CN204180162U - Image capture module - Google Patents
Image capture module Download PDFInfo
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- CN204180162U CN204180162U CN201420589202.XU CN201420589202U CN204180162U CN 204180162 U CN204180162 U CN 204180162U CN 201420589202 U CN201420589202 U CN 201420589202U CN 204180162 U CN204180162 U CN 204180162U
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- fixture
- master control
- control borad
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- fuselage
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Abstract
The utility model provides a kind of image capture module, comprise camera lens and fuselage, described fuselage is provided with circuit board assemblies, described circuit board assemblies comprises the master control borad of electric connection, image sensing plate and image processing plate, described image sensing plate has image sensor surface, described image sensing facing to described camera lens, and is basically perpendicular to the optical axis of described camera lens; Described master control borad is arranged on the side of described image sensing backboard from described camera lens, and has spacing with described image sensing plate; Described image processing plate is arranged on the side of described fuselage.By the circuit board in fuselage is disassembled into each parallel circuit plate, make fuselage spaces compact by such distribution, be beneficial to other element, the arrangement of such as radiator etc.
Description
Technical field
The utility model relates to a kind of image capture module.
Background technology
Image capture module is widely used in the various task of shooting, such as, be equipped on unmanned plane (Unmanned Aerial Vehicle, UAV) and aloft take.Image capture module is containing camera lens and fuselage, wherein contain the internal plate modules such as main control module, image sensor module and image processing module in fuselage, these modules are often all integrated on same pcb board at present, cause other parts, the arrangement of such as radiator is restricted, and fuselage interior space is not compact.
Utility model content
The technical problem that the utility model embodiment mainly solves is to provide a kind of image capture module, its fuselage interior spaces compact.
The utility model embodiment provides a kind of image capture module, comprise camera lens and fuselage, described fuselage is provided with circuit board assemblies, described circuit board assemblies comprises the master control borad of electric connection, image sensing plate and image processing plate, described image sensing plate has image sensor surface, described image sensing facing to described camera lens, and is basically perpendicular to the optical axis of described camera lens; Described master control borad is arranged on the side of described image sensing backboard from described camera lens, and has spacing with described image sensing plate; Described image processing plate is arranged on the side of described fuselage.
Described master control borad and image sensing plate substantially parallel, and therebetween by first flexible PCB realize be electrically connected.
Described first flexible PCB is bending shape, lower surface inside it is provided with one in the first public connector of built-in circuit and the first female connectors, lower surface outside it is provided with one in the second public connector of built-in circuit and the second female connectors, described master control borad be provided with in described first public connector and the first female connectors another, described image sensing plate be provided with in described second public connector and the second female connectors another, described master control borad realizes being connected with the grafting of the first female connectors by the first public connector with described first flexible PCB, described image sensing plate realizes being connected with the grafting of the second female connectors by the second public connector with described first flexible PCB.
Described image processing plate is basically parallel to the optical axis of described camera lens, and realizes being electrically connected by the second flexible PCB between described image processing plate and master control borad.
Described second flexible PCB extends the first connecting portion from its one end, and extends the second connecting portion from one side, and described first connecting portion is connected to described master control borad, and described second connecting portion is connected to described image sensing plate.
Described image processing plate is image Compression plate.
Described fuselage has supporting component, described supporting component comprises the first fixture and the second fixture that are oppositely arranged, described image sensing plate is fixed on the end face of described first fixture and the second fixture, described master control borad and the substantially parallel setting of described image sensing plate, described image processing plate is fixed to the side of described first fixture.
Described image sensing plate and be provided with the sealing gasket of hollow ring between described first fixture and the second fixture.
Multiple first joint pin is smoothly extended in the inner side of described first fixture and the second fixture, each described first joint pin adjacent position is provided with the second joint pin, described second joint pin along the height of the optical axis direction of described camera lens higher than the height of described first joint pin along the optical axis direction of described camera lens, described image sensing plate wears described sealing gasket by screw and is fixed on described multiple first joint pin, and described master control borad is fixed on described multiple second joint pin by stud.
