Quad rotor aircraft with fixed wing and variable tail surfaces
First Claim
Patent Images
1. An aircraft comprising:
- a wing attached to a fuselage and forming a first plane;
an empennage having two variable angle tail surfaces that rotate to positions above, below, and parallel to the first plane;
a forward source of thrust mounted to the wing;
a rear source of thrust mounted to at least one of the two variable angle tail surfaces; and
wherein the two variable angle tail surfaces extend horizontally at an angle substantially parallel to the first plane when the aircraft is in a vertical propulsion configuration, and rotate into a v-tail when the aircraft is in a horizontal propulsion configuration.
0 Assignments
0 Petitions
Accused Products
Abstract
An aircraft with four rotors, a fixed wing, and an adjustable v-tail to allow for both vertical take-off and landing and the capability to fly in straight and level flight. The angle of each rotor and engine, with respect to the airfoil surfaces to which they are attached, is adjustable, allowing for thrust to be directed either downwards, allowing the craft to hover, or backwards, allowing the aircraft to travel horizontally while lift is provided and controlled by the wing and v-tail.
38 Citations
10 Claims
-
1. An aircraft comprising:
-
a wing attached to a fuselage and forming a first plane; an empennage having two variable angle tail surfaces that rotate to positions above, below, and parallel to the first plane; a forward source of thrust mounted to the wing; a rear source of thrust mounted to at least one of the two variable angle tail surfaces; and wherein the two variable angle tail surfaces extend horizontally at an angle substantially parallel to the first plane when the aircraft is in a vertical propulsion configuration, and rotate into a v-tail when the aircraft is in a horizontal propulsion configuration. - View Dependent Claims (2, 3, 4, 5, 6, 7, 8, 9, 10)
-
Specification