Vollredundante triplex fly-by-wire-architektur
Patent Information
- Application Number
- AT2023167485T
- Authority / Receiving Office
- AT · AT
- Patent Type
- Patents
- Current Assignee / Owner
- Priority Date
- 2022-04-12
- Filing Date
- 2023-04-12
- Publication Date
- 2026-04-15
- Estimated Expiration
- 2043-04-12
AI Technical Summary
Current Vertical Take-Off and Landing (VTOL) aircraft Fly-By-Wire (FBW) systems lack the necessary redundancy and complexity to ensure high availability of effectors, particularly in urban air mobility applications, where weight reduction and simplified Flight Control System (FCS) architectures may compromise safety and controllability.
A triplex Flight Control Computer (FCC) architecture is implemented, where each FCC is connected to all controllers for effector actuation, with point-to-point links to reduce bus message collisions and ensure high availability of effectors, allowing for direct or indirect connections through retransmitters (RTXs) to maintain control in case of failures.
This configuration ensures that all or most effectors remain operational even in the event of loss of two flight control computers, enhancing safety and controllability by reducing the risk of unstable behavior during vertical takeoff, transition, and cruise phases.