CN206984415U - Split type camera component and the unmanned plane with camera - Google Patents
Split type camera component and the unmanned plane with camera Download PDFInfo
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- CN206984415U CN206984415U CN201720710444.3U CN201720710444U CN206984415U CN 206984415 U CN206984415 U CN 206984415U CN 201720710444 U CN201720710444 U CN 201720710444U CN 206984415 U CN206984415 U CN 206984415U
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- unmanned plane
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- 238000009434 installation Methods 0.000 claims description 58
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- 239000000463 material Substances 0.000 description 7
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- 241000276425 Xiphophorus maculatus Species 0.000 description 5
- 238000010276 construction Methods 0.000 description 4
- 230000005540 biological transmission Effects 0.000 description 3
- 238000005516 engineering process Methods 0.000 description 3
- 238000012986 modification Methods 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 230000006641 stabilisation Effects 0.000 description 2
- 238000011105 stabilization Methods 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000015572 biosynthetic process Effects 0.000 description 1
- 238000013461 design Methods 0.000 description 1
- 238000011161 development Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 239000007769 metal material Substances 0.000 description 1
- 230000000116 mitigating effect Effects 0.000 description 1
- 239000000203 mixture Substances 0.000 description 1
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Abstract
The utility model provides a kind of Split type camera component and the unmanned plane with camera, belongs to unmanned air vehicle technique field.Split type camera component is applied to the unmanned plane with camera.Unmanned plane with camera includes:Unmanned plane main body, unmanned plane main body are provided with multiple poles for being provided with rotor, and each pole is connected to form junction with remaining pole.Split type camera component includes:Master control borad, connecting line and camera.Master control borad is arranged on junction, and camera is arranged between two adjacent poles of unmanned plane main body, one end connection master control borad of connecting line, the other end connection camera of connecting line.By the diverse location that camera and master control borad are set to unmanned plane main body respectively so that the weight that unmanned plane main body is born is undertaken by different positions respectively, and reaches stress balance.It is thereby achieved that while unmanned plane volume minimizes, effectively prevent unmanned plane from being shaken in flight course.
Description
Technical field
Unmanned air vehicle technique field is the utility model is related to, is taken the photograph in particular to a kind of Split type camera component and band
As the unmanned plane of head.
Background technology
With the development of science and technology and improve, the performance of electronic equipment is stronger and stronger, and unmanned plane has obtained widely
Using.
With the more and more higher to unmanned plane during flying performance requirement, unmanned plane is while volume minimizes, it is also necessary to flies
It is higher and farther.Camera is the important composition part in unmanned plane, and the picture captured by camera can be helped effectively
Manipulator controls unmanned plane.In currently available technology, generally camera is entirely arranged on unmanned plane.With unmanned plane
Volume minimizes, and because whole camera is overweight, causes unmanned plane to be shaken in flight course, and then has had a strong impact on pair
The control of unmanned plane.
Therefore, how while unmanned plane volume minimizes, and effectively prevent unmanned plane from occurring in flight course
Shake is current industry a great problem.
Utility model content
In view of this, the purpose of this utility model is to provide a kind of Split type camera component and nobody with camera
Machine, to improve drawbacks described above.
Embodiment of the present utility model is accomplished by the following way:
In a first aspect, the utility model embodiment provides a kind of Split type camera component, applied to the nothing with camera
Man-machine, the unmanned plane with camera includes:Unmanned plane main body, the unmanned plane main body are provided with rotor provided with multiple
Pole, each pole is connected to form junction with pole remaining described.The Split type camera component includes:It is main
Control plate, connecting line and camera, the master control borad are arranged on the junction, and the camera is arranged on the unmanned machine host
Between two adjacent poles of body phase, one end of the connecting line connects the master control borad, and the other end of the connecting line connects
Connect the camera.
Further, one end of the connecting line and the master control borad are detachably connected.
Further, the master control borad is provided with connected slot, one end of the connecting line and the connected slot can
Dismantling connection.
Further, set location of the connected slot on the master control borad is close to the side of the master control borad.
Further, the master control borad and the junction are detachably connected.
Further, each drift angle of the master control borad is equipped with the first connecting hole, and the master control borad passes through each described
First connecting hole engages with the screw thread of the first screw and is detachably connected on the junction.
Further, the camera be detachably connected on two adjacent poles of the unmanned plane main body it
Between.
