TWM567130U - Helicopter gyro - Google Patents

Abstract

A helicopter gyro comprising a body, a rotating structure, a plurality of fan structures, a steering motor, and a power component. The center of the bottom surface of the body is provided with a rotating structural member; the rotating structure comprises a rotating shaft and at least two wings, the rotating shaft is not coplanar with the top surface of the body, and one end of the rotating shaft is installed at the center of the top surface of the body, and the wing is connected to The other ends of the rotating shaft are arranged symmetrically with each other at the other end; the plurality of fan structures are respectively disposed at the outer ends of the wing; the steering motor is disposed inside the body, and the steering motor includes a pivoting shaft and is connected to the rotating shaft.

Description

Helicopter gyro

A gyro, especially a gyro having a wing structure.

Gyro is one of the symbols of traditional Chinese children's play. In addition to being a child, it is also commonly found in folk sports, such as the top.

However, the traditional gyro is rotated by the power of the rope thrower, and the speed of rotation and the time of rotation are also determined by the force thrown. Therefore, for children, the rotation time of the gyro is not long and the rotation speed is not enough. fast.

In addition, the traditional gyro shape is relatively monotonous, not easy to attract children's eyes, therefore, how to create a gyro, suitable for all ages, easy to get started, and can increase the rotation speed of the gyro and the rotation time of the gyro, to promote the fun of play, is The subject person in the field is eager to solve the problem.

A helicopter gyro comprising a body, a rotating structure, a plurality of fan structures, and a steering motor. The center of the bottom surface of the body is provided with a rotating structural member; the rotating structure comprises a rotating shaft and at least two wings, the rotating shaft is not coplanar with the top surface of the body, and one end of the rotating shaft is installed at the center of the top surface of the body, and the wing is connected to The other ends of the rotating shaft are arranged symmetrically with each other at the other end; the plurality of fan structures are respectively disposed at the outer ends of the wing; the steering motor is disposed inside the body, and the steering motor includes a pivoting shaft and is connected to the rotating shaft.

The helicopter gyro as described above, in one embodiment, further comprises a magnetic member disposed in the body.

In one embodiment, the helicopter gyro further includes a steering gear disposed above the body to engage the rotating shaft, and the steering device can tilt the wing toward the rotating shaft.

In one embodiment, the helicopter gyro further includes a controller, the controller includes a signal receiver, the wing is respectively equipped with a transmitter, the transmitter transmits the first frequency signal to the signal receiver, and the other transmitter The second frequency signal is transmitted to the signal receiver.

In the helicopter gyro as described above, in one embodiment, the rotating shaft has a square columnar structure.

The helicopter gyro as described above, in one embodiment, further comprises a cord, the outer wall surface of the body having a thread, the cord being wound around the body along the thread.

In one embodiment, the helicopter gyro further includes an emission structure, the emission structure includes an elastic device and an emission port, the elastic device is disposed in the emission port, the body abuts the emission port, and the elastic device provides a rotating elastic force to cause self-emission of the body. The mouth is shot and rotated.

In a helicopter gyro as described above, in one embodiment, the wing structure includes a flange portion at a joint of the wing and the rotating shaft, and the flange portion is provided with the wing as a fulcrum toward the top surface or away from the top surface. Folding.

The helicopter gyro as described above, in one embodiment, further includes a rotating shaft located at the junction of the fan structure and the wing, and the fan structure is rotatable according to the rotating shaft.

In the helicopter gyro as described above, in one embodiment, the fan structure includes a illuminating device that emits bright light when the body rotates.

The helicopter gyro as described above, in one embodiment, the body is tapered, the top surface The caliber is larger than the bottom surface.

