Hybrid-Electric Powertrain Design for Enhanced Vehicle Performance

Aaron VanLandingham, David K. Hall, Edward Smith, Robert C. Bill

Research output: Contribution to conferencePaperpeer-review

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 languageEnglish (US)
DOIs
StatePublished - 2025
Event81st Annual Vertical Flight Society Forum and Technology Display, FORUM 2025 - Virginia Beach, United States
Duration: May 20 2025May 22 2025

Conference

Conference81st Annual Vertical Flight Society Forum and Technology Display, FORUM 2025
Country/TerritoryUnited States
CityVirginia Beach
Period5/20/255/22/25

All Science Journal Classification (ASJC) codes

  • Aerospace Engineering
  • Control and Systems Engineering

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