Further, the camera is provided with least two second connecting holes, and the camera passes through each described second
The screw thread engagement of connecting hole and the second screw is detachably connected between adjacent two poles of the unmanned plane main body.
Second aspect, the utility model embodiment provide a kind of unmanned plane with camera, nobody with camera
Machine includes:Unmanned plane main body and described Split type camera component, the unmanned plane main body include:Multiple poles and more
Individual rotor.One end of each pole is respectively mounted the rotor, the other end of each pole with pole remaining described
The other end connect to form junction, the master control borad of the Split type camera component is arranged on the junction, the split
The camera of formula CCD camera assembly is arranged between two adjacent poles.
Further, the unmanned plane main body also includes:Component installation panel, the other end of each pole with
The component installation panel connection, the master control borad of the Split type camera component are arranged on the component installation panel
On.
The beneficial effect of the utility model embodiment is:
Master control borad, the other end connection camera of connecting line, so that camera obtains figure are connected by one end of connecting line
As data can be transferred to master control borad by connecting line.Further through each branch that master control borad is arranged on to unmanned plane main body
Bar is connected the junction to be formed with pole remaining described, and camera is arranged on into two adjacent poles of unmanned plane main body
Between.And then ensure the view data acquired in camera can normal transmission while, by by camera and master control borad
The diverse location of unmanned plane main body is set respectively so that the weight that unmanned plane main body is born is held by different positions respectively
Load, and reach stress balance.It is thereby achieved that while unmanned plane volume minimizes, effectively prevent unmanned plane from flying
Shaken in journey.
Other feature and advantage of the present utility model will illustrate in subsequent specification, also, partly from specification
Become apparent, or understood by implementing the utility model embodiment.The purpose of this utility model and other advantages can
Realize and obtain by specifically noted structure in the specification, claims and accompanying drawing write.
Brief description of the drawings
, below will be to embodiment in order to illustrate more clearly of the utility model embodiment or technical scheme of the prior art
In the required accompanying drawing used be briefly described, it should be apparent that, drawings in the following description are only of the present utility model
Some embodiments, for those of ordinary skill in the art, on the premise of not paying creative work, can also be according to this
A little accompanying drawings obtain other accompanying drawings.By shown in accompanying drawing, above and other purpose of the present utility model, feature and advantage will more
Clearly.The identical reference instruction identical part in whole accompanying drawings.Do not painted by actual size equal proportion scaling deliberately
Accompanying drawing processed, it is preferred that emphasis is show purport of the present utility model.
Fig. 1 shows a kind of the first viewing angle constructions signal for unmanned plane with camera that the utility model embodiment provides
Figure;
Fig. 2 shows a kind of the second viewing angle constructions signal for unmanned plane with camera that the utility model embodiment provides
Figure;
Fig. 3 shows a kind of the first viewing angle constructions signal for Split type camera component that the utility model embodiment provides
Figure;
Fig. 4 shows a kind of the second viewing angle constructions signal for Split type camera component that the utility model embodiment provides
Figure.
Icon:Unmanned planes of the 100- with camera;110- unmanned plane main bodies;111- component installation panels;1111- first
Through hole;1112- supports;The through holes of 1113- second;112- poles;113- rotors;200- Split type camera components;210- master controls
Plate;The connecting holes of 211- first;212- slots;220- connecting lines;230- cameras;The connecting holes of 231- second.
Embodiment
It is new below in conjunction with this practicality to make the purpose, technical scheme and advantage of the utility model embodiment clearer
Accompanying drawing in type embodiment, the technical scheme in the embodiment of the utility model is clearly and completely described, it is clear that is retouched
The embodiment stated is the utility model part of the embodiment, rather than whole embodiments.Generally here described in accompanying drawing and
The component of the utility model embodiment shown can be configured to arrange and design with a variety of.
Therefore, the detailed description of the embodiment of the present utility model to providing in the accompanying drawings is not intended to limit requirement below
The scope of the utility model of protection, but it is merely representative of selected embodiment of the present utility model.Based in the utility model
Embodiment, the every other embodiment that those of ordinary skill in the art are obtained under the premise of creative work is not made, all
Belong to the scope of the utility model protection.
