CN110124327A - Flight finger tip gyro - Google Patents
Flight finger tip gyro Download PDFInfo
- Publication number
- CN110124327A CN110124327A CN201910341683.XA CN201910341683A CN110124327A CN 110124327 A CN110124327 A CN 110124327A CN 201910341683 A CN201910341683 A CN 201910341683A CN 110124327 A CN110124327 A CN 110124327A
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- flight
- main body
- bearing
- finger tip
- tip gyro
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- 230000000694 effects Effects 0.000 claims abstract description 5
- 238000000034 method Methods 0.000 abstract description 3
- 230000007547 defect Effects 0.000 abstract 1
- 210000003811 finger Anatomy 0.000 description 59
- 238000009434 installation Methods 0.000 description 11
- 238000009826 distribution Methods 0.000 description 8
- 239000002360 explosive Substances 0.000 description 4
- 238000003756 stirring Methods 0.000 description 3
- 238000010586 diagram Methods 0.000 description 2
- 239000011159 matrix material Substances 0.000 description 2
- 239000007787 solid Substances 0.000 description 2
- 230000001174 ascending effect Effects 0.000 description 1
- 230000004888 barrier function Effects 0.000 description 1
- 239000004744 fabric Substances 0.000 description 1
- 230000010006 flight Effects 0.000 description 1
- 210000004209 hair Anatomy 0.000 description 1
- 230000003993 interaction Effects 0.000 description 1
- 230000033001 locomotion Effects 0.000 description 1
- 238000002360 preparation method Methods 0.000 description 1
- 238000004064 recycling Methods 0.000 description 1
- 238000003860 storage Methods 0.000 description 1
- 239000000725 suspension Substances 0.000 description 1
- 210000003813 thumb Anatomy 0.000 description 1
- 238000005303 weighing Methods 0.000 description 1
Classifications
-
- A—HUMAN NECESSITIES
- A63—SPORTS; GAMES; AMUSEMENTS
- A63H—TOYS, e.g. TOPS, DOLLS, HOOPS OR BUILDING BLOCKS
- A63H1/00—Tops
-
- A—HUMAN NECESSITIES
- A63—SPORTS; GAMES; AMUSEMENTS
- A63H—TOYS, e.g. TOPS, DOLLS, HOOPS OR BUILDING BLOCKS
- A63H1/00—Tops
- A63H1/10—Tops able to be spun by whirling the axis with both hands
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- Toys (AREA)
Abstract
The application provides a kind of flight finger tip gyro, including rotating grip portion, main part and control unit；Rotating grip portion includes centre of rotation and bearing part, and centre of rotation bearing is connected to main part by bearing part；Main part includes main frame and at least two pairs of flight power-assisted units；Control unit is located in main part, flight power-assisted is provided for controlling at least two pairs of flight power-assisted units, to drive flight finger tip gyro hovering flight.The application solves the single defect of flight finger tip gyro playing method, greatly enhances its interest by making the effect of flight finger tip gyro lighter-than-air flight in the case where no external force clamps in finger tip Gyroscope Design flight power-assisted unit.
Description
Technical field
This application involves a kind of toy, in particular to a kind of flight finger tip gyro.
Background technique
Current finger tip gyro can only be operated on palm, need to mention by the power of pinching of thumb and another finger
For fixed pivot, recycling third finger to stir rotates it between two finger tips.
Summary of the invention
The application's is designed to provide a kind of flight finger tip gyro, is hanged with solving finger tip gyro under the clamping of no external force
The technical issues of empty flight.
