Patent Application
20240359112
The present invention relates to the technical field of flying toys, in particular to a flying toy with various playing modes.
With the development of science and technology and the continuous improvement of people's living standards, the types of electronic toys are becoming more and more abundant and their functions are becoming more and more powerful. Among these electronic toys, flying toys, as a high-grade electronic toy, are deeply loved by the majority of model airplane enthusiasts.
At present, the started flying toys are thrown by throwing, which realizes the control of flight and flight direction: In order to enhance the play of flying toys, control parts are equipped to increase the play of flying toys: for example, the prior patent with the publication number of CN213698828U discloses a multi-play French flying device, which comprises a flying toy, a control part and an external accessory, wherein the flying toy flies in the air based on airflow, the control part is arranged in signal communication with the flying toy, and the external accessory is arranged in connection or separation with the flying toy; the outer fitting is provided with an outer adsorption block, and the control piece is provided with an inner magnetic block, and the outer adsorption block and the inner magnetic block are arranged in an adsorption manner.
In the prior art, although flying toys have a variety of playing modes, the playing modes of flying toys only fly in the air are diversified, resulting in little change in the control methods for flying toys, and the uniqueness and diversity of playing modes of flying toys are insufficient.
The present invention aims to provide flying toys with various playing modes, and aims to solve the problem of insufficient playing modes of flying toys in the prior art.
The present invention is realized in the following way. A flying toy with various playing modes a flying toy with various playing modes, comprising a flying body and an elastic part, wherein the flying body comprises a flying shell, a blade part, a central shaft and a driving part: the central shaft and the driving part are respectively arranged on the flying shell: the central shaft penetrates through the blade part, and the driving part is used for driving the blade part to rotate: the elastic part is arranged elastically, the flying shell and the elastic part are arranged in an assemblable and detachable manner or integrally formed; and the elastic part reversely applies an elastic force by an external force to the flying body, and the flying body is in a bouncing arrangement due to the elastic force.
Further, the flying shell has a downward lower shell surface, the elastic part is installed on the lower shell surface, and the elastic part comprises an elastic plate, which is elastically arranged: the lower shell surface and the elastic part are overlapped and connected along a top-down direction, and the elastic plate is used for bouncing up the flying body.
Further, a plurality of contact surfaces are formed on an outer surface of the elastic plate, and the orientations of the contact surfaces are arranged inconsistently: alternatively, the outer surface of the elastic plate forms a contact surface, and the contact surface is irregularly arranged.
Further, the elastic element comprises a spring element and a stressed plate, which are arranged below the flying shell: the spring element is arranged in an elongated or contracted manner, and extends longitudinally in the direction away from the flying shell: an upper part of the spring element is connected with the flying shell: a lower part of the spring element is connected with the stressed plate; and the spring element is used for bouncing up the flying shell.
Further, the flying toy with various playing modes comprises a detection sensor, an upper stressed part and a lower stressed part: wherein the upper stressed part and the lower stressed part are respectively arranged in signal communication with the detection sensor: the detection sensor is used for controlling the rotating speed of the blade part: the upper stressed part is installed in the flying shell, and the upper stressed part outputs a deceleration signal when subjected to an external force: the lower stressed part is installed on the elastic part, outputs an acceleration signal based on the collision of the elastic part, the detection sensor reduces the rotation speed of the blade part based on the deceleration signal, and the detection sensor increases the rotation speed of the blade part based on the acceleration signal.
Further, the flying body comprises an inertia ring: the inertia ring sleeves the blade part, and the inertia ring is connected with the blade part: the driving part is used for synchronously driving the blade part and the inertia ring to rotate: the inertia ring generates rotational inertia when rotating, and the inertia ring is used for realizing internal rotation self-balance.
Further, the blade part comprises a blade seat and a plurality of blade bodies, and the central shaft is arranged through the blade seat: the central shaft is used for positioning the blade seat, the blade bodies are arranged at intervals around the circumference of the blade seat, and the inner ends of the blade bodies are connected with the blade seat: the inertia ring is arranged in a ring shape, and the outer ends of the blade bodies are arranged with the inertia ring.
