CN216154052U

CN216154052U - Unmanned aerial vehicle is from locking-type battery structure

Info

Publication number: CN216154052U
Application number: CN202121627024.1U
Authority: CN
Inventors: 胡伟
Original assignee: Shenzhen Iwinsky Intelligent Co ltd
Current assignee: Shenzhen Iwinsky Intelligent Co ltd
Priority date: 2021-07-17
Filing date: 2021-07-17
Publication date: 2022-04-01
Anticipated expiration: 2031-07-17

Abstract

The utility model discloses a self-locking battery structure of an unmanned aerial vehicle, which comprises an unmanned aerial vehicle battery and a battery frame, wherein the bottom of the unmanned aerial vehicle battery is connected with a battery bottom plate, a screw is arranged on the upper surface of the unmanned aerial vehicle battery, the outer wall of the unmanned aerial vehicle battery is connected with a movable plug, the upper end of the battery bottom plate is provided with a power plug, a position adjusting block is arranged at the corner of the unmanned aerial vehicle battery, a power socket is arranged inside the battery frame, the inner wall of the battery frame is provided with a plug groove, the bottom of the battery bottom plate is provided with a square hole, and a connecting column is connected below the square hole, the movable plug is inserted into the plug slot to realize the tight connection of the battery frame and the battery bottom plate.

Description

Unmanned aerial vehicle is from locking-type battery structure

Technical Field

The utility model relates to the field of unmanned aerial vehicle battery structures, in particular to a self-locking battery structure of an unmanned aerial vehicle.

Background

The unmanned plane is called unmanned plane for short, and is an unmanned plane operated by radio remote control equipment and a self-contained program control device. The machine has no cockpit, but is provided with an automatic pilot, a program control device and other equipment. The personnel on the ground, the naval vessel or the mother aircraft remote control station can track, position, remotely control, telemeter and digitally transmit the personnel through equipment such as a radar. The aircraft can take off like a common airplane under the radio remote control or launch and lift off by a boosting rocket, and can also be thrown into the air by a mother aircraft for flying.

Unmanned aerial vehicles are also very common in our lives, and are not mostly unmanned aerial vehicles for aerial photography, and are almost as common as large toys.

However, the problem of batteries of the aerial photography unmanned aerial vehicle is always a headache problem of people, and therefore a self-locking battery structure of the unmanned aerial vehicle is provided.

SUMMERY OF THE UTILITY MODEL

The utility model aims to solve the defects in the prior art, and provides a self-locking battery structure of an unmanned aerial vehicle.

In order to achieve the purpose, the utility model adopts the following technical scheme: the utility model provides an unmanned aerial vehicle is from locking-type battery structure, includes unmanned aerial vehicle battery and battery frame, the bottom of unmanned aerial vehicle battery is connected with the battery bottom plate, the upper surface at unmanned aerial vehicle battery is installed to the screw, be connected with movable plug on the outer wall of unmanned aerial vehicle battery, power plug is installed to the upper end of battery bottom plate, the corner of unmanned aerial vehicle battery is provided with the position control piece, the inside of battery frame is provided with supply socket, be provided with the plug groove on the inner wall of battery frame, the bottom of battery bottom plate is provided with the quad slit, the below of quad slit is connected with the spliced pole.

As a further description of the above technical solution:

the shape of unmanned aerial vehicle battery is the cube bodily form, battery bottom plate fixed connection is in the below of unmanned aerial vehicle battery, the shape of battery bottom plate is square, the size of battery bottom plate is greater than the size of unmanned aerial vehicle battery.

As a further description of the above technical solution:

screw threaded connection is on the surface of unmanned aerial vehicle battery, the quantity of screw is four, and the symmetric distribution is in the corner of unmanned aerial vehicle battery, activity plug swing joint is on the outer wall of unmanned aerial vehicle battery, the spring is installed to the one end of activity plug, can guarantee the reciprocating type activity of activity plug.

