A retractable runway edge sheave for use in an aircraft arresting system. The arresting system functions to extend a cable across a runway for capture by a tailhook of an aircraft. The retractable runway edge sheave is designed to raise and lower the cable. The disclosed system may also feature a ramping system.

A tailhook with a telescopic lever, a fixed jaw, a sliding jaw, a pivot arm, and a cam arm. The lever has a second lever and a first lever end attached to a ring to which a pulling force can be applied, which allows the tailhook to test and exercise an arresting cable. The sliding jaw and the fixed jaw communicate such that the arresting cable can be accepted and clamped. The second lever end is attached to the fixed jaw, while the fixed jaw includes a thumb screw that provides tension adjustment for the fixed jaw. The pivot arm provides a clamping force, and the cam arm provides a mechanical linkage between the fixed jaw and the sliding jaw such that when force is applied to the pivot arm, the cam arm moves the sliding jaw to clamp together or unclamp the fixed jaw and the sliding jaw.

A tailhook with a telescopic lever, a fixed jaw, a sliding jaw, a pivot arm, and a cam arm. The lever has a second lever and a first lever end attached to a ring to which a pulling force can be applied, which allows the tailhook to test and exercise an arresting cable. The sliding jaw and the fixed jaw communicate such that the arresting cable can be accepted and clamped. The second lever end is attached to the fixed jaw, while the fixed jaw includes a thumb screw that provides tension adjustment for the fixed jaw. The pivot arm provides a clamping force, and the cam arm provides a mechanical linkage between the fixed jaw and the sliding jaw such that when force is applied to the pivot arm, the cam arm moves the sliding jaw to clamp together or unclamp the fixed jaw and the sliding jaw.

An unmanned aerial vehicle that delivers a package includes a plurality of rotary wings, a plurality of first motors, a main body, a connector, a movable block, and a processor. When the connector is connected to a rail, the processor sets a rotation rate of the plurality of first motors to a rotation rate that is lower than a minimum rotation rate necessary for floating and higher than a minimum rotation rate necessary for propulsion along the rail. Furthermore, the processor causes the movable block to increase the angle formed by the normal direction of an imaginary plane containing the plurality of rotary wings relative to a support direction of the connector.

A system for anchoring unmanned aerial vehicles to surfaces includes a landing pad configured to be installed on an agricultural machine, with the landing pad defining a landing surface. Furthermore, the system includes an unmanned aerial vehicle (UAV) configured to land on the landing surface and a top surface of a field across which the agricultural machine is traveling. The UAV, in turn, includes an anchoring device configured to engage soil within the field to anchor the UAV to the field when the UAV has landed on the top surface of the field. Additionally, the anchoring device is further configured to engage the landing pad to anchor the UAV to the landing surface when the UAV has landed on the landing pad.

Unmanned aerial vehicle (UAV) tethered wing recovery is disclosed. An example apparatus includes a detachable portion of a wing that is couplable to a fixed portion of the wing, a lock configured to fasten the detachable portion to the fixed portion, where the lock is to disengage the detachable portion from the fixed portion upon contact of the wing with a recovery device, and a tether configured to extend between the detachable and fixed portions.

Unmanned aerial vehicle (UAV) tethered wing recovery is disclosed. An example apparatus includes a detachable portion of a wing that is couplable to a fixed portion of the wing, a lock configured to fasten the detachable portion to the fixed portion, where the lock is to disengage the detachable portion from the fixed portion upon contact of the wing with a recovery device, and a tether configured to extend between the detachable and fixed portions.

Aerial launch and/or recovery for unmanned aircraft, and associated systems and methods are described. A representative system includes a first, carrier aircraft having an airframe, a propulsion system carried by the airframe and positioned to support the carrier aircraft in hover, and a capture line carried by the carrier aircraft and deployable to hang from the carrier aircraft. The capture line is sized to releasably engage with a capture device of a second, carried aircraft. The system further includes a retrieval device positioned to support the carried aircraft for detachment from the capture line.

Aerial launch and/or recovery for unmanned aircraft, and associated systems and methods are described. A representative system includes a first, carrier aircraft having an airframe, a propulsion system carried by the airframe and positioned to support the carrier aircraft in hover, and a capture line carried by the carrier aircraft and deployable to hang from the carrier aircraft. The capture line is sized to releasably engage with a capture device of a second, carried aircraft. The system further includes a retrieval device positioned to support the carried aircraft for detachment from the capture line.

A tailhook with a telescopic lever, a fixed jaw, a sliding jaw, a pivot arm, and a cam arm. The lever has a second lever and a first lever end attached to a ring to which a pulling force can be applied, which allows the tailhook to test and exercise an arresting cable. The sliding jaw and the fixed jaw communicate such that the arresting cable can be accepted and clamped. The second lever end is attached to the fixed jaw, while the fixed jaw includes a thumb screw that provides tension adjustment for the fixed jaw. The pivot arm provides a clamping force, and the cam arm provides a mechanical linkage between the fixed jaw and the sliding jaw such that when force is applied to the pivot arm, the cam arm moves the sliding jaw to clamp together or unclamp the fixed jaw and the sliding jaw.