CN205131668U - Unmanned aerial vehicle with cooling fin structure radiator - Google Patents
Unmanned aerial vehicle with cooling fin structure radiator Download PDFInfo
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- CN205131668U CN205131668U CN201520871414.1U CN201520871414U CN205131668U CN 205131668 U CN205131668 U CN 205131668U CN 201520871414 U CN201520871414 U CN 201520871414U CN 205131668 U CN205131668 U CN 205131668U
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Abstract
The utility model discloses an unmanned aerial vehicle with cooling fin structure radiator through replaced the fan structure with cooling fin structure, had both saved the space, had satisfied the demand of product to the steadiness again, and the fin can be fixed on the circuit board well. In addition, included first camera and second camera, first camera is infrared imager, infrared imager is used for gathering infrared image information, the second camera is color video camera, color video camera is used for gathering color image information, detecting device sends infrared image information and color image information for control system through communication module, and problem through analysis infrared image information and color image information can solve the clear image acquisition under the multiple scene can satisfy user's user demand.
Description
Technical field
The utility model belongs to fire fighting monitoring technical field, particularly relates to a kind of with the unmanned plane with heat radiating fin structure radiator.
Background technology
Robot airplane is called for short " unmanned plane ", and english abbreviation is " UAV ", is the not manned aircraft utilizing radio robot to handle with the process controller provided for oneself.Unmanned plane, by application, can be divided into military and civilian.Unmanned plane is of many uses at civil area, is mainly used in the industries such as police, city management, agricultural, geology, meteorology, electric power, rescue and relief work, video capture.
Along with socioeconomic fast development, detector has been widely applied in the middle of fields such as comprising fire prevention, traffic, Intelligent Recognition.In some cases, detector cannot carry out monitoring effectively and timely, is especially difficult to the place arrived at harsh environment and personnel.Therefore, the unmanned plane with detector is devised out by people.
But existing detector, the radiator structure of its process chip is fan structure, easily drops, thus loses efficacy, and makes the heat radiation of process chip bad, seriously scaling loss process chip, brings great restriction to the application scenarios of detector.Given this, the utility model provides a kind of with the unmanned plane with heat radiating fin structure radiator.
Summary of the invention
The purpose of this utility model is a kind of with the unmanned plane with heat radiating fin structure radiator, to solve in prior art the existing detector existed, the radiator structure of its process chip is fan structure, easily drop, thus lost efficacy, make the heat radiation of process chip bad, seriously the problem of scaling loss process chip.
For realizing the purpose of this utility model, the utility model provides a kind of with the unmanned plane with heat radiating fin structure radiator, comprise unmanned plane body, fixed mount, detector, described fixed mount is arranged at the bottom of described unmanned plane body, described detector is connected with unmanned plane body by fixed mount, described detector comprises shell, upper cover, sheet metal component, circuit card, camera lens, buttock line, wherein, one end of described upper cover and described housing hinge, described circuit card is fixedly mounted on sheet metal component, described sheet metal component is fixedly mounted in described shell, described shell comprises protecgulum, centre portion and bonnet, described camera lens is arranged on described sheet metal component, described buttock line is connected with described circuit card through described bonnet, described circuit card is integrated with power module, described circuit card is provided with process chip, the upper surface of described process chip is connected with radiating gill, described radiating gill is fixedly connected with described circuit card.
Wherein, described detector also comprises the first camera and second camera, power module, communication module, described first camera is infrared thermoviewer, described infrared thermoviewer is for gathering Infrared Image Information, described second camera is colour TV camera, described colour TV camera is for gathering color image information, described power module is used for powering to described infrared thermoviewer and colour TV camera, and Infrared Image Information and color image information are sent to control system by communication module by described detector.
Wherein, described unmanned plane body comprises flying platform and power system and automatic control module, and described automatic control module comprises GPS navigation system, attitude control system, altimeter and The Cloud Terrace, and described detector is connected with The Cloud Terrace by fixed mount.
The utility model, by instead of fan structure with heat radiating fin structure, both saved space, met again the demand of product to steadiness, and radiating gill can be fixed on circuit boards well.In addition, include the first camera and second camera, first camera is infrared thermoviewer, described infrared thermoviewer is for gathering Infrared Image Information, described second camera is colour TV camera, described colour TV camera is for gathering color image information, Infrared Image Information and color image information are sent to control system by communication module by described detector, the problem that the brilliant image that can be solved under several scenes by analysis Infrared Image Information and color image information is gathered, can meet the user demand of user.