An embodiment of the present invention illustrates that when the helicopter gyro is rotated, it will be affected by multiple forces, that is, the user gives the gyro's rotational force, the resistance suffered during the rotation, and the force of the steering motor to drive the rotating structure, and the wing With the rotation of the fan structure, the angle between the fan structure and the wing will affect the resistance of the wing rotation. The greater the resistance, the more the power of the body will be rotated. Thus, the resistance of the helicopter gyro during the rotation is reduced, the speed and time of rotation. Can be improved.

In addition, an embodiment of the present invention illustrates that the helicopter gyro is different from the traditional gyro appearance, and has a wing like a helicopter, which increases the attractiveness of the appearance of the gyro, and makes the child easy to approach and play, and contributes to the promotion of the gyro.

100‧‧‧Helicopter

1‧‧‧ Ontology

11‧‧‧ top surface

12‧‧‧ bottom

13‧‧‧Rotating structural parts

15‧‧‧ thread

2‧‧‧Rotating structure

21‧‧‧ wing

211‧‧‧Folding

22‧‧‧Rotary axis

23‧‧‧transmitter

3‧‧‧Fan structure

31‧‧‧Lighting device

311‧‧‧Power source

312‧‧‧Lights

33‧‧‧ leaves

4‧‧‧ rope

5‧‧‧steering motor

51‧‧‧ pivot shaft

52‧‧‧Start switch

53‧‧‧ micro switch

6‧‧‧Emission structure

61‧‧‧ elastic device

62‧‧‧ Launch port

7‧‧‧Rotary axis

8‧‧‧Power components

‧‧‧‧ angle

9‧‧‧Steering gear

10‧‧‧ Controller

101‧‧‧Signal Receiver

[Fig. 1] A schematic structural view of an embodiment of a helicopter gyro of the present invention.

[Fig. 2] is a schematic structural view of an embodiment of a helicopter gyro of the present invention.

[Fig. 3A] is a schematic structural view of an embodiment of a helicopter gyro of the present invention.

[Fig. 3B] is a schematic structural view of an embodiment of the helicopter gyro of the present invention.

[Fig. 4] is a schematic structural view of an embodiment of a helicopter gyro of the present invention.

[Fig. 5] is a schematic structural view of an embodiment of a helicopter gyro of the present invention.

[Fig. 6] Fig. 6 is a schematic structural view of an embodiment of a helicopter gyro of the present invention.

Please refer to FIG. 1 to FIG. 2 , which are respectively schematic structural diagrams of an embodiment of a helicopter gyroscope. The helicopter gyro 100 includes a body 1, a rotating structure 2, a plurality of fan structures 3, and a steering Motor 5 and power assembly 8. The center of the bottom surface 12 of the body 1 is provided with a rotating structural member 13. The rotating structural member 13 can be a fixed bump or a rollable ball. The rotating structure 2 includes a rotating shaft 22 and at least two wings 21, and the rotating shaft 22 and the body 1 The top surface 11 is not coplanar, one end of the rotating shaft 22 is installed at the center of the top surface 11 of the body 1, and the wing 21 is connected to the other end of the rotating shaft 22, and is symmetrically arranged at the other end with each other; the plurality of fan structures 3 Each is disposed at an outer end of the wing 21; the steering motor 5 is disposed inside the body 1, and the steering motor 5 includes a pivot shaft 51 that connects the rotating shaft 22. In one embodiment, the steering motor 5 is a power motor. The power assembly 8 is disposed inside the body 1 and is connected to the steering motor 5 to provide power to the steering motor 5. In an embodiment, the power assembly 8 is a battery.

The steering motor 5 can drive the rotating structure 2, which is activated when the body 1 is in operation, and the powered wing 21 causes the body 1 to have an upward buoyancy and fly upward. When the wing 21 is in a rotational direction, the body 1 is caused to fly upward. Conversely, when rotated in the direction of rotation, the body 1 will be allowed to settle downward, which helps the body 1 to rotate.