The application provides a kind of flight finger tip gyro, including rotating grip portion, main part and control unit；The rotation is held
The portion of holding includes centre of rotation and bearing part, and the centre of rotation bearing is connected to the main part by the bearing part；Institute
Stating main part includes main frame and at least two pairs of flight power-assisted units；Described control unit is set in the main part, is used for
Control at least two pairs of flight power-assisted units provide flight power-assisted, to drive the flight finger tip gyro vacantly to fly；
Wherein, the main frame includes main body upper casing, main body rack and main body lower casing, the main body upper casing and the main body
Lower casing is relatively mounted on the two sides up and down of the main body rack, and the main body rack includes at least two pairs of separated regions, each
To separated region for placing a pair of flight power-assisted unit respectively；
Wherein, the main body upper casing and the main body lower casing are respectively equipped with two bearing positioning regions, and described two bearings are fixed
Position portion includes two finger caps for installing the bearing part, the centre of rotation, and described two finger caps pass through the axis
Bearing member bearing is connected to described two bearing positioning regions；
Wherein, the center of the main body upper casing and the main body lower casing is recessed to form two to the main body rack direction
A recessed groove, described two recessed grooves are respectively used to accommodate described two finger caps, the bearing positioning of the main body upper casing
Shell is recessed in the recessed groove to be formed portion's setting on the body, and the bearing positioning region of the main body lower casing is arranged described
Main body lower casing is recessed in the recessed groove to be formed；
Wherein, each bearing positioning region includes the bearing groove that opens up of groove bottom in the corresponding recessed groove, institute
It states bearing part to be contained in the bearing groove and can rotate relative to the bearing groove, the outer diameter face of the bearing part and the bearing
The inner wall of slot cooperates, and the aperture surface of the bearing part and the centre of rotation cooperate；
Wherein, each bearing positioning region includes the fixing lug boss in the groove bottom setting of the corresponding recessed groove,
The bearing part is contained in the bearing groove and can rotate relative to the bearing groove, the aperture surface of the bearing part with it is described solid
Determine boss cooperation, and the bearing part can be rotated around the fixing lug boss and relative to the fixing lug boss, the bearing part
Outer diameter face and the centre of rotation cooperate；
Wherein, through-hole is offered in the groove bottom of the recessed groove, the bearing positioning region is included in two through-holes
Two movable boss that inside is installed respectively, described two activity boss are by passing through a connection being arranged in through-hole
Axis is fixedly connected, and the connecting shaft is located at the main frame centre and through the main frame, the activity boss and institute
The aperture surface for stating bearing part is coupled, and the outer diameter face of the finger cap and the bearing part is coupled；
Wherein, the center of the main part is provided with the through hole through the main part upper and lower side, the rotation
Turning central part is a rotary shaft, and the rotary shaft is arranged in the through hole, and the master is stretched out at the both ends of the rotary shaft
After body upper casing and the main body lower casing, connected respectively by two bearing parts and the main body upper casing and the main body lower casing
It connects, the both ends of the rotary shaft are also separately installed with finger cap；
Wherein, the main body upper casing and the main body lower casing are equipped with bearing positioning region, and the bearing positioning region is used for and institute
Bearing part cooperation is stated, and the rotation is pivotally connected to the main body upper casing and the main body lower casing；
Wherein, the main body upper casing and main body lower casing center are recessed to form two to the main body rack direction
Recessed groove, the recessed groove just accommodate the finger cap, and the bearing positioning region is arranged inside the recessed groove；
Wherein, the bearing positioning region is the bearing groove that opens up respectively of groove bottom in the recessed groove, the bearing groove
For being coupled with the bearing part；
Wherein, the main body rack include be in criss-cross support arm, it is described in criss-cross support arm by the main body
Bracket is separated into two pairs of separated regions, and the main part includes two pairs of flight power-assisted units, each pair of flight power-assisted list
Member is respectively symmetrically distributed in corresponding a pair of of separated region；
Wherein, the flight power-assisted unit includes motor and the rotor that is mounted on the motor, and the motor accommodates
In the main body lower casing；
Wherein, the main body upper casing and the main body lower casing use hollow design；
Wherein, described control unit includes controller, and the controller includes at least one transmitter and at least one connects
Device is received, and is mounted on the periphery of the main frame, for transmitting and receiving signal；
Wherein, described control unit includes controller, and the controller includes at least one transceiver, it is described at least
One transceiver is mounted on the periphery of the main frame, for transmitting and receiving signal；
Wherein, 2 transmitters and 2 receivers are respectively equipped in the upper and lower end face of the main frame, in institute
The periphery for stating main frame has been uniformly distributed 4 transmitters and 4 receivers；
Wherein, 2 transmitters and 2 receivers are respectively equipped in the upper and lower end face of the main frame, in institute
The periphery for stating main frame has been uniformly distributed 4 transmitters；
Wherein, 2 transmitters and 2 receivers are respectively equipped in the upper and lower end face of the main frame, in institute
The periphery for stating main frame has been uniformly distributed 2 transmitters；
Wherein, described control unit includes rotation sensor, and the rotation sensor is used to detect oneself of the main part
Rotary speed controls the starting of the flight power-assisted unit.