Accompanying drawing explanation
Figure 1 shows that structural representation of the present utility model;
Figure 2 shows that the structural representation of the utility model detector;
In figure: 1. unmanned plane body, 2. fixed mount, 3. detector, 31. housings, 32. transparent windows, 33. first cameras, 34. second cameras, 35. power modules, 36. communication modules.
Detailed description of the invention
Below in conjunction with the drawings and specific embodiments, the utility model is described in further detail.Should be appreciated that specific embodiment described herein only in order to explain the utility model, and be not used in restriction the utility model.
Should be noted that, " connection " described in the application and the word for expressing " connection ", as " being connected ", " being connected " etc., both can comprise a certain parts with another parts is directly connected, and also can comprise a certain parts and is connected with another parts by miscellaneous part.
As Fig. 1, shown in Fig. 2, the utility model provides a kind of with the unmanned plane with heat radiating fin structure radiator, comprise unmanned plane body 1, fixed mount 2, detector 3, described fixed mount 2 is arranged at the bottom of described unmanned plane body 1, described detector 3 is connected with unmanned plane body 1 by fixed mount 2, described detector 3 comprises shell, upper cover, sheet metal component, circuit card, camera lens, buttock line, wherein, one end of described upper cover and described housing hinge, described circuit card is fixedly mounted on sheet metal component, described sheet metal component is fixedly mounted in described shell, described shell comprises protecgulum, centre portion and bonnet, described camera lens is arranged on described sheet metal component, described buttock line is connected with described circuit card through described bonnet, described circuit card is integrated with power module, described circuit card is provided with process chip, the upper surface of described process chip is connected with radiating gill, described radiating gill is fixedly connected with described circuit card.。Infrared thermoviewer wherein effectively can solve the deficiency of colorful digital video camera monitoring objective under night even pole extreme climate environment condition.
In a preferred embodiment, described detector also comprises housing 31, and described first camera and second camera, power module, communication module are installed in described housing, and the front end of described housing is provided with transparent window 32.
In a preferred embodiment, described unmanned plane body comprises flying platform and power system and automatic control module, described automatic control module comprises GPS navigation system, attitude control system, altimeter and The Cloud Terrace, and described detector is connected with The Cloud Terrace by fixed mount.Described The Cloud Terrace is stable platform, and stable platform can eliminate shake, improves picture quality, meanwhile, can also convert visual angle of taking photo by plane.Described control system is Background control or front-end control.
The utility model, be provided with heat radiating fin structure radiator, comprise know clearly the first camera and second camera, first camera is infrared thermoviewer, described infrared thermoviewer is for gathering Infrared Image Information, described second camera is colour TV camera, described colour TV camera is for gathering color image information, Infrared Image Information and color image information are sent to control system by communication module by described detector, the problem that the brilliant image that can be solved under several scenes by analysis Infrared Image Information and color image information is gathered, the user demand of user can be met.
In a preferred embodiment, convenient, safety is placed in order to make detector, following structure can be set: described unmanned plane body is provided with container cavity, described The Cloud Terrace is arranged in container cavity, described fixed mount is lifting mode fixed mount, particularly, described fixed mount comprises fixing cylinder, snap close, the upper end of described fixing cylinder is connected with The Cloud Terrace, the piston rod of fixing cylinder is fixedly connected with snap close, and described detection device casing upper surface is provided with coupling link, during use, use snap close locking coupling link, thus detector can be connected with fixing cylinder.When not using, cylinder can be utilized in detector retraction container cavity, thus can place detector well, unmanned plane also can comparatively random lifting and parking; When using, cylinder can be utilized to be stretched out outside container cavity by detector.
In a preferred embodiment, in order to make containment structure simple, make easy to process, shell can be divided into upper cover and lower shell structure, one end and the described lower casing of described upper cover are hinged, the other end is connected with lower casing by locking piece, described lower casing comprises protecgulum, centre portion and back cover, described camera lens is arranged on sheet metal component, described buttock line is connected with power supply source through described back cover, the inner side of described upper cover is pasted with sealing EVA foam, described lower casing and the described upper cover place of being tightly connected are provided with sealing rubber strip, described sealing EVA foam surface uniform pastes electrically conductive cloth, and it is seamless between the two after pasting, described sealing rubber strip surface is pasted with electrically conductive cloth completely, and electrically conductive cloth surface smoothing is seamless between the two after pasting.Utilize said structure, the electronic unit in shell can be avoided to be damaged by static electricity.
