CN115134503B - High-efficient radiating motion image sensor - Google Patents
High-efficient radiating motion image sensor Download PDFInfo
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- CN115134503B CN115134503B CN202211058092.XA CN202211058092A CN115134503B CN 115134503 B CN115134503 B CN 115134503B CN 202211058092 A CN202211058092 A CN 202211058092A CN 115134503 B CN115134503 B CN 115134503B
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Abstract
The invention relates to the field of image sensors, in particular to a moving image sensor with efficient heat dissipation. The fuel-oil-type model airplane aims to solve the technical problem that the normal work of a motion image sensor is influenced because the motion image sensor embedded in the fuel-oil-type model airplane can reduce resistance brought to the fuel-oil-type model airplane but cannot radiate heat in time. The invention provides a moving image sensor capable of efficiently dissipating heat, which comprises a side plate, a first heat-conducting fin and the like; the side plate is internally provided with a first heat-conducting fin. The moving image sensor with high-efficiency heat dissipation is provided with multiple heat dissipation modes, and besides the basic heat dissipation work that the second heat conducting fin quickly dissipates heat around the lens module, the displacement assembly pushes the tail block, controls the opening and closing of the bottom plate and the side plate, and respectively performs primary air-cooled heat dissipation work, tertiary air-cooled heat dissipation work and secondary air-cooled heat dissipation work, so that different high-efficiency heat dissipation modes are provided for different scenes.
Description
Technical Field
The invention relates to the field of image sensors, in particular to a moving image sensor with efficient heat dissipation.
Background
The motion image sensor has the advantage of clearly recording a picture under severe motion conditions, and therefore, the motion image sensor is widely applied to motion image pickup equipment and aerial photography equipment.
For example, in CN204422948U, the heat dissipation device for aerial photography equipment conducts the temperature inside the sensor outwards through the heat-conducting fins, and conducts the heat generated by the sensor and the surroundings in time, but the heat conduction efficiency of the heat dissipation mode is greatly affected by the heat-conducting property of the heat-conducting fins, and the heat dissipation amount is limited.
Disclosure of Invention
The invention provides a moving image sensor capable of efficiently radiating heat, and aims to overcome the defect that the moving image sensor embedded in a fuel oil type model airplane can reduce resistance brought to the fuel oil type model airplane, but normal work of the moving image sensor is influenced due to the fact that heat cannot be radiated in time.
The technical scheme of the invention is as follows: a motion image sensor with high-efficiency heat dissipation comprises a shell, a fixing frame, an installation barrel, a lens module, a side plate, a first heat-conducting fin, a second heat-conducting fin and a bottom plate; the bottom of the shell is connected with an ejection assembly; the lower side of the ejection component is connected with a bottom plate; the inner side of the shell is fixedly connected with a fixing frame; the inner side of the fixed frame is fixedly connected with an installation cylinder; the inner side of the mounting cylinder is provided with a lens module; the left side and the right side of the mounting cylinder are respectively provided with a plurality of radiating groove structures; the left side of the shell is connected with a side plate in a sliding way through an upper sliding rail and a lower sliding rail; the right side of the shell is also connected with a side plate in a sliding way through an upper sliding rail and a lower sliding rail; the two side plates are tightly attached to the fixing frame; an elastic fixing component is connected between each of the two side plates and the mounting cylinder; two heat conducting grooves are respectively formed in the inner sides of the two side plates; a first heat conducting fin is fixedly connected in each of the four heat conducting grooves; the front part of the lower side and the rear part of the lower side of the shell are respectively fixedly connected with a second heat-conducting fin; the first heat conducting sheet conducts heat around the installation cylinder to the second heat conducting sheet to carry out basic heat dissipation work; the displacement subassembly of casing rear side promotes the tail piece of installation cylinder rear side, it removes to drive the installation cylinder before, the first wedge groove of installation cylinder downside promotes ejecting subassembly, it leaves the casing to drive the bottom plate, carry out one-level forced air cooling heat dissipation work, the displacement subassembly continues to promote the installation cylinder, two ejector pads on the installation cylinder promote two curb plates respectively and open, two elastic fixation subassemblies are compressed, the bottom plate keeps leaving the casing, carry out tertiary forced air cooling heat dissipation work, the displacement subassembly promotes the installation cylinder once more, the first wedge groove of installation cylinder leaves ejecting subassembly, ejecting subassembly gets into in the second wedge groove of installation cylinder downside, the second wedge groove is located the rear side of first wedge groove, the bottom plate resets, the curb plate keeps opening, carry out second grade forced air cooling heat dissipation work.