Described image processing plate is fixed to the side of described first fixture by interior plate and outer panel, and described outer panel has receiving space, and described image processing plate is contained in this receiving space, and described interior plate covers described receiving space.
Described fuselage is also provided with radiating subassembly, and described radiating subassembly comprises fan and radiator, and described fan is fixed to the side of described second fixture, and described radiator is arranged on described master control borad.
Described fan comprises housing and rotating part, and described housing has the inner space of hollow and is positioned at the air outlet of side, and described rotating part is fitted in described housing; Described radiator comprises base and is arranged on the multiple fins on described base, described base has an end face and connects described air outlet, between two adjacent described fins, there is air channel, the arrival end in described air channel connects the end face of described base, and is filled with heat-conducting pad between described base and described master control borad.
Described fin is provided with air duct cover board, and auricle is extended in an end of described air duct cover board, and fastening piece is extended downwards in two sides, and described auricle covers the air outlet of described fan, and described two fastening pieces form spatial accommodation and accommodate described fin.
Each described fin has at the arrival end in described air channel the first inclined plane that relatively described base tilts, and described auricle has the second inclined plane that relatively described air duct cover board tilts towards the surface of described fin, and described first inclined plane coordinates with the second inclined plane.
Described fuselage is provided with rear end cap, and described rear end cap is arranged on described air duct cover board, and described rear end cap offers ventilating opening.
On the other hand, the utility model also provides a kind of image capture module, comprise fuselage, described fuselage has light inlet, described fuselage is provided with circuit board assemblies, described circuit board assemblies comprises the master control borad of electric connection, image sensing plate and image processing plate, described image sensing plate has towards the image sensor surface of the light inlet of described fuselage, described master control borad is arranged on the rear of described image sensing plate, and have spacing with described image sensing plate, and it is substantially parallel with described image sensing plate, described image processing plate is arranged on the side of described fuselage, and be basically perpendicular to described image sensing plate and described master control borad.
The utility model embodiment is by disassembling into each parallel circuit plate by the circuit board in fuselage, master control borad and image sensing plate are arranged on camera lens rear, and image processing plate is arranged on the side of fuselage, make fuselage spaces compact by such distribution, be beneficial to other element, the arrangement of such as radiator etc.
Accompanying drawing explanation
Fig. 1 is the schematic perspective view of a kind of image capture module that the utility model embodiment provides;
Fig. 2 is the decomposing schematic representation of the image capture module of Fig. 1;
Fig. 3 is the enlarged diagram of the element such as radiator, master control borad, image sensing plate of Fig. 2;
Fig. 4 is the arrangement schematic diagram after the circuit board assemblies of Fig. 2 is connected by flexible PCB;
Fig. 5 is the partial assembled schematic diagram of Fig. 2, and different from the visual angle angle of Fig. 2;
Fig. 6 is also the partial assembled schematic diagram of Fig. 2, but different from the visual angle angle of Fig. 5.
Main element symbol description
| Image capture module | 100 |
| Camera lens | 10 |
| Fuselage | 20 |
| First fixture | 211 |
| Second fixture | 212 |
| 3rd fixture | 213 |
| 4th fixture | 214 |
| Master control borad | 221 |
| Image sensor plate | 222 |
| Image sensor surface | 222f |
| Image processing plate | 223 |
| First public connector | 221a |
| Second public connector | 222a |
| First flexible PCB | 25 |
| First female connectors | 251 |
| Second female connectors | 252 |
| First joint pin | 256 |
| Second joint pin | 258 |
| Pilot hole | 256a，255a，258a |
| Sealing gasket | 26 |
| Copper stud | 255 |
| Interior plate | 225 |
| Outer panel | 226 |
| Receiving space | 227 |
| Second flexible PCB | 27 |
| First connecting portion | 272 |
| Second connecting portion | 274 |
| Brass screw | 228, 229，224，238 |
| Fan | 231 |
| Radiator | 232 |
| Housing | 231a |
| Rotating part | 231b |
| Air outlet | 231c |
| Side cover | 233 |
| Base | 232a |
| End face | 232c |
| Fin | 232b |
| Air channel | 232e |
| First inclined plane | 232d |
| Side Extendible flake | 232f |
| Air duct cover board | 235 |
| Auricle | 235a |
| Fastening piece | 235b |
| Second inclined plane | 235c |
| Rear end cap | 234 |
| Ventilating opening | 234a |
Following embodiment will further illustrate the utility model in conjunction with above-mentioned accompanying drawing.