Further, the driving part comprises a driven gear, a motor gear and a driving motor; the central shaft penetrates through the driven gear, the driven gear is connected with the blade seat, the driving motor is connected with the motor gear, the driving motor is used for driving the motor gear to rotate, and the motor gear is engaged with the driven gear:
Further, the flying shell comprises a first shell and a second shell, and two ends of the central shaft are respectively connected with the first shell and the second shell: the center of the first shell, the blade seat and the center of second shell are coaxially arranged correspondingly: the first shell and the second shell are buckled to form a fully enclosed cavity, and the blade part, the central shaft and the driving part are respectively located in the fully enclosed cavity:
Further, wherein the flying toy with various playing modes comprises a lamp strip for emitting light, and the lamp strip is installed on the outer surface of the flying shell.
Compared with the prior art, the flying toy with various playing modes provided by the present invention can directly throw the flying body in the starting state outward when flying, and the flying body is self-stabilized in the air according to the throwing angle, thus realizing the use of the air area: when the flying body is popped up for use, the flying body in the starting state is flapped towards the ground, and when the elastic part touches the ground, the elastic part is forced to reversely apply elastic force to the flying body, so that the flying body is popped up away from the ground to realize the use of the ground area: users can choose the air area to use, the ground area to use, and the air area and the ground area to switch based on the desired gameplay, thus increasing the use area of flying toys and realizing diversified uses of flying toys: at the same time, the air control is realized, and the control method of the ground flapping rebound of the aircraft is added. The hybrid control in different areas makes the flying toy more interactive and interesting.
In order to make the purpose, technical scheme and advantages of the present invention more clear, the present invention will be further described in detail with the attached drawings and examples. It should be understood that the specific embodiments described here are only for explaining the present invention, and are not used to limit the present invention.
The implementation of the present invention will be described in detail with reference to specific embodiments.
The same or similar reference numerals in the drawings of this embodiment correspond to the same or similar parts: In the description of the present invention, it should be understood that if the azimuth or positional relationship indicated by terms such as “up”, “down”, “left” and “right” is based on the azimuth or positional relationship shown in the attached drawings, it is only for the convenience of describing the present invention and simplifying the description, and it does not indicate or imply that the device or element referred to must have a specific orientation, be constructed and operated in a specific orientation, so the terms describing the positional relationship in the attached drawings are only used for exemplary explanation.
Referring to
A flying toy with various playing modes comprises a flying body 1 and an elastic part 2, wherein the flying body 1 is used for flying in the air, and the flying body 1 comprises a flying shell 11, a blade part 12, a central shaft 13 and a driving part 14, wherein the central shaft 13 and the driving part 14 are respectively arranged in the flying shell 11, and the central shaft 13 penetrates through the blade part 12: the driving part 14 is used for driving the blade part 12 to rotate: the elastic part 2 is arranged elastically, and the elastic part 2 reversely applies an elastic force by an external force to the flying body 1, and the flying body 1 is in a bouncing arrangement due to the elastic force.
The flying shell 11 and the elastic part 2 are arranged in an assemblable and detachable manner, that is, when in use, the flying shell 11 and the elastic part 2 are assembled, so that the flying shell 11 is sprung up under the action of the elastic part 2: at the same time, the flying shell 11 and the elastic part 2 are detached, so that the replacement is convenient.
Alternatively, the flying shell 11 and the elastic part 2 are integrally formed, so that the production and manufacturing are budgeted, and the cost is reduced, and at the same time, the assembly steps are reduced.
When the flying toy with various playing modes is used in flight, the flying body 1 in the starting state is directly thrown outwards, and the flying body 1 is self-stabilized in the air according to the throwing angle, thus realizing the use of the air area: when the flying body 1 is popped up for use, the started flying body 1 is flapped towards the ground, and when the elastic part 2 touches the ground, the elastic part 2 is forced to apply elastic force to the flying body 1 in the opposite direction, so that the flying body 1 is popped up away from the ground to realize the use of the ground area: users can choose the air area to use, or the ground area to use, or switch between the air area and the ground area based on the desired gameplay. In this way, the use area of flying toys is increased, and diversified use of flying toys is realized. At the same time, the air control is realized, and the control method of ground flapping and rebound of aircraft is increased. The hybrid control of different areas makes the flying toys more interactive and interesting.
The flying shell 11 has a downward lower shell surface, and the elastic part 2 is installed on the lower shell surface.
The blade part 12 and the central shaft 13 are arranged movably or rotationally: the blade part 12 and the central shaft 13 are respectively arranged independently or synchronously rotated.
