CN204760456U - Aircraft integrated device that charges - Google Patents
Aircraft integrated device that charges Download PDFInfo
- Publication number
- CN204760456U CN204760456U CN201520457027.3U CN201520457027U CN204760456U CN 204760456 U CN204760456 U CN 204760456U CN 201520457027 U CN201520457027 U CN 201520457027U CN 204760456 U CN204760456 U CN 204760456U
- Authority
- CN
- China
- Prior art keywords
- battery
- box
- charger
- casing
- controller
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Fee Related
Links
Classifications
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
- Y02E60/00—Enabling technologies; Technologies with a potential or indirect contribution to GHG emissions mitigation
- Y02E60/10—Energy storage using batteries
Abstract
The utility model discloses a charging device of aircraft, specifically speaking are aircraft integrated device that charges. It includes the box and articulates the case lid in box one side, and it has controller, ground satellite station's battery and power battery to settle in the box, and it has the picture peg that is located between controller and the ground satellite station's battery still to settle in the box, and it has charger power supply and the ground satellite station's battery special use charger that is located the bottom half still to settle in the box. After the structure of the utility model is adopted, because with the controller, ground satellite station's battery, power battery, charger power supply and the battery of the special charger integration of ground satellite station's battery in the box charge in the box, its degree of integrating is very high, interior each part overall arrangement mode of box is reasonable, compact structure, it is fixed reliable, high durability and convenient use, avoided traditionally when going out to shake down, need carry many moneys charger, spare part has more and mixed and disorderly phenomenon when having leaded to going out to shake down from this, trial voyage or flight efficiency has been improved from this, the convenience of carrying is greatly improved.
Description
Technical field
The utility model relates to a kind of charging device of aircraft, specifically a kind of aircraft charging integrating device.
Background technology
At present, aircraft is the demand meeting continuation of the journey, generally has multiple battery, and in order to charge to often kind of battery, therefore needs for wherein a part is furnished with special charger; The charger of various battery traditionally, particularly special charger is general independent separately, therefore when going out trial voyage or flight, many moneys charger need be carried, consequently leads to go out trial voyage or flight time parts innumerable and disordered, be not only unfavorable for improve trial voyage or flight efficiency, and portably use all very inconvenient.
Summary of the invention
The technical problems to be solved in the utility model be to provide a kind of rationally distributed, compact conformation, integration degree are high, portable aircraft charging integrating device.
In order to solve the problems of the technologies described above, aircraft charging integrating device of the present utility model, comprise casing and the case lid being hinged on casing side, controller, ground station's battery and electrokinetic cell is mounted with in casing, also be mounted with the plate between controller and ground station's battery in casing, in casing, be also mounted with the light source of charger being positioned at bottom half and ground station's battery special charger.
Described casing is provided with the handle being positioned at case lid opposite side.
Described ground station battery and electrokinetic cell are disposed side by side in casing.
Described controller, ground station's battery and electrokinetic cell, plate and light source of charger and ground station's battery special charger are integrated in a battery case, and described battery case is arranged in casing.
After adopting above-mentioned structure, due to controller, ground station's battery, electrokinetic cell, light source of charger and ground station's battery special charger are integrated in the cell charging box in casing, its integration degree is very high, the interior all parts layout type of casing is reasonable, compact conformation, fixing reliable, easy to use, avoid traditionally when going out trial voyage or flight, many moneys charger need be carried, consequently leads to the phenomenon that when going out to shake down, parts are innumerable and disordered, which thereby enhance trial voyage or flight efficiency, substantially increase the convenience of carrying.
Accompanying drawing explanation
Fig. 1 is the perspective view of the utility model aircraft charging integrating device;
Fig. 2 is the main TV structure schematic diagram of the utility model aircraft charging integrating device.
Embodiment
Below in conjunction with the drawings and specific embodiments, aircraft charging integrating device of the present utility model is described in further detail.