, it is necessary to explanation, the orientation of the instruction such as term " on ", " under ", " interior ", " outer " in description of the present utility model
Or position relationship be based on orientation shown in the drawings or position relationship, or the utility model product using when usually put
Orientation or position relationship, it is for only for ease of description the utility model and simplifies description, rather than indicates or imply signified dress
Put or element there must be specific orientation, with specific azimuth configuration and operation, therefore it is not intended that to the utility model
Limitation.
In description of the present utility model, it is also necessary to which explanation, unless otherwise clearly defined and limited, term " are set
Put ", " installation ", " connected ", " connection " should be interpreted broadly, for example, it may be fixedly connected or be detachably connected,
Or it is integrally connected;Can be mechanical connection or electrical connection;Can be joined directly together, intermediary can also be passed through
It is indirectly connected, can is the connection of two element internals.For the ordinary skill in the art, can be managed with concrete condition
Solve concrete meaning of the above-mentioned term in the utility model.
Referring to Fig. 1, the utility model embodiment provides a kind of unmanned plane 100 with camera, this is with camera
Unmanned plane 100 includes:Unmanned plane main body 110 and Split type camera component 200.Split type camera component 200 is arranged on
On unmanned plane main body 110.
Referring to Fig. 2, unmanned plane main body 110 includes:Component installation panel 111, pole 112, rotor 113.
Component installation panel 111 is used to provide installation sky for each functional control assembly of the unmanned plane 100 with camera
Between.Component installation panel 111 is platy structure, it is contemplated that component installation panel 111 needs to have regular in actual use
Space provides installing space to be embodied as each functional control assembly, and has certain aesthetic property.Preferably, component is installed
The shape of panel 111 can be:Circular plate-like shape structure, rectangular plate-like structure or polygon platy structure etc..In the present embodiment, group
Part installation panel 111 is shaped as sampling rectangular plate-like structure, but is not intended as to restriction of the present utility model, component mounting surface
The shape and size selection that plate 111 is actually implemented can be adjusted according to actual implementation demand.The material of component installation panel 111
Can be by being made up of plastic material.In the present embodiment, component installation panel 111 not only can be by being made up of plastic material, and it also may be used
Think:Metal material or wood materials.During in view of the manufacturing cost of the unmanned plane 100 with camera, weight and actual use
Structural strength, component installation panel 111 but is not intended as to limit of the present utility model preferably by being made up of plastic material
It is fixed.
Set in component installation panel 111 and Split type camera component 200 is installed, to make in component installation panel 111
After setting installation Split type camera component 200, the unmanned plane 100 with camera can ensure the balance of weight distribution, to protect
Demonstrate,prove the stabilization of its flight attitude in the air.Preferably, the one end of component installation panel 111 extends to the direction away from the other end, group
The other end of part installation panel 111 then extends to the direction away from one end, so that component installation panel 111 is in the rectangular slab of strip
Face.Also it is to mitigate the weight of component installation panel 111 to realize the mitigation of the weight of unmanned plane 100 with camera, component mounting surface
The both ends that plate 111 extends are in engraved structure.
A part of component of installation Split type camera component 200 can be set between the both ends of component installation panel 111.It is excellent
Choosing, a part of component of the settable installation Split type camera component 200 in middle part at the both ends of component installation panel 111.
Specifically, the middle part at the both ends of component installation panel 111 is provided with multiple first through hole 1111 for possessing internal thread.Wherein,
The quantity of first through hole 1111 can be four, but not limit.To cause the middle part at the both ends of component installation panel 111
Space can be made full use of, and each first through hole 1111 is respectively positioned on close to the edge of component installation panel 111, and four first logical
Hole 1111 surrounds rectangle.It should be noted that the also settable installation flight control system in the middle part at the both ends of component installation panel 111
Component, to realize that the flight of the unmanned plane 100 with camera controls.Flight control system component can be arranged on split in an overlapping manner
On a part of component of formula CCD camera assembly 200, to realize the height to the middle part space at the both ends of component installation panel 111
Effect utilizes.
The another of installation Split type camera component 200 can be set in either end in the both ends of component installation panel 111
Members.Specifically, wherein one end of component installation panel 111 is provided with support 1112, multiple second are set on support 1112
Through hole 1113.Wherein, the quantity of the second through hole 1113 can be two, respectively positioned at the both ends of support 1112.