In conclusion the flight finger tip gyro of the application is realized and is not being had by design flight power-assisted unit and controller
In the case where having external force clamping, to the control that flight finger tip gyro vacantly flies, so that the movement of flight finger tip gyro is diversified,
Interest and human-computer interaction playability are increased, solving existing gyro can only rotate in the hand, cannot fly in the sky
Technical problem.
Detailed description of the invention
In order to illustrate the technical solutions in the embodiments of the present application or in the prior art more clearly, to embodiment or will show below
There is attached drawing needed in technical description to be briefly described, it should be apparent that, the accompanying drawings in the following description is only this
Some embodiments of application for those of ordinary skill in the art without creative efforts, can be with
It obtains other drawings based on these drawings.
Fig. 1 is the structural schematic diagram of flight finger tip gyro provided by the present application；
Fig. 2 is the explosive view for the flight finger tip gyro that a kind of embodiment of the application provides；
Fig. 3 is the structure chart of main body upper casing and rotating grip portion in Fig. 2 embodiment；
Fig. 4 is the explosive view for the flight finger tip gyro that the application another kind embodiment provides；
Fig. 5 is the structure chart of main body upper casing and rotating grip portion in Fig. 4 embodiment；
Fig. 6 is the explosive view for the flight finger tip gyro that the application another kind embodiment provides；
Fig. 7 is the structure chart of main body upper casing and rotating grip portion in Fig. 6 embodiment；
Fig. 8 is the explosive view for the flight finger tip gyro that the application another kind embodiment provides；
Fig. 9 is the structure chart of main body upper casing and rotating grip portion in Fig. 8 embodiment；
Figure 10 is the top view of flight finger tip gyro provided by the present application；
Figure 11 is the spatial distribution map of controller in a kind of embodiment of the application；
Figure 12 is the spatial distribution map of controller in the application another kind embodiment；
Figure 13 is the spatial distribution map of controller in the application another kind embodiment；
Figure 14 is the spatial distribution map of controller in the application another kind embodiment；
Figure 15 is a kind of structural schematic diagram of embodiment axis bearing member of the application；
Figure 16 is the sectional view of A-A in Figure 15.
Specific embodiment
Below in conjunction with the attached drawing in the embodiment of the present application, technical solutions in the embodiments of the present application carries out clear, complete
Site preparation description.
The application provides a kind of flight finger tip gyro 100 referring to FIG. 1-2, comprising: including rotating grip portion 10, main body
Portion 20 and control unit 30；Rotating grip portion 10 includes centre of rotation 12, and connection centre of rotation 12 and main part 20
Bearing part 14；Main part 20 includes main frame 22 and at least two pairs of flight power-assisted units 24, and each pair of flight power-assisted unit 24 is distinguished
It is symmetrically positioned in the region separated by main frame 22；Control unit 30 is set in main part 20, for controlling flight power-assisted list
Member 24 generates flight power-assisted to realize the hanging flight of flight finger tip gyro 100, and control unit 30 includes 32 He of rotation sensor
Controller 34, when around 10 20 rotation of main part of rotating grip portion, rotation sensor 32 will test main part 20 from revolving speed
Degree, if 20 rotational velocity of main part reaches pre-set velocity, controller 34 controls the work of flight power-assisted unit 24 and generates flight power-assisted,
Realize 100 hovering flight of flight finger tip gyro.