The blade part 12 and the inertia ring 15 rotate at a high speed respectively to generate moment of inertia, so that the aircraft can maintain the corresponding angle when throwing. After the external force to be thrown disappears, the angle of the aircraft will still maintain the angle when throwing, while the wind generated by the high-speed rotation of the blade part 12 can be decomposed into lift force and offset force, and the direction of the offset force is consistent with the angle when the aircraft is thrown: the lift maintains the flying height of the aircraft, and the offset force controls the flying angle of the aircraft: therefore, the preset flight path can be achieved by presetting the angle when the aircraft is thrown.
Based on the rotation of the flying shell 11 and the airflow generated by the blade part 12, the stable flight is realized based on the gyro principle.
A flying toy with various playing modes includes a detection sensor, an upper stressed part 4 and a lower stressed part: wherein the upper stressed part 4 and the lower stressed part are respectively arranged in signal communication with the detection sensor: the detection sensor is used for controlling the rotating speed of the blade part 12: the upper stressed part 4 is installed in the flying shell 11, and the upper stressed part 4 outputs a deceleration signal when subjected to an external force: the lower stressed part is installed on the elastic part 2, outputs an acceleration signal based on the collision of the elastic part 2, the detection sensor reduces the rotation speed of the blade part 12 based on the deceleration signal, and the detection sensor increases the rotation speed of the blade part 12 based on the acceleration signal.
When in use, the upper stressed part 4 is tapped by hand or other tools, and the detection sensor appropriately reduces the rotation speed of the blade part 12, so that the lift of the whole flying toy is weakened, and the flying toy can descend at a better speed, which increases the rebound strength of the subsequent elastic part 2 and facilitates the bounce of the flying shell 11: at the same time, when the elastic part 2 collides with the ground, the lower stressed part synchronously receives the acting force and feeds back the acceleration signal to the detection sensor, which increases the rotating speed of the blade part 12, so as to enhance the lift of the flying body: in this way, the bouncing function of flying toys is more prominent, and the elastic effect is more excellent.
The detection sensor can be a gyroscope or accelerometer, or an electrical touch switch.
The upper stressed part 4 can be arranged on the upper part of the flying shell 11, so that it is convenient to apply the flapping force to the upper stressed part 4, so as to cooperate with the ground area and improve the use interest of the flying toy.
The upper stressed part 4 is arranged in a sheet shape, so that the stressed area of the upper stressed part 4 is increased, and it is convenient to slap the upper stressed part 4, thereby facilitating the output of deceleration signals.
The upper stressed part 4 can be a vibrating piece, such as a vibration sensor, which receives vibration such as flapping force to realize the output of deceleration signals: of course, the upper stressed part 4 can also be other elements, which are mainly used to output deceleration signals, and the application does not limit the specific elements used by the upper stressed part 4.
The lower stressed part is arranged in a sheet shape, and the lower stressed part and the elastic part 2 are arranged in a flat and abutting manner, so that the stressed area of the lower stressed part and the elastic part 2 is increased, and it is convenient to receive the acting force on the lower stressed part, thereby facilitating the output of acceleration signals.
The lower part of the lower stressed part is flush with the elastic part 2, which realizes the synchronous stress of the lower stressed part and the elastic part 2 and facilitates the output of accelerated signals.
The lower stress part can be an impact sensor, and the signal output is realized by the received impact force: of course, the lower stressed part can also be other elements, which are mainly used to accelerate the signal output, and the application does not limit the specific components used by the lower stressed part.
The flying shell 11 has a downward lower shell surface, and the elastic part 2 is installed on the lower shell surface.
The elastic part 2 includes an elastic plate 21, which is arranged elastically, and the lower shell surface and the elastic part 2 are arranged in a superposed connection along the top-down direction, and the elastic plate 21 is used for bouncing the flying body 1.
In this way, when the flying body 1 is slapped towards the ground, the elastic plate 21 contacts the ground first and is stressed first, and the flying body 1 is urged to bounce to a certain height by the elastic return of the elastic plate 21, and then the user can slap the flying body 1 again.
The lower shell surface is provided with an mounting part 114, which is arranged in a downward convex manner, and the mounting part 114 and the elastic plate 21 are arranged in a superposed connection manner along the top-down direction: Under the function of the mounting part 114, it is convenient to set the elastic plate 21, and at the same time, the distance between the elastic plate 21 and the flying body 1 is increased, so that the flying body 1 is prevented from directly colliding with the ground when being used on the ground, and the flying body 1 is protected.
