Articulated electric propulsion system and lightweight vertical take-off and landing aircraft using same
An aerial vehicle adapted for vertical takeoff and landing using pivoting thrust producing elements for takeoff and landing. An aerial vehicle which is adapted to takeoff with thrust units providing vertical thrust and then transitioning to a horizontal flight path. An aerial vehicle with pivoting thrust units with propellers, wherein some or all of the propellers are able to be stowed and fully nested during forward flight.
1. A vertical take-off and landing aircraft, said vertical take-off and landing aircraft comprising:
a left wing, said left wing comprising a plurality of left side propulsion assemblies; and
a right wing, said right wing comprising a plurality of right side propulsion assemblies, wherein said propulsion assemblies comprise a stowable propeller system, said stowable propeller system comprising:
a central hub, said central hub comprising a first rotation axis;
a drive motor, said drive motor rigidly coupled to said central hub; and
a plurality of stowable propeller blades, said plurality of stowable propeller blades pivotally attached to said central hub, said stowable propeller blades comprising blade tips at an end away from said central hub,
wherein one or more of said plurality of left side propulsion assemblies further comprise an alternate forward flight propeller, and wherein one or more of said plurality of right side propulsion assemblies further comprise an alternate forward flight propeller.
2. The vertical take-off and landing aircraft of claim 1 wherein said blade tips of said stowable propeller blades when stowed reside forward of the leading edge of said left wing and said right wing.
3. The vertical take-off and landing aircraft of claim 1 wherein said propulsion assemblies further comprise a nacelle body, said nacelle body comprising recesses in its outer surface when said stowable propeller blades are in a deployed position, and wherein said stowable propeller blades are adapted to stow into said recesses in the outer surface of the nacelle body.
4. The vertical take-off and landing aircraft of claim 2 wherein said propulsion assemblies further comprise a nacelle body, said nacelle body comprising recesses in its outer surface when said stowable propeller blades are in a deployed position, and wherein said stowable propeller blades are adapted to stow into said recesses in the outer surface of the nacelle body.
5. The vertical take-off and landing aircraft of claim 1 wherein said stowable propeller system further comprises a first principal axis along its center, and wherein said stowable propeller blades are adapted to pivot from a stowed position in the recesses of the nacelle body to a deployed position to a deployed position substantially perpendicular to said first rotation axis.
6. The vertical take-off and landing aircraft of claim 1 further comprising a rotary positional sensor adapted to sense the rotary position of said stowable propeller blades relative to said nacelle body.
7. The vertical take-off and landing aircraft of claim 2 further comprising a rotary positional sensor adapted to sense the rotary position of said stowable propeller blades relative to said nacelle body.
8. The vertical take-off and landing aircraft of claim 1 further comprising a stowing mechanism, said stowing mechanism adapted to stow said stowable propeller blades into said recesses in the outer surface of the nacelle body.
9. The vertical take-off and landing aircraft of claim 2 further comprising a stowing mechanism, said stowing mechanism adapted to stow said stowable propeller blades into said recesses in the outer surface of the nacelle body.
10. The vertical take-off and landing aircraft of claim 8 further comprising a spring system adapted to deploy the stowable propeller blades from their stowed position.
11. The vertical take-off and landing aircraft of claim 9 further comprising a spring system adapted to deploy the stowable propeller blades from their stowed position.
12. The vertical take-off and landing aircraft of claim 3 wherein the stowed propeller blades comprise all or most of the effective wetted area of portions of the nacelle.
13. The vertical take-off and landing aircraft of claim 4 wherein the stowed propeller blades comprise all or most of the effective wetted area of portions of the nacelle.
14. The vertical take-off and landing aircraft of claim 1 wherein said alternate forward flight propellers reside forward along said first rotation axis than said stowable propeller blades.
15. The vertical take-off and landing aircraft of claim 2 wherein said alternate forward flight propellers reside forward along said first rotation axis than said stowable propeller blades.
16. The vertical take-off and landing aircraft of claim 4 wherein said alternate forward flight propellers reside forward along said first rotation axis than said stowable propeller blades.