As shown in Fig. 2, main frame 22 includes main body upper casing 222, main body rack 224 and main body lower casing 226, main body upper casing
222 and main body lower casing 226 be relatively mounted on the two sides up and down of main body rack 224, main body rack 224 include be in criss-cross branch
Main body rack 224 is separated into two pairs of separated regions in criss-cross support arm by boom, and main part 20 includes two pairs of flights
Power-assisted unit 24, each pair of flight power-assisted unit 24 are respectively symmetrically distributed in corresponding a pair of of separated region.It is this symmetrical
Stability of the product in flight course can be improved in the design of distribution, in some embodiments, two in each pair of separated region
A separated region is non-conterminous.
Main frame 22 is the installation shell and frame of entire flight finger tip gyro 100.Main body cover 222 and main body lower casing
226 are connect with post support 224 respectively by screw 228, and the two forms the shell of entire product, plays to flight finger tip top
The protection of 100 inner body of spiral shell.Main body rack 224 divides flight finger tip gyro 100 for multiple sections, and different sections is for receiving
Hold different flight power-assisted units 24.Fixed flight power-assisted is separately provided on main body upper casing 222 and main body lower casing 226
The fixed lid 2222 of the flight power-assisted unit of unit 24 and flight power-assisted unit fixing seat 2262.
Meanwhile main body cover 222 in embodiment and main body lower casing 226 are all using hollow design, one side of this design
Face is conducive to the light-weight design of flight finger tip gyro 100, is on the other hand also that flight power-assisted unit 24 generates ascending air
Design consideration.
In one embodiment, as shown in Fig. 2, centre of rotation 12 includes two finger caps, it is used for fingerhold；?
The opposite position of main body upper casing 222 and the center of main body lower casing 226 is respectively equipped with two bearing positioning regions 225, two finger caps with
Two bearing positioning regions 225 for being set to main body upper casing 222 and main body lower casing 226 are connected by bearing part 14 respectively, realize hand
Refer to that cap is connect with the bearing of main part 20.User lives in down symmetrically arranged finger cap by finger clamp, stirs main part 20
Can realize the rotation of flight finger tip gyro 100, controller 34 when rotation sensor 32 sense main part 20 from revolving speed
When degree reaches pre-set velocity, it just will start flight power-assisted unit 24 and generate flight power-assisted, such flight finger tip gyro 100
Realize hovering flight.
Specifically, as shown in figure 3, due to upper casing main body 222 with the structure of lower casing main body 226 here identical, Fig. 3
It is with upper casing main body 222 for signal, 226 structure of lower casing main body is same as shown in Figure 3, in upper casing main body 222 and lower casing main body 226
It entreats position to be recessed respectively to 224 direction of main body rack, is respectively formed 2 recessed grooves 221 up and down.2 recessed grooves 221 are respectively used to
Two finger caps of corresponding receiving installation.The round bearing slot for installing bearing part 14 is provided in 2 221 groove bottoms of recessed groove
2212, which is the bearing positioning region 225 of main frame 22.As shown in figure 16, the outer diameter face 144 of bearing part 14 with
The inner wall of bearing groove 2212 is coupled, so that bearing part 14 is contained in bearing groove 2212 and can be 2212 turns relative to bearing groove
It is dynamic.Finger cap is coupled with bearing part 14 respectively and is housed in recessed groove 221, finger cap at this time be in bearing part
Diametric plane 142 is coupled.The design of this storage type installation facilitates the light and handy of whole design, and main frame 22 is effectively utilized
Inner space.
Separately there is an embodiment, referring to Figure 4 together and Fig. 5, here due to upper casing main body 222 and lower casing main body 226
Structure is identical, therefore Fig. 5 is with upper casing main body 222 for signal, and 226 structure of lower casing main body is same as shown in Figure 5, upper casing main body
222 and 226 central location of lower casing main body respectively to 224 direction of main body rack be recessed, be respectively formed up and down 2 recessed grooves 221,2
A recessed groove 221 is respectively used to receiving installation finger cap.As shown in Fig. 5 and Figure 16, in the groove bottom of upper and lower 2 recessed grooves 221
Two fixing lug boss 2214 are respectively equipped with, which is the bearing positioning region 225 of main frame 22.Fixing lug boss
2214 and the aperture surface 142 of bearing part 14 be coupled, and bearing part 14 is around fixing lug boss 2214 and can be convex relative to fixation
Platform 2214 rotates, and the outer diameter face 144 of finger cap and bearing part 14 is coupled and is housed in recessed groove 221.
