05 - Propulsion
SAFETY-DRIVEN BASELINING OF HYBRID ELECTRIC AIRCRAFT ELECTRICAL POWER SYSTEM ARCHITECTURES
K. Fong¹, P. Norman¹, C.E. Jones¹; ¹University of Strathclyde, United Kingdom
Existing approaches to electrical power system (EPS) design for electrical propulsion aircraft assume a starting point with a comprehensive set of baseline requirements. This paper presents a safety-driven methodology to capture baseline requirements for a new concept aircraft with minimal initial design criteria, and translation of these requirements into a resilient EPS architecture solution.