Aurora Flight Sciences Corporation

Dorian Colas

Francesco Giannini

Daniel B Cottrell

Martin Gomez

Dan Cottrell

Carl G Schaefer, Jr

Herbert E Hunter

Jean-Charles Lede

Tom Roberts

Timothy Nuhfer

Jonathan Grohs

Steve Petullo

Thomas Roberts

Brian Whipple

Herb Hunter

Jonathon Grohs

Tim Nuhfer

Carl G Schaefer

A hybrid propulsion aircraft is described having a distributed electric propulsion system. The distributed electric propulsion system includes a turbo shaft engine that drives one or more generators through a gearbox. The generator provides AC power to a plurality of ducted fans (each being driven by an electric motor). The ducted fans may be integrated with the hybrid propulsion aircraft's wings. The wings can be pivotally attached to the fuselage, thereby allowing for vertical take-off and landing. The design of the hybrid propulsion aircraft mitigates undesirable transient behavior traditionally encountered during a transition from vertical flight to horizontal flight. Moreover, the hybrid propulsion aircraft offers a fast, constant-altitude transition, without requiring a climb or dive to transition. It also offers increased efficiency in both hover and forward flight versus other VTOL aircraft and a higher forward max speed than traditional rotorcraft.

Hybrid propulsion vertical take-off and landing aircraft

Growing community of inventors

Seattle, WA, United States of America

Dorian Colas