Unmanned supply delivery aircraft
A heavy payload, autonomous UAV able to deliver supply by way of airdrop with more precision and at a lower cost. The UAV is equipped with two movable wing systems that rotate from a stowed position to a deployed position upon jettison of the UAV from a mothership. The UAV can be controlled remotely or it can operate autonomously and the movable wings can include ailerons to effectuate flight control of the UAV. The UAV can be reusable or can be an expendable UAV.
1. An unmanned delivery aircraft comprising:
a fuselage;
a lid capable of engaging the fuselage;
a first pivoting wing system connected to the lid;
a second pivoting wing system connected to the lid;
wherein each of the first and second pivoting wing systems fits inside the fuselage when the lid is engaged to the fuselage in a wings-down orientation; and
wherein each of the first and second pivoting wing systems are configured to rotate from a stowed position to a deployed position outside of the fuselage when the lid is engaged to the fuselage in a wings-up orientation.
2. The unmanned delivery aircraft of claim 1 , wherein the first and second pivoting wing systems each comprises two wings configured to rotate between a stowed position and a deployed position.
3. The unmanned delivery aircraft of claim 2 , wherein a rotation angle between the stowed position and deployed position is 90 degrees.
4. The unmanned delivery aircraft of claim 2 , wherein the two wings of the first pivoting wing system are vertically spaced at different elevations relative to the two wings of the second pivoting wing system.
5. The unmanned delivery aircraft of claim 2 wherein the first and second pivoting wing systems comprise at least one of:
a spring-loaded plunger;
a latch;
a pin;
configured to hold at least one wing in a stowed and/or deployed position.
6. An unmanned delivery aircraft comprising:
a fuselage;
a lid;
a first pivoting wing attached to a first end portion of the lid;
a second pivoting wing attached to a second end portion of the lid;
a spring connecting the first pivoting wing to the second pivoting wing;
a release mechanism restraining first and second pivoting wings in stowed positions and resisting the potential energy of the spring;
wherein the triggering of the release mechanism causes the potential energy of the spring to move first and second pivoting wings from stowed positions to deployed positions, and
wherein in the stowed positions the first and second pivoting wings fit inside the fuselage when the lid is engaged to the fuselage in a wings-down orientation.
7. The unmanned delivery aircraft of claim 6 , wherein the stowed and deployed positions are determined by the geometry of a lock plate.
8. The unmanned delivery aircraft of claim 6 , wherein the spring is an extension spring and connects to first and second pivoting wings through a pivot arm on each wing configured to provide mechanical leverage to cause the wings to pivot from stowed positions to deployed positions by the potential energy of the extension spring.
9. The unmanned delivery aircraft of claim 6 , further comprising a third pivoting wing attached to the first end portion of the lid and a fourth pivoting wing attached to the second end portion of the lid.
10. The unmanned delivery aircraft of claim 9 , wherein the first, second, third, and fourth pivoting wings are vertically spaced to form a vertical wing stack with alternating front and rear wings.
11. An unmanned delivery aircraft comprising:
a fuselage with an open side to receive cargo;
a lid to engage the open side of the fuselage;
a front pivoting wing system connected to the lid;
a rear pivoting wing system connected to the lid;
wherein each of the front and rear pivoting wing systems fits inside the fuselage when the lid is attached to the fuselage in a wings-down orientation; and
wherein each of the front and rear pivoting wing systems are configured to rotate from a stowed position to a deployed position when the lid is attached to the fuselage in a wings-up orientation.
12. The unmanned delivery aircraft of claim 11 , wherein the fuselage is rectangular.
13. The unmanned delivery aircraft of claim 11 , further comprising a nose cone and tail cone.
14. The unmanned delivery aircraft of claim 13 , wherein at least one of the nose cone and tail cone are configured to be assembled by an operator from pieces located inside the fuselage.
15. The unmanned delivery aircraft of claim 11 , further comprising an on-board autopilot capable of autonomous flight control.
16. The unmanned delivery aircraft of claim 15 , wherein the autopilot is located in a nose cone attached to the fuselage.
17. The unmanned delivery aircraft of claim 15 , wherein the autopilot controls one or more actuators connected to one or more flight control surfaces located in one or more wings of the first or second pivoting wing system.
18. The unmanned delivery aircraft of claim 11 , wherein the wings are triggered to rotate from a stowed position to a deployed position by one or more static lines operating on one or more release mechanisms.
19. The unmanned delivery aircraft of claim 11 , further comprising a drogue parachute.
20. The unmanned delivery aircraft of claim 11 , wherein each of the front and rear pivoting wing systems comprise two wings.