The helicopter gyro 100 of the present embodiment will be subjected to three forces during operation, namely, the rotational force of the body 1, the running force of the steering motor 5 (the rotation of the wing 21), and the resistance encountered during the rotation (with the fan structure 3) In relation to the angle between the wings 21, the resistance contributes to the rotation of the body 1, and the three-force reaches the state in which the helicopter gyro 100 is balancedly rotated.

In one embodiment, the helicopter gyro 100 further includes a magnetic member disposed in the body 1. The body 1 is the magnetic member, so that the helicopter gyro 100 can be synchronously rotated and raised in a magnetic field environment by using the principle of magnetic levitation.

In an embodiment, the user can directly adjust the relative position of the wing 21 and the fan structure 3 in a manual manner, for example, in a folding manner, so as to achieve the purpose of setting or changing the flight direction of the helicopter gyro 100.

Please refer to FIG. 3A to FIG. 3B , which are respectively schematic structural diagrams of an embodiment of the helicopter gyro of the present invention. The helicopter gyro 100 further includes a steering gear 9 disposed above the body 1 to engage the rotating shaft 22, and the steering gear 9 can tilt the wing 21 toward the rotating shaft 22. In other words, the diverter 9 allows the wing 21 to be tilted forward, backward, left, and right, and when the wing 21 is tilted toward one side, the helicopter gyro 100 will fly in a particular direction. In an embodiment, the steering gear 9 has an adjuster inside, and automatically switches and adjusts the tilt angle of the wing 21 in a certain time, so that the helicopter gyro 100 can balance flying.

The helicopter gyro 100 further includes a controller 10, which may be an external remote controller that is coupled to the steering gear 9, the fan structure 3, and the steering motor 5, respectively. When the helicopter gyro 100 is in the unbalanced gravity, the controller 10 can be manipulated in time to change the steering gear 9, adjust the relative position of the wing 21 and the fan structure 3 (for example, to rotate in an axis parallel to the wing 21), and The running speed of the steering motor 5 (changing the rotational speed of the wing 21) is balanced by gravity.

The controller 10 includes a signal receiver 101. The wing 21 is respectively provided with a transmitter 23, the transmitter 23 transmits a first frequency signal to the signal receiver 101, and the other transmitter 23 transmits a second frequency signal to the signal receiver 101. In other words, the user can determine the tilt of the wing 21 by the strength of the frequency signal received by the signal receiver 101. For example, the first frequency signal has a strong intensity, indicating that the wing transmitting the first frequency signal transmitter 23 is installed. 21 is quite close to the rotating shaft 22, and the flight condition of the helicopter gyro 100 is quite deviated. The user can further manipulate the controller 10 to transmit signals to the steering gear 9, correct the wing 21, and make the helicopter gyro 100 fly in balance. The present invention is not limited thereto. In an embodiment, the controller 10 is provided with an automatic detection and adjustment function, and does not wait for the user to operate, when a preset deviation occurs (the first frequency signal or the second frequency signal) Up to the preset value, the controller 10 transmits a signal to the steering gear 9, and the corresponding movable wing 21 is relatively offset, and is corrected to be flat. Balance status. In an embodiment, when the first frequency signal or the second frequency signal strength is equal or both are zero, it indicates that the helicopter gyro 100 balances flight, and no deviation occurs.

In an embodiment, the user can also use the controller 10 to tilt the rotating structure 2 (or the wing 21) in a remotely controlled manner to fly or deviate the helicopter gyro 100 in a certain direction. The user can determine the deviation of the helicopter gyro 100 by receiving the first frequency signal or the second frequency signal as the signal receiver 101, and the user further operates the controller 10 to adjust the rotating structure 2 (or the wing 21). The tilt condition to change or change the direction in which the helicopter gyro 100 is flying.

In an embodiment, the rotating shaft 22 has a square columnar structure, so that it can be combined with the steering gear 9 to achieve the function of tilting the wing 21 forward, backward, leftward, and rightward.

