Hybrid Electric Aircraft Propulsion Case Study for Skydiving Mission
Abstract
1. Introduction
1.1. Skydiving Lift Mission
1.2. Hybrid Electric Propulsion Suitability
2. Materials and Methods
2.1. Mission Profile
2.2. The Proposed Models
2.3. Mission Energy
- Potential energy requirements to climb;
- Drag energy expended in climb;
- Energy regeneration during descent.
2.4. ICE Limitations
2.5. Rated ICE Power
2.6. Recharge Cases
3. Results
3.1. Hybrid Electric
3.2. Model Assumptions
- High power/weight (where battery storage capacity requirements are low);
- Ease of adding propeller area for any given installed power, allowing greater propulsive efficiency under particular conditions.
3.3. All-Electric
4. X-Plane Modeling
4.1. Multi-Role
4.2. Modularity
5. Future Analysis
Safety and Certification
6. Conclusions
Acknowledgments
Author Contributions
Conflicts of Interest
References
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Component | Energy Density (Wh/kg) | Power Density (kW/kg) | Efficiency |
---|---|---|---|
EM | − | 6 | 0.9 |
Power Electronics | − | 6 | 0.9 |
Battery | 200 | − | 0.9 |
ICE | 4 | 0.26 |
Aircraft Model | Installed Power (kW) | Empty Weight 1 (kg) | Payload Weight 1 (kg) | Oswald Efficiency Factor | Propeller Effciency |
---|---|---|---|---|---|
AUXX Conventional | 670 | 2700 | 800 | 0.835 | 0.75 |
AUXX Hybrid | 670 | 2700 + %EPS | 800 | 0.835 | Scaled |
AUXX All-Electric | 670 | 3500 | 800 | 0.835 | 0.85 |
Aircraft Model | Installed Power (kW) | Empty Weight 1 (kg) | Payload Weight 1 (kg) | Climb Time Analytic (minutes) | Climb Time Simulation (minutes) |
---|---|---|---|---|---|
AUXX Conventional | 670 | 2400 | 800 | 9 | 10.6 |
AUXX Hybrid | 670 | 3300 | 800 | 7.4 | 8.6 |
X-Plane Aircraft Model | Installed Power (kW) | Empty Weight 1 (kg) | Payload Weight 1 (kg) | Average Climb Rate to 14,000 ft (ft/min) |
---|---|---|---|---|
AUXX Conventional | 670 | 2400 | 800 | 1320 |
AUXX Hybrid 2 | 670 | 3300 | 800 | 1620 |
C208 Conventional | 670 | 2200 | 800 | 1550 |
C208 Hybrid 2 | 670 | 3000 | 800 | 2150 |
Real Aircraft Data | ||||
850HP C208 3 | 635 | 2200 | 1800 | * 1460 4 |
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Glassock, R.; Galea, M.; Williams, W.; Glesk, T. Hybrid Electric Aircraft Propulsion Case Study for Skydiving Mission. Aerospace 2017, 4, 45. https://doi.org/10.3390/aerospace4030045
Glassock R, Galea M, Williams W, Glesk T. Hybrid Electric Aircraft Propulsion Case Study for Skydiving Mission. Aerospace. 2017; 4(3):45. https://doi.org/10.3390/aerospace4030045
Chicago/Turabian StyleGlassock, Richard, Michael Galea, Warren Williams, and Tibor Glesk. 2017. "Hybrid Electric Aircraft Propulsion Case Study for Skydiving Mission" Aerospace 4, no. 3: 45. https://doi.org/10.3390/aerospace4030045
APA StyleGlassock, R., Galea, M., Williams, W., & Glesk, T. (2017). Hybrid Electric Aircraft Propulsion Case Study for Skydiving Mission. Aerospace, 4(3), 45. https://doi.org/10.3390/aerospace4030045