Reliability evaluation of non-repairable propulsion systems of hybrid-electric helicopter with different level of hybridization

Igor Bolvashenkov; Jorg Kammermann; Hans Georg Herzog; Wenbin Zeng

doi:10.1109/EVER.2019.8813588

Reliability evaluation of non-repairable propulsion systems of hybrid-electric helicopter with different level of hybridization

Igor Bolvashenkov, Jorg Kammermann, Hans Georg Herzog, Wenbin Zeng

Professur für Energiewandlungstechnik

Publikation: Beitrag in Buch/Bericht/Konferenzband › Konferenzbeitrag › Begutachtung

2 Zitate (Scopus)

Abstract

The paper describes the reliability comparative analysis of a hybrid-electric helicopter traction drive with two competitive topologies. The entire propulsion system reliability assessment is based on the reliability evaluation of the system components. The dependency of reliability of the helicopter's propulsion system on the degree of hybridization is presented. Additionally, with the graphs of the variation in the probability of failure-free operation, recommendations how to improve the reliability indices of the hybrid-electric helicopter's traction drive was made.

Originalsprache	Englisch
Titel	2019 14th International Conference on Ecological Vehicles and Renewable Energies, EVER 2019
Herausgeber (Verlag)	Institute of Electrical and Electronics Engineers Inc.
ISBN (elektronisch)	9781728137032
DOIs	https://doi.org/10.1109/EVER.2019.8813588
Publikationsstatus	Veröffentlicht - Mai 2019
Veranstaltung	14th International Conference on Ecological Vehicles and Renewable Energies, EVER 2019 - Monte-Carlo, Monaco Dauer: 8 Mai 2019 → 10 Mai 2019

Publikationsreihe

Name	2019 14th International Conference on Ecological Vehicles and Renewable Energies, EVER 2019

Konferenz

Konferenz	14th International Conference on Ecological Vehicles and Renewable Energies, EVER 2019
Land/Gebiet	Monaco
Ort	Monte-Carlo
Zeitraum	8/05/19 → 10/05/19

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10.1109/EVER.2019.8813588

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Bolvashenkov, I., Kammermann, J., Herzog, H. G., & Zeng, W. (2019). Reliability evaluation of non-repairable propulsion systems of hybrid-electric helicopter with different level of hybridization. in 2019 14th International Conference on Ecological Vehicles and Renewable Energies, EVER 2019 Artikel 8813588 (2019 14th International Conference on Ecological Vehicles and Renewable Energies, EVER 2019). Institute of Electrical and Electronics Engineers Inc.. https://doi.org/10.1109/EVER.2019.8813588

Bolvashenkov, Igor ; Kammermann, Jorg ; Herzog, Hans Georg et al. / Reliability evaluation of non-repairable propulsion systems of hybrid-electric helicopter with different level of hybridization. 2019 14th International Conference on Ecological Vehicles and Renewable Energies, EVER 2019. Institute of Electrical and Electronics Engineers Inc., 2019. (2019 14th International Conference on Ecological Vehicles and Renewable Energies, EVER 2019).

@inproceedings{fed6dac3599d4c7cb00f5b1c64a815d9,

title = "Reliability evaluation of non-repairable propulsion systems of hybrid-electric helicopter with different level of hybridization",

abstract = "The paper describes the reliability comparative analysis of a hybrid-electric helicopter traction drive with two competitive topologies. The entire propulsion system reliability assessment is based on the reliability evaluation of the system components. The dependency of reliability of the helicopter's propulsion system on the degree of hybridization is presented. Additionally, with the graphs of the variation in the probability of failure-free operation, recommendations how to improve the reliability indices of the hybrid-electric helicopter's traction drive was made.",

keywords = "Electric propulsion system, Hybrid-electric helicopter, Level of redundancy, Markov Model, Non-repairable system, Reliability, The degree of hybridization",

author = "Igor Bolvashenkov and Jorg Kammermann and Herzog, {Hans Georg} and Wenbin Zeng",

note = "Publisher Copyright: {\textcopyright} 2019 IEEE.; 14th International Conference on Ecological Vehicles and Renewable Energies, EVER 2019 ; Conference date: 08-05-2019 Through 10-05-2019",

year = "2019",

month = may,

doi = "10.1109/EVER.2019.8813588",

language = "English",

series = "2019 14th International Conference on Ecological Vehicles and Renewable Energies, EVER 2019",

publisher = "Institute of Electrical and Electronics Engineers Inc.",

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}

Bolvashenkov, I, Kammermann, J, Herzog, HG & Zeng, W 2019, Reliability evaluation of non-repairable propulsion systems of hybrid-electric helicopter with different level of hybridization. in 2019 14th International Conference on Ecological Vehicles and Renewable Energies, EVER 2019., 8813588, 2019 14th International Conference on Ecological Vehicles and Renewable Energies, EVER 2019, Institute of Electrical and Electronics Engineers Inc., 14th International Conference on Ecological Vehicles and Renewable Energies, EVER 2019, Monte-Carlo, Monaco, 8/05/19. https://doi.org/10.1109/EVER.2019.8813588

Reliability evaluation of non-repairable propulsion systems of hybrid-electric helicopter with different level of hybridization. / Bolvashenkov, Igor; Kammermann, Jorg; Herzog, Hans Georg et al.
2019 14th International Conference on Ecological Vehicles and Renewable Energies, EVER 2019. Institute of Electrical and Electronics Engineers Inc., 2019. 8813588 (2019 14th International Conference on Ecological Vehicles and Renewable Energies, EVER 2019).

Publikation: Beitrag in Buch/Bericht/Konferenzband › Konferenzbeitrag › Begutachtung

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AU - Zeng, Wenbin

PY - 2019/5

Y1 - 2019/5

N2 - The paper describes the reliability comparative analysis of a hybrid-electric helicopter traction drive with two competitive topologies. The entire propulsion system reliability assessment is based on the reliability evaluation of the system components. The dependency of reliability of the helicopter's propulsion system on the degree of hybridization is presented. Additionally, with the graphs of the variation in the probability of failure-free operation, recommendations how to improve the reliability indices of the hybrid-electric helicopter's traction drive was made.

AB - The paper describes the reliability comparative analysis of a hybrid-electric helicopter traction drive with two competitive topologies. The entire propulsion system reliability assessment is based on the reliability evaluation of the system components. The dependency of reliability of the helicopter's propulsion system on the degree of hybridization is presented. Additionally, with the graphs of the variation in the probability of failure-free operation, recommendations how to improve the reliability indices of the hybrid-electric helicopter's traction drive was made.

KW - Electric propulsion system

KW - Hybrid-electric helicopter

KW - Level of redundancy

KW - Markov Model

KW - Non-repairable system

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KW - The degree of hybridization

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Bolvashenkov I, Kammermann J, Herzog HG, Zeng W. Reliability evaluation of non-repairable propulsion systems of hybrid-electric helicopter with different level of hybridization. in 2019 14th International Conference on Ecological Vehicles and Renewable Energies, EVER 2019. Institute of Electrical and Electronics Engineers Inc. 2019. 8813588. (2019 14th International Conference on Ecological Vehicles and Renewable Energies, EVER 2019). doi: 10.1109/EVER.2019.8813588

Reliability evaluation of non-repairable propulsion systems of hybrid-electric helicopter with different level of hybridization

Abstract

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