More preferably, a plurality of heat dissipation fins are respectively fixedly connected to the lower sides of the two second heat conduction sheets.
More preferably, the bottom plate is provided with a plurality of slot structures for inserting the heat dissipation fins.
More preferably, the elastic fixing component comprises a fixing shaft and a first spring; a fixed shaft is fixedly connected to the middle part of the mounting cylinder; a first spring is fixedly connected between the two side plates and the fixed shaft respectively, and the first spring is sleeved on the outer surface of the fixed shaft.
More preferably, the ejection assembly comprises a limiting rod, a third spring and a wedge-shaped block; four corners of the lower side of the shell are respectively connected with a limiting rod in a sliding manner; the lower ends of the four limiting rods are fixedly connected with a bottom plate; a third spring is fixedly connected between each of the four limiting rods and the shell, and the third springs are respectively sleeved on the outer surfaces of the adjacent limiting rods; the middle part of the bottom plate is fixedly connected with a wedge-shaped block which is matched with the first wedge-shaped groove structure.
More preferably, the displacement assembly comprises a screw rod and a driving motor; a driving motor is fixedly connected to the rear side of the shell; a screw rod is fixedly connected with an output shaft of the driving motor; the front end of the screw rod is connected with the tail block in a screwing way.
More preferably, the upper side of each heat conduction groove is respectively and rotatably connected with a baffle plate through a rotating shaft; a second spring is fixedly connected between each baffle sheet and the first heat-conducting sheet; each baffle is pressed outwards by the mounting cylinder to be in an inclined state, and the second spring is in a compressed state.
More preferably, each of the heat dissipating grooves is provided in a structure inclined rearward from the inside to the outside of the mounting tube.
More preferably, the front sides of the two side plates are each provided with a structure which inclines forwards from the side close to the fixed frame to the side far from the fixed frame.
More preferably, the rear sides of the two side plates are respectively provided with a cambered surface structure.
Has the beneficial effects that: the high-efficiency heat-dissipation motion image sensor is provided with a plurality of heat dissipation modes, when the flight equipment is in a normal flight state, the first heat conduction sheet conducts heat around the installation cylinder to the second heat conduction sheet, the second heat conduction sheet quickly dissipates heat around the lens module to perform basic heat dissipation work, when a temperature sensor arranged in the flight equipment detects that the temperature of a machine body is higher, a displacement component arranged at the rear side of a shell pushes a tail block arranged at the rear side of the installation cylinder to drive the installation cylinder to move forwards, a first wedge-shaped groove arranged at the lower side of the installation cylinder pushes an ejection component to drive a bottom plate to leave the shell, a heat dissipation fin of the second heat conduction is completely exposed in the air at the moment, primary air cooling heat dissipation work is performed on the second heat conduction sheet through the heat dissipation fin to accelerate the heat dissipation efficiency of the second heat conduction sheet, when the temperature sensor arranged in the flight equipment detects that the temperature of the machine body is sharply increased, the displacement subassembly continues to promote the installation section of thick bamboo, two ejector pads of installation section of thick bamboo rear side promote two curb plates respectively and open to both sides, two elastic fixation subassemblies are compressed by two open curb plates, the bottom plate keeps leaving the casing this moment, and the curb plate is after keeping away from the installation section of thick bamboo, the radiating groove of installation section of thick bamboo exposes in the air completely, directly carry out tertiary air-cooled heat dissipation work to the camera lens module, if need reduce the resistance that brings the fuel-fired model aeroplane and model ship on the basis of tertiary air-cooled heat dissipation work, the displacement subassembly promotes the installation section of thick bamboo once more, the first wedge groove of installation section of thick bamboo leaves ejecting subassembly, ejecting subassembly gets into in the second wedge groove of installation section of thick bamboo downside, let the bottom plate reset, and the curb plate keeps opening, carry out second grade air-cooled heat dissipation work, realize providing different high-effect radiating mode to different scenes.
