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FUELEAP Model-Based System Safety AnalysisNASA researchers, in a partnership with Boeing, are investigating a fuel-cell powered variant of the X-57 “Maxwell” Mod-II electric propulsion aircraft, which is itself derived from a stock Tecnam P2006T. The “Fostering Ultra-Efficient Low-Emitting Aviation Power” (FUELEAP) project will replace the X-57 power subsystem with a hybrid Solid-Oxide Fuel Cell (SOFC) system to increase the potential range of the electric-propulsion aircraft while dramatically improving efficiency and emissions over stock internal-combustion engines. Our FUELEAP safety analysis faces two primary challenges. First, the Part 23 certificated Tecnam P2006T is undergoing significant modifications to host the hybrid electric-propulsion system, and the challenge is to assure that the safety inherent in the stock aircraft (and subsequently in X-57 Mod-II) is not compromised by changes in avionics, aircraft structural loading, weight and balance, or other considerations. Secondly, because the SOFC power system has little (if any) relevant in-service precedent, our challenge is to assure that we identify and mitigate all reasonably plausible hazards introduced by unique FUELEAP equipage. We are investigating and utilizing Model-Based Safety Analysis (MBSA) methods to help us address these FUELEAP safety challenges. We captured aircraft-level system hazard conditions using instances of a SysML hazard block via aircraft-level Functional Hazard Analysis (FHA). Then, using SysML models of the FUELEAP architecture, we related the hazard conditions to initiating system events and possible mitigations, such as design architecture modifications or operational constraints. We are continuing to define our approach to MBSA by developing a component-by-component inventory of local failure modes and tracing their possible contribution to hazard conditions. Finally, we are applying an argument-based approach to FUELEAP assurance. Through a FUELEAP “safety case,” we are providing an explicit argument for FUELEAP safety by associating assurance evidence with overarching safety claims through a structured argument.

Document ID
20190033416
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Woodham, Kurt P.
(NASA Langley Research Center Hampton, VA, United States)
Graydon, Patrick J.
(NASA Langley Research Center Hampton, VA, United States)
Borer, Nicholas K.
(NASA Langley Research Center Hampton, VA, United States)
Papathakis, Kurt P.
(NASA Armstrong Flight Research Center Edwards, CA, United States)
Stoia, Tina
(Boeing Company Huntington Beach, CA, United States)
Balan, Chellappa
(Boeing Company Huntington Beach, CA, United States)
Date Acquired
December 6, 2019
Publication Date
June 25, 2018
Subject Category
Aircraft Propulsion And Power
Systems Analysis And Operations Research
Report/Patent Number
NF1676L-28662
Meeting Information
Meeting: AIAA Aviation
Location: Atlanta, GA
Country: United States
Start Date: June 25, 2018
End Date: June 29, 2018
Sponsors: American Institute of Aeronautics and Astronautics (AIAA)
Funding Number(s)
WBS: 533127.02.17.07.01
Distribution Limits
Public
Copyright
Public Use Permitted.
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