Abstract
Electrification could improve full-size rotorcraft performance by reducing peak turbine power demand, reducing transmission system weight and complexity, and reducing operating costs. Integrating electric machines with mechanical powertrains requires careful consideration of the system-level weight and efficiency impacts. This paper presents an optimization framework for evaluating parallel hybrid powertrain configurations using Geometric Programming (GP). Both retrofit and clean-sheet vehicle designs are considered. The results show that high-speed electric motors integrated into a parallel hybrid configuration using batteries can reduce the sized gas turbine power, enabling more efficient engine operation at lower power levels. For retrofit designs, with a fixed vehicle gross weight, adding batteries and motors reduces usable fuel, decreasing mission capability. Clean-sheet designs offer additional flexibility to re-size the vehicle and rotor, resulting in energy savings for an equivalent design mission.
| Original language | English (US) |
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| DOIs | |
| State | Published - 2025 |
| Event | 81st Annual Vertical Flight Society Forum and Technology Display, FORUM 2025 - Virginia Beach, United States Duration: May 20 2025 → May 22 2025 |
Conference
| Conference | 81st Annual Vertical Flight Society Forum and Technology Display, FORUM 2025 |
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| Country/Territory | United States |
| City | Virginia Beach |
| Period | 5/20/25 → 5/22/25 |
All Science Journal Classification (ASJC) codes
- Aerospace Engineering
- Control and Systems Engineering