CN115134503A - High-efficient radiating motion image sensor - Google Patents
High-efficient radiating motion image sensor Download PDFInfo
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- CN115134503A CN115134503A CN202211058092.XA CN202211058092A CN115134503A CN 115134503 A CN115134503 A CN 115134503A CN 202211058092 A CN202211058092 A CN 202211058092A CN 115134503 A CN115134503 A CN 115134503A
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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, according to CN204422948U, the heat dissipation device for aerial photography equipment conducts the temperature inside the sensor outwards through the heat-conducting fins, so as to dissipate the heat generated by the sensor and the surroundings in time, but the heat conduction efficiency of the heat dissipation method is greatly affected by the heat-conducting properties of the heat-conducting fins, and the heat dissipation amount is limited, when the fuel model airplane performs various complex flight actions with high difficulty in the air for a long time, the heat generated by the fuel model airplane is much larger than that generated in the conventional cruise mode, and if no efficient heat dissipation method is available, the heat dissipation treatment of the motion image sensor is facilitated in time, so as to affect the normal operation of the motion image sensor.
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 assembly 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 mounting cylinder to the second heat conducting sheet to perform 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; the output shaft of the driving motor is fixedly connected with a screw rod; 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 plate and the first heat-conducting fin; 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 advantages that: the high-efficiency heat-dissipation motion image sensor is provided with a plurality of heat dissipation modes, the flight equipment conducts heat around the installation cylinder to the second heat conduction sheet under the normal flight state through the first heat conduction sheet, the heat around the lens module is quickly dissipated through the second heat conduction sheet to carry out basic heat dissipation work, when the temperature sensor arranged in the flight equipment detects that the temperature of the machine body is higher, the displacement component arranged at the rear side of the shell pushes the tail block arranged at the rear side of the installation cylinder to drive the installation cylinder to move forwards, the first wedge-shaped groove arranged at the lower side of the installation cylinder pushes the ejection component to drive the bottom plate to leave the shell, the heat dissipation fins of the second heat conduction are completely exposed in the air at the moment, primary air cooling heat dissipation work is carried out on the second heat conduction sheet through the heat dissipation fins to accelerate the heat dissipation efficiency of the second heat conduction sheet, and when the temperature sensor arranged in the flight equipment detects that the temperature of the machine body rises sharply, the displacement component continues to push the installation cylinder, 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 keeping away from behind the installation section of thick bamboo, the radiating groove of installation section of thick bamboo exposes in the air completely, directly carry out tertiary forced air cooling 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 forced air cooling 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 forced air cooling 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 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 of 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 will be described in detail below with reference to the accompanying drawings.
Examples
A high-efficiency heat-dissipation 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 cylinder 3; a second wedge-shaped groove 342 positioned at the rear side of the first wedge-shaped groove 341 is formed in the lower side of the mounting barrel 3; the inner side of the installation 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 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 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 stop tab 611 abuts against the mounting barrel 3.
This high-efficient radiating motion image sensor is embedded on flying equipment's fuselage through two fixed axles 52, flying equipment is in the working period of flying, shoot the work to the picture by lens module 4, heat around the lens module 4 distributes to each heat-conducting groove 51 of curb plate 5 through the radiating groove 31 of installation section of thick bamboo 3 in, and on with heat conduction to second conducting strip 62 through first conducting strip 61, 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 normal work of each part in the guarantee lens module 4 goes on steadily.
When a temperature sensor arranged in the flight equipment detects that the temperature of the airplane body is higher, an output shaft of a driving motor 72 drives a screw rod 71 to rotate, the screw rod 71 pushes a tail block 33 to drive an installation cylinder 3 to move forwards along a fixed frame 2, the installation cylinder 3 pushes a wedge block 84 to drive a bottom plate 8 to move downwards through a first wedge-shaped groove 341, the bottom plate 8 drives a limiting rod 82 to slide downwards along a shell 1, a third spring 83 is compressed downwards by the moving limiting rod 82, as shown in fig. 11, when the bottom plate 8 is separated from the housing 1, each of the heat dissipating fins 621 of the second heat conductive sheet 62 is exposed to the air, in the flying process of the flying equipment, the airflow enters between the shell 1 and the bottom plate 8 to contact with each heat radiation fin 621, the heat radiation efficiency of the heat radiation fins 621 to the second heat conduction sheet 62 is increased, thereby increasing the heat dissipation speed of the lens module 4, and performing a primary air-cooling heat dissipation operation on the second heat conducting strip 62 through the heat dissipating fins 621.
When a temperature sensor arranged in the flying device detects that the temperature of the aircraft body rises sharply, an output shaft of a driving motor 72 drives a screw rod 71 to rotate, so that a mounting cylinder 3 pushes a wedge block 84 to drive a bottom plate 8 to leave the housing 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 mounting cylinder 3 to move forward continuously along a fixing frame 2, two push blocks 32 of the mounting cylinder 3 are respectively attached to arc 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 mounting 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 the moment, a heat dissipation groove 31 of the mounting cylinder 3 is directly exposed in the air, at the moment, the wedge block 84 is positioned between a first wedge groove 341 and a second wedge groove 342 of the mounting cylinder 3, the bottom plate 8 keeps leaving the housing 1, and the flying device is in the flying process, the air current gets into between curb plate 5 and the installation section of thick bamboo 3 along the front side inclined plane of curb plate 5 to take the heat around the heat dissipation groove 31 fast, realize directly carrying out tertiary forced air cooling heat dissipation work, the efficient heat dissipation work of accomplishing to lens module 4.
