Articulated electric propulsion system with fully stowing blades 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 method for operating a vertical take-off and landing aircraft, said method comprising the steps of:
rotating a plurality of motor driven propeller units to a vertical thrust configuration;
providing power to said motor driven propeller units, thereby rotating the propellers of said motor driven propeller units;
taking off the aircraft from the ground;
transitioning the plurality of motor driven propeller units from a vertical thrust configuration towards a horizontal configuration, thereby gaining horizontal speed for the aircraft;
flying the aircraft in a forward flight configuration;
discontinuing the provision of power to some or all of the plurality of motor driven propeller units; and
stowing the propeller blades of some or all of the propellers of the motor driven propeller units while flying the aircraft in a forward flight configuration;
wherein the step of stowing the propeller blades of some or all of the propellers comprises stowing the propeller blades into recesses on the exterior surfaces of the nacelles of the motor driven propeller units, and wherein the stowed propeller blades comprise all or most of the effective wetted area of portions of the nacelle.
2. The method of claim 1 further comprising the step of re-deploying the stowed propeller blades in preparation for vertical landing.
3. The method of claim 2 further comprising providing power to the previously stowed propellers.
4. The method of claim 3 further comprising the step of transitioning the plurality of motor driven propeller units from a horizontal configuration towards a vertical thrust configuration, thereby reducing horizontal speed of the aircraft.
5. The method of claim 4 further comprising the step of vertically landing the aircraft.
6. The method of claim 1 wherein said propeller blades are forward swept propeller blades.
7. The method of claim 5 wherein said propeller blades are forward swept propeller blades.
8. A method for operating a vertical take-off and landing aircraft, said method comprising the steps of:
rotating a plurality of motor driven propeller units to a vertical thrust configuration, said plurality of motor driven propeller units coupled wings of a vertical take-off and landing aircraft;
providing power to said motor driven propeller units, thereby rotating the propellers of said motor driven propeller units;
taking off the aircraft from the ground;
transitioning the plurality of motor driven propeller units from a vertical thrust configuration towards a horizontal configuration, thereby gaining horizontal speed for the aircraft;
flying the aircraft in a forward flight configuration;
discontinuing the provision of power to some or all of the plurality of motor driven propeller units; and
stowing the propeller blades of some or all of the propellers of the motor driven propeller units while flying the aircraft in a forward flight configuration;
wherein the step of stowing the propeller blades of some or all of the propellers comprises stowing the propeller blades into recesses on the exterior surfaces of the nacelles of the motor driven propeller units, and wherein the stowed propeller blades reside fully forward of the leading edge of the wing at the location at which they are coupled to the wing.
9. The method of claim 8 further comprising the step of re-deploying the stowed propeller blades in preparation for vertical landing.
10. The method of claim 9 further comprising providing power to the previously stowed propellers.
11. The method of claim 10 further comprising the step of transitioning the plurality of motor driven propeller units from a horizontal configuration towards a vertical thrust configuration, thereby reducing horizontal speed of the aircraft.
12. The method of claim 11 further comprising the step of vertically landing the aircraft.
13. The method of claim 8 wherein said propeller blades are forward swept propeller blades.
14. The method of claim 12 wherein said propeller blades are forward swept propeller blades.