In another specific embodiment, referring to Figure 6 together and Fig. 7, herein due to upper casing main body 222 and lower casing main body 226
The structure at place is identical, therefore Fig. 7 is with upper casing main body 222 for signal, upper casing master same as shown in Figure 7 in lower casing main structure
Body 222 and 226 central location of lower casing main body are recessed to 224 direction of main body rack respectively, are respectively formed 2 recessed grooves 221 up and down.
Recessed groove 221 has through-hole 223 in the groove bottom of 2 recessed grooves 221, two are opened respectively for accommodating installation finger cap
It is corresponding set on the position of the through-hole 223 of the groove bottom of a recessed groove 221 and not through that is, two through-holes 223 are blind hole.?
The inside of 2 through-holes 223 is separately installed with 2 movable boss 2232, which is that the bearing of main frame 22 is fixed
Position portion 225.2 movable boss 2232 are fixedly connected by a connecting shaft 227 being arranged in through-hole, connecting shaft 227
Positioned at the centre of main frame 22, and can rotate through main frame 22 and relative to main frame 22.As shown in figure 16, movable boss
2232 are coupled and can mutually rotate with the aperture surface 142 of bearing part 14, and the outer diameter face 144 of finger cap and bearing part 14 cooperates
It installs and is fixed to each other.The installation of the bearing between movable convex block 2232 and finger cap is realized by bearing part 14, and then is realized
Main part 20 is connect with the bearing of centre of rotation 12.
Wherein, in the present embodiment, the through-hole 223 is square through hole, it is clear that in other embodiments, the through-hole
223 can be also circular through hole etc..
Separately there is an embodiment, as shown in figure 8, being provided in the center of main part 20 through 20 upper and lower side of main part
Through hole, a rotary shaft are arranged in the through hole and can rotate in through hole, which is rotating grip
The centre of rotation 12 in portion 10.Rotary shaft (centre of rotation 12) is fixedly connected by bearing part 14 with main part 20, and
The upper and lower ends of rotary shaft (centre of rotation 12) are mounted with the finger cap for fingerhold respectively.User passes through two hands
Finger clamps finger cap, then stirs main part 20, so that main part 20 is rotated around rotary shaft 124.
Specifically, main body upper casing 222 and main body lower casing 226 are equipped with bearing positioning region 225, the work of the bearing positioning region 225
With being to connect bearing part 14 and main part 20, to realize that rotary shaft 124 and the bearing of main part 20 are connect.
Specifically, as shown in Figure 9 (due to upper casing main body 222 with the structure of lower casing main body 226 here identical, Fig. 9
It is with upper casing main body 222 for signal, same as shown in Figure 9 in lower casing main structure), main body upper casing 222 and main body lower casing 226
Center is recessed to form 2 recessed grooves 221 up and down to 224 direction of main body rack.2 recessed grooves 221 formed are just used for
Finger cap is accommodated, while bearing positioning region 225 is also disposed in 2 recessed grooves 221.The design of recessed groove 221 on the one hand can be with
Finger cap 122 is accommodated, keeps the design of entire product more small and exquisite；On the other hand finger cap is contained in recessed groove 221, it can be with
Protection finger cap avoids finger cap with the collision on ground when entire finger tip flight gyro 100, which takes off, to land well.
Specifically, as shown in figure 16, offering upper 2 bearing grooves respectively in the groove bottom of upper and lower 2 recessed grooves 221
2212, this 2 bearing grooves 2212 are bearing positioning region 225, are coupled for the outer diameter face 144 with bearing part 14.At this time
The aperture surface 142 of bearing part 14 is coupled with rotary shaft 124, the outer diameter face 144 of bearing part 14 and the inner wall of bearing groove 2212
It matches, is connect to realize bearing groove 2212 with the bearing of rotary shaft 124, and then realize main part 20 and rotation center
The bearing of part 12 connects.
