CN218141070U

CN218141070U - Unmanned aerial vehicle battery charger

Info

Publication number: CN218141070U
Application number: CN202222270614.4U
Authority: CN
Inventors: 张彩辉; 杨俊�
Original assignee: Shenzhen Zhian New Energy Technology Co ltd
Current assignee: Shenzhen Zhian New Energy Technology Co ltd
Priority date: 2022-08-26
Filing date: 2022-08-26
Publication date: 2022-12-27
Anticipated expiration: 2032-08-26

Abstract

The utility model provides an unmanned aerial vehicle battery charger for charge for the unmanned aerial vehicle battery, the top side of unmanned aerial vehicle battery is provided with the lug, and one side of the bottom towards the unmanned aerial vehicle battery of lug is provided with battery input interface, and unmanned aerial vehicle battery charger includes main part and charger output interface. The main body is provided with a top surface and a positioning groove, the positioning groove is provided with an upward opening, the opening is used for inserting the unmanned aerial vehicle battery into the positioning groove, and the positioning groove is used for positioning and containing the unmanned aerial vehicle battery. Charger output interface sets up on the top surface, and is located one side of constant head tank, and charger output interface is used for pegging graft with battery input interface, and the grafting direction of the two is on a parallel with the unmanned aerial vehicle battery and the direction of plugging out of constant head tank. The utility model discloses an unmanned aerial vehicle battery charger for charger output interface just with be located battery top side, and battery input interface down pegs graft, makes charger output interface and battery input interface connection convenient.

Description

Unmanned aerial vehicle battery charger

Technical Field

The utility model relates to a charger technical field, in particular to unmanned aerial vehicle battery charger.

Background

With the rise of unmanned aerial vehicles and the rapid development of relevant model airplanes and unmanned aerial vehicle field technologies, unmanned aerial vehicles are also applied in more and more occasions. The unmanned aerial vehicle battery is an important component of the unmanned aerial vehicle, and needs to be taken out and put into an unmanned aerial vehicle battery charger for charging. At present, unmanned aerial vehicle battery charger draws forth with the wire rod and comes to rely on the manual plug to hold to the battery socket externally, and easy to the inaccurate battery socket, it is inconvenient to use, and the lead wire goes out inconvenient accomodating.

The problem needs to be solved by providing a battery charger for unmanned aerial vehicles.

SUMMERY OF THE UTILITY MODEL

The utility model provides an unmanned aerial vehicle battery charger for charger output interface and battery input interface connection are convenient.

The technical scheme of the utility model is that:

the utility model provides an unmanned aerial vehicle battery charger for charge for the unmanned aerial vehicle battery, the top side of unmanned aerial vehicle battery is provided with the lug, the orientation of lug one side of the bottom of unmanned aerial vehicle battery is provided with battery input interface, unmanned aerial vehicle battery charger includes:

a body having a top surface, the body having a detent with an upward facing opening for inserting the UAV battery into the detent, the detent for locating and receiving the UAV battery; and (c) a second step of,

the charger output interface is arranged on the top surface and located on one side of the positioning groove, the charger output interface is used for being connected with the battery input interface in an inserting mode, and the inserting direction of the charger output interface and the battery input interface is parallel to the inserting direction of the unmanned aerial vehicle battery and the inserting direction of the positioning groove.

In the battery charger of the unmanned aerial vehicle, the battery of the unmanned aerial vehicle is provided with two guide grooves which are respectively positioned on two opposite side surfaces of the battery of the unmanned aerial vehicle; the positioning groove is provided with two guide blocks, the two guide blocks are respectively positioned on two opposite groove walls in the positioning groove, and the guide blocks are used for being in sliding connection with the guide grooves.

Unmanned aerial vehicle battery charger in, the top of guide slot is provided with the stopper, be provided with the spacing groove on the guide block, the spacing groove is used for right the stopper carries on spacingly.

Unmanned aerial vehicle battery charger in, the cell wall and the unmanned aerial vehicle battery interval of constant head tank set up.

Unmanned aerial vehicle battery charger in, be provided with the recess on the top surface, its with the constant head tank intercommunication is used for holding the lug, charger output interface sets up the bottom of recess.

In the unmanned aerial vehicle battery charger of the present invention, the main body includes a main frame and two supports, the charger output interface is disposed on the main frame, and the main frame has two opposite first sides and two opposite second sides; the host is fixed between the two brackets, the two brackets are respectively positioned on the two second sides, the two brackets protrude out of the first side, and the positioning groove is formed between the two brackets.

