An unmanned aerial vehicle according to certain embodiments generally includes a chassis, a power supply mounted to the chassis, a control system operable to receive power from the power supply, at least one rotor operable to generate lift under control of the control system, and a winch mounted to the chassis. The winch includes a reel and a motor. The reel has a line wound thereon, the line having a free end. The reel includes a circumferential channel in which a wound portion of the line is wound onto the reel. The circumferential channel includes an inner portion, an outer portion, and a passage connecting the inner portion and the outer portion. The motor is operable to rotate the reel under control of the control system to thereby cause the line to wind onto and off of the reel, thereby causing the free end of the line to raise and lower.

An unmanned aerial vehicle according to certain embodiments generally includes a chassis, a power supply mounted to the chassis, a control system operable to receive power from the power supply, at least one rotor operable to generate lift under control of the control system, and a winch mounted to the chassis. The winch includes a reel and a motor. The reel has a line wound thereon, the line having a free end. The reel includes a circumferential channel in which a wound portion of the line is wound onto the reel. The circumferential channel includes an inner portion, an outer portion, and a passage connecting the inner portion and the outer portion. The motor is operable to rotate the reel under control of the control system to thereby cause the line to wind onto and off of the reel, thereby causing the free end of the line to raise and lower.

A hybrid aerial vehicle (HAV) comprising: a fuselage of the HAV; a first mechanism within the fuselage for accepting a plurality of wings of the HAV, the first mechanism allowing coordinated contraction of the plurality of wings essentially into the fuselage such that tips of the wings are position in proximity of the fuselage and coordinated extension of the wings such that tips of each wing are positioned away from the fuselage; a first wing extending from the port side of the fuselage and connected to the first mechanism; a second wing extending from the starboard side of the fuselage and connected to the first mechanism; a second mechanism placed within the fuselage in proximity to its front end, the second mechanism allowing motion of propellers of the HAV affixed there to between a first plain and a second plain; a first set of propellers affixed at the port side of the fuselage to the second mechanism; a second set of propellers affixed at the starboard side of the fuselage to the second mechanism; a third mechanism placed within the fuselage in proximity to its rear end, the third mechanism allowing motion of propellers of the HAV affixed there to between a first plain and a second plain, and further placing the propellers affixed thereto to be at a vertical displacement with respect to the propellers affixed to the second mechanism; a third set of propellers affixed at the port side of the fuselage to the third mechanism; and a fourth set of propellers affixed at the starboard side of the fuselage to the third mechanism.

A parcel safe for remote vehicle pickup and delivery of packages including a container having an opening for receiving or deploying packages. The container has a lockable lid associated with the opening and has a closed position and an open position. The container and associated lid define a package receiving surface in the open position. Alignment apparatus is associated with the package receiving surface and provides an index for a receiving point of the package receiving surface. The alignment apparatus is designed for use by a remote vehicle in a pickup or delivery process.

A parcel safe for remote vehicle pickup and delivery of packages including a container having an opening for receiving or deploying packages. The container has a lockable lid associated with the opening and has a closed position and an open position. The container and associated lid define a package receiving surface in the open position. Alignment apparatus is associated with the package receiving surface and provides an index for a receiving point of the package receiving surface. The alignment apparatus is designed for use by a remote vehicle in a pickup or delivery process.

An exemplary embodiment may provide a robotic powered cargo handling system. An embodiment may implement a pallet-lift mechanism to lift cargo or pallets. Powered rollers may be embedded into the forks of a pallet-lift mechanism and on top of the vehicle body. An exemplary embodiment may be fully autonomous. A user or software may direct the vehicle to a pallet or piece of cargo and set a destination for the cargo. Sensors, cameras, GPS, and computer vision may be implemented to navigate and avoid obstacles. An exemplary embodiment may include independent 4-wheel steering, 4 corner height adjustment, in-hub electric motors, and pneumatic or solid tires.

Cargo may be optimally placed within a cargo hold using a cargo mover comprising a flexible conveyor belt extending from a ground location to a cargo hold, data defining a dimensional map of available space existing within the cargo hold for placement of cargo, a conveyor controller operatively in communication with the flexible conveyer belt and comprising packing software, and a smart loader comprising a predetermined set of scanning sensors operative to scan the cargo hold and a processor operatively in communication with the predetermined set of sensors and the conveyor controller. An interior of the cargo hold is scanned to create a dimensional map of the cargo hold and cargo placed onto the flexible conveyor belt where certain of each piece is cargo's physical dimensions are scanned. The processor compares the scanned cargo hold data set with the cargo's physical dimensions as well as with an order in which that piece of cargo will arrive at the smart loader to determine the placement of each piece of cargo. As each piece of cargo is placed into cargo hold, the smart loader continues to scan and update the dimensional map of the cargo hold to determine where each subsequent piece of cargo will be placed in the cargo hold.

Cargo may be optimally placed within a cargo hold using a cargo mover comprising a flexible conveyor belt extending from a ground location to a cargo hold, data defining a dimensional map of available space existing within the cargo hold for placement of cargo, a conveyor controller operatively in communication with the flexible conveyer belt and comprising packing software, and a smart loader comprising a predetermined set of scanning sensors operative to scan the cargo hold and a processor operatively in communication with the predetermined set of sensors and the conveyor controller. An interior of the cargo hold is scanned to create a dimensional map of the cargo hold and cargo placed onto the flexible conveyor belt where certain of each piece is cargo's physical dimensions are scanned. The processor compares the scanned cargo hold data set with the cargo's physical dimensions as well as with an order in which that piece of cargo will arrive at the smart loader to determine the placement of each piece of cargo. As each piece of cargo is placed into cargo hold, the smart loader continues to scan and update the dimensional map of the cargo hold to determine where each subsequent piece of cargo will be placed in the cargo hold.

A cargo receiving facility includes a net and a transport mechanism. The net is suspended among supports. The net is configured to receive a cargo dropped from an unmanned aircraft in flight. The transport mechanism is configured to transport the cargo received by the net. The net has an elasticity corresponding to a mass of the cargo. The net has openings each having a size corresponding to a pressure of down-wash from the unmanned aircraft.

A cargo receiving facility includes a net and a transport mechanism. The net is suspended among supports. The net is configured to receive a cargo dropped from an unmanned aircraft in flight. The transport mechanism is configured to transport the cargo received by the net. The net has an elasticity corresponding to a mass of the cargo. The net has openings each having a size corresponding to a pressure of down-wash from the unmanned aircraft.