Pole 112 can be multiple, and each pole 112 is used to be connected in component installation panel 111, with to rotor
113 form support.The quantity of pole 112 can be:Three, four or five etc..In the present embodiment, the quantity of pole 112 is
Four, but be not intended as that restriction of the present utility model, the quantity of pole 112 can be adjusted according to actual performance.
Each the shape and structure of pole 112 can be:Strip structure, arc shape structure or more arcuate structures etc..This reality
Apply in example, the shape and structure of each pole 112 is strip structure, but is not intended as limiting each pole to of the present utility model
The 112 shape and structure selections actually implemented can be adjusted according to actual implementation demand.One end of each pole 112 is respectively mounted rotation
The wing 113, the other end of each pole 112 are connected to form junction with the other end of remaining pole 112.It is understood that should
The junction of formation is component installation panel 111, and then the other end of each pole 112 connects with component installation panel 111
Connect.Connect as one shaping of the other end of each pole 112 with component installation panel 111, i.e., the material of each pole 112
Can be by being made up of plastic material.Certainly, in the present embodiment the other end of each pole 112 with component installation panel 111 1
Body formed is the present embodiment preferred embodiment, is not intended as the restriction to the present embodiment, and its actual implementation can be according to reality
Situation is adjusted, for example, using modes such as stickup, fixture connections.Also can be protected for unmanned plane 100 of the guarantee with camera
The balance of weight distribution is demonstrate,proved, to ensure the stabilization of its flight attitude in the air.Preferably, the other end of each pole 112 connects
The edge of component installation panel 111 is connected on, and is connected to the middle part at the both ends of component installation panel 111.In addition, four poles
Two poles 112 are respectively positioned on the side of component installation panel 111 in 112, and the then equal position of another two pole 112 in four poles 112
In the opposite side of component installation panel 111, realize that the weight balancing for ensureing the unmanned plane 100 with camera distributes with further.
The quantity of rotor 113 and the quantity Matching of pole 112, the i.e. quantity of rotor 113 are multiple.In the present embodiment, branch
The quantity of bar 112 is four, then the quantity of rotor 113 is also four.Each rotor 113 is used to produce lift by rotating, so that
Unmanned plane 100 with camera can fly.Each the blade quantity of rotor 113 can be:Three, four or five etc..This
In embodiment, the blade quantity of each rotor 113 is three, but is not intended as to restriction of the present utility model, each rotor 113
Blade quantity can be adjusted according to actual performance.Each rotor 113 is fixedly mounted on the another of corresponding pole 112
End, the present embodiment, not each rotor 113, which is fixedly mounted, to be defined, and it can be realized installed in the another of corresponding pole 112
One end.Each rotor 113, with certain rotational speed, realizes the nothing with camera according to the control of flight system component
Man-machine 100 flight, and the adjustment of the 100 various flight attitudes of unmanned plane with camera.
As shown in Fig. 2 Split type camera component 200 is used to gather view data, and the view data of collection is transmitted
To flight control system, so that it is passed through wireless network transmissions to ground based terminal by flight control system again.In the present embodiment, split type shooting
A part of component of head assembly 200 is real by multiple first through hole 1111 of the middle part with the both ends of component installation panel 111
Now be detachably connected, another part component of Split type camera component 200 by with the wherein one end institute of component installation panel 111
The second through hole 1113 provided with support 1112, which is also realized, to be detachably connected, and then Split type camera component 200 is arranged on
On unmanned plane main body 110.
Fig. 2 and Fig. 3 are referred to, the utility model embodiment provides a kind of Split type camera component 200, and this is split type
CCD camera assembly 200 includes:Master control borad 210, connecting line 220 and camera 230.Wherein, one end connection master control of connecting line 220
Plate 210, the other end connection camera 230 of connecting line 220.
Master control borad 210 is platy structure, and the shape of master control borad 210 can be:Rectangular plate-like structure, circular plate-like shape structure or
Polygon platy structure.It is main for ease of being detachably connected for the middle part at master control borad 210 and the both ends of component installation panel 111
Control 210 preferably rectangular platy structure of plate.It should be appreciated that the rectangular plate-like structure of master control borad 210 is not in the present embodiment
For that can be carried out to the actual implementation of restriction of the present utility model, master control borad 210 according to actual conditions to Adjusting Shape.It is in addition, main
The geomery of control plate 210 should match with the middle part at the both ends of component installation panel 111.