Unmanned aerial vehicle battery charger in, two the support salient respectively in two first side forms two respectively the constant head tank.

Unmanned aerial vehicle battery charger in, unmanned aerial vehicle battery charger still includes first radiator fan, its setting is in first side, and its air outlet orientation the constant head tank.

Unmanned aerial vehicle battery charger in, the main part still includes the heating panel, it is connected two between the support, and with first side sets up relatively, be provided with first louvre on the heating panel.

Unmanned aerial vehicle battery charger in, unmanned aerial vehicle battery charger still includes second radiator fan, the host computer is hollow structure, one of them the second side is provided with the second louvre, second radiator fan sets up another the second side.

The utility model discloses compare in prior art, its beneficial effect is: the utility model discloses an unmanned aerial vehicle battery charger inserts the unmanned aerial vehicle battery in the constant head tank through opening up, when the unmanned aerial vehicle battery location was placed in the constant head tank, through setting up charger output interface in the top surface of main part to be located one side of constant head tank, and set up, make charger output interface just with be located battery top side, and battery input interface peg graft down, make charger output interface and battery input interface connection convenient.

Drawings

In order to more clearly illustrate the embodiments of the present invention or the technical solutions in the prior art, the drawings required to be used in the embodiments are briefly introduced below, and the drawings in the following description are only corresponding drawings of some embodiments of the present invention.

Fig. 1 is a schematic structural diagram of an unmanned aerial vehicle battery matched with an unmanned aerial vehicle battery charger provided by the preferred embodiment of the present invention.

Fig. 2 is a schematic structural diagram of an unmanned aerial vehicle battery at another angle matched with the unmanned aerial vehicle battery charger provided by the preferred embodiment of the present invention.

Fig. 3 is a schematic structural diagram of a battery charger for a drone according to a preferred embodiment of the present invention.

Fig. 4 is a schematic structural diagram of the unmanned aerial vehicle battery charger according to the preferred embodiment of the present invention after being inserted into the unmanned aerial vehicle battery.

Wherein the content of the first and second substances,

100. the battery of the unmanned aerial vehicle is provided with a battery,

1001. a bump 1002, a battery input interface 1003, a guide groove 1004, a limit block,

11. a main body which is provided with a plurality of grooves,

111. the top surface, 1111, the groove,

112. a positioning groove is arranged on the upper surface of the base,

113. a main unit 1131, a first side 1132, a second side 1133, a second heat sink,

114. a support frame is arranged on the base plate,

115. a heat dissipation plate 1151, a first heat dissipation hole,

12. an output interface of the charger is connected with the charger,

13. a guide block, 131 and a limit groove,

14. a first heat-dissipating fan for dissipating heat generated by the heat-dissipating fan,

15. a second heat-dissipating fan for dissipating heat generated by the heat-dissipating fan,

16. and a power output port.

In the drawings, elements having similar structures are denoted by the same reference numerals.

Detailed Description

The technical solutions in the embodiments of the present invention will be described clearly and completely with reference to the drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only some embodiments of the present invention, not all embodiments. Based on the embodiments in the present invention, all other embodiments obtained by the skilled in the art without creative work belong to the protection scope of the present invention.

In the present invention, the directional terms, such as "up", "down", "front", "back", "left", "right", "inner", "outer", "side", "top" and "bottom", refer to the orientation of the drawings, and the directional terms are used for illustration and understanding, but not for limiting the present invention.

The terms "first," "second," and the like in the terms of the present invention are used for descriptive purposes only and are not to be construed as indicating or implying relative importance or any order limitation.

In the present invention, unless otherwise expressly stated or limited, the terms "mounted," "connected," and "fixed" are to be construed broadly and may, for example, be fixedly connected, detachably connected, or integrally formed; can be mechanically or electrically connected; either directly or indirectly through intervening media, either internally or in any other relationship. The specific meaning of the above terms in the present invention can be understood according to specific situations by those skilled in the art.

At present, unmanned aerial vehicle battery charger draws forth with the wire rod and comes to rely on the manual plug to hold to the battery socket externally, and easy to the inaccurate battery socket, it is inconvenient to use, and the lead wire goes out inconvenient accomodating.

Do as follows the utility model provides a pair of unmanned aerial vehicle battery charger's that can solve above technical problem preferred embodiment.

Referring to fig. 1 and 3, a preferred embodiment of the present invention provides an unmanned aerial vehicle battery charger for charging an unmanned aerial vehicle battery 100, a bump 1001 is disposed on a side surface of a top end of the unmanned aerial vehicle battery 100, and a battery input interface 1002 is disposed on one side of the bump 1001 facing a bottom end of the unmanned aerial vehicle battery 100. The drone battery charger comprises a main body 11 and a charger output interface 12. Main part 11 has top surface 111, and main part 11 is provided with constant head tank 112, and constant head tank 112 has upwards opening, and the opening is used for inserting unmanned aerial vehicle battery 100 in to constant head tank 112, and constant head tank 112 is used for the location holding unmanned aerial vehicle battery 100. Charger output interface 12 sets up on top surface 111, and is located one side of constant head tank 112, and charger output interface 12 is used for pegging graft with battery input interface 1002, and the grafting direction of the two is on a parallel with unmanned aerial vehicle battery 100 and the direction of plugging and unplugging of constant head tank 112.

The utility model discloses an unmanned aerial vehicle battery charger, insert unmanned aerial vehicle battery 100 in constant head tank 112 through opening up, when unmanned aerial vehicle battery 100 location is placed in constant head tank 112, through setting up charger output interface 12 in the top surface 111 of main part 11, and be located one side of constant head tank 112, and set up, make charger output interface 12 just with be located battery top side, and battery input interface 1002 peg graft down, make charger output interface 12 and battery input interface 1002 be connected conveniently.

Referring to fig. 2 and 3, the drone battery 100 is provided with two guide slots 1003, and the two guide slots 1003 are respectively located on two opposite side surfaces of the drone battery 100. The positioning groove 112 is provided with two guide blocks 13, the two guide blocks 13 are respectively located on two opposite groove walls of the positioning groove 112, and the guide block 13 is used for being slidably connected with the guide groove 1003. This structure facilitates positioning of drone battery 100 in positioning slot 112.

Referring to fig. 2 and fig. 3, a limiting block 1004 is disposed at the top end of the guide slot 1003, a limiting groove 131 is disposed on the guide block 13, and the limiting groove 131 is used for limiting the limiting block 1004. This structure can be so that unmanned aerial vehicle battery 100 is stable places in constant head tank 112, and spacing through stopper 1004 and spacing groove 131 of upper end, then constant head tank 112 need not set up the bottom that is used for bearing, can set up the lower extreme of constant head tank 112 into uncovered structure, and the heat dissipation of being convenient for also can alleviate the weight of main part 11 simultaneously.

Please refer to fig. 3, and also refer to fig. 4. The cell wall of constant head tank 112 sets up with unmanned aerial vehicle battery 100 interval. This structure is convenient for unmanned aerial vehicle battery 100 heat dissipation.

Referring to fig. 3, a recess 1111 is disposed on the top surface 111, and is communicated with the positioning groove 112 for accommodating the bump 1001, and the charger output interface 12 is disposed at the bottom of the recess 1111. The structure can effectively protect the charger output interface 12 and avoid damage.

Referring to fig. 3, the main body 11 includes a main body 113 and two brackets 114, the charger output interface 12 is disposed on the main body 113, and the main body 113 has two opposite first sides 1131 and two opposite second sides 1132. The host 113 is fixed between two brackets 114, the two brackets 114 are respectively located on two second sides 1132, the two brackets 114 protrude from the first side 1131, and a positioning groove 112 is formed between the two brackets. With this structure, the positioning groove 112 can be formed by assembling the main body 113 and the two holders 114 together, and there is no need to separately process the positioning groove 112. And the upper edges of the two brackets 114 protrude out of the top of the main frame 113, which is convenient for carrying and transportation.

Referring to fig. 3, the two brackets 114 respectively protrude from the two first sides 1131 to respectively form two positioning slots 112. Adopt this structure, can charge two unmanned aerial vehicle batteries 100 simultaneously.

Referring to fig. 3, the drone battery charger further includes a first heat dissipation fan 14 disposed on the first side 1131, and an air outlet of the first heat dissipation fan faces the positioning slot 112. Adopt this structure, can dispel the heat to unmanned aerial vehicle battery 100 to be convenient for first radiator fan 14 wiring.

Referring to fig. 3, the main body 11 further includes a heat dissipation plate 115 connected between the two brackets 114 and disposed opposite to the first side 1131, and the heat dissipation plate 115 is disposed with a first heat dissipation hole 1151. In this structure, heating panel 115 can play the guard action to unmanned aerial vehicle battery 100, can dispel the heat to unmanned aerial vehicle battery 100 through setting up first louvre 1151.

