01.2 - Aircraft Design and Integrated System (Applications)
DETERMINISTIC HYBRID POWER RATIOS CONSIDERING VARIOUS FAILURE CASES FOR QUAD TILTROTOR AIRCRAFT
M. Park¹, N. Roh¹; ¹Hanwha systems, South Korea
This paper proposes deterministic hybrid power ratios for a light series hybrid electric propulsion system in a generic quad tiltrotor aircraft, guided by five sizing rules. It compares four failure scenarios against three, with a focus on reducing aircraft weight. The paper also suggests the best configuration of the hybrid power sources, specifically tailored to the current battery technology.