Embodiment
Below in conjunction with the accompanying drawing in the utility model embodiment, be clearly and completely described the technical scheme in the utility model embodiment, obviously, described embodiment is only the utility model part embodiment, instead of whole embodiments.Based on the embodiment in the utility model, those of ordinary skill in the art are not making the every other embodiment obtained under creative work prerequisite, all belong to the scope of the utility model protection.
The image capture module that the utility model embodiment provides is specially adapted to large-scale capture apparatus, certainly also not getting rid of is applied in middle-size and small-size capture apparatus, its fuselage interior component arrangement is compact, especially circuit board and radiating subassembly distribution rationally, radiating subassembly good heat dissipation effect.
Concrete, refer to Fig. 1 and Fig. 2, the image capture module 100 that the utility model embodiment provides comprises camera lens 10 and fuselage 20.This fuselage 20 is provided with support body assembly, circuit board assemblies and radiating subassembly.
This support body assembly comprises integrated first fixture 211, second fixture 212, the 3rd fixture 213 and the 4th fixture 214 with fuselage 20, this the first fixture 211 and this second fixture 212 are oppositely arranged, and the 3rd fixture 213 and the 4th fixture 214 are oppositely arranged.The height along camera lens 10 optical axis direction of this first fixture 211 is identical along the height of camera lens 10 optical axis direction with this second fixture 212, the height along camera lens 10 optical axis direction of the 3rd fixture 213 is identical along the height of camera lens 10 optical axis direction with the 4th fixture 214, this first fixture 211 and the second fixture 212 along camera lens 10 optical axis direction height lower than the 3rd fixture 213 and the 4th fixture 214(as shown in Figure 2) along the height of camera lens 10 optical axis direction, for arranging circuit board assemblies and radiating subassembly.3rd fixture 213 and the 4th fixture 214 are for arranging the effects such as the button of dismounting camera lens.This first fixture 211, second fixture 212, the 3rd fixture 213 and the 4th fixture 214 surround a hollow space jointly, can be used for camera lens 10 to move forward and backward and stretch.
Please also refer to Fig. 3 and Fig. 4, this circuit board assemblies comprises master control borad 221, image sensor plate 222 and image processing plate 223.This master control borad 221 and the substantially parallel setting of image sensor plate 222, and the first type surface at its length and width place is basically perpendicular to the optical axis direction of camera lens 10, and this master control borad 221 is positioned at the top of this image sensor plate 222, and has spacing therebetween.The length of this image processing plate 223 and the first type surface at width place are basically parallel to the optical axis direction of camera lens 10.
Particularly, multiple first joint pin 256 is smoothly extended in the inner side of this first fixture 211 and the second fixture 212, and each first joint pin 256 all offers a pilot hole 256a, and this first joint pin 256 is placed with the sealing gasket 26 of annular hollow.This image sensor plate 222 is worn by brass screw 224 multiple on limit, the plurality of brass screw 224 further passs through sealing pad 26 and is fitted in this pilot hole 256a, image sensor plate 222 is arranged on this first fixture 211 and the second fixture 212, and makes its image sensor surface 222f towards camera lens 10.Sealing pad 26 plays and prevents light from exposing outside effect.In the present embodiment, sealing pad 26 is made up of rubber.