The resistance to the fuel type model airplane needs to be reduced on the basis of the three-level air-cooled heat dissipation work, the output shaft of the driving motor 72 drives the screw rod 71 to rotate again, the screw rod 71 pushes the tail block 33 to drive the mounting cylinder 3 to move forwards along the fixing frame 2 until the second wedge-shaped groove 342 of the mounting cylinder 3 is aligned with the wedge-shaped block 84, at the moment, the wedge-shaped block 84 loses the blocking of the mounting cylinder 3, the compressed third spring 83 pushes the limiting rod 82 to drive the bottom plate 8 to reset upwards, the wedge-shaped block 84 enters the second wedge-shaped groove 342, the bottom plate 8 returns to the bottom of the shell 1, the bottom plate 8 and the bottom of the shell 1 form a complete arc surface, the resistance generated by the impact of the airflow on the bottom plate 8 is reduced, at the moment, the two side plates 5 are still far away from the mounting cylinder 3 and are opened left and right, the airflow continuously enters between the side plates 5 and the mounting cylinder 3, and carrying out secondary air-cooling heat dissipation work on the lens module 4, and providing different efficient heat dissipation modes for different scenes.
During the curb plate 5 kept away from installation section of thick bamboo 3, because the radiating groove 31 all sets up to the outside structure that inclines backward from the installation section of thick bamboo 3 inside, the dirt particle that carries in the air current between entering curb plate 5 and the installation section of thick bamboo 3 is difficult directly to get into in the radiating groove 31, but the dirt particle that carries in the air current between entering curb plate 5 and the installation section of thick bamboo 3, easily get into the bottom of heat-conducting groove 51, and blow in the radiating groove 31 along the upper portion export of heat-conducting groove 51, in the installation section of thick bamboo 3 in-process is kept away from to curb plate 5, separation blade 611 loses the blockking of installation section of thick bamboo 3, be popped out and promote separation blade 611 upwards upset by compressed state's second spring 612, separation blade 611 blocks in the upper portion export of heat-conducting groove 51, the heat-conducting groove 51 no longer forms the logical groove that runs through from top to bottom at this moment, the dirt particle that carries in the air current also is difficult to pass through heat-conducting groove 51 and gets into in the radiating groove 31, play the guard action to radiating groove 31.
The above description is only an embodiment of the present invention, and not intended to limit the scope of the present invention, and all modifications of equivalent structures and equivalent processes, which are made by the present specification, or directly or indirectly applied to other related technical fields, are 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 assembly 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 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 carry out basic heat dissipation work; the displacement component at the rear side of the shell (1) pushes a tail block (33) at the rear side of the installation barrel (3) to drive the installation barrel (3) to move, a first wedge-shaped groove (341) at the lower side of the installation barrel (3) pushes an ejection component to drive the bottom plate (8) to leave the shell (1) to perform primary air-cooling heat dissipation work, the displacement component continues to push the installation barrel (3), two push blocks (32) on the installation barrel (3) respectively push two side plates (5) to open, two elastic fixing components are compressed, the bottom plate (8) keeps leaving the shell (1) to perform tertiary air-cooling heat dissipation work, the displacement component pushes the installation barrel (3) again, the first wedge-shaped groove (341) of the installation barrel (3) leaves the ejection component, the ejection component enters a second wedge-shaped groove (342) at the lower side of the installation barrel (3), the second wedge-shaped groove (342) is positioned at the rear side of the first wedge-shaped groove (341), and the bottom plate (8) resets, the side plates (5) are kept open to carry out secondary air cooling heat dissipation work.
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 a plurality of slot structures (81) for inserting the heat dissipation fins (621) are formed in the bottom plate (8).
4. A high efficiency heat dissipating motion image sensor according to claim 1, wherein the elastic fixing member comprises a fixing shaft (52) and a first spring (53); a fixed shaft (52) is fixedly connected with 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. A high efficiency heat dissipating motion image sensor according to claim 1, wherein the ejector assembly comprises 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 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 sleeved on the outer surfaces of the adjacent limiting rods (82) respectively; a wedge-shaped block (84) which is matched with the first wedge-shaped groove (341) in structure is fixedly connected with the middle part of the bottom plate (8).
6. A moving image sensor with high heat dissipation efficiency as claimed in claim 1, wherein the displacement assembly comprises a screw rod (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 connected with the tail block (33) in a screwing way.
7. A moving image sensor with high heat dissipation efficiency as claimed in claim 1, wherein the upper side of each heat conduction groove (51) is rotatably connected with a baffle (611) 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 heat-efficient moving image sensor as claimed in claim 1, wherein each of the heat-dissipating grooves (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.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| 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 |
|---|---|---|---|
| CN202211058092.XA CN115134503B (en) | 2022-08-30 | 2022-08-30 | High-efficient radiating motion image sensor |
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| CN115134503A true CN115134503A (en) | 2022-09-30 |
| CN115134503B CN115134503B (en) | 2022-11-01 |
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| Publication number | Priority date | Publication date | Assignee | Title |
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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 |
| US20210289110A1 (en) * | 2020-03-10 | 2021-09-16 | Panasonic Intellectual Property Management Co., Ltd. | Imaging device |
| 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 |
-
2022
- 2022-08-30 CN CN202211058092.XA patent/CN115134503B/en active Active
Patent Citations (7)
| 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 |
| US20210289110A1 (en) * | 2020-03-10 | 2021-09-16 | Panasonic Intellectual Property Management Co., Ltd. | Imaging device |
| 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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| Publication number | Publication date |
|---|---|
| CN115134503B (en) | 2022-11-01 |
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