Drawings
Fig. 1 is a schematic perspective view of a first embodiment of the present disclosure;
FIG. 2 is a schematic perspective view of a second embodiment of the present application;
FIG. 3 is an exploded view of the present application;
FIG. 4 is a perspective view of the elastic fixing component of the present application;
FIG. 5 is a schematic perspective view of a first thermally conductive sheet and a second thermally conductive sheet according to the present application;
fig. 6 is a schematic perspective view of a first thermally conductive sheet and a baffle plate according to the present application;
FIG. 7 is a schematic perspective view of a push block and a cambered surface structure according to the present application;
FIG. 8 is a perspective view of the mounting barrel of the present application;
FIG. 9 is a perspective view of the displacement assembly of the present application;
fig. 10 is a perspective view of the ejection assembly of the present application;
FIG. 11 is a schematic diagram of the primary air-cooled heat dissipation of the present application;
fig. 12 is a schematic diagram of the three-stage air-cooling heat dissipation operation of the present application.
In the reference symbols: 1-shell, 11-slide rail, 2-fixing frame, 3-installation barrel, 31-heat dissipation groove, 32-pushing block, 33-tail block, 341-first wedge-shaped groove, 342-second wedge-shaped groove, 4-lens module, 5-side plate, 51-heat conduction groove, 52-fixing shaft, 53-first spring, 54-arc structure, 61-first heat conduction sheet, 611-baffle sheet, 612-second spring, 62-second heat conduction sheet, 621-heat dissipation fin, 71-screw rod, 72-driving motor, 8-bottom plate, 81-slot structure, 82-limiting rod, 83-third spring and 84-wedge block.
Detailed Description
Embodiments of the present invention are described in detail below with reference to the accompanying drawings.
Examples
A high-efficiency heat-radiation motion image sensor is shown in figures 1-12 and comprises a shell 1, a fixed frame 2, an installation cylinder 3, a lens module 4, a side plate 5, a first heat-conducting fin 61, a second heat-conducting fin 62 and a bottom plate 8; the bottom of the shell 1 is connected with an ejection assembly; the lower side of the ejection assembly is connected with a bottom plate 8; the inner side of the shell 1 is connected with a fixed frame 2 through bolts; the inner side of the fixed frame 2 is connected with an installation cylinder 3 through bolts; a push block 32 is fixedly connected to the left part and the right part of the rear side of the mounting cylinder 3 respectively; a tail block 33 is fixedly connected to the rear side of the mounting cylinder 3; a first wedge-shaped groove 341 is formed in the lower side of the mounting barrel 3; a second wedge-shaped groove 342 positioned at the rear side of the first wedge-shaped groove 341 is formed at the lower side of the mounting barrel 3; the inner side of the mounting cylinder 3 is provided with a lens module 4; the left side and the right side of the mounting cylinder 3 are respectively provided with a plurality of heat dissipation groove 31 structures; each heat dissipation groove 31 is provided in a structure inclined rearward from the inside to the outside of the mounting tube 3; the upper side and the lower side of the shell 1 are respectively provided with a slide rail 11; a side plate 5 is connected between the left sides of the two slide rails 11 in a sliding manner; a side plate 5 is also connected between the right sides of the two slide rails 11 in a sliding manner; the front sides of the two side plates 5 are both provided with structures inclining forwards from one side close to the fixed frame 2 to one side far away from the fixed frame 2; the rear sides of the two side plates 5 are respectively provided with a cambered surface structure 54; the two side plates 5 are tightly attached to the fixed frame 2; an elastic fixing component is respectively connected between the two side plates 5 and the mounting cylinder 3; the front side and the rear side of the two side plates 5 are respectively provided with a heat conducting groove 51; a first heat-conducting fin 61 is fixedly connected in each of the four heat-conducting grooves 51; a second heat conducting fin 62 is fixedly connected to the lower front part and the lower rear part of the shell 1 respectively; two second heat-conducting fins 62 are respectively attached to the first heat-conducting fins 61 on the left and right sides; the rear side of the shell 1 is connected with a displacement component; the displacement assembly is connected to the tail block 33.