In an embodiment, the user can timely manipulate the controller 10 to change the direction of rotation of the steering gear 9, and adjust the relative position of the wing 21 and the fan structure 3 in a remote manner to set or change the flight direction of the helicopter gyro 100.

In other words, the user can use the controller 10 (such as a remote control) to change the position of the wing 21, or / and change the position of the structure 3 of the fan, for example, adjust the rotating shaft 22 forward, backward, left or right, or It is to adjust the inclination of the wing 21, and the user prefers to change the flight direction of the helicopter gyro 100, and there is no limitation in this creation.

In an embodiment, the controller 10 can further control the direction of rotation of the steering motor 5, such as changing the forward direction to the reverse direction, so that the operating condition of the helicopter gyro 100 rotation and rotating structure 2 can be further changed.

Referring again to FIG. 2, in this embodiment, the helicopter gyro further comprises a rope 4 having an outer wall surface having a thread 15 around which the rope 4 is wound. In other words, rising The machine top 100 can be wound around the body 1 with the rope 4 along the thread 15 in the manner of the conventional spinning top, and the helicopter gyro 100 is thrown from the tangled rope to achieve the purpose of rotating the gyro. As described above, in addition to the rotation of the gyro body 1 itself, The rotating structure 2 and the fan structure 3 can convert the resistance received by the rotation of the gyro to form an upward buoyancy of the gyro body 1 to make the helicopter gyro 100 fly upward.

Please refer to FIG. 4 , which is a schematic structural view of an embodiment of the helicopter gyroscope of the present invention. In this embodiment, the helicopter gyro 100 further includes an emission structure 6 including an elastic device 61 and an emission port 62. The elastic device 61 is disposed in the emission port 62. The body 1 abuts the emission port 62, and the elastic device 61 provides rotation. The elastic body 1 is ejected from the launch port 62 and rotated. In other words, the elastic device 61 provides the power to rotate the gyro 100, and the user can activate the elastic device 61 by pressing a button (for example, the transmitting structure 6 is a pedestal, and the elastic device 61 is disposed therein); in an embodiment, the transmitting structure 6 is, for example, a pistol. The shape, the elastic device 61 is disposed inside, and the user can use the trigger to activate the elastic device 61 to further launch the body 1 of the gyro 100. However, there is no limit to this creation.

Please refer to FIG. 5 , which is a schematic structural view of an embodiment of the helicopter gyroscope of the present invention. In the embodiment shown in FIG. 4, the wing 21 includes a folding portion 211 at a joint of the wing 21 and the rotating shaft 22, and the folding portion 211 is provided with the wing 21 as a fulcrum toward the top surface 11 or away from the top. The direction of the face 11 is folded. The wing 21 forms an angle α with the rotating shaft 22. In the embodiment shown in FIG. 4, the helicopter gyro 100 further includes a rotating shaft 7 located at the junction of the fan structure 3 and the wing 21, and the fan structure 3 is rotatable according to the rotating shaft 7.

In other words, the user can adjust the angle α between the wing 21 and the axis of rotation 22, where α ≦ 180 degrees; on the other hand, the user can rotate the fan structure 3. As described above, the rotation of the helicopter gyro 100 has a considerable relationship with the wind flow. The above-mentioned structural design allows the user to adjust the angle α and the angle of rotation of the fan structure 3 to change the wind flow during rotation, which is advantageous for reducing the resistance. The rotation force of the main body 1 is converted to make the helicopter gyro 100 rotate more smoothly and maintain a long-term rotation state.

Please refer to FIG. 6 , which is a schematic structural view of an embodiment of a helicopter gyroscope. In this embodiment, the fan structure 3 includes a light emitting device 31, which is included when the body 1 rotates, and the light emitting device 31 emits bright light. In an embodiment, the light-emitting device 31 includes a power source 311 and an illuminant 312. When the gyro 100 is rotating, the power source 311 has power to provide the illuminant 312 energy to illuminate. Thus, the gyro 100 can generate glare, light and shadow effects. Full.

