Airborne Collision Severity Evaluation - Engine Ingestion
The research goal for this project is to better understand the interaction of a fan and UAV during an ingestion scenario. The objectives of this research are to: (i) create a generic high bypass ratio fan model that has features that are representative of a fan in a modern engine typically found on a large commercial transport; (ii) develop a component and full scale validated model of a quadcopter UAV (initially validated critical components in the first phase of the airborne collision research at different conditions) at the conditions of the ingestion event; and (iii) simulate various ingestion events to understand the sensitivity of a collision to various parameters of the ingestion.
- Contract to a Performing Organization has not yet been awarded.
- Status: Active
Federal Aviation Administration800 Independence Avenue, SW
Washington, DC United States 20591
- Start Date: 20180830
- Expected Completion Date: 0
- Actual Completion Date: 0
- TRT Terms: Air transportation crashes; Aircraft; Crash severity; Drones; Fans; Jet engines; Simulation
- Subject Areas: Aviation; Safety and Human Factors;
- Accession Number: 01682810
- Record Type: Research project
- Source Agency: Alliance for System Safety of UAS through Research Excellence (ASSURE)
- Files: RIP, USDOT
- Created Date: Oct 8 2018 1:51PM