Systems and methods for controlling an electric vertical take-off and landing aircraft
Patent Information
- Application Number
- EP2023805434
- Authority / Receiving Office
- EP · EP
- Patent Type
- Applications
- Current Assignee / Owner
- Priority Date
- 2023-05-30
- Filing Date
- 2023-10-30
- Publication Date
- 2025-09-03
AI Technical Summary
Conventional electric vertical take-off and landing (eVTOL) aircraft face challenges in designing components that withstand frequent use, generate low noise and vibration, and ensure safety with distributed propulsion systems, while also meeting regulatory requirements for safety and efficiency.
The eVTOL aircraft employs a distributed electrical propulsion system with multiple electrical engines mounted on booms, capable of tilting for vertical and horizontal flight, along with a flight control system that uses inceptors to control aircraft movement and orientation, and incorporates safety features like fire protection and redundancy to minimize single points of failure.
This configuration enables efficient, safe, and reliable eVTOL operations, reducing noise and vibration, and meeting regulatory standards for passenger transportation, while ensuring aircraft performance and compliance with aviation laws.