As a further description of the above technical solution:

power plug fixed connection is in the upper end of battery bottom plate, power plug's shape is square, power plug's size is less than the size of unmanned aerial vehicle battery, power plug's quantity is two, and the symmetric distribution is in the both sides of unmanned aerial vehicle battery, position control piece fixed connection is in the corner of unmanned aerial vehicle battery, the surface of position control piece is the cambered surface, the quantity of position control piece is a plurality of.

As a further description of the above technical solution:

the battery frame is in a cube shape, the battery frame is hollow, the hollow size of the battery frame is matched with the size of an unmanned aerial vehicle battery, the power sockets are arranged on the surface of the battery frame, the number of the power sockets is two, the power sockets are symmetrically distributed according to the battery frame, and the size of the power sockets is matched with the size of a power plug layer.

As a further description of the above technical solution:

the plug grooves are formed in the inner wall of the battery frame, the number of the plug groove layers is a plurality, the size of each plug groove is matched with that of the corresponding movable plug, and the plug grooves are circular.

As a further description of the above technical solution:

the bottom at battery bottom plate is seted up to the quad slit, the quantity of quad slit is a plurality of, the spliced pole is fixed in the below of movable plug, and passes the quad slit, and the spliced pole can carry out reciprocating motion in the within range of quad slit, and the movable plug that links stretches into or withdraws from the plug groove, makes unmanned aerial vehicle battery and battery frame carry out the joint or separate.

The utility model has the following beneficial effects:

according to the unmanned aerial vehicle battery fixing device, the unmanned aerial vehicle battery can be tightly fixed together by clamping the power socket in the battery frame and the power plug of the battery bottom plate, so that the position of the unmanned aerial vehicle battery can be adjusted, the movable plug is smooth, when the battery frame and the battery bottom plate are buckled with each other, the movable plug can be inserted into the plug groove, the battery frame and the battery bottom plate are tightly connected, the device can be easily disassembled and assembled by manpower and a mechanical arm, the device is very convenient, the device has universality and universality for the unmanned aerial vehicle with the battery installed below, and an all-carbon fiber structure is used, so that the unmanned aerial vehicle battery fixing device has the characteristics of light weight and high strength, and can bear a plurality of batteries.

Drawings

Fig. 1 is a schematic overall structure diagram of a self-locking battery structure of an unmanned aerial vehicle according to the present invention;

fig. 2 is a schematic structural diagram of a battery frame of a self-locking battery structure of an unmanned aerial vehicle according to the present invention;

fig. 3 is a bottom view of an unmanned aerial vehicle battery with a self-locking battery structure of the unmanned aerial vehicle provided by the utility model.

Illustration of the drawings:

1. an unmanned aerial vehicle battery; 2. a battery chassis; 3. a screw; 4. a movable plug; 5. a power plug; 6. a position adjusting block; 7. a battery frame; 8. a power socket; 9. a plug slot; 10. a square hole; 11. connecting columns.

Detailed Description

The technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only a part of the embodiments of the present invention, and not all of the embodiments. All other embodiments, which can be derived by a person skilled in the art from the embodiments given herein without making any creative effort, shall fall within the protection scope of the present invention.

In the description of the present invention, it should be noted that the terms "center", "upper", "lower", "left", "right", "vertical", "horizontal", "inner", "outer", etc., indicate orientations or positional relationships based on the orientations or positional relationships shown in the drawings, and are only for convenience of description and simplicity of description, but do not indicate or imply that the device or element being referred to must have a particular orientation, be constructed and operated in a particular orientation, and thus, should not be construed as limiting the present invention; the terms "first," "second," and "third" are used for descriptive purposes only and are not to be construed as indicating or implying relative importance, and furthermore, unless otherwise explicitly stated or limited, the terms "mounted," "connected," and "connected" are to be construed broadly and may be, for example, fixedly connected, detachably connected, or integrally connected; can be mechanically or electrically connected; they may be connected directly or indirectly through intervening media, or they may be interconnected between two elements. The specific meanings of the above terms in the present invention can be understood in specific cases to those skilled in the art.

