CN210912877U

CN210912877U - Unmanned aerial vehicle battery structure of arranging

Info

Publication number: CN210912877U
Application number: CN201921577420.0U
Authority: CN
Inventors: 朱秋阳
Original assignee: Shenzhen Xiangnong Innovation Technology Co ltd
Current assignee: Shenzhen Xiangnong Innovation Technology Co ltd
Priority date: 2019-09-20
Filing date: 2019-09-20
Publication date: 2020-07-03
Anticipated expiration: 2029-09-20

Abstract

The utility model discloses an unmanned aerial vehicle battery structure of arranging belongs to the unmanned aerial vehicle field. The utility model discloses an unmanned aerial vehicle battery structure of arranging includes the main part, the front-mounted of main part has first battery, the second battery is installed at the rear portion of main part, first battery with second battery symmetry set up in the main part. The utility model discloses an unmanned aerial vehicle battery structure of arranging has reserved more installation space for the fuselage middle part, helps reducing unmanned aerial vehicle's whole volume.

Description

Unmanned aerial vehicle battery structure of arranging

Technical Field

The utility model belongs to the technical field of the unmanned air vehicle technique and specifically relates to an unmanned aerial vehicle battery structure of arranging.

Background

In order to satisfy the normal motion of the drone, the battery of the drone is generally large in volume and weight. At present, the mounting means of unmanned aerial vehicle battery is in the middle part position of installing the fuselage of unmanned aerial vehicle with the battery is concentrated in the market to unmanned aerial vehicle's middle part position department often still needs some load modules of carrying on, leads to unmanned aerial vehicle's whole volume too big.

SUMMERY OF THE UTILITY MODEL

In order to solve the not enough of prior art, the embodiment of the utility model provides an unmanned aerial vehicle battery structure of arranging can reserve more installation space for unmanned aerial vehicle fuselage middle part.

The embodiment of the utility model provides a solve the technical scheme who above-mentioned technical problem took and be: the utility model provides an unmanned aerial vehicle battery arrangement structure, includes the main part, the forward-mounted of main part has first battery, the second battery is installed at the rear portion of main part, first battery with the second battery symmetry set up in the main part.

As a further improvement of the above technical solution, the battery pack includes a plurality of first batteries, and the number of the second batteries is equal to the number of the first batteries.

As a further improvement of the above technical solution, the first battery and the second battery are connected in parallel.

As a further improvement of the technical scheme, a hollow cavity is arranged in the middle of the main body.

As a further improvement of the above technical solution, a first battery compartment for accommodating the first battery is provided at the front of the main body.

As a further improvement of the above technical scheme, first battery compartment includes first loading face, first fender face and first spigot surface, first loading face is located the bottom of first battery, first fender face is located both sides around the first battery, just first fender face is located the upper portion of first battery, first spigot surface is located the left and right sides of first battery is from last to down, is located two of the first battery left and right sides distance between the first spigot surface reduces gradually.

As a further improvement of the above technical solution, a first positioning claw is disposed on the first bearing surface, and the first positioning claw is disposed on the front side and the rear side of the first battery.

As a further improvement of the above technical solution, a second battery compartment for accommodating the second battery is provided at the rear of the main body.

As a further improvement of the above technical solution, the second battery compartment includes a second bearing surface, a second stop surface and a second guide surface, the second bearing surface is located at the bottom of the second battery, the second stop surface is located at the front and rear sides of the second battery, the second stop surface is located at the upper portion of the second battery, the second guide surface is located at the left and right sides of the second battery, from top to bottom, is located at two of the left and right sides of the second battery, and the distance between the second guide surfaces is gradually reduced.

As a further improvement of the above technical solution, a second positioning claw is disposed on the second bearing surface, and the second positioning claw is disposed on the front side and the rear side of the second battery.

The utility model has the advantages that:

the utility model discloses an unmanned aerial vehicle battery structure of arranging includes the main part, the front-mounted of main part has first battery, the second battery is installed at the rear portion of main part, first battery with second battery symmetry set up in the main part. The utility model discloses an unmanned aerial vehicle battery structure of arranging, the space at fuselage middle part is not taken in arranging of first battery and second battery, has reserved more installation space for the fuselage middle part, helps reducing unmanned aerial vehicle's whole volume.

Drawings

The present invention will be further explained with reference to the drawings and examples.

Fig. 1 is a schematic structural view of an embodiment of a bottom view angle of an unmanned aerial vehicle battery arrangement structure of the present invention;

fig. 2 is the utility model discloses the structural schematic diagram of an embodiment of unmanned aerial vehicle battery arrangement structure top visual angle.

Detailed Description

The conception, specific structure and technical effects of the present invention will be described clearly and completely with reference to the accompanying drawings and embodiments, so as to fully understand the objects, aspects and effects of the present invention. It should be noted that the embodiments and features of the embodiments in the present application may be combined with each other without conflict.

It should be noted that, unless otherwise specified, when a feature is referred to as being "fixed" or "connected" to another feature, it may be directly fixed or connected to the other feature or indirectly fixed or connected to the other feature. Furthermore, the description of the upper, lower, left, right, front, rear, etc. used in the present invention is only relative to the mutual position relationship of the components of the present invention in the drawings.

Furthermore, unless defined otherwise, all technical and scientific terms used herein have the same meaning as commonly understood by one of ordinary skill in the art. The terminology used in the description herein is for the purpose of describing particular embodiments only and is not intended to be limiting of the invention. As used herein, the term "and/or" includes any combination of one or more of the associated listed items.

