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