Referring to fig. 3 and 4, the unmanned aerial vehicle battery charger further includes a second heat dissipation fan 15, the host 113 is a hollow structure, circuit modules such as a circuit board are disposed inside the host 113, one of the second sides 1132 is provided with a second heat dissipation hole 1133, the second side 1132 is further provided with a switch and a display screen, which are convenient for controlling and displaying a charging state, and the second heat dissipation fan 15 is disposed on the other second side 1132. In this structure, the second heat dissipation fan 15 can dissipate heat of electronic components inside the host 113, and the second heat dissipation hole 1133 can allow air blown by the first heat dissipation fan 14 and the second heat dissipation fan 15 to circulate.

The utility model discloses preferred embodiment's unmanned aerial vehicle battery charger's application method and theory of operation:

1. installing a host 113 and two supports 114 together, and respectively forming two positioning grooves 112 at two ends;

2. the unmanned aerial vehicle battery 100 is inserted into the positioning groove 112 from the opening downwards, the two guide grooves 1003 are respectively aligned to the two guide blocks 13 during insertion, and when the limiting groove 131 is just clamped with the limiting block 1004, the charger output interface 12 positioned below is just inserted into the battery input interface 1002 positioned above;

3. the unmanned aerial vehicle battery 100 can be charged by connecting the power output port 16 with a power supply;

4. two unmanned aerial vehicle batteries 100 are respectively radiated through two first cooling fans 14, electronic components inside the host 113 are radiated through a second cooling fan 15, and the second cooling holes 1133 enable air blown out by the first cooling fans 14 and the second cooling fan 15 to circulate.

The utility model discloses an unmanned aerial vehicle battery charger inserts the unmanned aerial vehicle battery in the constant head tank through opening up, when the unmanned aerial vehicle battery location was placed in the constant head tank, through setting up charger output interface in the top surface of main part to be located one side of constant head tank, and set up, make charger output interface just with be located battery top side, and battery input interface peg graft down, make charger output interface and battery input interface connection convenient.

In summary, although the present invention has been disclosed with reference to the preferred embodiments, the scope of the present invention is not limited thereto, and any person skilled in the art can substitute or change the technical solution of the present invention within the technical scope of the present invention.

Claims

1. The utility model provides an unmanned aerial vehicle battery charger which characterized in that for charge for the unmanned aerial vehicle battery, the top side of unmanned aerial vehicle battery is provided with the lug, the orientation of lug one side of the bottom of unmanned aerial vehicle battery is provided with battery input interface, unmanned aerial vehicle battery charger includes:

a body having a top surface, the body having a detent with an upward facing opening for inserting the UAV battery into the detent, the detent for locating and receiving the UAV battery; and the number of the first and second groups,

2. The UAV battery charger of claim 1, wherein the UAV battery has two guide slots disposed thereon, one on each of two opposite sides of the UAV battery; the guide block is arranged in the positioning groove, the number of the guide blocks is two, the two guide blocks are respectively located on two opposite groove walls in the positioning groove, and the guide blocks are used for being connected with the guide grooves in a sliding mode.

3. The unmanned aerial vehicle battery charger of claim 2, wherein the top end of the guide slot is provided with a limiting block, the guide block is provided with a limiting groove, and the limiting groove is used for limiting the limiting block.

4. The drone battery charger of claim 1, wherein the slot walls of the detents are spaced from the drone battery.

5. The UAV battery charger of claim 1, wherein the top surface has a recess therein, the recess being in communication with the positioning slot for receiving the protrusion, the charger output port being disposed at a bottom of the recess.

6. The drone battery charger of claim 1, wherein the main body includes a main frame and two brackets, the charger output interface being disposed on the main frame, the main frame having two opposing first sides and two opposing second sides; the host is fixed between the two brackets, the two brackets are respectively positioned on the two second sides, the two brackets protrude out of the first side, and the positioning groove is formed between the two brackets.

7. The UAV battery charger of claim 6, wherein two of the brackets protrude from the two first sides to form two of the positioning slots.

8. The drone battery charger of claim 6, further comprising a first heat dissipation fan disposed on the first side with an outlet facing the detent.

9. The UAV battery charger of claim 6, wherein the main body further comprises a heat sink plate connected between the two brackets and disposed opposite to the first side, the heat sink plate having a first heat dissipating hole.

10. The UAV battery charger of claim 6, further comprising a second fan, wherein the main unit is a hollow structure, one of the second sides is provided with a second heat dissipation hole, and the second fan is disposed on the other second side.