B64F1/22

MULTI-LEVEL STRUCTURE CONVEYING SYSTEM AND METHOD FOR ASSISTING UNMANNED AERIAL VEHICLE LANDING

A multi-level structure conveying system and method for assisting UAV landing are provided. The system includes conveying units and modular bottom plates. The modular bottom plate provides line connection between a power supply and a controller for the conveying unit. The conveying unit drives a UAV to move through driving a conveyor to move. Placement of the conveying units in different directions is used to control a movement direction of the UAV. The conveying units are connected through side plate modules to be arranged into conveying modules with different trajectories. The UAV moves on the conveying modules under driving of each conveying unit to reach a target position. A side plate bump of each conveying unit is sleeved opposite to a side plate recess of the adjacent conveying unit. A hollow channel formed by side plate holes of the adjacent conveying units is fixed by adopting a connecting shaft.

MULTI-LEVEL STRUCTURE CONVEYING SYSTEM AND METHOD FOR ASSISTING UNMANNED AERIAL VEHICLE LANDING

A multi-level structure conveying system and method for assisting UAV landing are provided. The system includes conveying units and modular bottom plates. The modular bottom plate provides line connection between a power supply and a controller for the conveying unit. The conveying unit drives a UAV to move through driving a conveyor to move. Placement of the conveying units in different directions is used to control a movement direction of the UAV. The conveying units are connected through side plate modules to be arranged into conveying modules with different trajectories. The UAV moves on the conveying modules under driving of each conveying unit to reach a target position. A side plate bump of each conveying unit is sleeved opposite to a side plate recess of the adjacent conveying unit. A hollow channel formed by side plate holes of the adjacent conveying units is fixed by adopting a connecting shaft.

Noise-reducing aircraft landing gear tow bar fitting

A tow bar fitting for towing an aircraft is disclosed. The tow bar fitting includes a mount, a pin support, and a tow pin. The mount includes an upper attachment and a lower attachment for affixing the tow bar fitting to a landing gear of the aircraft. The pin support extends from the mount away from the landing gear. The tow pin is positioned in the pin support such that a tow pin plane that horizontally bisects the tow pin is lower than a mount plane that horizontally bisects the upper attachment and the lower attachment when the aircraft is right-side-up on the ground.

Systems and methods for automated ground handling of aerial vehicles

Systems and methods relating to automated handline of aerial vehicles are disclosed. The described systems and methods can include a plurality of robots operating on a continuous, closed-loop track. A plurality of aerial vehicle handling stations can be disposed along the continuous, closed-loop track, and each of the plurality of robots can engage an aerial vehicles and transport it to the aerial vehicle handling station, as needed, in accordance with a workflow associated with the aerial vehicle. The described systems and methods can provide a fully automated system for the ground handling of multiple aerial vehicles simultaneously.

UNMANNED AERIAL VEHICLE AIRPORT, UNMANNED AERIAL VEHICLE SYSTEM, TOUR INSPECTION SYSTEM AND UNMANNED AERIAL VEHICLE CRUISE SYSTEM
20220396373 · 2022-12-15 ·

An unmanned aerial vehicle airport, an unmanned aerial vehicle system, a tour inspection system and an unmanned aerial vehicle cruise system. The unmanned aerial vehicle airport comprises a support base, a parking apron, a protective cover and a protective cover opening and closing driving device. The parking apron is installed on the top of the support base; the protective cover covers the top of the apron; the protective cover opening and closing driving device is installed between the support base and the protective cover, and the protective cover opening and closing driving device is configured to cause a bar linkage mechanism to drive the protective cover to switch between an open position and a closed position. The unmanned aerial vehicle airport is provided with the protective cover for the parking apron. If the protective cover is open, the unmanned aerial vehicle is parked on the parking apron, and takes off from the parking apron.

Ducted fan unmanned aerial vehicle docking station
11524798 · 2022-12-13 ·

A ducted fan unmanned aerial vehicle (UAV) docking station is provided. The docking station comprises: a guide sized to receive a ducted fan UAV; and a housing communicatively coupled to the guide. The housing comprises: a storage assembly comprising: at least one compartment sized to store the UAV; and at least one dampening system coupled to the at least one storage compartment for cushioning the UAV.

UNMANNED AERIAL SYSTEM KIOSK

A kiosk for use an unmanned aerial system (UAS) delivery system is disclosed. In one embodiment, the kiosk includes an enclosure comprising at least one vertical wall having a secured entrance therethrough to prevent unauthorized persons from entering the enclosure, wherein an external appearance of the enclosure corresponds to a location of the kiosk; a landing zone for an unmanned aerial vehicle (UAV) of the UAS located within the enclosure, the landing zone comprising infrastructure from which the UAV can take off and on which the UAV can land; sensors for detecting an environment of at least one of the kiosk and the enclosure; and a guidance system for providing signals to the UAV to guide the UAV into the enclosure and onto the landing zone.

UAV take-off and landing platform
11511886 · 2022-11-29 ·

An unmanned aerial vehicle's (UAV) take-off and landing platform. It includes a driving device, a bottom plate, a movable plate and a tractor. The tractor is connected to the front end of a bearing platform, and the tractor can drive the bearing platform to move; the bearing platform comprises the bottom plate and the movable plate. The movable plate has a first side plate, a second side plate and a third side plate. The first side plate and the second side plate are symmetrically arranged on both sides of the bottom plate, and the third side plate is arranged at the tail end of the bottom plate. The movable plate movably connects with the bottom plate and can move relative to the bottom plate with the drive of the driving device, so that the bearing platform can switch between the folded state and the unfolded state.

UAV take-off and landing platform
11511886 · 2022-11-29 ·

An unmanned aerial vehicle's (UAV) take-off and landing platform. It includes a driving device, a bottom plate, a movable plate and a tractor. The tractor is connected to the front end of a bearing platform, and the tractor can drive the bearing platform to move; the bearing platform comprises the bottom plate and the movable plate. The movable plate has a first side plate, a second side plate and a third side plate. The first side plate and the second side plate are symmetrically arranged on both sides of the bottom plate, and the third side plate is arranged at the tail end of the bottom plate. The movable plate movably connects with the bottom plate and can move relative to the bottom plate with the drive of the driving device, so that the bearing platform can switch between the folded state and the unfolded state.

TRAM SYSTEM AND METHODS FOR AUTONOMOUS TAKEOFF AND LANDING OF AIRCRAFT
20230055331 · 2023-02-23 ·

One variation of a tram system includes: a chassis; a latch configured to selectively engage a latch receiver mounted to an aircraft; an alignment feature adjacent the latch and configured to engage an alignment receiver mounted to the aircraft and to communicate acceleration and braking forces from the chassis into the aircraft; an optical sensor facing upwardly from the chassis; a drivetrain configured to accelerate and decelerate the chassis along a runway; and a controller configured to detect an optical fiducial arranged on the aircraft in optical images recorded by the optical sensor adjust a speed of the drivetrain to longitudinally align the alignment feature with the alignment receiver based on positions of the optical fiducial detected in the optical images, trigger the latch to engage the latch receiver once the aircraft has descended onto the chassis, and trigger the drivetrain to actively decelerate the chassis during a landing routine.