In the above embodiment, the body 1 of the helicopter gyro 100 has a tapered shape, and the top surface 11 has a larger diameter than the bottom surface 12. However, the present creation is not limited thereto. In some embodiments, the body 1 of the helicopter gyro 100 may be cylindrical or square.

Furthermore, in an embodiment, the fan structure 3 comprises a blade 33. However, the present creation is not limited thereto, and in some embodiments, each fan structure 3 includes at least two blades 33. As described above, the number of blades 33 can also affect the direction of the wind flow when the helicopter gyro 100 rotates, and the user or the operator can add a plurality of blades 33 according to actual needs to improve the rotation and rotation time of the helicopter gyro 100.

In one embodiment, the body 1 weighs 80 to 90% of the weight of the helicopter gyro 100.

An embodiment of the present invention is characterized in that the helicopter gyro has a steering motor. When the helicopter gyro is rotated, the internal steering motor operates, and the overall gyro structure can still achieve dynamic balance, for example, by steering of the steering motor, rotation of the gyro body, The tilting or rotational position of the rotating structure or fan structure allows the integral gyro to be balanced during flight and is therefore distinct from prior art gyros.

An embodiment of the present invention illustrates that when the helicopter is rotated, the force of the gyro is affected by a plurality of forces, that is, the force of the gyro rotation (given by the user or the launching device), the resistance, and the upward lifting (the steering motor drives the rotating structure). According to the wing and fan structure of the helicopter gyro, the resistance can be converted into the force of the body rotation, so that the helicopter gyro can fly and rotate at the same time. Thus, the resistance of the gyro is reduced, the speed of rotation can be maintained and the time of rotation is increased. . Moreover, the appearance of the helicopter gyro according to an embodiment of the present invention is different from the traditional gyro, and can attract children to play.

Claims (10)

A helicopter gyro comprising: a body having a rotating structural member at a center thereof; a rotating structure comprising a rotating shaft and at least two wings, the rotating shaft being not coplanar with a top surface of the body, the rotating shaft being mounted at one end Provided at a center of a top surface of the body, the wings are connected to the other end of the rotating shaft, and are symmetrically arranged at a point of the other end; a plurality of fan structures are disposed at the outer ends of the wing; and a The steering motor is disposed inside the body, and the steering motor includes a pivoting shaft connected to the rotating shaft, and the steering motor is started when the body rotates. The helicopter gyro according to claim 1, further comprising a magnetic component disposed in the body. The helicopter gyro according to claim 1, further comprising a steering gear disposed above the body to sleeve the rotating shaft, the steering device tilting the wings toward the rotating shaft. The helicopter gyro of claim 3, further comprising a controller, the controller comprising a signal receiver, each of the wings being provided with a transmitter, the transmitter transmitting a first frequency signal to the signal receiver The other transmitter transmits a second frequency signal to the signal receiver. The helicopter gyro according to claim 3, wherein the rotating shaft has a columnar structure. The helicopter gyro according to claim 1, further comprising a rope, the outer wall surface of the body having a thread along which the rope is wound around the body. The helicopter gyro of claim 1, further comprising a launching structure, the launching structure comprising a resilient device and an emitting port, the resilient device being disposed in the transmitting port, the body abutting the transmitting port, the elastic device providing A rotating elastic force causes the body to be ejected from the launch port and rotated. The helicopter gyro according to claim 1, wherein the wing includes a folding portion at a connection between the wing and the rotating shaft, the folding portion is provided with the connecting portion as a fulcrum toward the top surface or Fold away from the top surface. The helicopter gyro according to claim 1, further comprising a rotating shaft located at a joint of the fan structure and the wing, wherein the fan structure is rotatable according to the rotating shaft. The helicopter gyro of claim 1, wherein the fan structure comprises a light-emitting device that emits light when the body rotates.