In one embodiment, divided referring to Figure 2 together with Figure 10, main frame 22 by main body rack 224 for four areas
Domain is in matrix pattern.Main part 20 includes two pairs of flight power-assisted units 24, and two pairs of flight power-assisted units 24 are symmetrically distributed in the master
In body frame.Two pairs of flight power-assisted units 24 are conducive to flight finger tip gyro 100 in flight to flat in the symmetrical of matrix pattern
The holding of weighing apparatus, convenient for the control of 30 pairs of flight power-assisted units 24 of control unit.
Specifically, as shown in Fig. 2, flight power-assisted unit 24 includes 244 two components of motor 242 and rotor, under main body
It is provided with the container 2263 of special receiving motor 242 on shell 226, and also has and container 2263 on main body rack 224
The receiving lid 2243 of cooperation.Motor 242 is placed in inside container 2263, and is covered to close by receiving lid 2243 and be fixed.By in master
Container 2263 and receiving lid 2243 are respectively set on body lower casing 226 and main body rack 224, realizes solid to the position of motor 242
Fixed, rational deployment spatially makes the whole design of flight finger tip gyro 100 compact ingenious.
In one embodiment, as shown in Fig. 2, the control unit of flight finger tip gyro 100 includes rotation sensor 32
With controller 34, rotation sensor 32 is used to detect the speed of the rotation when being struck of main part 20, sets when rotational velocity reaches
When definite value, rotation sensor 32 will send enabling signal to flight power-assisted unit 24, realize the suspension of flight finger tip gyro 100
Flight.Controller 34 includes at least one transmitter 342 and at least one receiver 344, these transmitters 342 and receiver
344 are distributed in the periphery of main frame 22, and design in this way is conducive to sending and receiving for transmitter 342 and 344 signal of receiver, with
It is anti-to be blocked because of signal by main frame 22.Preferably, transmitter 342 and receiver 344 it is pairs of it is arranged side by side together, in this way
Be conducive to sending and receiving for signal.
In a specific embodiment, controller 34 includes at least one transceiver, which can
Transmitting and receiving signal, transceiver are mounted on the periphery of the main frame, for transmitting and receiving signal.
Specifically, transmitter 342 can emit component for signal, signal can be launched outward, receiver 344 is signal
Component is received, can receive the signal being reflected back, being launched with received signal includes electromagnetic signal and acoustic signals.
In a specific embodiment, transmitter 342 is infrared transmitting tube, and receiver 344 is infrared receiving tube, infrared transmitting tube pair
Outer transmitting infrared signal, reflects when infrared signal encounters barrier, and infrared receiving tube receives reflected letter at this time
Number, to control the adjustment flight of flight power-assisted unit 24.
In a specific embodiment, it please also refer to Fig. 2 and Figure 11, is respectively equipped in the upper and lower end face of main frame 22
2 transmitter 342 and 2 receivers 344 (i.e. in Z-direction, Z axis is the axis perpendicular to 22 upper and lower end face of main frame), i.e.,
1 transmitter 342 and 1 receiver 344 is installed in the upper surface of main body upper casing 222, installs 1 in the lower end surface of main body lower casing 226
A transmitter 342 and 1 receiver 344；4 transmitter 342 and 4 receivers are spaced apart in the periphery of main frame 22 simultaneously
344 (i.e. in X-axis and Y direction, X-axis and Y-axis are the axis that main frame 22 is bisected into 4 regions), main body rack 224 and master
The outer edge of body lower casing 226 is provided with the mounting groove 346 of special installation transmitter 342 and receiver 344.
In another specific embodiment, (it is in main frame 22 as shown in figure 12 for distribution of the controller 34 in space
Installation can refer to the situation of Fig. 2), it can refer to the situation of Fig. 2 distribution, be respectively equipped with 2 hairs in the upper and lower end face of main frame 22
Emitter 342 and 2 receiver 344, the i.e. upper surface of main body upper casing 222 install 1 transmitter 342 and 1 receiver 344,
The lower end surface of main body lower casing 226 is installed by 1 transmitter 342 and 1 receiver 344；Simultaneously at the periphery interval of main frame 22 point
The outer edge of 4 transmitters 342 of cloth, main body rack 224 and main body lower casing 226 is provided with the peace of special installation transmitter 342
Tankage 346.
