Powerplant Design and Performance Analysis of a Manned All-Electric Helicopter

Abstract

This paper describes the conceptual design of three all-electric powerplants—a battery-only, a fuel-cell-only, and a battery–fuel cell hybrid powerplant—for a manned ultralight utility helicopter (Robinson R 22 Beta II-like) and carries out a comparative evaluation of performance delivered by each. The new powerplants consist of a combination of high-pressure proton exchange membrane fuel cells, 700 bar type-4 hydrogen storage, a compressor–expander, lithium-ion batteries, and an alternating current synchronous permanent magnet motor. The key conclusion is that a hybrid powerplant that combines high specific power of batteries in hover and high calorific value of hydrogen in cruise delivers a superior performance compared to either system alone. The efficiency is higher than current rotorcraft piston engines but the key limitation is its low specific power, which is half of the current engines. Only 60% of the original payload can be flown (90 kg solo pilot) for a duration of 35 min (including 11 min hover) over a range of 47 km under high/hot () conditions. The paper lays the foundations of performance analysis for all-electric rotorcraft, benchmarks the best performance achievable with current state of the art, and quantifies future technology targets to enable performance comparable to existing internal combustion engines.