Impact resistant propeller system, fast response 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. An aerial vehicle adapted to withstand impacts upon its propellers. An aerial vehicle able to quickly alter the thrust of its propellers.
1. An impact resistant propeller system, said impact resistant propeller system comprising:
a propeller, said propeller having a primary spin direction along a first spin axis to provide positive thrust, said propeller comprising:
a central hub, said central hub comprising a first rotation axis;
a plurality of propeller blades, each of said plurality of propeller blades pivotally attached along a first pivot axis to said central hub,
wherein the first pivot axis is angled such that pivoting a propeller blade backwards along said first spin axis causes the propeller blade to rotate counter to said primary spin direction.
2. The impact resistant propeller system of claim 1 wherein said first pivot axis of each of said plurality of propeller blades is angled to a plane normal to the first spin axis.
3. The impact resistant propeller system of claim 2 wherein said propeller blades comprise a hinge pin, said hinge pin extending from a leading edge of said propeller blade.
4. The impact resistant propeller system of claim 3 wherein said hinge pin comprises a first end at the leading edge of said propeller blade and a second end away from said leading edge of said propeller blade, and wherein said first end is forward of said second end along said first spin axis.
5. The impact resistant propeller system of claim 4 wherein said propeller system further comprises a nacelle, and wherein said blades are adapted to pivot from a deployed configuration substantially perpendicular to said spin axis to a stowed position along the exterior of said nacelle.
6. The impact resistant propeller system of claim 5 wherein said nacelle comprises recesses around its exterior, and wherein said blades reside in said recesses when in said stowed position.
7. The impact resistant propeller system of claim 6 further comprising a stowing mechanism, said stowing mechanism adapted to stow said propeller blades into said recesses in the outer surface of the nacelle.
8. The impact resistant system of claim 7 further comprising a spring system adapted to deploy the propeller blades from their stowed position.
9. The impact resistant propeller system of claim 8 further comprising a propeller deployment mechanism, said propeller deployment mechanism adapted to deploy said central hub from a first position wherein said first spin axis is horizontal to a second position wherein said first spin axis is vertical.
10. A quick response propeller system for an aerial vehicle, said system comprising:
a central hub;
a plurality of propeller blades, each of said plurality of propeller blades pivotally attached along a first pivot axis to said central hub,
wherein the first pivot axis is angled such that pivoting a propeller blade backwards along said first spin axis from a position forward of normal to the spin axis causes a change in pitch of the propeller blade.
11. The quick response propeller system of claim 10 further comprising an electric motor coupled to said central hub.
12. The quick response propeller system of claim 11 wherein said first pivot axis is angled to a plane normal to the first spin axis.
13. The quick response propeller system of claim 12 wherein said propeller blades comprise a hinge pin, said pivot pin extending from a leading edge of said propeller blade.
14. The quick response propeller system of claim 3 wherein said hinge pin comprises a first end at the leading edge of said propeller blade and a second end away from said leading edge of said propeller blade, and wherein said first end is forward of said second end along said first spin axis.
15. The impact resistant propeller system of claim 1 further comprising an electric motor coupled to said central hub.
16. The impact resistant propeller system of claim 2 further comprising an electric motor coupled to said central hub.