In another specific embodiment, (it is in main body as shown in Figure 13 and Figure 14 for distribution of the controller 34 in space
The installation of frame 22 can refer to the situation of Fig. 2), 2 transmitters 342 and 2, which are respectively equipped with, in the upper and lower end face of main frame 22 connects
Device 344 is received, i.e. 1 transmitter 342 and 1 receiver 344 is installed in the upper surface of main body upper casing 222, under main body lower casing 226
End face is installed by 1 transmitter 342 and 1 receiver 344；2 transmitters 342 are spaced apart in the periphery of main frame 22 simultaneously,
The outer edge of main body rack 224 and main body lower casing 226 is provided with the mounting groove 346 of special installation transmitter 342.
In the above embodiments, bearing part 14 can use radial bearing, such as centripetal ball bearing, radial needle roller bearing
Deng.In a specific embodiment, as shown in Figure 15 and Figure 16, bearing part 14 is centripetal ball bearing, including outer diameter face 144
With aperture surface 142, main part 20 by being coupled with bearing part 14, thus realization body portion 20 around rotating grip portion 10 from
Turn.
Above disclosed is only the application preferred embodiment, cannot limit the right model of the application with this certainly
It encloses, those skilled in the art can understand all or part of the processes for realizing the above embodiment, and wants according to the application right
Made equivalent variations is sought, still falls within and applies for covered range.
Claims (20)
1. a kind of flight finger tip gyro, which is characterized in that including rotating grip portion, main part and control unit；The rotation is held
The portion of holding includes centre of rotation and bearing part, and the centre of rotation bearing is connected to the main part by the bearing part；Institute
Stating main part includes main frame and at least two pairs of flight power-assisted units；Described control unit is set in the main part, is used for
Control at least two pairs of flight power-assisted units provide flight power-assisted, to drive the flight finger tip gyro vacantly to fly.
2. flight finger tip gyro according to claim 1, which is characterized in that the main frame includes main body upper casing, main body
Bracket and main body lower casing, the main body upper casing and the main body lower casing are relatively mounted on the two sides up and down of the main body rack,
The main body rack includes at least two pairs of separated regions, and every a pair of separated region for placing a pair of flight power-assisted list respectively
Member.
3. flight finger tip gyro according to claim 2, which is characterized in that the main body upper casing and the main body lower casing point
It does not set there are two bearing positioning region, for installing the bearing part, the centre of rotation includes for described two bearing positioning regions
Two finger caps, described two finger caps are connected to described two bearing positioning regions by the bearing part bearing.
4. flight finger tip gyro according to claim 3, which is characterized in that the main body upper casing and the main body lower casing
Center is recessed to form two recessed grooves to the main body rack direction, and described two recessed grooves are respectively used to accommodate described two
A finger cap, shell is recessed the recessed groove to be formed on the body for the bearing positioning region setting of the main body upper casing
In, the bearing positioning region of the main body lower casing is arranged in the main body lower casing and is recessed in the recessed groove to be formed.
5. flight finger tip gyro according to claim 4, which is characterized in that each bearing positioning region is included in correspondence
The recessed groove the bearing groove that opens up of groove bottom, the bearing part is contained in the bearing groove and can be relative to the bearing
The inner wall of slot rotation, the outer diameter face of the bearing part and the bearing groove cooperates, the aperture surface of the bearing part and the rotation
Central part cooperation.
6. flight finger tip gyro according to claim 4, which is characterized in that each bearing positioning region is included in correspondence
The recessed groove groove bottom setting fixing lug boss, the bearing part is contained in the bearing groove and can be relative to the axis
Hold slot rotation, the aperture surface of the bearing part and the fixing lug boss cooperate, and the bearing part around the fixing lug boss and
It can be rotated relative to the fixing lug boss, the outer diameter face of the bearing part and the centre of rotation cooperate.
