Power management device for unmanned aerial vehicle

Abstract

The utility model relates to the field of unmanned aerial vehicles, and particularly discloses an unmanned aerial vehicle power supply management device, which comprises a storage mechanism, the storage mechanism comprises a placement bin and a power supply bin, two mounting slots are arranged in the placement bin, and a charging mechanism is arranged on one side, close to the power supply bin, of each mounting slot and located on the inner side wall of the placement bin. The charging mechanism comprises a warping plate and a movable lug plate, electric guide plates are mounted at the two ends of the warping plate and correspond to the inner sides of the two mounting slots, positioning sockets are formed in the electric guide plates, inserting buckles are mounted at the positions, corresponding to the positioning sockets, of the inner side wall of the placement bin, and charging connectors are mounted on the rear surfaces of the electric guide plates and correspond to the inner side wall of the placement bin. According to the unmanned aerial vehicle, the battery can be circularly charged and stored through an arranged storage bin, the endurance of the unmanned aerial vehicle is prolonged, an electric guide plate integrally drives a warping plate and a movable lug plate to rotate, a positioning insertion opening in the electric guide plate is buckled into the outer side of an insertion buckle, the situation of open circuit is avoided, and the temperature of the stored battery can be guaranteed under the action of a positioning round ball.

Description

TECHNICAL FIELD

[0001] The utility model relates to unmanned plane field, concretely is a kind of unmanned plane power management device. BACKGROUND

[0002] With the rapid development of unmanned plane industry, higher requirements are put forward to unmanned plane power, because power supply is the source power of unmanned plane work, the life of power supply directly determines the working life of unmanned plane, since the power consumption of unmanned plane user is relatively rapid, usually adopt to carry spare battery to switch power supply, but the number of spare battery carried in the internal storage mechanism of unmanned plane is limited, and the battery after disassembly cannot be charged, therefore the needs of unmanned plane cannot be guaranteed. INVENTION CONTENTS

[0003] In view of the deficiencies of the prior art, the utility model provides a kind of unmanned plane power management device, solve the problem mentioned in the above background.

[0004] The utility model provides the following technical scheme: a kind of unmanned plane power management device, including storage mechanism, the storage mechanism includes: placement warehouse, power supply store, the inside of the placement warehouse is provided with two installation slot, two the installation slot is close to the side of the power supply store and is located in the inside wall of the placement warehouse installation charging mechanism, the charging mechanism includes: hinged plate, movable ear plate, the both ends of the hinged plate correspond the inside of two installation slot are equipped with electrically conductive plate, the electrically conductive plate is equipped with positioning socket, the inside wall of the placement warehouse is equipped with snap buckle in the position corresponding the positioning socket, the rear surface of the electrically conductive plate is equipped with charging connector in the inside wall of the placement warehouse.

[0005] As a further scheme of the utility model: the inside of the power supply store is provided with battery, and the outside wall of the power supply store is equipped with electric lead.

[0006] As a further scheme of the utility model: the inside of the installation slot is equipped with positioning ball, and the front surface of the placement warehouse is equipped with closure plate.

[0007] As a further scheme of the utility model: the movable ear plate and the hinged plate are equipped with shaft, and the hinged plate is insulating material member.

[0008] As a further scheme of the utility model: the snap buckle and the positioning socket are connected.

[0009] As a further scheme of the utility model: the battery and the charging connector are electrically connected.

[0010] As a further scheme of the utility model: the electrically conductive plate and the hinged plate are fixedly connected.

[0011] As a further scheme of the utility model: spring is installed between the positioning ball and the installation slot, and the hinge is installed between the closed plate and the placing bin.

[0012] Compared with the prior art, the utility model has the beneficial effects that:

[0013] The placing bin can realize the cyclic charging and storage of the battery and the backup battery, increase the endurance time of the unmanned aerial vehicle, and drive the hinged plate and the movable ear plate to rotate as a whole. BRIEF DESCRIPTION OF DRAWINGS

[0014] Figure 1 It is a structural schematic view of an unmanned aerial vehicle power management device.

[0015] Figure 2 It is a structural schematic view of a placing bin in an unmanned aerial vehicle power management device.

[0016] Figure 3 It is a structural schematic view of a charging mechanism in an unmanned aerial vehicle power management device.

[0017] Figure 4 It is a sectional view of a storage mechanism in an unmanned aerial vehicle power management device.

[0018] Figure 5 It is a front view of a storage mechanism in an unmanned aerial vehicle power management device.

[0019] In the figure: 1, storage mechanism; 2, placing bin; 3, power supply bin; 4, closed plate; 5, power supply wire; 6, charging mechanism; 201, installation slot; 202, positioning ball; 301, storage battery; 601, hinged plate; 602, movable ear plate; 603, electric guide plate; 604, positioning socket; 605, plug; 606, rotating shaft; 607, charging connector. DETAILED DESCRIPTION

[0020] The technical scheme in the embodiments of the utility model will be clearly and completely described below with reference to the drawings in the embodiments of the utility model. Obviously, the described embodiments are only part of the embodiments of the utility model, rather than all the embodiments. Based on the embodiments in the utility model, all other embodiments obtained by those skilled in the art without creative labor fall within the protection scope of the utility model.