The inner side adjacent between two of this first fixture 211, second fixture 212, the 3rd fixture 213 and the 4th fixture 214 is provided with multiple second joint pin 258, the height along camera lens optical axis direction of the plurality of second joint pin 258 all higher than the height along camera lens optical axis direction of the first joint pin 256, but lower than the 3rd fixture 213 and the 4th fixture 214 height along camera lens optical axis direction.This second joint pin 258 each all offers a pilot hole 258a, and this master control borad 221 is worn by copper stud 255 multiple on limit, and the plurality of copper stud 255 is fitted in this pilot hole 258a, and this master control borad 221 is fixed on the plurality of second joint pin 258.This master control borad 221 and this image sensor plate 222 have spacing that circuit can be avoided to be connected in series and short circuit.
This master control borad 221 and image sensor plate 222 are electrically connected by the first flexible PCB 25.Particularly, this master control borad 221 is provided with the first public connector 221a of built-in circuit, and this image sensor plate 222 is provided with the second public connector 222a of built-in circuit.This first flexible PCB 25 vertically bending is "] " shape, the lower surface inside it is provided with the first female connectors 251 of built-in circuit, and the lower surface in outside is provided with the second female connectors 252 of built-in circuit.This first public connector 221a inserts this first female connectors 251, and this second public connector 222a inserts this second female connectors 252, is electrically connected with this master control borad 221 to make this image sensor plate 222.
Be understandable that, other modes also can be adopted between this image sensor plate 222 and this master control borad 221 to be electrically connected, as by connector connection etc., be not limited to present embodiment.
This image processing plate 223 is fixed on the outside of the first fixture 211 by the cooperation of an interior plate 225 and an outer panel 226.This outer panel 226 has the receiving space 227 of a hollow, and this image processing plate 223 is fixed in this receiving space 227 by brass screw 229, and this interior plate 225 is as a cover plate.This image processing plate 223 is electrically connected with master control borad 221 by the second flexible PCB 27, and this second flexible PCB 27 has the first connecting portion 272 extended from one end and the second connecting portion 274 extended from another side.This first connecting portion 272 connects this master control borad 221, and this second connecting portion 274 connects this image processing plate 223, to make to be electrically connected between described master control borad 221, image sensor plate 222, image processing plate 223 three.This image processing plate 223 is an inverted L-shaped with the arrangement of this master control borad 221 and image sensor plate 222, this image processing plate 223 is vertical portions of this inverted L-shaped, and this master control borad 221 and image sensor plate 222 are horizontal components (as shown in Figure 4) of this inverted L-shaped.This image processing plate 223, interior plate 225 and outer panel 226 are connected in series by brass screw 228, and are fixed to the lateral surface of above-mentioned first fixture 211 by brass screw 229.In the present embodiment, this image processing plate 223 is image Compression plate.
Be understandable that, in other embodiments, the second flexible PCB 27 can be electrically connected with image sensor plate 222, to make to be electrically connected between described master control borad 221, image sensor plate 222, image processing plate 223 three.First connecting portion 272 of this second flexible PCB 27 can connect this image sensor plate 222, and this second connecting portion 274 can connect this image processing plate 223, or is not limited to present embodiment.
This radiating subassembly comprises fan 231 and radiator 232.This fan 231 comprises housing 231a and rotating part 231b.This housing 231a inner hollow, side has air outlet 231c, and the air-out direction of this air outlet 231c is approximately perpendicular to this rotating part 231b.This rotating part 231b is fit in the inner space of this housing 231a from the surface of this housing 231a, and it rotates the air flowing caused and discharges from this air outlet 231c.This fan 231 is fixed to the outside of the second fixture 212 by a side cover 233, and air outlet 231c upward (as shown in Figure 5).This radiator 232 is fixed on the copper stud 255 on this master control borad 221 by multiple brass screw 238, and this copper stud 255 offers pilot hole 255a, and this brass screw 238 is fitted in pilot hole 255a through the side Extendible flake 232f of this radiator 232.This radiator 232 has gap with master control borad 221, is filled with heat-conducting pad, contacts this master control borad 221, thus gone out by the heat conduction of master control borad 221 by this heat-conducting pad in gap.This radiator 232 has base 232a and the multiple fin 232bs that extend one-body molded with base 232a, and above-mentioned side Extendible flake 232f extends to both sides from this base 232a.This base 232a has a level and smooth end face 232c and is located on the edge of this air outlet 231c, and the air-out direction of this air outlet 231c is roughly parallel to this end face 232c.The plurality of fin 232b be arranged in parallel, and its length direction is parallel to the first type surface of this master control borad 221.Between adjacent two fin 232b, there is air channel 232e, and the arrival end of air channel 232e connects the end face 232c of this base 232a.Each fin 232b forms at the arrival end of air channel 232e the first rake 232d tilted relative to base 232a.