The lower shell surface is provided with an extended cambered surface, which is arranged in an arc shape and is arranged in the middle, and the elastic plate 21 is arranged on the extended cambered surface: in this way, the overall aircraft is more stable, and at the same time, it is convenient for the elastic plate 21 to contact the ground when flapping.
The thickness of the elastic plate 21 is based on the requirement of springing up, and the higher the height of springing up, the thicker the elastic plate 21 is.
Generally, the pop-up height is between 50 cm and 30 cm, which is convenient for users to slap again.
The mounting part 114 has a mounting groove, and the upper part of the elastic plate 21 is embedded with the mounting groove, and the lower part of the elastic plate 21 extends downward to the outside of the mounting groove, and the lower part of the elastic plate 21 is used to contact the ground to pop up the flying body 1.
Under the action of the installation groove, the elastic plate 21 is positioned and reinforced, which is convenient for the installation of the elastic plate 21 and improves the installation stability of the elastic plate 21.
A plurality of contact surfaces are formed on the outer surface of the elastic plate 21, and the contact surfaces are used for contacting with the ground, and the orientations of the contact surfaces are arranged inconsistently: In this way, when the contact surface of the elastic plate 21 is in contact with the ground, the bouncing angle and direction of the flying body 1 are uncertain under the action of each contact surface, so that the bouncing angle and direction of the flying body 1 are uncertain, and the use interest of the flying body 1 is enhanced.
Alternatively, the outer surface of the elastic plate 21 forms a contact surface which is irregularly arranged: in this way, when the contact surface of the elastic plate 21 is in contact with the ground, the bouncing angle and direction of the flying body 1 are uncertain under the action of each contact surface, so that the bouncing angle and direction of the flying body 1 are uncertain, and the use interest of the flying body 1 is enhanced.
The elastic plate 21 is a silicone rubber plate, which can be deformed by force and exert elastic force in the opposite direction after reset.
Alternatively, the elastic plate 21 is a rubber plate, so that it can be deformed by force and exert elastic force in the opposite direction after returning.
Alternatively, the elastic plate 21 is made of EVA material, so that it can be deformed by force and exert elastic force in the opposite direction after returning.
The central shaft 13 extends through the flying shell 11 and is connected with the elastic part 2. The central shaft 13 is driven to rotate, and the central shaft 13 is used to drive the elastic part 2 to rotate.
In this way, when in use, the elastic part 2 is arranged in a rotating way. When the elastic part 2 is in contact with the ground, under the action of the rotating force, the bouncing angle of the flying body 1 is easy to be irregular, and the angle and direction for realizing the bouncing of the flying body 1 are uncertain, thus enhancing the use interest of the flying body 1.
Alternatively, the elastic plate 21 is movably arranged with the central shaft 13, that is, the elastic plate 21 is not driven by the central shaft 13, but the central shaft 13 plays a role in reinforcing and positioning the elastic plate 21, thus improving the installation stability and product stability of the elastic plate 21. At the same time, when the elastic plate 21 touches the ground, the elastic plate 21 is still used to bounce up the flying body 1.
The mounting part 114 includes a plurality of clamping bars 1141 and a mounting rings 1142, which are arranged in an annular shape, and each clamping bar 1141 is arranged at intervals along the circumference. After the elastic plate 21 is assembled in the mounting part 114, the clamping bars 1141 are arranged at intervals along the circumferential direction of the elastic plate 21, and each clamping bar 1141 is arranged in an abutting manner simultaneously with the elastic plate 21. In this way, when the elastic plate 21 is in contact with the ground, the locking bar 1141 is more easily stressed, which is convenient for applying elastic force in the opposite direction to make the flying body 1 bounce.
The clamping bars 1141 are arranged in an arc shape, so that the contact area between the clamping bars 1141 and the elastic plate 21 is increased, and the stress strength of the clamping bars 1141 is improved, which is convenient for feedback to make the flying body 1 bounce.
The mounting part 114 is arranged elastically, which highlights the bouncing function of the flying toy, and the elastic effect is more excellent.
The retaining bar 1141 and the mounting ring 1142 are respectively arranged elastically, which further highlights the bouncing function of the flying toy, and the elastic effect is more excellent.
