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

Associate Professorship of Energy Conversion Technology

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution › peer-review

2 Scopus citations

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.

Original language	English
Title of host publication	2019 14th International Conference on Ecological Vehicles and Renewable Energies, EVER 2019
Publisher	Institute of Electrical and Electronics Engineers Inc.
ISBN (Electronic)	9781728137032
DOIs	https://doi.org/10.1109/EVER.2019.8813588
State	Published - May 2019
Event	14th International Conference on Ecological Vehicles and Renewable Energies, EVER 2019 - Monte-Carlo, Monaco Duration: 8 May 2019 → 10 May 2019

Publication series

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

Conference

Conference	14th International Conference on Ecological Vehicles and Renewable Energies, EVER 2019
Country/Territory	Monaco
City	Monte-Carlo
Period	8/05/19 → 10/05/19

Keywords

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

UN SDGs

This output contributes to the following UN Sustainable Development Goals (SDGs)

Access to Document

10.1109/EVER.2019.8813588

Cite this

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 Article 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).

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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).

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution › peer-review

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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.

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M3 - Conference contribution

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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

Publication series

Conference

Keywords

UN SDGs

Access to Document

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