Autonomous package delivery aircraft
An autonomous package delivery aircraft is operable to transition between thrust-borne lift in a VTOL orientation and wing-borne lift in a forward flight orientation. The aircraft includes an airframe with a distributed thrust array coupled thereto. A flight control system is operably associated with the distributed thrust array and is configured to independently control each of the propulsion assemblies of the distributed thrust array. A package delivery module is coupled to the airframe. In the VTOL orientation, a first pair of propulsion assemblies is forward of the package delivery module while a second pair of propulsion assemblies is aft of the package delivery module. In a forward flight orientation, the first pair of propulsion assemblies is below the package delivery module and the second pair of propulsion assemblies is above the package delivery module.
1. An aircraft operable to transition between thrust-borne lift in a VTOL orientation and wing-borne lift in a forward flight orientation, the aircraft comprising:
an airframe including first and second wings having a generally parallel relationship with first and second pylons each extending between the first and second wings;
a distributed thrust array coupled to the airframe including at least a first pair of propulsion assemblies and a second pair of propulsion assemblies;
a flight control system operably associated with the distributed thrust array and configured to independently control each of the propulsion assemblies; and
a package delivery module coupled to the airframe;
wherein, in the VTOL orientation, the first wing is forward of the package delivery module, the second wing is aft of the package delivery module, the first and second pylons are lateral of the package delivery module, the first pair of propulsion assemblies is forward of the package delivery module and the second pair of propulsion assemblies is aft of the package delivery module; and
wherein, in the forward flight orientation, the first wing is below the package delivery module, the second wing is above the package delivery module, the first and second pylons are lateral of the package delivery module, the first pair of propulsion assemblies is below the package delivery module and the second pair of propulsion assemblies is above the package delivery module.
2. The aircraft as recited in claim 1 wherein each of the propulsion assemblies is a non thrust vectoring propulsion assembly.
3. The aircraft as recited in claim 1 wherein each of the propulsion assemblies is a single-axis thrust vectoring propulsion assembly.
4. The aircraft as recited in claim 1 wherein each of the propulsion assemblies is an omnidirectional thrust vectoring propulsion assembly.
5. The aircraft as recited in claim 1 wherein each propulsion assembly of the first pair is coupled to the first wing and each propulsion assembly of the second pair is coupled to the second wing.
6. The aircraft as recited in claim 1 wherein each propulsion assembly of the first pair is coupled to a respective outboard end of the first wing and each propulsion assembly of the second pair is coupled to a respective outboard end of the second wing.
7. The aircraft as recited in claim 1 wherein each of the propulsion assemblies is coupled to the airframe outboard of the package delivery module.
8. The aircraft as recited in claim 1 wherein the distributed thrust array includes a third pair of propulsion assemblies that are symmetrically disposed to one another and a fourth pair of propulsion assemblies that are symmetrically disposed to one another.
9. The aircraft as recited in claim 8 wherein, in both the VTOL orientation and the forward flight orientation, the third pair of propulsion assemblies is operable to generate thrust having a first direction while the fourth pair of propulsion assemblies is operable to generate thrust having a second direction that is different from the first direction.
10. The aircraft as recited in claim 8 wherein, in the VTOL orientation, one of the propulsion assemblies of each of the third and fourth pairs of propulsion assemblies is forward of the package delivery module and the other of the propulsion assemblies of each of the third and fourth pairs of propulsion assemblies is aft of the package delivery module; and
wherein, in the forward flight orientation, one of the propulsion assemblies of each of the third and fourth pairs of propulsion assemblies is below the package delivery module and the other of the propulsion assemblies of each of the third and fourth pairs of propulsion assemblies is above the package delivery module.
11. The aircraft as recited in claim 1 wherein each of the propulsion assemblies further comprises an electric motor and a rotor assembly coupled to the electric motor.
12. The aircraft as recited in claim 1 wherein the distributed thrust array further comprises a two-dimensional thrust array.
13. The aircraft as recited in claim 1 wherein the flight control system is configured for autonomous flight control.
14. The aircraft as recited in claim 1 wherein the flight control system is configured to independently control a rotor speed of each of the propulsion assemblies.
15. The aircraft as recited in claim 1 wherein, in the forward flight orientation, the package delivery module has a level flight attitude.
16. The aircraft as recited in claim 1 wherein the package delivery module is nonrotatable relative to the airframe.
17. The aircraft as recited in claim 1 wherein the flight control system is configured to enable vertical takeoffs and landings relative to unlevel surfaces.
18. The aircraft as recited in claim 1 wherein the flight control system is configured to enable self-docking.
19. The aircraft as recited in claim 1 wherein the package delivery module further comprises an unmanned package delivery module.
20. An aircraft operable to transition between thrust-borne lift in a VTOL orientation and wing-borne lift in a forward flight orientation, the aircraft comprising:
an airframe including first and second wings having a generally parallel relationship with first and second pylons each extending between the first and second wings;
a distributed thrust array coupled to the airframe including a first pair of propulsion assemblies and a second pair of propulsion assemblies;
a flight control system operably associated with the distributed thrust array and configured for autonomous flight control including independent speed control of each of the propulsion assemblies; and
a package delivery module coupled to the airframe;
wherein, in the VTOL orientation, the first wing and the first pair of propulsion assemblies are forward of the package delivery module and the second wing and the second pair of propulsion assemblies are aft of the package delivery module; and
wherein, in the forward flight orientation, the first wing and the first pair of propulsion assemblies are below the package delivery module and the second wing and the second pair of propulsion assemblies are above of the package delivery module.