Master control borad 210 is provided with the first connecting hole 211, to be detachably connected on component mounting surface by the first connecting hole 211
The middle part at the both ends of plate 111.Specifically, the first connecting hole 211 that master control borad 210 is provided with is multiple, to cause the first connection
First through hole 1111 on hole 211 and component installation panel 111 matches, and the quantity of the first connecting hole 211 can be four.Also it is
Ensure being detachably connected for master control borad 210 and component installation panel 111, each first connecting hole 211 is respectively positioned on master control borad 210
Vertex.When master control borad 210 is arranged on the middle part at the both ends of component installation panel 111, the vertex of master control borad 210 it is each
First connecting hole 211 can first through hole 1111 corresponding with component installation panel 111 overlap.There is external screw thread when each
The first screw sequentially pass through the first connecting hole 211 and first through hole 1111 of coincidence, and cause external screw thread and first through hole
When internal thread engages in 1111, the pars intermedia that master control borad 210 is detachably connected on to the both ends of component installation panel 111 is just realized
Position.
Connected for ease of master control borad 210 by connecting line 220 and camera 230, master control borad 210 is provided with slot 212.Insert
Groove 212 can be common model on the market, for example, FPDRCXX-0.3H10-X-1 types.To ensure the space on master control borad 210
The various circuit components of installation that can be concentrated, set location of the slot 212 on master control borad 210 is close to the side of master control borad 210
Side.Certainly, the set location of slot 212 is the present embodiment preferred embodiment in the present embodiment, is not intended as to this implementation
The restriction of example, its actual particular location implemented can be adjusted according to actual conditions.
As a kind of embodiment, slot 212 can have movable control piece to realize one with connecting line 220 by itself
End is detachably connected.For example, movable control piece original state is fitted in the upper surface of slot 212, so that slot 212 is sealed
Close.When operating personnel pull up movable control piece, slot 212 is opened, and one end of connecting line 220 can insert slot 212.This
When, operating personnel again pull down movable control piece, so that movable control piece restPoses, insert the connecting line of slot 212
220 one end is just fixed by slot 212.It is appreciated that, it is necessary to when one end of connecting line 220 and slot 212 are separated, also such as
Above-mentioned steps, just excessively tired state is not being done herein.
By being detachably connected for slot 212 and the one end of connecting line 220, one end that slot 212 passes through connecting line 220 obtains
The view data that camera 230 gathers, and exported view data is obtained to other circuit elements on master control borad 210.Master control
Other circuit elements on plate 210 are handled the view data is further, for example, the view data is parsed.Enter
And master control borad 210 again exports the view data after further processing to flight control system.
Fig. 2 and Fig. 4 are referred to, camera 230 is used to gather light, and view data is generated according to the light collected, and
View data is exported to the other end of connecting line 220.In the present embodiment, to ensure the weight of the unmanned plane 100 with camera
Equilibrium assignmen, the support 1112 that camera 230 is provided with the wherein one end of component installation panel 111 are detachably connected.Specifically, take the photograph
Picture first 230 is provided with least two second connecting holes 231.As a kind of mode, to make the second connecting hole 231 and the second through hole 1113
Matching, the quantity of the second connecting hole 231 can be two.Two the second connecting holes 231 are located at the both ends of camera 230 respectively,
And each second connecting hole 231 is equipped with internal thread.When camera 230 is arranged on the branch of the wherein one end of component installation panel 111
When on frame 1112, each second connecting hole 231 of camera 230 being capable of the weight of second through hole 1113 corresponding with support 1112
Close.When each the second through hole 1113 and the second connecting hole 231 that coincidence is sequentially passed through with externally threaded second screw, and cause
When internal thread engages in external screw thread and the second connecting hole 231, just realize and camera 230 is detachably connected on component mounting surface
On the support 1112 that the wherein one end of plate 111 is provided with, and camera 230 is caused to be located at two adjacent branch of unmanned plane main body 110
Between bar 112.
In summary, the utility model embodiment provides a kind of Split type camera component and nobody with camera
Machine.Split type camera component is applied to the unmanned plane with camera.Unmanned plane with camera includes:Unmanned plane main body,
Unmanned plane main body is provided with multiple poles for being provided with rotor, and each pole is connected to form junction with remaining pole.Split
Formula CCD camera assembly includes:Master control borad, connecting line and camera.Master control borad is arranged on junction, and camera is arranged on unmanned plane
Between two adjacent poles of main body, one end connection master control borad of connecting line, the other end connection camera of connecting line.
