Flight Simulator Demonstration and Certification Implications of Powertrain Failure Mitigation in a Partial Turboelectric Aircraft

Abstract

Verbatim from NASA NTRS. Not paraphrased, not summarized.

The Single-aisle Turboelectric AiRCraft with Aft Boundary Layer propulsor (STARC ABL) is a concept aircraft with a partial turboelectric powertrain. The complexity and integrated nature of the partial turboelectric powertrain architecture presents failure modes and hazards not found in conventional aircraft propulsion designs. Previously, various electrical and mechanical faults and associated recovery modes were demonstrated in a dynamic model of the powertrain. It was shown that certain faults were catastrophic without recovery logic, due specifically to the interaction of the subsystems. However, in each case, the logic, known as a reversionary control mode, enabled continued operation with assumed sufficient thrust to maintain safe flight. The current work evaluates the powertrain faults and recovery strategies using a full aircraft model in a piloted flight simulator, and places it in the context of current regulatory practice. Faults initiated in flight were successfully mitigated, with the accommodated aircraft subsequently evaluated against certification requirements for three-engine aircraft, which were shown to be appropriate for the STARC-ABL configuration.

Authors

• Jonathan S Litt Glenn Research Center
• Jonah J Sachs-Wetstone Glenn Research Center
• Donald L Simon Glenn Research Center
• T Shane Sowers HX5, LLC
• A Karl Owen HX5, LLC
• Mark E Bell HX5, LLC
• Brenden E Guthrie GRC-LERCIP
• Julian Lehan GRC-LERCIP
• Amado Castro GRC-LERCIP

Keywords

• STARC-ABL
• Reversionary Control
• Flight Simulation
• certification