Design and Reliability Analysis of a Series/Parallel Hybrid System with a Rotary Engine for Safer Ultralight Aviation

Design and Reliability Analysis of a Series/Parallel Hybrid System with a Rotary Engine for Safer Ultralight Aviation

The conventional powertrain for ultralight aviation consists of a fixed pitch propeller connected to an internal combustion engine (ICE). Since ICEs have a limited thermal efficiency (

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Veröffentlicht in:Applied sciences 2023-04, Vol.13 (7), p.4155
Hauptverfasser: Donateo, Teresa, Spada Chiodo, Ludovica
Format: Artikel
Sprache:eng
Schlagworte:
Aeronautics
Automotive engines
Aviation
Design
Electric power
Electric power systems
Electricity distribution
Energy consumption
Energy efficiency
Engine failure
Engines
Fuel economy
hybrid electric aircraft
Hybrid vehicles
Hybridization
Internal combustion engines
Power plants
power split device
Powertrain
Reliability analysis
Rotary engines
Safety
Thermodynamic efficiency
ultralight aviation
Vehicles
Wankel engine
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Beschreibung
Zusammenfassung:The conventional powertrain for ultralight aviation consists of a fixed pitch propeller connected to an internal combustion engine (ICE). Since ICEs have a limited thermal efficiency (
ISSN:2076-3417
2076-3417
DOI:10.3390/app13074155