The present invention discloses a rotor control system where rapid changes in rotor torque are transferred into moment forces acting about the blade pitch axis of a rotor blade in a thrust-generating rotor, to ultimately control the movements of a rotary wing aircraft. The moment forces acting on the rotor blade are transferred through a carefully adjusted damping member in order to allow rapid changes in rotor torque to create cyclic changes in blade pitch angle, while slow or permanent changes are cancelled out and affects the rotational speed and the thrust generated by the rotor, without permanently affecting the blade pitch angle of individual rotor blades.

A gaming system for enabling three-dimensional game play of remote-control craft controlled by a controller, each craft including a communication system with both radio frequency (RF) and infrared (IR) capabilities. The system can include a plurality of hovering remote-control flying craft each controlled by a handheld controller, and further may include at least one additional game accessory elements, such as a puck, a ground station or a gun. Each pairing of craft and controllers communicate via an RF protocol that transmits at least control communications between the controller and the craft based on pair identification information in an RF communication protocol. The craft and game-accessory elements also communicate via at least an IR protocol that communicates game-play information. Selectable pairs of craft and controllers may be assigned to different teams for playing multiplayer team games based on team identification information in the RF communication protocol.

A hovering remote-control flying craft having a molded frame assembly includes a plurality of arms extending from a center body with an electric motor and corresponding propeller on each arm. In various embodiments, the motor and propeller are mounted downward-facing at a distal portion of each arm with a motor cover over the motor. The center body can be formed of a two-piece molded structure that sandwiches a circuit board to provide structural support for the frame. The circuit board can include a plurality of tabs that facilitate mounting of wire connectors, and can also provide antennas and emitters for both IR and RF communications. In some embodiments, a removable safety ring protects the propellers from lateral contact.

A toy (10) comprising a rotor (20) and a centrally arranged capsule (30), wherein the capsule comprises an actuator mechanism (33) that is configured to cooperate with a launch element (40) and an actuator means (50), wherein the actuator means is configured for engaging with the actuator mechanism (33) to transfer a momentum to the rotor (20), whereby the rotor can rotate and be launched from the launch element (40), wherein the capsule (30) is a separate part relative to the rotor, and the capsule (30) comprises at least two capsule parts (31, 32) whereby the two capsule parts can be opened when the rotor and the capsule are separated, and wherein rotor (20), capsule (30) and actuator mechanism (33) are connected to each other to the effect that the momentum from the actuator means (50) is transferred to the actuator mechanism (33) that conveys the momentum on from the capsule (30) to the rotor (20), when the at least to capsule parts (31, 32) are closed.

A frisbee, including a main body, a plurality of LEDs, and a battery. The main body includes a central disc portion and an outer ring periphery. The plurality of LEDs are arranged on the central disc portion. The central disc portion is provided with a plurality of light-guiding ribs. One end of each of the plurality of light-guiding ribs is arranged close to the plurality of LEDs, and the other end of each of the plurality of light-guiding ribs is connected to the outer ring periphery. The plurality of light-guiding ribs and the outer ring periphery are both made of an light-guide material.

The invention relates to drones for a combat game, preferably a drone (1) and at least one opponent drone (2), said drones comprising radio control means, signal transmitters, receivers, and cameras. The invention further relates to a system for a combat game, the system comprising a drone (1) comprising a weapon (3), and at least one opponent drone (2) comprising an opponent weapon (4), wherein the drones are equipped with radio control means, signal transmitters, signal receivers and cameras. The drones and the system are characterised in that the opponent signal transmitters (6) disposed on the opponent drone (2) and on an opponent weapon (4) are in control connection, via a control unit (15) of the drone (1), with the signal receivers (7) of the drone (1), the connection being adapted for transmitting the signals generated through targeting by an opponent player (26) utilizing a display (22) of the opponent player as control means, and for controlling the rotational speed, position, and operation of the light source (9), sound source (11), and smoke source (13) disposed on the drone (1), and the motors (19) of the propellers (17) thereof, and in that the signal transmitters (5) disposed on the drone (1) and on a weapon (3) are in control connection, via a control unit (16) of the opponent drone (2), with the opponent signal receivers (8) of the opponent drone (2), the connection being adapted for transmitting the signals generated through targeting by a player (25) utilizing a player's display (21) as control means, and for controlling the rotational speed, position, and operation of the opponent light source (10), opponent sound source (12), and opponent smoke source (14) disposed on the opponent drone (2), and the opponent motors (20) of the opponent propellers (18) thereof.

A lighter-than-air toy drone having at least one balloon that is inflated with a lift gas. The drone has a first conduit progresses along a first axis and a second conduit that progresses along a perpendicular second axis. At least one motorized propeller is provided that can selectively moving air through the first conduit and the second conduit to propel the drone. The motorized propeller can also generate a gyroscopic force that acts to rotate said at least one balloon for directional steering.

The present invention discloses a gaming system that is comprised of a plurality of computing devices, where a computing device initially exhibits an active state of an instance of a Virtual Focal Point (VFP), and another computing device initially exhibit an IN-active state of the instance of the Virtual Focal Point of the computing device. The active state of the instance of the VFP of the computing device may be transferred to the other computing device with the IN-active state of the instance of the VFP.

A rotary aircraft includes a cover, a driving shaft in the cover, an electric control board on the cover, and a flight assembly mounted on the driving shaft and coupled electrically with the electrical control board, a driving assemble mounted on the flight assembly and coupled electrically with the electrical control board, connected with the driving shaft and driving it to rotate so as to rotate the cover, and a light bar mounted on the cover and coupled electrically with the electrical control board, used for displaying a presetting pattern or text, which achieves enlightening education and improves enjoyment of the flight toy and satisfies the demands of the users.

An aeronautical vehicle that rights itself from an inverted state to an upright state has a self-righting frame assembly has a protrusion extending upwardly from a central vertical axis. The protrusion provides an initial instability to begin a self-righting process when the aeronautical vehicle is inverted on a surface. A propulsion system, such as rotor driven by a motor can be mounted in a central void of the self-righting frame assembly and oriented to provide a lifting force. A power supply is mounted in the central void of the self-righting frame assembly and operationally connected to the at least one rotor for rotatably powering the rotor. An electronics assembly is also mounted in the central void of the self-righting frame for receiving remote control commands and is communicatively interconnected to the power supply for remotely controlling the aeronautical vehicle to take off, to fly, and to land on a surface.