B64U30/291

OPTICAL-BASED AERIAL GAMING SYSTEMS
20180207540 · 2018-07-26 ·

An optical-based aerial gaming system comprises: a multirotor unmanned flying device comprising: a main body; a plurality of propulsion units, a wireless receiver configured to receive data via radio communication; a wireless transmitter configured to send data via radio communication; one or more light generators configured to project laser or infrared light from the unmanned flying device; and one or more light sensors configured to detect laser or infrared light projected by a separate unmanned flying device; and a remote control unit comprising: a wireless transmitter configured to send data via radio communication; and a wireless receiver configured to receive data via radio communication, wherein the unmanned flying device is configured to transmit to the remote control unit, using the wireless transmitter of the unmanned flying device, at least a portion of encoded data of the detected laser or infrared light.

SYSTEMS AND METHODS FOR FOLDABLE ARMS
20180170541 · 2018-06-21 ·

An unmanned aerial vehicle (UAV) comprises a central body, a plurality of arms that extend out from the central body, and a plurality of rotors. Each arm has one or more joints that segment the arm into a stem portion proximal to the central body and one or more branch portions distal to the central body. The one or more joints permit the one or more branch portions to move horizontally relative to the stem portion between an extended state and a compacted state. The one or more branch portions are arranged substantially parallel to a perimeter edge of the central body in the compacted state. Each rotor in the plurality is attached to the one or more branch portions.

Detachable propeller holder device

A detachable propeller holder device includes a propeller holder module, a fixed seat and a motor module. Paddles are located the propeller holder module, a buckling component is located on the propeller holder module, the buckling component includes two elastic arms and two hooks, the two elastic arms are symmetrically located at two sides of the propeller holder module, the hooks are respectively located at an end of the two elastic arms and are respectively buckled with two limit portions which are symmetrically located at the fixed seat, so as to fix the propeller holder module to the fixed seat. In the present invention, only the buckling component at the side of the propeller holder module is pinched by fingers to deform inwardly till the hooks are detached from the limit portions of the fixed seat, and then the propeller holder module is pulled upwardly to be removed.

FLEXIBLE PRINTED CIRCUIT BOARDS AND RELATED METHODS

Flexible printed circuit boards and related methods are disclosed herein. An example printed circuit board includes a controller interface coupled to a surface of the printed circuit board between a first end of the printed circuit board and a second end of the printed circuit board. The example printed circuit board includes a connector coupled to the surface proximate to the first end. The example printed circuit board includes a notch formed between the controller interface and the connector. The notch is to form a narrowed portion of the printed circuit board to enable the printed circuit board to bend at the narrowed portion.

Unmanned aerial vehicles including wing capture devices and related methods

Unmanned aerial vehicles including wing capture devices and related methods are disclosed. An example unmanned aerial vehicle includes a fuselage and a wing assembly, the wing assembly including a shoulder coupled to the fuselage, the shoulder including a joint, the joint distal to the fuselage, a wing coupled to the joint, and a hook, the hook coupled to the shoulder, the hook including a groove to receive a cable to arrest flight of the unmanned aerial vehicle.

Systems and methods for foldable arms

Systems and methods are provided for transformation of a UAV from an extended state to a compacted state. The UAV can be transported in the compacted state. The UAV can comprise one or more segmented arms that can be folded to reduce the volume of the UAV. The segmented arms can be sealed to prevent ambient air, dirt, and or water vapor from entering the segmented arm. The UAV can comprise a cooling and air filtering system on-board the UAV.

Nose Cone
20180057145 · 2018-03-01 ·

Disclosed here are systems for detachable airframe components including detachable nose cones, propeller assemblies and motors. In some example embodiments, the assemblies include a nose cone with a connection receiver, a motor assembly with a rotatable section, where the rotatable section includes torque arms configured to secure with the nose cone connection receiver, and a propeller assembly, configured to connect to the nose cone.

Counter rotating torque drive for rotary wing vehicle propulsion

An aircraft for generating torque. The aircraft includes a motor coupling a lifting rotor and a torque rotor, and is configured to spin the lifting rotor in a first direction to generate lift and spin the torque rotor in a second direction to generate drag-torque. The torque rotor and the lifting rotor are coupled or decoupled from one another during flight or on ground.

Counter rotating torque drive for rotary wing vehicle propulsion

An aircraft for generating torque. The aircraft includes a motor coupling a lifting rotor and a torque rotor, and is configured to spin the lifting rotor in a first direction to generate lift and spin the torque rotor in a second direction to generate drag-torque. The torque rotor and the lifting rotor are coupled or decoupled from one another during flight or on ground.

Reverse propulsion aerial gaming systems, methods, and devices

An optical-based aerial gaming system comprises: a multirotor unmanned flying device comprising: a main body; a plurality of propulsion units, a wireless receiver configured to receive data via radio communication; a wireless transmitter configured to send data via radio communication; one or more light generators configured to project laser or infrared light from the unmanned flying device; and one or more light sensors configured to detect laser or infrared light projected by a separate unmanned flying device; and a remote control unit comprising: a wireless transmitter configured to send data via radio communication; and a wireless receiver configured to receive data via radio communication, wherein the unmanned flying device is configured to transmit to the remote control unit, using the wireless transmitter of the unmanned flying device, at least a portion of encoded data of the detected laser or infrared light.