The elastic element 2 includes a spring element 22 and a stressed plate 23, which is arranged below the flying body 1, is extended or contracted, is longitudinally extended, is connected with the flying body 1 at the upper part, and is connected with the stressed plate 23 at the lower part, and is used for bouncing up the flying body 1.
In this way, when the flying body 1 is slapped toward the ground, the stress plate 23 first contacts the ground, and the impact force is transmitted to the spring part 22, so that the spring part 22 is deformed into a compressed state, and then the flying body 1 is urged to bounce to a certain height by the elastic return of the spring part 22, and then the user can slap the flying body 1 again.
The lower shell surface is provided with a mounting part 114, which is arranged in a downward convex manner, and the mounting part 114 is provided with a mounting groove, and the upper part of the spring element 22 is embedded with the mounting groove, and the mounting groove has a mounting wall which surrounds the upper part of the spring element 22; under the action of the mounting wall, the installation stability of the spring element 22 is enhanced, and at the same time, the deformation of the spring element 22 is smoother, and it is convenient for the spring element 22 to deform and reset longitudinally and to pop up the flying body 1.
The mounting part 114 includes a shell rotating plate, the upper part of the spring part 22 is connected with the shell rotating plate, the central shaft 13 extends through the flying shell 11 and is connected with the shell rotating plate, and the rotating shaft is used for synchronously driving the shell rotating plate to rotate.
When in use, the shell rotating plate is rotationally arranged under the driving of the rotating shaft, and the shell rotating plate drives the spring element 22 and the stressed plate 23 to rotate in a synchronous rotation arrangement: when the stress plate 23 is in contact with the ground, under the action of the rotating force, the bouncing angle of the flying body 1 is easy to be irregular, and the angle and direction of realizing the bouncing of the flying body 1 are uncertain, thus enhancing the use interest of the flying body 1.
When in use, the shell rotating plate is rotationally arranged under the drive of the central shaft 13, and the stressed plate 23 is also synchronously rotated. When the stressed plate 23 is in contact with the ground, under the action of the rotating force, the bouncing angle of the flying body 1 is easy to be irregular, and the angle and direction for realizing the bouncing of the flying body 1 are uncertain, thus enhancing the use interest of the flying body 1.
The outer surface of the stressed plate 23 has a plurality of stressed surfaces, which are arranged obliquely and irregularly. In this way, when the stressed surface touches the ground, the bouncing angle and direction of the flying body 1 are uncertain under the action of each stressed surface, so that the bouncing angle and direction of the flying body 1 are uncertain, and the use interest of the flying body 1 is enhanced.
The flying body 1 includes an inertia ring 15, which sleeves the blade part 12, and the inertia ring 15 is connected with the blade part 12, and the driving part 14 is used for synchronously driving the blade part 12 and the inertia ring 15 to rotate: the inertia ring 15 generates rotational inertia when rotating, and the inertia ring 15 is used to realize internal rotation self-balance.
When in use in the air, the driving part 14 drives the blade part 12 and the inertia ring 15 to rotate. When the flying shell 11 is thrown out, the flying shell 11 rotates due to the reverse torque of the rotation of the blade part 12, and the flying shell 11 and the blade part 12 jointly generate the angular momentum of the aircraft to achieve self-stable flight in the air. During hand-holding, due to the moment of inertia generated by the synchronous high-speed rotation of the inertia ring 15 and the blade part 12, the internal rotation self-balance of the aircraft can be realized without the rotation of the flying shell 11, so the whole flying shell 11 is a hand-held part, which greatly reduces the entry difficulty of user operation and the convenience of control.
Inertia refers to angular momentum, that is, the flying shell 11 and the blade part 12 jointly produce the angular momentum of aircraft self-stabilization.
The blade part 12 rotates synchronously with the inertia ring 15 at high speed to generate the moment of inertia, so that when the aircraft is thrown, the corresponding angle can be maintained. After the external force to be thrown disappears, the angle of the rotary aircraft is still maintained at the moment of inertia of the blade part 12 and the inertia ring 15, and the wind generated by the high-speed rotation of the blade part 12 can be decomposed into lift force and offset force, and the direction of the offset force is the same as that of the rotary aircraft when it is thrown. The lift maintains the flying height of the gyro, and the offset force controls the flying angle of the gyro. Therefore, the preset flight path can be achieved by presetting the angle of the aircraft when it is thrown.
The central shaft 13 is movably arranged with the flying shell 11, and the flying shell 11 is driven to rotate by the airflow generated by the blade part 12 without being driven by the central shaft 13. It is convenient to realize smooth flight.
