigation reports provide the datasets for the framework. The key elements and considerations of the framework are outlined, including terminology, dataset information, dataset format, probability and severity of cascading fault modes, visualisation, and future aircraft assumptions. Within the framework, bowtie diagrams demonstrate the link between fault modes and fault management strategies. The framework is applied to a case study of the electrical wiring and interconnection system.
| Original language | English |
|---|---|
| Title of host publication | 2025 IEEE Workshop on Power Electronics for Aerospace Applications (PEASA) |
| Place of Publication | Piscataway, NJ |
| Publisher | IEEE |
| Number of pages | 6 |
| ISBN (Electronic) | 979-8-3315-8926-4 |
| ISBN (Print) | 979-8-3315-8927-1 |
| Publication status | Published - 29 Sept 2025 |
| Event | 2025 Workshop on Power Electronics for Aerospace Applications (PEASA): Electrical Systems - University of Strathclyde, Glasgow, United Kingdom Duration: 23 Jul 2025 → 24 Jul 2025 https://www.peasa25.org/ |
Conference
| Conference | 2025 Workshop on Power Electronics for Aerospace Applications (PEASA) |
|---|---|
| Abbreviated title | PEASA 2025 |
| Country/Territory | United Kingdom |
| City | Glasgow |
| Period | 23/07/25 → 24/07/25 |
| Internet address |
Funding
This work was undertaken as part of an EPSRC PhD Studentship (2918820) with support from Vertical Aerospace Plc and the National Manufacturing Institute Scotland.
Keywords
- fault management
- future hybrid/electric aircraft
- bowtie diagram