Master control borad, the other end connection camera of connecting line, so that camera obtains figure are connected by one end of connecting line
As data can be transferred to master control borad by connecting line.Further through each branch that master control borad is arranged on to unmanned plane main body
Bar is connected the junction to be formed with pole remaining described, and camera is arranged on into two adjacent poles of unmanned plane main body
Between.And then ensure the view data acquired in camera can normal transmission while, by by camera and master control borad
The diverse location of unmanned plane main body is set respectively so that the weight that unmanned plane main body is born is held by different positions respectively
Load, and reach stress balance.It is thereby achieved that while unmanned plane volume minimizes, effectively prevent unmanned plane from flying
Shaken in journey.
Preferred embodiment of the present utility model is these are only, is not limited to the utility model, for this area
Technical staff for, the utility model can have various modifications and variations.It is all within the spirit and principles of the utility model,
Any modification, equivalent substitution and improvements made etc., should be included within the scope of protection of the utility model.
Claims (10)
- A kind of 1. Split type camera component, it is characterised in that applied to the unmanned plane with camera, the nothing with camera It is man-machine including:Unmanned plane main body, the unmanned plane main body are provided with multiple poles for being provided with rotor, and each pole is equal It is connected to form junction with pole remaining described, the Split type camera component includes:Master control borad, connecting line and camera, The master control borad is arranged on the junction, and the camera is arranged on two adjacent poles of the unmanned plane main body Between, one end of the connecting line connects the master control borad, and the other end of the connecting line connects the camera.
- 2. Split type camera component according to claim 1, it is characterised in that one end of the connecting line and the master Control plate is detachably connected.
- 3. Split type camera component according to claim 2, it is characterised in that the master control borad is provided with connection and inserted Groove, one end of the connecting line and the connected slot are detachably connected.
- 4. Split type camera component according to claim 3, it is characterised in that the connected slot is in the master control borad On set location close to the side of the master control borad.
- 5. Split type camera component according to claim 1, it is characterised in that the master control borad and the junction can Dismantling connection.
- 6. Split type camera component according to claim 5, it is characterised in that each drift angle of the master control borad is all provided with There is the first connecting hole, the master control borad is engaged with the screw thread of the first screw by each first connecting hole and is detachably connected on The junction.
- 7. Split type camera component according to claim 1, it is characterised in that the camera is detachably connected on institute State between two adjacent poles of unmanned plane main body.
- 8. Split type camera component according to claim 7, it is characterised in that the camera is provided with least two the Two connecting holes, the camera engaged by each second connecting hole with the screw thread of the second screw be detachably connected on it is described Between two adjacent poles of unmanned plane main body.
- 9. a kind of unmanned plane with camera, it is characterised in that the unmanned plane with camera includes:Unmanned plane main body and Split type camera component as described in claim 1-8 any one, the unmanned plane main body include:Multiple poles and more Individual rotor, one end of each pole are respectively mounted the rotor, the other end of each pole with pole remaining described The other end connect to form junction, the master control borad of the Split type camera component is arranged on the junction, the split The camera of formula CCD camera assembly is arranged between two adjacent poles.
- 10. the unmanned plane according to claim 9 with camera, it is characterised in that the unmanned plane main body also includes: Component installation panel, the other end of each pole are connected with the component installation panel, the Split type camera group The master control borad of part is arranged in the component installation panel.
Priority Applications (1)
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CN201720710444.3U CN206984415U (en) | 2017-06-19 | 2017-06-19 | Split type camera component and the unmanned plane with camera |
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CN201720710444.3U CN206984415U (en) | 2017-06-19 | 2017-06-19 | Split type camera component and the unmanned plane with camera |
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Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN110636200A (en) * | 2019-10-22 | 2019-12-31 | 成都市喜爱科技有限公司 | Camera and amusement apparatus |
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2017
- 2017-06-19 CN CN201720710444.3U patent/CN206984415U/en active Active
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
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CN110636200A (en) * | 2019-10-22 | 2019-12-31 | 成都市喜爱科技有限公司 | Camera and amusement apparatus |
CN110636200B (en) * | 2019-10-22 | 2020-12-15 | 成都市喜爱科技有限公司 | Camera and amusement apparatus |
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