7. flight finger tip gyro according to claim 4, which is characterized in that offered in the groove bottom of the recessed groove logical
Hole, the bearing positioning region include the two movable boss installed respectively inside two through-holes, and described two activities are convex
For platform by being fixedly connected by a connecting shaft being arranged in through-hole, the connecting shaft is located at the main frame central part
Position and run through the main frame, it is described activity boss and the bearing part aperture surface be coupled, the finger cap with it is described
The outer diameter face of bearing part is coupled.
8. flight finger tip gyro according to claim 2, which is characterized in that be provided in the center of the main part
Through the through hole of the main part upper and lower side, the centre of rotation is a rotary shaft, and the rotary shaft is arranged in described
In through hole, after the main body upper casing and the main body lower casing are stretched out in the both ends of the rotary shaft, pass through two axis respectively
Bearing member is connect with the main body upper casing and the main body lower casing, and the both ends of the rotary shaft are also separately installed with finger cap.
9. flight finger tip gyro according to claim 8, which is characterized in that the main body upper casing and the main body lower casing are set
There is bearing positioning region, the bearing positioning region is used to cooperate with the bearing part, and the rotation is pivotally connected to the main body
Upper casing and the main body lower casing.
10. flight finger tip gyro according to claim 9, which is characterized in that the main body upper casing and the main body lower casing
Center is recessed to form two recessed grooves to the main body rack direction, and the recessed groove just accommodates the finger cap, institute
Bearing positioning region is stated to be arranged inside the recessed groove.
11. flight finger tip gyro according to claim 10, which is characterized in that the bearing positioning region is in the recess
The bearing groove that the groove bottom of slot opens up respectively, the bearing groove is used for and the bearing part is coupled.
12. flight finger tip gyro according to claim 2, which is characterized in that the main body rack includes in criss-cross
Support arm, described that the main body rack is separated into two pairs of separated regions in criss-cross support arm, the main part includes two
To the flight power-assisted unit, each pair of flight power-assisted unit is respectively symmetrically distributed in corresponding a pair of of separated region.
13. flight finger tip gyro according to claim 12, which is characterized in that the flight power-assisted unit include motor and
The rotor being mounted on the motor, and the motor is contained in the main body lower casing.
14. according to flight finger tip gyro described in claim 2-13, which is characterized in that under the main body upper casing and the main body
Shell uses hollow design.
15. flight finger tip gyro according to claim 1, which is characterized in that described control unit includes controller, described
Controller includes at least one transmitter and at least one receiver, is mounted on the periphery of the main frame, for emitting and connecing
The collection of letters number.
16. flight finger tip gyro according to claim 1, which is characterized in that described control unit includes controller, described
Controller includes at least one transceiver, at least one described transceiver is mounted on the periphery of the main frame, is used
In transmitting and receive signal.
17. flight finger tip gyro according to claim 15, which is characterized in that distinguish in the upper and lower end face of the main frame
Equipped with 2 transmitters and 2 receivers, 4 transmitters and 4 have been uniformly distributed in the periphery of the main frame
A receiver.
18. flight finger tip gyro according to claim 17, which is characterized in that distinguish in the upper and lower end face of the main frame
Equipped with 2 transmitters and 2 receivers, 4 transmitters have been uniformly distributed in the periphery of the main frame.
19. flight finger tip gyro according to claim 18, which is characterized in that distinguish in the upper and lower end face of the main frame
Equipped with 2 transmitters and 2 receivers, 2 transmitters have been uniformly distributed in the periphery of the main frame.
20. flight finger tip gyro described in -19 according to claim 1, which is characterized in that described control unit includes rotation sensing
Device, the rotation sensor are used to detect the rotational velocity of the main part to control the starting of the flight power-assisted unit.
Priority Applications (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910341683.XA CN110124327B (en) | 2019-04-25 | 2019-04-25 | Flying finger tip top |
| PCT/CN2020/080358 WO2020215946A1 (en) | 2019-04-25 | 2020-03-20 | Flying fidget spinner |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910341683.XA CN110124327B (en) | 2019-04-25 | 2019-04-25 | Flying finger tip top |
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| CN110124327A true CN110124327A (en) | 2019-08-16 |
| CN110124327B CN110124327B (en) | 2024-03-22 |
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|---|---|
| CN110124327B (en) | 2024-03-22 |
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