As shown in fig. 2 and fig. 3, a plurality of heat dissipation fins 621 are welded on the lower sides of the two second heat conduction sheets 62; the bottom plate 8 is provided with a plurality of slot structures 81 for inserting the heat dissipation fins 621.
As shown in fig. 4, the elastic fixing member includes a fixing shaft 52 and a first spring 53; a fixed shaft 52 is fixedly connected to the middle part of the mounting cylinder 3; a first spring 53 is fixedly connected between each of the two side plates 5 and the fixed shaft 52, and the first spring 53 is sleeved on the outer surface of the fixed shaft 52.
As shown in fig. 9 and 10, the ejection assembly includes a stopper rod 82, a third spring 83, and a wedge block 84; four corners of the lower side of the shell 1 are respectively connected with a limiting rod 82 in a sliding manner; the lower ends of the four limiting rods 82 are fixedly connected with the bottom plate 8; a third spring 83 is fixedly connected between each of the four limit rods 82 and the shell 1, and the third springs 83 are respectively sleeved on the outer surfaces of the adjacent limit rods 82; the middle part of the bottom plate 8 is bolted with a wedge-shaped block 84 which is adaptive to the structure of the first wedge-shaped groove 341.
As shown in fig. 9, the displacement assembly includes a screw 71 and a driving motor 72; a driving motor 72 is connected to the rear bolt of the housing 1; a screw rod 71 is fixedly connected to an output shaft of the driving motor 72; the front end of the screw rod 71 is screwed with the tail block 33.
As shown in fig. 5 and 6, a blocking piece 611 is rotatably connected to the upper side of each heat-conducting groove 51 through a rotating shaft; a second spring 612 is fixedly connected between each baffle piece 611 and the first heat-conducting fin 61; each flap 611 abuts the mounting tube 3.
This high-efficient radiating motion image sensor is embedded on flight equipment's fuselage through two fixed axles 52, flight equipment is in the working period that flies, shoot the work to the picture by lens module 4, heat around the lens module 4 distributes out to each heat-conducting groove 51 of curb plate 5 through the radiating groove 31 of installation section of thick bamboo 3, and conduct the heat to second conducting strip 62 through first conducting strip 61 on, the heat of conduction passes through heat radiation fins 621 outside dispersion in the second conducting strip 62, carry out the basic heat dissipation work that lasts to lens module 4, the stability of each part normal work in the guarantee lens module 4 goes on.
When a temperature sensor arranged in the flight device detects that the temperature of the aircraft body is high, an output shaft of the driving motor 72 drives the screw rod 71 to rotate, the screw rod 71 pushes the tail block 33 to drive the installation cylinder 3 to move forward along the fixing frame 2, the installation cylinder 3 pushes the wedge block 84 to drive the bottom plate 8 to move downward through the first wedge-shaped groove 341, the bottom plate 8 drives the limiting rod 82 to slide downward along the housing 1, the third spring 83 is compressed downward by the moving limiting rod 82, as shown in fig. 11, at this time, the bottom plate 8 leaves the housing 1, each heat dissipation fin 621 of the second heat conduction sheet 62 is exposed in the air, during the flight process of the flight device, the air flow enters between the housing 1 and the bottom plate 8 and contacts with each heat dissipation fin 621, the heat dissipation efficiency of the heat dissipation fins 621 to the second heat conduction sheet 62 is improved, the heat dissipation speed to the lens module 4 is further improved, and the first-level air cooling heat dissipation work is performed on the second heat conduction sheet 62 through the heat dissipation fins 621.
