at Google ScholarTitle data
Schwarz, R. ; Waller, R. ; Wenger, Martin M. ; Akdere, M. ; Neureuther, J. ; Gepp, Markus ; Koffel, S. ; Lorentz, Vincent ; März, Martin ; Holtsmark, A. ; Gribov, V. ; Lange, A.:
Aviation battery monitoring electronics in lithium-ion based battery systems for electrified sailplanes and aircrafts.
2016
Event: 2016 International Conference on Electrical Systems for Aircraft, Railway, Ship Propulsion and Road Vehicles & International Transportation Electrification Conference (ESARS-ITEC)
, Nov. 2–4, 2016
, Toulouse, France.
(Conference item: Conference
,
Speech with paper
)
DOI: https://doi.org/10.1109/ESARS-ITEC.2016.7841387
Project information
| Project title: |
Project's official title Project's id eDAS: Holistic Energy Management for third and fourth generation of EVs: eDAS = efficiency powered by smart Design meaningful Architecture connected Systems 608770 OSEM-EV: Optimised and Systematic Energy Management in Electric Vehicles 653514 3Ccar: Integrated Components for Complexity Control in affordable electrified cars 662192 |
|---|---|
| Project financing: |
7. Forschungsrahmenprogramm für Forschung, technologische Entwicklung und Demonstration der Europäischen Union Part of the research leading to these results has received funding from the European Union's Seventh Framework Program (FP7/2007-2013) under grant agreement n°608770 (“eDAS”); from the European Union's Horizon 2020 Research and Innovation Actions (RIA) program under grant agreement n°653514 (OSEM-EV); and from the ECSEL Joint Undertaking under grant agreement n°662192 (3Ccar). The ECSEL JU receives support from the European Union's Horizon 2020 research and innovation program and the ECSEL member states (i.e., BMBF for Germany). The authors acknowledge the Panasonic Semiconductors Division for the supply of integrated circuits and MOSFET products and their technical support. |
Abstract in another language
This paper presents the hardware and software design of a battery monitoring circuit developed to be used in aviation applications employing lithium-ion batteries in their electrified powertrain. The considered aircraft is a manned sailplane able to take-off and climb by using its electric propulsion system supplied by NCA/Graphite lithium-ion batteries. The battery monitoring electronics was developed with the highest considerations in terms of fail-safe and fail-operational requirements. The electronic design of the battery monitoring circuit integrates the battery busbars and uses new passive balancing components with an innovative busbar cooling solution, thus increasing the reliability and the robustness of the whole battery system. The software also contributes to the high safety level by employing crosscheck and plausibility check mechanisms.
Further data
| Item Type: | Conference item (Speech with paper) |
|---|---|
| Refereed: | Yes |
| Keywords: | Lithium-Ion Battery; Fail-Operational; High-Availability; Redundant Architecture; Electrified Powertrain; Electrical Energy Storage System; Electric Sailplane; Aviation |
| Institutions of the University: | Research Institutions > Research Centres > Bayerisches Zentrum für Batterietechnik - BayBatt Research Institutions Research Institutions > Research Centres |
| Result of work at the UBT: | No |
| DDC Subjects: | 600 Technology, medicine, applied sciences > 620 Engineering |
| Date Deposited: | 03 Jun 2022 10:25 |
| Last Modified: | 12 Oct 2022 13:35 |
| URI: | https://eref.uni-bayreuth.de/id/eprint/69865 |