In a preferred embodiment, in order to ensure the clean of transparent window, shell outside transparent window is provided with air-flow shower nozzle, described air-flow shower nozzle is connected with air pump by pipeline, described air pump is connected with controller, described air-flow shower nozzle can be multiple, and shower nozzle air extractor duct, towards transparent window, arranges injecting time and the interval time of air-flow shower nozzle by controller.
The above is only preferred implementation of the present utility model; it should be noted that; for those skilled in the art; under the prerequisite not departing from the utility model principle; can also make some improvements and modifications, these improvements and modifications also should be considered as protection domain of the present utility model.
Claims (3)
1. one kind with the unmanned plane with heat radiating fin structure radiator, it is characterized in that, comprise unmanned plane body, fixed mount, detector, described fixed mount is arranged at the bottom of described unmanned plane body, described detector is connected with unmanned plane body by fixed mount, described detector comprises shell, upper cover, sheet metal component, circuit card, camera lens, buttock line, wherein, one end of described upper cover and described housing hinge, described circuit card is fixedly mounted on sheet metal component, described sheet metal component is fixedly mounted in described shell, described shell comprises protecgulum, centre portion and bonnet, described camera lens is arranged on described sheet metal component, described buttock line is connected with described circuit card through described bonnet, described circuit card is integrated with power module, described circuit card is provided with process chip, the upper surface of described process chip is connected with radiating gill, described radiating gill is fixedly connected with described circuit card.
2. according to claim 1 with the unmanned plane with heat radiating fin structure radiator, it is characterized in that, described detector also comprises the first camera and second camera, power module, communication module, described first camera is infrared thermoviewer, described infrared thermoviewer is for gathering Infrared Image Information, described second camera is colour TV camera, described colour TV camera is for gathering color image information, described power module is used for powering to described infrared thermoviewer and colour TV camera, Infrared Image Information and color image information are sent to control system by communication module by described detector.
3. according to claim 1 with the unmanned plane with heat radiating fin structure radiator, it is characterized in that, described unmanned plane body comprises flying platform and power system and automatic control module, described automatic control module comprises GPS navigation system, attitude control system, altimeter and The Cloud Terrace, and described detector is connected with The Cloud Terrace by fixed mount.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520871414.1U CN205131668U (en) | 2015-11-03 | 2015-11-03 | Unmanned aerial vehicle with cooling fin structure radiator |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520871414.1U CN205131668U (en) | 2015-11-03 | 2015-11-03 | Unmanned aerial vehicle with cooling fin structure radiator |
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| Publication Number | Publication Date |
|---|---|
| CN205131668U true CN205131668U (en) | 2016-04-06 |
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| Application Number | Title | Priority Date | Filing Date |
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| CN201520871414.1U Active CN205131668U (en) | 2015-11-03 | 2015-11-03 | Unmanned aerial vehicle with cooling fin structure radiator |
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Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105764304A (en) * | 2015-11-03 | 2016-07-13 | 天津艾思科尔科技有限公司 | Aircraft provided with detector with stable heat dissipation structure |
| JPWO2018029739A1 (en) * | 2016-08-08 | 2019-06-27 | エスゼット ディージェイアイ テクノロジー カンパニー リミテッドＳｚ Ｄｊｉ Ｔｅｃｈｎｏｌｏｇｙ Ｃｏ．，Ｌｔｄ | Mobile body and method of manufacturing imaging device |
-
2015
- 2015-11-03 CN CN201520871414.1U patent/CN205131668U/en active Active
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105764304A (en) * | 2015-11-03 | 2016-07-13 | 天津艾思科尔科技有限公司 | Aircraft provided with detector with stable heat dissipation structure |
| CN105764304B (en) * | 2015-11-03 | 2018-10-16 | 天津艾思科尔科技有限公司 | Detector carries the aircraft of steady type radiator structure |
| JPWO2018029739A1 (en) * | 2016-08-08 | 2019-06-27 | エスゼット ディージェイアイ テクノロジー カンパニー リミテッドＳｚ Ｄｊｉ Ｔｅｃｈｎｏｌｏｇｙ Ｃｏ．，Ｌｔｄ | Mobile body and method of manufacturing imaging device |
| JP7009696B2 (en) | 2016-08-08 | 2022-01-26 | エスゼット ディージェイアイ テクノロジー カンパニー リミテッド | Mobile |
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