The central shaft 13 plays a role in positioning and facilitating the installation of the blade part 12.
The inertia ring 15 is annularly arranged, and the blade part 12 includes a blade seat 122 and a plurality of blade bodies 121, each blade body 121 is circumferentially arranged at intervals along the circumference of the blade seat 122, the inner ends of the blade bodies 121 are connected with the blade seat 122, and the outer ends of the blade bodies 121 are connected with the inertia ring 15: in this way, under the action of the inertia ring 15, the blade part 121 are synchronously connected and arranged, so that the blade part 121 and the inertia ring 15 are integrated, and the rotation stability is improved.
The blade body 121 is arranged in an inclined manner, and the outer end of the blade body 121 is embedded with the inertia ring 15: in this way, the connection stability between the inertia ring 15 and the blade body 121 is improved, and at the same time, the airflow generation of the blade body 121 is not affected.
The inertia ring 15 is integrally arranged with the outer ends of each blade body 121, which is convenient for production and manufacturing, and at the same time, reduces the use of connecting parts.
The inertia ring 15 is suspended, and the inertia ring 15 is movably arranged with the flying shell 11: in this way, the inertia ring 15 and the flying shell 11 are arranged independently, and the rotation between the inertia ring 15 and the flying shell 11 will not affect each other. When the flying shell 11 is held, the inertia ring 15 and the blade part 12 are in a state of internal rotation and self-balance, which is convenient for the subsequent single-paddle self-stabilizing aircraft to throw:
The blade part 12 is movably arranged with the central shaft 13, and the central shaft 13 is used for positioning the blade part 12: it is convenient for the arrangement of the blade part 12 and the central arrangement of the blade part 12, thus improving the flight stability of the single-paddle self-stabilizing aircraft.
Alternatively, the blade part 12 is connected with the central shaft 13, and the central shaft 13 and the blade part 12 are synchronously rotated.
The flying shell 11 includes a plurality of flow-around blade part, which are arranged in a circumferential interval and corresponding to the blade part 12, and the flow-around blade part and the blade part 12 are arranged in a corresponding manner. When a user throws a single-slurry self-stabilized aircraft, the blade body 121 and the inertia ring 15 rotate at high speed to generate flying airflow respectively, and at the same time, the rotational inertia generated by the high-speed rotation makes the aircraft angle self-stabilized, and at the same time, the reverse torque of the rotation of the blade body 121 and the inertia ring 15 drives the whole flying shell 11 to rotate, which is further maintained.
The flying shell 11 and the blade part 12 are arranged in a coaxial rotation mode, so that the rotation of the whole single-paddle self-stabilizing aircraft is kept in a concentric arrangement, so as to avoid eccentricity and interference to the self-stabilization of the single-paddle self-stabilizing aircraft.
The flying shell 11 has an inertia zone, and the inertia ring 15 is horizontally placed in the inertia zone, and the cross-sectional diameter of the inertia zone is larger than the diameter of the inertia ring 15, such that the flying shell 11 does not interfere with the rotation of the inertia ring 15.
The flying shell 11 is fully enclosed, which protects the internal components of the flying shell 11 and is convenient to throw out. At the same time, the hand-held area of the flying toy is enlarged, which is convenient for the use of the flying toy.
The flying shell 11 includes a first shell 111 and a second shell 112. Two ends of the central shaft 13 are respectively connected with the first shell 111 and the second shell 112, and the centers of the first shell 111, the blade seat 122 and the second shell 112 are coaxially arranged correspondingly. The first shell 111 and the second shell 112 form a fully enclosed cavity in a snap arrangement, and the blade part 12, the central shaft 13 and the driving part 14 are respectively located in the fully enclosed cavity.
Furthermore, the flying shell 11 is arranged in a spherical shape, which is convenient for throwing out the flying shell 11, and at the same time, the hand-held area of the flying toy is enlarged, which is convenient for the use of the flying toy.
The first shell 111 has a shell column 113, which extends in the direction towards the second shell 112, and the end of the central shaft 13 is embedded with the shell column 113, which is coaxially arranged corresponding to the blade seat 122. Under the action of the shell column 113, it is convenient to connect the central shaft 13 with the first shell 111, and at the same time, it is convenient to arrange the blade part 12 in the center to avoid eccentricity.
