Distributed Electric Propulsion

Source: ONERA

Research Areas

Distributed Electric Propulsion Technologies and Aircraft Concepts

The desire for eVTOL capabilities coupled with improved cruise efficiency over conventional multi-rotor configurations has also led to the development of several DEP tiltwing aircraft concepts

Distributed Electric Propulsion Enabled Aero-Propulsive Coupling

This involve integrating a ducted fan within a wing section. An embedded ducted fan on the aerodynamics of a wing section as a function of fan integration location, thrust level, and the airfoil shape itself.

Distributed Electric Propulsion Enabled Vehicle Control

This approach could lead to a more generalized understanding of how distributed propulsion systems and the associated PAI effects can be incorporated into aircraft dynamics models, rather than a single dynamics model for a specific DEP-enabled aircraft.

Distributed Electric Propulsion Enabled Noise Reduction

An additional advantage of retaining flexibility in the placement of propulsors is the ability to leverage noise shielding of wing-body surfaces or noise-reducing effects of boundary-layer ingestion

Example — Traction system architecture of NASA’s X-57 (Mod IV)

all-electric aircraft