Referring to fig. 1-3, one embodiment of the present invention is provided: the utility model provides an unmanned aerial vehicle is from locking-type battery structure, including unmanned aerial vehicle battery 1 and battery frame 7, the bottom of unmanned aerial vehicle battery 1 is connected with battery bottom plate 2, screw 3 installs the upper surface at unmanned aerial vehicle battery 1, be connected with movable plug 4 on unmanned aerial vehicle battery 1's the outer wall, power plug 5 is installed to battery bottom plate 2's upper end, unmanned aerial vehicle battery 1's corner is provided with position control piece 6, battery frame 7's inside is provided with supply socket 8, be provided with plug socket 9 on battery frame 7's the inner wall, battery bottom plate 2's bottom is provided with quad slit 10, the below of quad slit 10 is connected with spliced pole 11.

According to the unmanned aerial vehicle battery 1, the unmanned aerial vehicle battery 1 is cubic, the battery bottom plate 2 is fixedly connected below the unmanned aerial vehicle battery 1, the battery bottom plate 2 is square, the size of the battery bottom plate 2 is larger than that of the unmanned aerial vehicle battery 1, the battery bottom plate 2 can ensure the stability of the unmanned aerial vehicle battery 1, and the unmanned aerial vehicle battery cannot shake in the installation process.

Screw 3 threaded connection is on unmanned aerial vehicle battery 1's surface, and the quantity of screw 3 is four, and the symmetric distribution is in unmanned aerial vehicle battery 1's corner, and movable plug 4 swing joint is on unmanned aerial vehicle battery 1's outer wall, and the spring is installed to movable plug 4's one end, can guarantee the reciprocating type activity of movable plug 4, and spring and movable plug 4 combine together, can guarantee movable plug 4's activity, can easily carry out reciprocating type motion.

Power plug 5 fixed connection is in the upper end of battery bottom plate 2, power plug 5's shape is square, power plug 5's size is less than unmanned aerial vehicle battery 1's size, power plug 5's quantity is two, the symmetric distribution is in unmanned aerial vehicle battery 1's both sides, 6 fixed connection of position control piece are in unmanned aerial vehicle battery 1's edge, position control piece 6's surface is the cambered surface, position control piece 6's quantity is a plurality of, power plug 5's setting can combine together with supply socket 8, realize unmanned aerial vehicle battery 1's installation, position control piece 6's setting can increase unmanned aerial vehicle battery 1's stability, can prevent unmanned aerial vehicle battery 1 activity when the installation.

Battery frame 7 shape is the cube bodily form, battery frame 7's inside is hollow, battery frame 7 hollow size and unmanned aerial vehicle battery 1's size looks adaptation, supply socket 8 sets up on battery frame 7's surface, supply socket 8's quantity is two, and according to battery frame 7 symmetric distribution, supply socket 8's size and 5 layers of size looks adaptations of power plug, through battery frame 7 and unmanned aerial vehicle battery 1's mutual gomphosis, just can fix unmanned aerial vehicle battery 1.

Plug groove 9 is seted up on battery frame 7's inner wall, and plug groove 9 layer quantity is a plurality of, and plug groove 9's size and movable plug 4's size looks adaptation, and plug groove 9 is circular, and through the plug groove 9 set up the convenient movable plug 4's of inserting, can consolidate unmanned aerial vehicle battery 1.

Square hole 10 sets up in the bottom of battery bottom plate 2, and the quantity of square hole 10 is a plurality of, spliced pole 11 is fixed in the below of movable plug 4, and passes square hole 10, and spliced pole 11 can carry out reciprocating motion at the within range of square hole, and linkage movable plug 4 stretches into or withdraws from plug groove 9, makes unmanned aerial vehicle battery 1 and battery frame 7 join or separate, through square hole 10 and spliced pole 11's setting, can make unmanned aerial vehicle battery 1 and organism install, and square hole 10 leaves certain installation space, makes things convenient for unmanned aerial vehicle battery 1 to adjust.