Please also refer to Fig. 5 and Fig. 6, be provided with an air duct cover board 235 above the fin 232b of this radiator 232, a sloped-end of this air duct cover board 235 extends auricle 235a, and buckling plate 235b is extended respectively straight down in the both sides adjacent with this end.The bottom surface of this auricle 235a forms the second inclined plane 235c, to coordinate with the first inclined plane 232d of fin 232b, this auricle 235a covers the air outlet 231c of this fan 231, being combined with of this first inclined plane 232d and the second inclined plane 235c helps to make to blow out from air outlet 231c, blowing direction perpendicular to this base 232a is changed into and is roughly parallel to base 232a direction, more effectively enter this to make radiation air and enter air channel 232e, it can not be each heat dissipation for circuit board that the wind part simultaneously air outlet 231c can being avoided to blow out is overflowed in radiator 232, add heat radiation power.These two buckling plate 235b form spatial accommodation and accommodate this fin 232b, and can be fixed on the side Extendible flake 232f of base 232a.
The top of this air duct cover board 235 is provided with rear end cap 234, and this rear end cap 234 covers the rearward end of whole fuselage 20, and form heat-dissipating space in this fuselage 20, this rear end cap 234 has ventilating opening 234a, is convenient to heat and sheds.
Above-mentioned outer panel 226 can connect outside further, such as The Cloud Terrace.
To sum up, the circuit board disassembling of the image capture module 100 that the utility model embodiment provides is three pieces, upper and lower spaced master control borad 221 and image sensor plate 222 respectively, and be arranged on the image processing plate 223 of fuselage one side, and fan 231 and radiator 232 decomposition are come, fan 231 is arranged at another side of fuselage, and radiator 232 is arranged at above master control borad 221, heat-dissipating space is formed in fuselage 20, rear end cap 234 has ventilating opening 234a and extraneous exchange of air, fuselage 20 component arrangement like this is compact, radiating subassembly good heat dissipation effect.
The foregoing is only embodiment of the present utility model; not thereby the scope of the claims of the present utility model is limited; every utilize the utility model specification and accompanying drawing content to do equivalent structure or equivalent flow process conversion; or be directly or indirectly used in other relevant technical fields, be all in like manner included in scope of patent protection of the present utility model.
Claims (23)
1. an image capture module, comprise camera lens and fuselage, it is characterized in that: described fuselage is provided with circuit board assemblies, described circuit board assemblies comprises the master control borad of electric connection, image sensing plate and image processing plate, described image sensing plate has image sensor surface, described image sensing facing to described camera lens, and is basically perpendicular to the optical axis of described camera lens; Described master control borad is arranged on the side of described image sensing backboard from described camera lens, and has spacing with described image sensing plate; Described image processing plate is arranged on the side of described fuselage.
2. image capture module as claimed in claim 1, is characterized in that, described master control borad and image sensing plate substantially parallel, and realize being electrically connected by the first flexible PCB therebetween.
3. image capture module as claimed in claim 2, it is characterized in that, described first flexible PCB is bending shape, lower surface inside it is provided with one in the first public connector of built-in circuit and the first female connectors, lower surface outside it is provided with one in the second public connector of built-in circuit and the second female connectors, described master control borad be provided with in described first public connector and the first female connectors another, described image sensing plate be provided with in described second public connector and the second female connectors another, described master control borad realizes being connected with the grafting of the first female connectors by the first public connector with described first flexible PCB, described image sensing plate realizes being connected with the grafting of the second female connectors by the second public connector with described first flexible PCB.
