An aircraft store ejector systems and subsystems thereof. Embodiments can include a two-reservoir re-pressurization system wherein a remote reservoir is used to maintain desired pressure in a local ejector reservoir. The system can include a release valve having a vent valve and valve piston. The release valve can control release of pressurized gas to a pitch control valve. The pitch control valve can be configured to distribute the pressurized gas between two or more ejector piston assemblies. One or more of the ejector piston assemblies can include multiple concentric piston stages and piston chambers, the piston chambers configured to contain a volume of gas. The ejector piston assemblies can be configured to compress the volume of gas within the piston chambers as the piston stages are extended out from the aircraft. Such compression can provide a return force to the piston stages.

A method for passive aerial cord release mechanisms and an aerial cord release mechanism for an aerial vehicle (AV). A method includes determining a retracting force to be applied to a winch of an aerial vehicle (AV), wherein the determined retracting force is a force required to retract a cord to be coiled around the winch within the AV, and the cord is temporarily coupled to the winch, such that an external force exceeding a predetermined threshold causes decoupling between the cord and the winch.

A method for passive aerial cord release mechanisms and an aerial cord release mechanism for an aerial vehicle (AV). A method includes determining a retracting force to be applied to a winch of an aerial vehicle (AV), wherein the determined retracting force is a force required to retract a cord to be coiled around the winch within the AV, and the cord is temporarily coupled to the winch, such that an external force exceeding a predetermined threshold causes decoupling between the cord and the winch.

In various embodiments, the present disclosure relates to robot systems configured to operate on a cell tower to inspect, install, reconfigure, and repair cellular equipment. The present disclosure provides a robot system for performing audit tasks of cell towers. The robot system includes an Unmanned Arial Vehicle (UAV) adapted to transport a robot to the cell tower; and a robot including a body portion configured to hold various electronic components of the robot including monitoring equipment disposed thereon, one or more arms extending from the body portion adapted to manipulate components of a cell tower and to facilitate movement of the robot on the cell tower, and wireless interfaces adapted to allow wireless control of the robot. The robot is configured to be controlled by one of a user in a remote location, a user at the cell tower site, and autonomously via direct programing.

In various embodiments, the present disclosure relates to robot systems configured to operate on a cell tower to inspect, install, reconfigure, and repair cellular equipment. The present disclosure provides a robot system for performing audit tasks of cell towers. The robot system includes an Unmanned Arial Vehicle (UAV) adapted to transport a robot to the cell tower; and a robot including a body portion configured to hold various electronic components of the robot including monitoring equipment disposed thereon, one or more arms extending from the body portion adapted to manipulate components of a cell tower and to facilitate movement of the robot on the cell tower, and wireless interfaces adapted to allow wireless control of the robot. The robot is configured to be controlled by one of a user in a remote location, a user at the cell tower site, and autonomously via direct programing.

The present disclosure belongs to the technical field of unmanned aerial vehicles, and specifically relates to an airdrop device used with an unmanned aerial vehicle. The airdrop device includes a clamping jaw bearing block, a control panel, a power supply, a power source, and a photosensitive sensor. The clamping jaw bearing block is used to be detachably connected with an unmanned aerial vehicle; the control panel, the power supply, the power source, and the photosensitive sensor are all mounted on the clamping jaw bearing block; and the output end of the power source is provided with an engine arm used to hang a material bag. The power supply, the power source, and the photosensitive sensor are all connected with the control panel; and the control panel receives a light signal detected by the photosensitive sensor and controls the power source to act. The airdrop device used with the unmanned aerial vehicle of the present disclosure has a simple and reasonable structure. The clamping claw bearing block is detachably connected to the unmanned aerial vehicle, and the material bag is hung on the engine arm. When materials need to be thrown in air, light below the fuselage of the unmanned aerial vehicle is turned on, and the control panel receives the light signal detected by the photosensitive sensor and controls the power source to act so that the engine arm rotates to detach the material bag.

Presented are corner attachment assemblies for cargo suspension systems, methods for making/using such assemblies, and aircraft equipped with underbody suspension systems using corner attachment assemblies for securing payload containers. Mounting assemblies are presented for securing objects to tether cables of suspension systems. A representative cargo mounting assembly includes a pair of shoulder clamps, each of which includes a flap that projects from a cup. Each shoulder clamp flap mechanically attaches, e.g., via a flap through-hole with a structurally reinforcing grommet, to a respective segment of a tether cable of a cargo suspension system. In addition, each shoulder clamp cup includes multiple noncoplanar, mutually adjoining contact surfaces. For instance, the cup may have a tetrahedral geometry with three mutually orthogonal, triangular-shaped contact surfaces. Each contact surface attaches, e.g., via a high-strength adhesive, to a respective surface of a corner of a cargo container.

Delivery systems for aerial vehicles include a plurality of securement straps configured to secure a package during flight of an aerial vehicle, at least one retaining strap, and a release mechanism. A proximal end region of each securement strap and a first end region of the at least one retaining strap are coupled to the aerial vehicle. A distal end region of each securement strap is coupled to the release mechanism such that when the release mechanism is actuated the release mechanism releases the distal end region of at least one securement strap of the plurality of securement straps, thereby delivering the package. The release mechanism remains coupled to a second end region of the at least one retaining strap when the release mechanism is actuated such that the securement straps, release mechanism, and retaining strap all may be pulled up and away from the package after delivery.

Delivery systems for aerial vehicles include a plurality of securement straps configured to secure a package during flight of an aerial vehicle, at least one retaining strap, and a release mechanism. A proximal end region of each securement strap and a first end region of the at least one retaining strap are coupled to the aerial vehicle. A distal end region of each securement strap is coupled to the release mechanism such that when the release mechanism is actuated the release mechanism releases the distal end region of at least one securement strap of the plurality of securement straps, thereby delivering the package. The release mechanism remains coupled to a second end region of the at least one retaining strap when the release mechanism is actuated such that the securement straps, release mechanism, and retaining strap all may be pulled up and away from the package after delivery.

A parafoil for operation at high altitudes, in low density air, or at low airspeeds, and methods for opening same. Some versions of the parafoil comprise flexible members connected to the parafoil canopy. When the parafoil canopy is in a stowed configuration, the members are deformed, storing elastic energy. When the canopy is released from its stowed configuration, the members spring back to their undeformed shapes, thereby opening or assisting with opening the canopy. The flexible member may also be attached to a base structure, which is attached to the payload. The members may comprise rods or hollow tubes that can be flexed using a fulcrum near the base structure, or a spacer plate, so that the ends connected to the canopy are restrained by a parachute bag containing the stowed or packed canopy. The parachute bag can be opened prior to or during detachment of the parafoil from the flight vehicle.