As shown in the figure, aircraft charging integrating device of the present utility model, comprise casing 1 and the case lid 2 being hinged on casing side, casing 1 is provided with the handle 7 being positioned at case lid opposite side, being provided with controller in casing 1 settles position, ground station's battery arrangement position and electrokinetic cell to settle position, controller 3, ground station's battery 4 and electrokinetic cell 5 are placed in respective arrangement position, wherein, ground station's battery arrangement position and electrokinetic cell arrangement position are disposed side by side in casing 1 and make ground station's battery 4 and electrokinetic cell 5 be disposed side by side in casing 1; Also be mounted with the plate 6 between controller 3 and ground station's battery 4 in casing 1, be also mounted with in casing 1 and be positioned at light source of charger bottom casing 1 and ground station's battery special charger.
Further, said controller 3, ground station's battery 4 and electrokinetic cell 5, plate 6 and light source of charger and ground station's battery special charger are integrated in a battery case 8, battery case 8 is arranged in casing 1, makes its integration degree higher thus and settles easy for installation.
During charging, directly connecting circuit can settle position to charge to ground station battery 4 and electrokinetic cell 5 in ground station's battery arrangement position and electrokinetic cell, when completing charging, powered-down switch, ground station battery settles position and electrokinetic cell to settle inherently ground station's battery 4 and electrokinetic cell 5 storeroom, position simultaneously, meets the demand be convenient for carrying.
Claims (4)
1. an aircraft charging integrating device, it is characterized in that: comprise casing (1) and be hinged on the case lid (2) of casing side, controller (3), ground station's battery (4) and electrokinetic cell (5) is mounted with in described casing (1), also be mounted with the plate (6) be positioned between controller (3) and ground station's battery (4) in described casing (1), in described casing (1), be also mounted with the light source of charger and ground station's battery special charger that are positioned at casing (1) bottom.
2., according to aircraft charging integrating device according to claim 1, it is characterized in that: described casing (1) is provided with the handle (7) being positioned at case lid opposite side.
3., according to aircraft charging integrating device according to claim 1, it is characterized in that: described ground station battery (4) and electrokinetic cell (5) are disposed side by side in casing (1).
4. according to aircraft charging integrating device according to claim 1, it is characterized in that: described controller (3), ground station's battery (4) and electrokinetic cell (5), plate (6) and light source of charger and ground station's battery special charger are integrated in a battery case (8), and described battery case (8) is arranged in casing (1).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520457027.3U CN204760456U (en) | 2015-06-30 | 2015-06-30 | Aircraft integrated device that charges |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520457027.3U CN204760456U (en) | 2015-06-30 | 2015-06-30 | Aircraft integrated device that charges |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN204760456U true CN204760456U (en) | 2015-11-11 |
Family
ID=54475136
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201520457027.3U Expired - Fee Related CN204760456U (en) | 2015-06-30 | 2015-06-30 | Aircraft integrated device that charges |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN204760456U (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106505681A (en) * | 2016-11-29 | 2017-03-15 | 湖北大秀天域科技发展有限公司 | A kind of wireless charging device of unmanned plane |
| CN106787018A (en) * | 2017-03-14 | 2017-05-31 | 苏州极目机器人科技有限公司 | A kind of charging method of plant protection UAV Intelligent lithium battery |
| KR101805124B1 (en) * | 2016-11-02 | 2017-12-05 | 주식회사 라텍 | Battery charger/discharger set for aircraft equipped with analysis function |
| KR101811574B1 (en) * | 2016-11-02 | 2017-12-22 | 주식회사 라텍 | Battery charger set for aircraft battery being convenient for carrying and keeping |
-
2015
- 2015-06-30 CN CN201520457027.3U patent/CN204760456U/en not_active Expired - Fee Related
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| KR101805124B1 (en) * | 2016-11-02 | 2017-12-05 | 주식회사 라텍 | Battery charger/discharger set for aircraft equipped with analysis function |
| KR101811574B1 (en) * | 2016-11-02 | 2017-12-22 | 주식회사 라텍 | Battery charger set for aircraft battery being convenient for carrying and keeping |
| CN106505681A (en) * | 2016-11-29 | 2017-03-15 | 湖北大秀天域科技发展有限公司 | A kind of wireless charging device of unmanned plane |
| CN106787018A (en) * | 2017-03-14 | 2017-05-31 | 苏州极目机器人科技有限公司 | A kind of charging method of plant protection UAV Intelligent lithium battery |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20151111 Termination date: 20210630 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |