CN205081532U - Power for unmanned aerial vehicle - Google Patents
Power for unmanned aerial vehicle Download PDFInfo
- Publication number
- CN205081532U CN205081532U CN201520903628.2U CN201520903628U CN205081532U CN 205081532 U CN205081532 U CN 205081532U CN 201520903628 U CN201520903628 U CN 201520903628U CN 205081532 U CN205081532 U CN 205081532U
- Authority
- CN
- China
- Prior art keywords
- battery
- power
- plug
- unmanned plane
- power supply
- 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
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- Charge And Discharge Circuits For Batteries Or The Like (AREA)
Abstract
The utility model discloses a power for unmanned aerial vehicle, battery (1) and intelligent protection circuit board (5) in including the protection casing and arranging the protection casing in, the protection casing be the square cover body, the protection casing includes upper cover (2), lower cover (3) and end cover (4), power for unmanned aerial vehicle is still including balanced connect (6) and power cable connector (7) of charging, power cable connector passes through the power cord and links to each other with the battery, and balanced joint of charging links to each other with the battery through the winding displacement, power cable connector be a face contact plug, charge balanced the joint for contact pin formula joint. The battery establish ties by 12 electric cores and form. Power cable connector adopts PP75 type plug. This power for unmanned aerial vehicle reliability is high, easy to carry out.
Description
Technical field
The utility model relates to a kind of unmanned plane power supply.
Background technology
In use there is the major issue that three affect safety and efficiency in existing unmanned plane rechargable power supplies, one is that the serial connection charge of multistage battery core need adopt and carries out before charging being connected in series (as 12S battery core is connected in series by two groups of 6S battery cores), add joint and create reliability decrease, two be change power supply operating process in, usually battery to be connected on unmanned plane at that moment, plug gives off sparks, and with the sound of striking sparks, along with the increase of time and number of times, the connection reliability of plug just reduces, plug can be caused to generate heat, melt even in the air.The case causing unmanned plane to crash because of plug problem of aging is much.Three is balancing head quality of charger, because what now general XH series balance keyset adopted is Open architecture, in the process of charging, the electric conductivity of the balancing head of charger makes battery control circuit plate generate heat to make inner part to cause damage compared with missionary society, external dust has entered in plug and has caused short circuit simultaneously, also can cause power supply short circuit and burn.
Therefore, be necessary to design a kind of novel unmanned plane power supply.
Utility model content
Technical problem to be solved in the utility model is to provide a kind of unmanned plane power supply, and this unmanned plane power supply reliability is high, easy to implement.
The technical solution of utility model is as follows:
A kind of unmanned plane power supply, comprises protective cover and the battery (1) that is placed in protective cover and intelligent protection circuit plate (5); Described protective cover is square cover body; Protective cover comprises upper cover (2), lower cover (3) and end cap (4);
Unmanned plane power supply also comprises charging balancing plug (6) and power cord connector (7); Power cord connector is connected with battery by power line, and charging balancing plug is connected with battery by winding displacement;
Described power cord connector is plane contact plug; Charging balancing plug is contact pin type joint.
Described battery is in series by 12 battery cores.
Power cord connector adopts PP75 type plug.
Intelligent protection circuit plate is provided with charging circuit (comprising controller), is existing mature technology.Intelligent protection circuit plate has the function of automatic detection temperature, display electricity, electric discharge, is existing mature technology.
Beneficial effect:
Unmanned plane power supply of the present utility model, (1) 12 battery cores are directly together in series the allocation plan replacing 2*6 battery core, terminal is less, in addition, (2) power cord connector (i.e. attaching plug, comprise a whole set of charging system and comprise charger, power supply, attaching plug on aircraft): change face contact type (model: Anderson PP75 into by original point contact type plug (model XT90), be specially PP75ORDERINGINFORMATION connector joint), (3) balancing plug (i.e. balance plate joint) that charges becomes contact pin type joint (contact pin type model: 3001 series by original spring-piece type compression joint type (model XH series), as 3001-2*8P), above measure makes this unmanned plane power supply reliability high, and it is easy to implement.
Accompanying drawing explanation
Fig. 1 is the general structure schematic diagram of unmanned plane power supply of the present utility model.
Label declaration: 1-battery, 2-upper cover, 3-lower cover, 4-end cap, 5-intelligent protection circuit plate, 6-charges balancing plug, 7-power cord connector.
Embodiment
Below with reference to the drawings and specific embodiments, the utility model is described in further details:
Embodiment 1:
As shown in Figure 1, a kind of unmanned plane power supply, comprises protective cover and the battery 1 that is placed in protective cover and intelligent protection circuit plate 5; Described protective cover is square cover body; Protective cover comprises upper cover 2, lower cover 3 and end cap 4;
Unmanned plane power supply also comprises charging balancing plug 6 and power cord connector 7; Power cord connector is connected with battery by power line, and charging balancing plug is connected with battery by winding displacement;
Described power cord connector is plane contact plug; Charging balancing plug is contact pin type joint.
Described battery is in series by 12 battery cores.
Power cord connector adopts PP75 type plug.
The tactic pattern of 12 battery core serial connection charges, solves work operations amount and the Data Consistency of battery on a polling module that 26 battery core patterns charge respectively.
Claims (3)
1. a unmanned plane power supply, is characterized in that, comprises protective cover and the battery (1) that is placed in protective cover and intelligent protection circuit plate (5); Described protective cover is square cover body; Protective cover comprises upper cover (2), lower cover (3) and end cap (4);
Unmanned plane power supply also comprises charging balancing plug (6) and power cord connector (7); Power cord connector is connected with battery by power line, and charging balancing plug is connected with battery by winding displacement;
Described power cord connector is plane contact plug; Charging balancing plug is contact pin type joint.
2. unmanned plane power supply according to claim 1, is characterized in that, described battery is in series by 12 battery cores.
3. unmanned plane power supply according to claim 1 and 2, is characterized in that, power cord connector adopts PP75 type plug.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520903628.2U CN205081532U (en) | 2015-11-13 | 2015-11-13 | Power for unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520903628.2U CN205081532U (en) | 2015-11-13 | 2015-11-13 | Power for unmanned aerial vehicle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205081532U true CN205081532U (en) | 2016-03-09 |
Family
ID=55433906
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201520903628.2U Expired - Fee Related CN205081532U (en) | 2015-11-13 | 2015-11-13 | Power for unmanned aerial vehicle |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN205081532U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106058591A (en) * | 2016-07-15 | 2016-10-26 | 天峋（常州）智能科技有限公司 | Unmanned plane power source quick plugging device and unmanned plane |
-
2015
- 2015-11-13 CN CN201520903628.2U patent/CN205081532U/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106058591A (en) * | 2016-07-15 | 2016-10-26 | 天峋（常州）智能科技有限公司 | Unmanned plane power source quick plugging device and unmanned plane |
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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 | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20160309 Termination date: 20171113 |