4. image capture module as claimed in claim 1, it is characterized in that, described image processing plate is basically parallel to the optical axis of described camera lens, and realizes being electrically connected by the second flexible PCB between described image processing plate and master control borad.
5. image capture module as claimed in claim 4, it is characterized in that, described second flexible PCB extends the first connecting portion from its one end, and extend the second connecting portion from one side, described first connecting portion is connected to described master control borad, and described second connecting portion is connected to described image sensing plate.
6. image capture module as claimed in claim 1, it is characterized in that, described image processing plate is image Compression plate.
7. image capture module as claimed in claim 1, it is characterized in that, described fuselage has supporting component, described supporting component comprises the first fixture and the second fixture that are oppositely arranged, described image sensing plate is fixed on the end face of described first fixture and the second fixture, described master control borad and the substantially parallel setting of described image sensing plate, described image processing plate is fixed to the side of described first fixture.
8. image capture module as claimed in claim 7, is characterized in that, is provided with the sealing gasket of hollow ring between described image sensing plate and described first fixture, the second fixture.
9. image capture module as claimed in claim 8, it is characterized in that, multiple first joint pin is smoothly extended in the inner side of described first fixture and the second fixture, each described first joint pin adjacent position is provided with the second joint pin, described second joint pin along the height of the optical axis direction of described camera lens higher than the height of described first joint pin along the optical axis direction of described camera lens, described image sensing plate wears described sealing gasket by screw and is fixed on described multiple first joint pin, and described master control borad is fixed on described multiple second joint pin by stud.
10. image capture module as claimed in claim 7, it is characterized in that, described image processing plate is fixed to the side of described first fixture by interior plate and outer panel, described outer panel has receiving space, described image processing plate is contained in this receiving space, and described interior plate covers this receiving space.
11. image capture modules as claimed in claim 7, it is characterized in that, described fuselage is also provided with radiating subassembly, and described radiating subassembly comprises fan and radiator, described fan is fixed to the side of described second fixture, and described radiator is arranged on described master control borad.
12. image capture modules as claimed in claim 11, it is characterized in that, described fan comprises housing and rotating part, and described housing has the inner space of hollow and is positioned at the air outlet of side, and described rotating part is fitted in described housing; Described radiator comprises base and is arranged on the multiple fins on described base, described base has an end face and connects described air outlet, between two adjacent described fins, there is air channel, the arrival end in described air channel connects the end face of described base, and is filled with heat-conducting pad between described base and described master control borad.
13. image capture modules as claimed in claim 12, it is characterized in that, described fin is provided with air duct cover board, auricle is extended in one end of described air duct cover board, fastening piece is extended downwards in two sides, described auricle covers the air outlet of described fan, and described two fastening pieces form spatial accommodation and accommodate described fin.
14. image capture modules as claimed in claim 13, it is characterized in that, each described fin has the first inclined plane of relatively described base inclination at the arrival end in described air channel, described auricle has the second inclined plane that relatively described air duct cover board tilts towards the surface of described fin, and described first inclined plane coordinates with the second inclined plane.
15. image capture modules as claimed in claim 13, it is characterized in that, described fuselage is provided with rear end cap, and described rear end cap is arranged on described air duct cover board, and described rear end cap offers ventilating opening.
16. 1 kinds of image capture modules, comprise fuselage, described fuselage has light inlet, it is characterized in that: described fuselage is provided with circuit board assemblies, described circuit board assemblies comprises the master control borad of electric connection, image sensing plate and image processing plate, described image sensing plate has towards the image sensor surface of the light inlet of described fuselage, described master control borad is arranged on the rear of described image sensing plate, and it is substantially parallel with described image sensing plate, and have spacing with described image sensing plate, described image processing plate is arranged on the side of described fuselage, and be basically perpendicular to described image sensing plate and described master control borad.