When a temperature sensor arranged in the flight equipment detects that the temperature of the camera body rises sharply, an output shaft of a driving motor 72 drives a screw rod 71 to rotate, so that an installation cylinder 3 pushes a wedge block 84 to drive a bottom plate 8 to leave the shell 1, then an output shaft of the driving motor 72 continues to drive the screw rod 71 to rotate, the screw rod 71 pushes a tail block 33 to drive the installation cylinder 3 to continue to move forwards along a fixed frame 2, two push blocks 32 of the installation cylinder 3 respectively cling to cambered structures 54 of two side plates 5 and respectively push the side plates 5 towards the left side and the right side, so that the two side plates 5 both keep away from the installation cylinder 3 and open towards the left side and the right side, as shown in fig. 12, the side plates 5 push a first spring 53 to compress, at this time, a heat dissipation groove 31 of the installation cylinder 3 is directly exposed in the air, at this time, the wedge block 84 is located between a first wedge groove 341 and a second wedge groove 342 of the installation cylinder 3, the bottom plate 8 keeps leaving the shell 1, during the flight equipment, air flow enters between the side inclined plane 5 and the installation cylinder 3 along the front inclined plane of the side plates 5, and rapidly carries heat dissipation groove 31 around the heat dissipation groove, so as to directly carry out the three-stage air cooling work of the lens module 4, and finish the high-efficiency heat dissipation work.
Need reduce the resistance that brings the fuel-fired model airplane on the basis of tertiary forced air cooling heat dissipation work, the output shaft of driving motor 72 drives lead screw 71 once more and rotates, lead screw 71 promotes tail piece 33 and drives installation section of thick bamboo 3 and move along mount 2, until the second wedge 342 of installation section of thick bamboo 3 aligns wedge 84, wedge 84 loses stopping of installation section of thick bamboo 3 this moment, compressed third spring 83 promotes gag lever post 82 and drives bottom plate 8 upwards to reset, wedge 84 gets into in the second wedge 342, let bottom plate 8 get back to the bottom of casing 1, make bottom plate 8 and the bottom of casing 1 form complete cambered surface, reduce the resistance that the air current assaulted and produced on bottom plate 8, two curb plates 5 still keep away from installation section of thick bamboo 3 and open about this moment, the air current lasts to get into between curb plate 5 and the installation section of thick bamboo 3, carry out second grade forced air cooling heat dissipation work to lens module 4, realize providing different high-efficient heat dissipation modes to different scenes.
During the side plate 5 is far away from the installation cylinder 3, because the heat dissipation grooves 31 are all set to be of a structure which inclines backwards from the inside to the outside of the installation cylinder 3, dust particles carried in air flow between the side plate 5 and the installation cylinder 3 are not easy to directly enter the heat dissipation grooves 31, but dust particles carried in air flow between the side plate 5 and the installation cylinder 3 are easy to enter the bottom of the heat conduction groove 51 and are blown into the heat dissipation grooves 31 along the upper outlet of the heat conduction groove 51, in the process that the side plate 5 is far away from the installation cylinder 3, the blocking sheet 611 loses the blocking of the installation cylinder 3, the second spring 612 in a compressed state pops up and pushes the blocking sheet 611 to turn upwards, the blocking sheet 611 blocks in the upper outlet of the heat conduction groove 51, at the moment, the heat conduction groove 51 does not form a through groove which penetrates up and down, dust particles carried in air flow are not easy to enter the heat dissipation grooves 31 through the heat conduction groove 51, and the heat dissipation grooves 31 are protected.
The above description is only an embodiment of the present invention, and is not intended to limit the scope of the present invention, and all equivalent structures or equivalent processes performed by the present invention or directly or indirectly applied to other related technical fields are also included in the scope of the present invention.
