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  5. Prototyping and evaluation of a fault-tolerant three-level TNPC inverter for aircraft propulsion

Prototyping and evaluation of a fault-tolerant three-level TNPC inverter for aircraft propulsion

Publication date
2025-06-30
Document type
Konferenzbeitrag
Author
Chaisakdanugull, Chanuch  
Sprätz, Bengt O. S.
Hoffmann, Klaus  
Organisational unit
Leistungselektronik  
DOI
10.30420/566541183
URI
https://openhsu.ub.hsu-hh.de/handle/10.24405/21027
Scopus ID
2-s2.0-105013835374
Conference
PCIM Conference 2025 - International Exhibition and Conference for Power Electronics, Intelligent Motion, Renewable Energy and Energy Management ; Nuremberg, Germany ; May 6-8, 2025
Publisher
VDE Verlag
Series or journal
Pcim Europe Conference Proceedings
Book title
PCIM 2025: International Exhibition and Conference for Power Electronics, Intelligent Motion, Renewable Energy and Energy Management
ISBN
978-3-8007-6541-6
First page
1408
Last page
1414
Peer-reviewed
✅
Part of the university bibliography
✅
Additional Information
Language
English
Abstract
This paper presents the prototyping of a fault-tolerant three-level T-type Neutral Point Clamped (TNPC) inverter for electric aircraft propulsion systems. To enhance robustness against various semiconductor failures, disconnecting devices are integrated in series with both the high-side and low-side switches. However, this implementation also increases parasitic inductance in the commutation loop. To mitigate the challenges associated with a highly inductive commutation path, a DC snubber circuit is designed to suppress overvoltage and damp switching oscillations. The switching behavior is analyzed through double-pulse testing (DPT). Additionally, a three-phase, three-level inverter employing space vector pulse-width modulation (SVPWM) is implemented, and its performance under normal operating conditions is evaluated. Furthermore, post-fault operation is investigated when one phase is connected to the neutral point.
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Published version
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