A buckle is formed on the first shell 111, and a buckle position is formed on the second shell 112. The buckle and the buckle position are in a snap fit, and the first shell 111 and the second shell 112 are buckled.
Because the first shell 111 and the second shell 112 are arranged in a locked manner, it is convenient to separate the flying shell 11, thus facilitating the hardware upgrade or maintenance of the flying body 1.
Alternatively, the first shell 111 and the second shell 112 can be detachably and fixedly connected by means of screws, so as to further increase the stability of the flying shell 11.
The first shell 111 and the second shell 112 are buckled to form a semi-enclosed cavity and a peripheral cavity. The second shell 112 has an outer holding part, and the semi-enclosed cavity and the peripheral cavity are arranged in communication. The blade part 12 and the central shaft 13 are in the semi-enclosed cavity, and the driving part 14 is embedded with the peripheral cavity. Under the action of the peripheral cavity, the arrangement of the driving part 14 is facilitated.
Furthermore, the flying shell 11 is arranged in a flying saucer shape, which is convenient for holding the flying shell 11 up and down, and is convenient for the flying shell 11 to rotate on the hand, thus improving the interest of holding.
The driving part 14 comprises a driven gear 142, a motor gear and a driving motor 141, wherein the central shaft 13 penetrates through the driven gear 142, the driven gear 142 is connected with the blade seat 122, the driving motor 141 is connected with the motor gear, the driving motor 141 is used for driving the motor 141 to rotate, and the motor gear is engaged with the driven gear 142.
In this way, the driving force output by the driving motor 141 urges the motor gear to rotate, and the motor gear transmits the driving force to the driven gear 142, and the driven gear 142 drives the blade seat 122 to rotate, thus realizing the rotary driving of the blade part 12.
The driving part 14 includes a battery, a control panel and an assembly rack. The driving motor 141, the battery and the control panel are respectively installed in the assembly rack, which is installed in the flying shell 11 and movably arranged with the central shaft 13. The driving motor 141 is used to output driving force, the battery is used to provide electric energy, the control panel is used to output control programs, and the driving motor 141 and the battery are correspondingly arranged along both sides of the central shaft 13.
The motor and the battery are correspondingly arranged along both sides of the central shaft 13: in this way, the overall counterweight of the single-paddle self-stabilizing aircraft is more uniform, so that the flight stability of the single-paddle self-stabilizing aircraft is more stable.
The central shaft 13 penetrates through the driven gear 142, and the central shaft 13 is connected with the driven gear 142, the motor gear is engaged with the driven gear 142, the driving motor 141 is used to drive the motor 141 to rotate, the motor gear is used to synchronously drive the driven gear 142 and the central shaft 13 to rotate, and the central shaft 13 is used to drive the flying shell 11 to rotate synchronously.
The driving motor 141 is used to drive the central shaft 13 to rotate synchronously with the flying shell 11. That is, the central shaft 13 penetrates through the driven gear 142 and the blade seat 122 synchronously, and is connected with the driven gear 142 and the blade seat 122 synchronously, or is connected with the driven gear 142 or the blade seat 122.
In this way, when the driving motor 141 outputs the driving force to urge the motor gear to rotate, the motor gear transmits the driving force to the driven gear 142, so as to realize synchronous driving rotation of the blade part 12 and the central shaft 13.
The flying toy with various playing modes includes a lamp strip 3 for emitting light, and the lamp strip 3 is installed on the outer surface of the flying shell 11: the single-paddle self-stabilizing aircraft can emit light at the outer edge, which is convenient for light emission, improves the atmosphere and improves the use interest of the single-paddle self-stabilizing aircraft.
In addition, the advantage of installing the lamp strip 3 on the surface is that when the whole aircraft rotates, the whole aircraft is in a luminous state, and a whole luminous body is visually seen.
The outer surface of the flying shell 11 is provided with a lamp groove, and the lamp groove is arranged in a concave way, and the lamp strip 3 is embedded in the lamp groove, which is convenient for wiring and arrangement of the lamp strip 3.
The above is only the preferred embodiment of the present invention, and it is not used to limit the present invention. Any modification, equivalent substitution and improvement made within the spirit and principle of the present invention should be included in the protection scope of the present invention.
| Number | Date | Country | Kind |
|---|---|---|---|
| 2023210189230 | Apr 2023 | CN | national |
| 2023211343156 | May 2023 | CN | national |