Claims (10)
1. A motion image sensor with high-efficiency heat dissipation comprises a shell (1), a fixed frame (2), an installation cylinder (3) and a lens module (4); the inner side of the shell (1) is fixedly connected with a fixed frame (2); the inner side of the fixed frame (2) is fixedly connected with an installation cylinder (3); the inner side of the mounting cylinder (3) is provided with a lens module (4); the heat-conducting plate is characterized by also comprising a side plate (5), a first heat-conducting fin (61), a second heat-conducting fin (62) and a bottom plate (8); the bottom of the shell (1) is connected with an ejection assembly; the lower side of the ejection component is connected with a bottom plate (8); the left side and the right side of the mounting cylinder (3) are respectively provided with a plurality of heat dissipation groove (31) structures; the left side of the shell (1) is connected with a side plate (5) through two sliding rails (11) in a sliding manner; the right side of the shell (1) is also connected with a side plate (5) in a sliding way through two sliding rails (11); an elastic fixing component is respectively connected between the two side plates (5) and the mounting cylinder (3); two heat conducting grooves (51) are respectively arranged on the inner sides of the two side plates (5); a first heat-conducting fin (61) is fixedly connected in each of the four heat-conducting grooves (51); the front part of the lower side and the rear part of the lower side of the shell (1) are respectively fixedly connected with a second heat-conducting fin (62); the first heat conducting fin (61) conducts heat to the second heat conducting fin (62) to perform basic heat dissipation work; the tail block (33) at the rear side of the installation cylinder (3) is pushed by a displacement component at the rear side of the shell (1), the installation cylinder (3) is driven to move, the first wedge-shaped groove (341) on the lower side of the installation cylinder (3) pushes the ejection component, the bottom plate (8) is driven to leave the shell (1), one-level air-cooled heat dissipation work is carried out, the displacement component continues to push the installation cylinder (3), two push blocks (32) on the installation cylinder (3) respectively push two side plates (5) to open, the two elastic fixing components are compressed, the bottom plate (8) is kept to leave the shell (1), three-level air-cooled heat dissipation work is carried out, the displacement component pushes the installation cylinder (3) again, the first wedge-shaped groove (341) of the installation cylinder (3) leaves the ejection component, the ejection component enters the second wedge-shaped groove (342) on the lower side of the installation cylinder (3), the second wedge-shaped groove (342) is located at the rear side of the first wedge-shaped groove (341), the bottom plate (8) is reset, the side plates (5) are kept to open, and the second-level air-cooled heat dissipation work is carried out.
2. The motion image sensor with high heat dissipation efficiency as recited in claim 1, wherein a plurality of heat dissipation fins (621) are respectively fixed on the lower sides of the two second heat conduction fins (62).
3. The motion image sensor with high heat dissipation efficiency as claimed in claim 2, wherein the bottom plate (8) is provided with a plurality of slot structures (81) for inserting the heat dissipation fins (621).
4. The motion image sensor with high heat dissipation efficiency as recited in claim 1, wherein the elastic fixing member comprises a fixing shaft (52) and a first spring (53); a fixed shaft (52) is fixedly connected to the middle part of the mounting cylinder (3); a first spring (53) is fixedly connected between the two side plates (5) and the fixed shaft (52), and the first spring (53) is sleeved on the outer surface of the fixed shaft (52).
5. The motion image sensor with high heat dissipation efficiency as recited in claim 1, wherein the ejection assembly comprises a limit rod (82), a third spring (83) and a wedge block (84); four corners of the lower side of the shell (1) are respectively connected with a limiting rod (82) in a sliding manner; the lower ends of the four limiting rods (82) are fixedly connected with a bottom plate (8); a third spring (83) is fixedly connected between each of the four limiting rods (82) and the shell (1), and the third springs (83) are respectively sleeved on the outer surfaces of the adjacent limiting rods (82); the middle part of the bottom plate (8) is fixedly connected with a wedge-shaped block (84) which is matched with the first wedge-shaped groove (341) in structure.
