Patent classifications
B64D1/22
Robot and Unmanned Aerial Vehicle (UAV) Systems for Cell Sites and Towers
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.
Aircraft
To provide an aircraft that can efficiently improve speed performance and fuel efficiency, the aircraft is an aircraft capable of forward flight and hovering, and includes a lift generating part, a frame for holding the lift generating part, and a loadable object provided on the frame and to be mounted. The front projection area of the frame and the mounting part during forward flight is smaller than the front projection area of the frame and the mounting part during hovering.
Aircraft
To provide an aircraft that can efficiently improve speed performance and fuel efficiency, the aircraft is an aircraft capable of forward flight and hovering, and includes a lift generating part, a frame for holding the lift generating part, and a loadable object provided on the frame and to be mounted. The front projection area of the frame and the mounting part during forward flight is smaller than the front projection area of the frame and the mounting part during hovering.
Automated water volume estimation
According to an aspect, a computer-implemented method for water volume estimation includes detecting water based at least in part on sensor-based data; determining a volume of water based at least in part on the sensor-based data; determining a location at the water for an aircraft to retrieve water via a water retrieving apparatus; and translating the location of the water into pilot inputs to guide the aircraft to the water.
Automated water volume estimation
According to an aspect, a computer-implemented method for water volume estimation includes detecting water based at least in part on sensor-based data; determining a volume of water based at least in part on the sensor-based data; determining a location at the water for an aircraft to retrieve water via a water retrieving apparatus; and translating the location of the water into pilot inputs to guide the aircraft to the water.
Corner attachment assemblies for suspended payload containers of aircrafts
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.
Corner attachment assemblies for suspended payload containers of aircrafts
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.
PACKAGE DELIVERY SYSTEMS AND RELATED METHODS
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.
PACKAGE DELIVERY SYSTEMS AND RELATED METHODS
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.
Systems, devices, and methods for agricultural sample collection
The present subject matter relates to systems, devices, and methods for agricultural sample collection. In one aspect, a sample collection system includes an aerial robotic platform, an arm assembly coupled to the aerial robotic platform and comprising an arm that extends away from the aerial robotic platform, and a sample collector connected to a distal end of the arm, wherein the sample collector is configured to selectively remove one or more samples of agricultural material from a plant to be analyzed.