A remote controlled hovering toy figure having a propulsion system, a control system, a winged body, and a wing actuation assembly. The winged body is mounted to the propulsion system, which is controlled by the control system. The wing actuation assembly is mounted to the winged body, and the wing
A remote controlled hovering toy figure having a propulsion system, a control system, a winged body, and a wing actuation assembly. The winged body is mounted to the propulsion system, which is controlled by the control system. The wing actuation assembly is mounted to the winged body, and the wing actuation assembly is powered by the control system. The wing actuation assembly drives the wings in an oscillating flapping motion. The wings comprise apertures permitting air to pass through the wing, thus reducing the aerodynamic effect of the flapping motion. In this manner, the wings produce a softened “bouncing” flight action, thus creating a realistic flight motion. In another embodiment, the propulsion system comprises one or more rotors in a coaxial arrangement, and a rotor mast housing in the shape of a rider riding the hovering toy figure.
대표청구항▼
1. A remote controlled hovering toy figure comprising: a body having at least two wings, each wing having a support and a tip;a propulsion system mounted to the body, said propulsion system configured for producing a hovering form of flight for the hovering toy figure;a control system for controllin
1. A remote controlled hovering toy figure comprising: a body having at least two wings, each wing having a support and a tip;a propulsion system mounted to the body, said propulsion system configured for producing a hovering form of flight for the hovering toy figure;a control system for controlling the propulsion system, said control system configured to receive electronic signals from a wireless control device; anda wing actuation system for actuating the wings in a flapping motion, thereby simulating the flapping motion of the hovering toy figure. 2. The hovering toy figure of claim 1, wherein the propulsion system comprises at least three propeller units arranged in a substantially co-planar configuration. 3. The hovering toy figure of claim 1, wherein at least one of the wings comprises a first spine and a second spine, the first spine having has a base and a distal end, the base being operably connected to the wing actuation assembly such that the first spine extends along the wing and the distal end extends beyond a first spine connectivity termination point, the second spine being attached to the wing at a second spine connectivity termination point that is located on the wing between the first spine connectivity termination point and the tip of the wing such that a space between the first spine connectivity termination point and the second spine connectivity termination point is a flex zone in the wing, wherein the second spine is oriented such that the distal end of the first spine and a tip of the second spine cross in proximity to the flex zone. 4. The hovering toy figure of claim 2, wherein at least one of the wings comprises a first spine and a second spine, the first spine having has a base and a distal end, the base being operably connected to the wing actuation assembly such that the first spine extends along the wing and the distal end extends beyond a first spine connectivity termination point, the second spine being attached to the wing at a second spine connectivity termination point that is located on the wing between the first spine connectivity termination point and the tip of the wing such that a space between the first spine connectivity termination point and the second spine connectivity termination point is a flex zone in the wing, wherein the second spine is oriented such that the distal end of the first spine and a tip of the second spine cross in proximity to the flex zone. 5. The hovering toy figure of claim 1, wherein at least one of the wings comprises one or more apertures configured to enable the passage of air through the wing, thereby reducing aerodynamic forces produced by the wing during the flapping motion, and producing a bouncing effect to the hovering form of flight. 6. The hovering toy figure of claim 2, wherein at least one of the wings comprises one or more apertures configured to enable the passage of air through the wing, thereby reducing aerodynamic forces produced by the wing during the flapping motion, and producing a bouncing effect to the hovering form of flight. 7. The hovering toy figure of claim 3, wherein at least one of the wings comprises one or more apertures configured to enable the passage of air through the wing, thereby reducing aerodynamic forces produced by the wing during the flapping motion, and producing a bouncing effect to the hovering form of flight. 8. The hovering toy figure of claim 1, wherein the propulsion system comprises a motor drive driving a primary rotor via a rotor mast. 9. The hovering toy figure of claim 8, further comprising a housing to support the rotor mast against lateral vibration. 10. The hovering toy figure of claim 8, wherein at least one of the wings comprises a first spine and a second spine, the first spine having has a base and a distal end, the base being operably connected to the wing actuation assembly such that the first spine extends along the wing and the distal end extends beyond a first spine connectivity termination point, the second spine being attached to the wing at a second spine connectivity termination point that is located on the wing between the first spine connectivity termination point and the tip of the wing such that a space between the first spine connectivity termination point and the second spine connectivity termination point is a flex zone in the wing, wherein the second spine is oriented such that the distal end of the first spine and a tip of the second spine cross in proximity to the flex zone. 11. The hovering toy figure of claim 9, wherein at least one of the wings comprises a first spine and a second spine, the first spine having has a base and a distal end, the base being operably connected to the wing actuation assembly such that the first spine extends along the wing and the distal end extends beyond a first spine connectivity termination point, the second spine being attached to the wing at a second spine connectivity termination point that is located on the wing between the first spine connectivity termination point and the tip of the wing such that a space between the first spine connectivity termination point and the second spine connectivity termination point is a flex zone in the wing, wherein the second spine is oriented such that the distal end of the first spine and a tip of the second spine cross in proximity to the flex zone. 12. The hovering toy figure of claim 8, wherein at least one of the wings comprises one or more apertures configured to enable the passage of air through the wing, thereby reducing aerodynamic forces produced by the wing during the flapping motion, and producing a bouncing effect to the hovering form of flight. 13. The hovering toy figure of claim 1, wherein the propulsion system comprises a motor drive driving a primary rotor and a secondary rotor via at least one rotor mast, wherein the primary rotor and the secondary rotor are arranged in a co-axial configuration, and the secondary rotor is located at a height on the at least one rotor mast that is lower than the height of the primary rotor. 14. The hovering toy figure of claim 13, further comprising a housing to support the at least one rotor mast against lateral vibration, wherein the housing comprises a lower segment and an upper segment, the lower segment being attached to the body and disposed around the at least one rotor mast below the location of the primary rotor, and the upper segment is disposed around the at least one rotor mast above the location of the primary rotor. 15. The hovering toy figure of claim 13, wherein at least one of the wings comprises a first spine and a second spine, the first spine having has a base and a distal end, the base being operably connected to the wing actuation assembly such that the first spine extends along the wing and the distal end extends beyond a first spine connectivity termination point, the second spine being attached to the wing at a second spine connectivity termination point that is located on the wing between the first spine connectivity termination point and the tip of the wing such that a space between the first spine connectivity termination point and the second spine connectivity termination point is a flex zone in the wing, wherein the second spine is oriented such that the distal end of the first spine and a tip of the second spine cross in proximity to the flex zone. 16. The hovering toy figure of claim 14, wherein at least one of the wings comprises a first spine and a second spine, the first spine having has a base and a distal end, the base being operably connected to the wing actuation assembly such that the first spine extends along the wing and the distal end extends beyond a first spine connectivity termination point, the second spine being attached to the wing at a second spine connectivity termination point that is located on the wing between the first spine connectivity termination point and the tip of the wing such that a space between the first spine connectivity termination point and the second spine connectivity termination point is a flex zone in the wing, wherein the second spine is oriented such that the distal end of the first spine and a tip of the second spine cross in proximity to the flex zone. 17. The hovering toy figure of claim 13, wherein at least one of the wings comprises one or more apertures configured to enable the passage of air through the wing, thereby reducing aerodynamic forces produced by the wing during the flapping motion, and producing a bouncing effect to the hovering form of flight. 18. The hovering toy figure of claim 14, wherein at least one of the wings comprises one or more apertures configured to enable the passage of air through the wing, thereby reducing aerodynamic forces produced by the wing during the flapping motion, and producing a bouncing effect to the hovering form of flight.
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