AeroVironment, Inc.
Vertical Takeoff and Landing (VTOL) Air Vehicle
Last updated:
Abstract:
A flight control apparatus for fixed-wing aircraft includes a first port wing and first starboard wing, a first port swash plate coupled between a first port rotor and first port electric motor, the first port electric motor coupled to the first port wing, and a first starboard swash plate coupled between a first starboard rotor and first starboard electric motor, the first starboard electric motor coupled to the first starboard wing.
Status:
Application
Type:
Utility
Filling date:
26 Feb 2019
Issue date:
23 Jan 2020