The working principle and the using process thereof are as follows: when the user need install unmanned aerial vehicle battery 1, at first combine together unmanned aerial vehicle battery 1 and battery bottom plate 2, then detain power plug 5 and supply socket 8 mutually together, make it form a whole, during movable plug 4 inserts plug slot 9 automatically under the effect of spring, accomplish above-mentioned operation after, unmanned aerial vehicle battery 1 and battery bottom plate 2 just combine to accomplish the installation battery operation together tightly.

Finally, it should be noted that: although the present invention has been described in detail with reference to the foregoing embodiments, it will be apparent to those skilled in the art that modifications may be made to the embodiments or portions thereof without departing from the spirit and scope of the utility model.

Claims

1. The utility model provides an unmanned aerial vehicle is from locking-type battery structure, includes unmanned aerial vehicle battery (1) and battery frame (7), screw (3), its characterized in that: the bottom of unmanned aerial vehicle battery (1) is connected with battery bottom plate (2), the upper surface at unmanned aerial vehicle battery (1) is installed in screw (3), be connected with movable plug (4) on the outer wall of unmanned aerial vehicle battery (1), power plug (5) are installed to the upper end of battery bottom plate (2), the corner of unmanned aerial vehicle battery (1) is provided with position control piece (6), the inside of battery frame (7) is provided with supply socket (8), be provided with plug groove (9) on the inner wall of battery frame (7), the bottom of battery bottom plate (2) is provided with quad slit (10), the below of quad slit (10) is connected with spliced pole (11).

2. The self-locking battery structure of the unmanned aerial vehicle according to claim 1, wherein: the shape of the unmanned aerial vehicle battery (1) is cubic, the battery bottom plate (2) is fixedly connected below the unmanned aerial vehicle battery (1), the shape of the battery bottom plate (2) is square, and the size of the battery bottom plate (2) is larger than that of the unmanned aerial vehicle battery (1).

3. The self-locking battery structure of the unmanned aerial vehicle according to claim 1, wherein: screw (3) threaded connection is on the surface of unmanned aerial vehicle battery (1), the quantity of screw (3) is four, and the symmetric distribution is in the corner of unmanned aerial vehicle battery (1), activity plug (4) swing joint is on the outer wall of unmanned aerial vehicle battery (1), the spring is installed to the one end of activity plug (4), can guarantee the reciprocating type activity of activity plug (4).

4. The self-locking battery structure of the unmanned aerial vehicle according to claim 1, wherein: attaching plug (5) fixed connection is in the upper end of battery bottom plate (2), the shape of attaching plug (5) is square, the size of attaching plug (5) is less than the size of unmanned aerial vehicle battery (1), the quantity of attaching plug (5) is two, and the symmetric distribution is in the both sides of unmanned aerial vehicle battery (1), position control piece (6) fixed connection is in the edge of unmanned aerial vehicle battery (1), the surface of position control piece (6) is the cambered surface, the quantity of position control piece (6) is a plurality of.

5. The self-locking battery structure of the unmanned aerial vehicle according to claim 1, wherein: the battery frame (7) is in a cube shape, the battery frame (7) is hollow, the hollow size of the battery frame (7) is matched with that of the unmanned aerial vehicle battery (1), the power sockets (8) are arranged on the surface of the battery frame (7), the number of the power sockets (8) is two, the power sockets are symmetrically distributed according to the battery frame (7), and the size of the power sockets (8) is matched with that of the power plug (5).

6. The self-locking battery structure of the unmanned aerial vehicle according to claim 1, wherein: the plug grooves (9) are formed in the inner wall of the battery frame (7), the number of the plug groove (9) layers is a plurality, the size of each plug groove (9) is matched with that of the movable plug (4), and the plug grooves (9) are circular.

7. The self-locking battery structure of the unmanned aerial vehicle according to claim 1, wherein: square hole (10) are seted up in the bottom of battery bottom plate (2), the quantity of square hole (10) is a plurality of, spliced pole (11) are fixed in the below of activity plug (4), and pass square hole (10), and reciprocating motion can be carried out in the within range of square hole in spliced pole (11), and linkage activity plug (4) stretch into or withdraw from plug groove (9), makes unmanned aerial vehicle battery (1) and battery frame (7) joint or separation.