17. image capture modules as claimed in claim 16, it is characterized in that, realize being electrically connected by the first flexible PCB between described master control borad and image sensing plate, and realize being electrically connected by the second flexible PCB between described image processing plate and master control borad.
18. image capture modules as claimed in claim 16, it is characterized in that, described fuselage has supporting component, described supporting component comprises the first fixture and the second fixture that are oppositely arranged, described image sensing plate is fixed on the end face of described first fixture and the second fixture, and described image processing plate is fixed to the side of described first fixture.
19. image capture modules as claimed in claim 18, it is characterized in that, described fuselage is also provided with radiating subassembly, and described radiating subassembly comprises fan and radiator, described fan is fixed to the side of described second fixture, and described radiator is arranged on described master control borad.
20. image capture modules as claimed in claim 19, it is characterized in that, described fan comprises housing and rotating part, and described housing has the inner space of hollow and is positioned at the air outlet of side, and described rotating part is fitted in described housing; Described radiator comprises base and is arranged on the multiple fins on described base, described base has an end face and connects described air outlet, between two adjacent described fins, there is air channel, the arrival end in described air channel connects the end face of described base, and by heat-conducting glue thermal contact conductance between described base and described master control borad.
21. image capture modules as claimed in claim 20, it is characterized in that, described fin is provided with air duct cover board, auricle is extended in one end of described air duct cover board, fastening piece is extended downwards in two sides, described auricle covers the air outlet of described fan, and described two fastening pieces form spatial accommodation and accommodate described fin.
22. image capture modules as claimed in claim 21, it is characterized in that, each described fin has the first inclined plane of relatively described base inclination at the arrival end in described air channel, described auricle has the second inclined plane that relatively described air duct cover board tilts towards the surface of described fin, and described first inclined plane coordinates with the second inclined plane.
23. image capture modules as claimed in claim 21, it is characterized in that, described fuselage is provided with rear end cap, and described rear end cap is arranged on described air duct cover board, and described rear end cap offers ventilating opening.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201420589202.XU CN204180162U (en) | 2014-10-13 | 2014-10-13 | Image capture module |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201420589202.XU CN204180162U (en) | 2014-10-13 | 2014-10-13 | Image capture module |
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| CN204180162U true CN204180162U (en) | 2015-02-25 |
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| CN201420589202.XU Expired - Fee Related CN204180162U (en) | 2014-10-13 | 2014-10-13 | Image capture module |
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Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
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| CN105519090A (en) * | 2014-10-13 | 2016-04-20 | 深圳市大疆创新科技有限公司 | Image capturing module |
| CN106483736A (en) * | 2015-08-25 | 2017-03-08 | 奥林巴斯株式会社 | Filming apparatus |
| CN106851069A (en) * | 2017-03-10 | 2017-06-13 | 深圳电航空技术有限公司 | Device for image and head |
| TWI596465B (en) * | 2015-06-11 | 2017-08-21 | 鴻富錦精密工業（武漢）有限公司 | Heat dissipation device and heat dissipation assembly |
-
2014
- 2014-10-13 CN CN201420589202.XU patent/CN204180162U/en not_active Expired - Fee Related
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105519090A (en) * | 2014-10-13 | 2016-04-20 | 深圳市大疆创新科技有限公司 | Image capturing module |
| US10250786B2 (en) | 2014-10-13 | 2019-04-02 | SZ DJI Technology Co., Ltd. | Image capturing module which has an image processing board disposed at a side edge of the body of the image capturing module |
| TWI596465B (en) * | 2015-06-11 | 2017-08-21 | 鴻富錦精密工業（武漢）有限公司 | Heat dissipation device and heat dissipation assembly |
| CN106483736A (en) * | 2015-08-25 | 2017-03-08 | 奥林巴斯株式会社 | Filming apparatus |
| CN106851069A (en) * | 2017-03-10 | 2017-06-13 | 深圳电航空技术有限公司 | Device for image and head |
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