6. The motion image sensor with high heat dissipation efficiency as recited in claim 1, wherein the displacement assembly comprises a lead screw (71) and a driving motor (72); a driving motor (72) is fixedly connected to the rear side of the shell (1); a screw rod (71) is fixedly connected with an output shaft of the driving motor (72); the front end of the screw rod (71) is screwed with the tail block (33).
7. The motion image sensor of claim 1, wherein a baffle (611) is rotatably connected to the upper side of each heat-conducting groove (51) through a rotating shaft; a second spring (612) is fixedly connected between each baffle sheet (611) and the first heat-conducting sheet (61); each shutter piece (611) is pressed outward by the mounting tube (3) to assume an inclined state, and the second spring (612) assumes a compressed state.
8. A moving image sensor with high heat dissipation efficiency as set forth in claim 1, wherein each heat dissipation groove (31) is provided in a structure inclined rearward from the inside to the outside of the mounting tube (3).
9. A moving image sensor with high heat dissipation efficiency as claimed in claim 1, wherein the front sides of the two side plates (5) are each provided in a structure that inclines forward from the side close to the fixed frame (2) to the side far from the fixed frame (2).
10. A heat-efficient motion image sensor according to claim 1, characterized in that the rear sides of the two side plates (5) are provided with a cambered surface structure (54), respectively.
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| Application Number | Priority Date | Filing Date | Title |
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| CN202211058092.XA CN115134503B (en) | 2022-08-30 | 2022-08-30 | High-efficient radiating motion image sensor |
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| Application Number | Priority Date | Filing Date | Title |
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| CN202211058092.XA CN115134503B (en) | 2022-08-30 | 2022-08-30 | High-efficient radiating motion image sensor |
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| CN115134503A CN115134503A (en) | 2022-09-30 |
| CN115134503B true CN115134503B (en) | 2022-11-01 |
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| CN101403847A (en) * | 2007-10-04 | 2009-04-08 | 奥林巴斯株式会社 | Electronic image pick-up device |
| CN105519245A (en) * | 2014-08-29 | 2016-04-20 | 深圳市大疆创新科技有限公司 | Image capturing module |
| CN207764535U (en) * | 2018-01-03 | 2018-08-24 | 浙江舜宇智能光学技术有限公司 | The more mesh cameras of high-cooling property and its radiator structure |
| CN110839122A (en) * | 2018-08-15 | 2020-02-25 | 杭州海康机器人技术有限公司 | Camera with camera lens |
| CN111031223A (en) * | 2019-12-30 | 2020-04-17 | 深圳市道通智能航空技术有限公司 | Image acquisition device, cloud platform subassembly and unmanned aerial vehicle |
| WO2022077240A1 (en) * | 2020-10-13 | 2022-04-21 | 深圳市大疆创新科技有限公司 | Heat dissipation structure, camera and unmanned aerial vehicle |
Family Cites Families (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP6924974B1 (en) * | 2020-03-10 | 2021-08-25 | パナソニックＩｐマネジメント株式会社 | Imaging device |
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2022
- 2022-08-30 CN CN202211058092.XA patent/CN115134503B/en active Active
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN101403847A (en) * | 2007-10-04 | 2009-04-08 | 奥林巴斯株式会社 | Electronic image pick-up device |
| CN105519245A (en) * | 2014-08-29 | 2016-04-20 | 深圳市大疆创新科技有限公司 | Image capturing module |
| CN207764535U (en) * | 2018-01-03 | 2018-08-24 | 浙江舜宇智能光学技术有限公司 | The more mesh cameras of high-cooling property and its radiator structure |
| CN110839122A (en) * | 2018-08-15 | 2020-02-25 | 杭州海康机器人技术有限公司 | Camera with camera lens |
| CN111031223A (en) * | 2019-12-30 | 2020-04-17 | 深圳市道通智能航空技术有限公司 | Image acquisition device, cloud platform subassembly and unmanned aerial vehicle |
| WO2022077240A1 (en) * | 2020-10-13 | 2022-04-21 | 深圳市大疆创新科技有限公司 | Heat dissipation structure, camera and unmanned aerial vehicle |
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