[0021] For example, Figures 1-5As shown, the unmanned aerial vehicle power management device provided by the embodiment comprises a storage mechanism 1, which comprises a placing bin 2 and a power supply bin 3. The inside of the placing bin 2 is provided with two mounting slots 201. The two mounting slots 201 are close to one side of the power supply bin 3. A charging mechanism 6 is mounted on the inside wall of the placing bin 2. The charging mechanism 6 comprises a flap 601 and a movable lug plate 602. The flap 601 is made of insulating material. A rotating shaft 606 is mounted between the flap 601 and the movable lug plate 602. The two ends of the flap 601 are provided with electrically conductive plates 603 corresponding to the inside of the two mounting slots 201. The electrically conductive plates 603 are fixedly connected with the flap 601. A positioning socket 604 is formed in the electrically conductive plate 603. A clasp 605 is mounted on the inside wall of the placing bin 2 corresponding to the position of the positioning socket 604. The clasp 605 is clamped with the positioning socket 604. A charging connector 607 is mounted on the rear surface of the electrically conductive plate 603 corresponding to the inside wall of the placing bin 2.

[0022] As shown, Figures 2-3 In the embodiment, a storage battery 301 is arranged in the inside of the power supply bin 3. The storage battery 301 is electrically connected with the charging connector 607. An electrically connected wire 5 is mounted on the outside wall of the power supply bin 3. A positioning ball 202 is arranged in the inside of the mounting slot 201. A spring is arranged between the positioning ball 202 and the mounting slot 201. A closing plate 4 is mounted on the front surface of the placing bin 2. The closing plate 4 is arranged between the placing bin 2 and the hinge.

[0023] The working principle of the utility model is as follows: when in use, the storage mechanism 1 is integrally arranged with the storage mechanism of the unmanned aerial vehicle. In preparation for work, the storage battery 301 is fully charged by connecting an external power supply to the electrically connected wire 5. When the power of the unmanned aerial vehicle is consumed, the battery is replaced. The battery that has been consumed is pushed into the inside of one of the mounting slots 201. The battery is limited by the positioning ball 202. When the battery is integrally inserted, the end with the charging connector is in contact with the electrically conductive plate 603. The electrically conductive plate 603 drives the flap 601 to rotate by the rotating shaft 606 and the movable lug plate 602. The electrically conductive plate 603 is in contact with the charging connector 607. The positioning socket 604 on the electrically conductive plate 603 is buckled into the outside of the clasp 605 to avoid the occurrence of a broken circuit. The electrically conductive path of the storage battery 301, the charging connector 607 and the battery is connected. The charging process is completed. When the power of the replaced battery is consumed again, the replaced battery is inserted into the inside of the idle mounting slot 201. The battery that is internally charged is ejected under the action of the flap 601. Therefore, the endurance time of the unmanned aerial vehicle can be increased.

[0024] It is to be noted that, in the present text, relational terms such as first and second and the like can be used solely to distinguish one entity or action from another entity or action without necessarily requiring or implying any actual such relationship or order between such entities or actions, and the terms "comprises", "comprising", or any other variation thereof, are intended to cover a non-exclusive inclusion, such that a process, method, article, or apparatus that comprises a list of elements does not include only those elements but can also include other elements not expressly listed or inherent to such process, method, article, or apparatus.

[0025] While the embodiments of the present application have been illustrated and described, it will be understood by those skilled in the art that various changes, modifications, substitutions, and alterations can be made therein without departing from the spirit and scope of the application, which is defined by the appended claims and their equivalents.

Claims

1. A power management device for unmanned aerial vehicles comprising a housing mechanism (1), characterized in that, The accommodation mechanism (1) includes: a placing bin (2), a power supply bin (3), the inside of the placing bin (2) is provided with two installation slots (201), two installation slots (201) are close to the side of the power supply bin (3), the inside wall of the placing bin (2) is provided with a charging mechanism (6), the charging mechanism (6) includes: a hinged plate (601), a movable ear plate (602), both ends of the hinged plate (601) are provided with electrically conductive plates (603) corresponding to the inside of two installation slots (201), the electrically conductive plates (603) are provided with positioning sockets (604), the inside wall of the placing bin (2) is provided with a buckle (605) corresponding to the position of the positioning socket (604), the rear surface of the electrically conductive plate (603) is provided with a charging connector (607) corresponding to the inside wall of the placing bin (2), the inside of the power supply bin (3) is provided with a battery (301), the outside wall of the power supply bin (3) is provided with an electric wire (5).

2. The power management device for unmanned aerial vehicle according to claim 1, wherein, The inside of the installation slot (201) is provided with a positioning ball (202), the front surface of the placing bin (2) is provided with a sealing plate (4).

3. The power management device for unmanned aerial vehicle according to claim 1, wherein, The movable ear plate (602) and the hinged plate (601) are provided with a rotating shaft (606), the hinged plate (601) is an insulating material member.

4. The power management device for unmanned aerial vehicle according to claim 1, wherein, The buckle (605) and the positioning socket (604) are clamped.

5. The power management device for unmanned aerial vehicle according to claim 1, wherein, The battery (301) and the charging connector (607) are electrically connected.

6. The power management device for unmanned aerial vehicle according to claim 1, wherein, The electrically conductive plate (603) and the hinged plate (601) are fixedly connected.

7. The power management device for UAV of claim 2, wherein, The positioning ball (202) and the installation slot (201) are provided with a spring, the sealing plate (4) and the placing bin (2) are provided with a hinge.

Images