Patent classifications
B64U2101/69
PORTABLE EMERGENCY TELEHEALTH SYSTEM AND METHOD
A system and method for providing remote healthcare. The system includes a server and a medical kit. A remote patient in need of medical care or a bystander (user) may access and use the medical kit. The remote patient and/or other user may enter data of the condition of the patient via a user interface of the medical kit. A processor of the medical kit receives data and sends the data over a wireless network to the server via communications interfaces. The processor of the medical kit than receives data including instructions for using the plurality of medical tools from the server and produces the instructions to the user via the user interface.
Aircraft with independently controllable propulsion assemblies
In some embodiments, an aircraft includes a flying frame having an airframe, a distributed propulsion system attached to the airframe, a flight control system operably associated with the distributed propulsion system and a pod assembly selectively attachable to the flying frame. The distributed propulsion system includes a plurality of propulsion assemblies that are independently controlled by the flight control system, thereby enabling the flying frame to have a vertical takeoff and landing mode and a forward flight mode.
DISTANCE SENSED VERTICAL DESCENT ARREST SYSTEM AND METHODS
An aerial payload vehicle descent arrest system, method operating and device, including an aerial payload vehicle configured to descend along a predetermined flightpath toward a target destination, a descent state detection system configured to receive sensor output information from a plurality of sensors, to compute a sensed distance to the target destination based on sensor output information from at least two sensors of the plurality of sensors, and to generate a descent arrest device trigger signal based on a sensed altitude, and a descent arrest device configured to receive the descent arrest device trigger signal from the descent state detection system and to decelerate the aerial payload vehicle before a payload from the aerial payload vehicle is delivered to the target destination.
Aerial package delivery system
Systems and methods for delivering packages via aerial vehicles are disclosed. The system can comprise a label that includes a parachute to enable the packages to be dropped from the aerial vehicle, yet land at the package's destination without damage. The system can include a self-adhesive backing, a plurality of parachute cords, a parachute, and a breakaway cover. The parachute cords can include a shock absorber to reduce the shock on the package of the parachute opening. The parachute and/or the breakaway cover can include graphics to provide address, velocity, or spin information for the package. The parachute cords can include a harness to separate the cords and reduce tangling of the cords and spinning of the parachute canopy with respect to the package.
Drone location signature filters
Techniques for providing a verification of a flight path or landing zone may be provided. For example, during delivery an unmanned aerial vehicle (UAV) may capture one or more images of a plurality of delivery locations within an area. A computer system may generate one or more image templates or filters using the one or more images and subsequently use the image filters to verify a flight path or landing zone for a delivery by the UAV during flight.
Unmanned aerial vehicle protection airbag
An unmanned aerial vehicle (UAV) airbag may protect protection for a UAV or other objects when making contact with one another. The UAV airbag may at least partially surround the UAV while allowing the UAV to remain at least partially operable. In some embodiments, the UAV airbag may be inflated just prior to making contact with another object. After inflation, the UAV airbag may be at least partially sealed to reduce or inhibit deflation of the UAV airbag, but possibly not to completely prevent airflow from the UAV airbag upon contact with another object. The UAV airbag may exhaust some air upon impact, thereby reducing a deceleration of a UAV contained inside of the UAV airbag.
Radio controlled aircraft, remote controller and methods for use therewith
A radio controlled (RC) vehicle includes a receiver configured to receive a radio frequency (RF) signal from a remote control device. The RF signal indicates command data in accordance with a first coordinate system that is from a perspective of the remote control device. The command data includes a lift command associated with a hovering state of the RC vehicle. One or more motion sensors are configured to generate motion data that indicates a position of the RC vehicle and an orientation of the RC vehicle. A processor is configured to transform the command data into control data based on the motion data and in accordance with a second coordinate system that is from a perspective of the RC vehicle. A plurality of control devices are configured to control motion of the RC vehicle based on the control data.
Plug-and-play multifunctional attachment of remote control rotorcraft
A plug-and-play multifunctional attachment of a remote control rotorcraft, which includes: an attachment body that includes a device board and a remote control receiver unit. The device board has a top surface to which a first coupling member is mounted. The remote control receiver unit is mounted to and electrically connected to a bottom surface of the device board. Wireless transmission of a signal is enabled between a remote control device and the remote control receiver unit. A second coupling member is mounted to a bottom of an unmanned aircraft to enable selective engagement and coupling between the second coupling member and the first coupling member.
FLYING VEHICLE SYSTEMS AND METHODS
A method according to certain embodiments generally involves operating a system including an unmanned aerial vehicle (UAV) and a base station. The base station includes a nest including an upper opening having an upper opening diameter and a lower opening having a lower opening diameter less than the upper opening diameter. The lower opening is accessible from within the base station. The method generally includes landing the UAV within the nest such that a portion of the UAV is accessible via the lower opening, releasably attaching a load to the UAV, and operating the UAV to deliver the load to a destination.
Drone load release system
A drop kit that attaches to a pair of parallel picatinny rails one drone uses a pair of drop mechanisms that hold one side of a load bearing basket. The opposing side of the basket is pivotally secured to a goggle plate. Each drop mechanism is attached to one of the rails and the goggle plate to both of the rails via a spring-loaded centering clamp system. The drop mechanisms use a drop cam that rotates between and open and closed position so that when the drone arrives at a desired spot, a signal is provided to a pair of motors, each motor associated with one of the drop mechanisms, in order to rotate the drop cam into its open position, releasing its side of the basket with the opposing side of the basket pivoting and then falling free of the goggle plate.