Referring to fig. 1, the utility model provides an unmanned aerial vehicle battery structure of arranging, including main part 1, be equipped with first battery 2 in the front portion of main part 1, be equipped with second battery 3 at the rear portion of main part 1, first battery 2 sets up on main part 1 with second battery 3 symmetry.

The first cell 2 and the second cell 3 are symmetrically arranged by taking the gravity center of the main body 1 as a symmetrical point, so that the arrangement structure of the first cell 2 and the second cell 3 does not affect the balance of the main body 1.

In one embodiment, the first battery 2 includes a number of second batteries 3, and for this, the number of the second batteries 3 is equal to the number of the first batteries 2 to ensure that the first batteries 2 and the second batteries 3 are symmetrical about the center of gravity of the main body 1.

Preferably, first battery 2 and second battery 3 adopt parallel mode to be connected, and at the during operation, can choose for use first battery 2 or second battery 3 as main power supply for unmanned aerial vehicle power supply, another power is as stand-by power supply, and when one of them power broke down, another power still can provide continuation of the journey for unmanned aerial vehicle.

Since the first battery 2 and the second battery 3 are respectively located at the front side and the rear side of the main body 1, the batteries are mounted without occupying the middle portion of the main body 1, and in addition, in a preferred embodiment, as shown in fig. 2, a hollow cavity 10 is disposed at the middle portion of the main body 1, more mounting space can be reserved by the arrangement of the hollow cavity 10, and the weight of the main body 1 can be remarkably reduced.

Further, as shown in fig. 1, in one embodiment, a first battery compartment 4 is provided at the front of the main body 1 for accommodating the first battery 2. Wherein, the first battery compartment 4 includes a first carrying surface 40, a first blocking surface 41 and a first guiding surface 42, the first carrying surface 40 is located at the bottom of the first battery 2, the first carrying surface 40 plays a role of carrying the first battery 2, the first blocking surfaces 41 are located at the front and rear sides of the first battery 2, the first blocking surfaces 41 are located at the upper portion of the first battery 2, the distance between the two first blocking surfaces 41 is greater than the thickness of the first battery 2, so that the first battery 2 is placed between the two first blocking surfaces 41 from the upper portions of the two first blocking surfaces 41, the first guiding surfaces 42 are located at the left and right sides of the first battery 2, the distance between the two first guiding surfaces 42 is gradually reduced from top to bottom to form a guiding structure, wherein the upper portion of the first guiding surface 42 is connected with the end portion of the first blocking surface 41, the lower portion of the first guiding surface 42 is connected with the first carrying surface 40, in the process of placing the first battery 2, the first guide surface 42 guides the movement of the first battery 2, and ensures that the first battery 2 is embedded in the range of the first bearing surface 40.

Preferably, the first bearing surface 40 is provided with a first positioning claw 400, the first positioning claw 400 extends upwards from the first bearing surface 40 and is arranged at the front side and the rear side of the first battery 2, and the first battery 2 is clamped by the first positioning claw 400, so that the installation tightness of the first battery 2 is ensured. The first positioning claw 400 is preferably elastic, and the upper portion of the first positioning claw 400 is preferably in a circular arc shape, so as to ensure that the first battery 2 can smoothly enter the first bearing surface 40 and be stably mounted in the range of the first bearing surface 40.

In one embodiment, the rear of the main body 1 is provided with a second battery compartment 5 for accommodating a second battery 3. Wherein, the second battery compartment 5 includes a second bearing surface 50, a second blocking surface 51 and a second guiding surface 52, the second bearing surface 50 is located at the bottom of the second battery 3, the second bearing surface 50 plays a role of bearing the second battery 3, the second blocking surfaces 51 are located at the front and rear sides of the second battery 3, the second blocking surfaces 51 are located at the upper portion of the second battery 3, the distance between the two second blocking surfaces 51 is greater than the thickness of the second battery 3, so that the second battery 3 is placed between the two second blocking surfaces 51 from the upper portions of the two second blocking surfaces 51, the second guiding surfaces 52 are located at the left and right sides of the second battery 3, the distance between the two second guiding surfaces 52 is gradually reduced from top to bottom to form a guiding structure, wherein the upper portion of the second guiding surface 52 is connected with the end portion of the second blocking surface 51, the lower portion of the second guiding surface 52 is connected with the second bearing surface 50, in the process of placing the second battery 3, the second guiding surface 52 guides the movement of the second battery 3, and ensures that the second battery 3 is embedded in the second bearing surface 50.

Preferably, the second bearing surface 50 is provided with a second positioning claw 500, the second positioning claw 500 extends upwards from the second bearing surface 50 and is arranged at the front side and the rear side of the second battery 3, and the second battery 3 is clamped by the second positioning claw 500, so as to ensure the installation tightness of the second battery 3. The second positioning pawl 500 is preferably elastic, and the upper portion of the second positioning pawl 500 is preferably in a circular arc shape, so as to ensure that the second battery 3 can smoothly enter the second bearing surface 50 and be stably mounted in the range of the second bearing surface 50.

While the invention has been described with reference to a preferred embodiment, it will be understood by those skilled in the art that various changes in form and details may be made therein without departing from the spirit and scope of the invention as defined by the appended claims.

Claims

1. The utility model provides an unmanned aerial vehicle battery arrangement structure, a serial communication port, includes the main part, the forward-mounted of main part has first battery, the second battery is installed at the rear portion of main part, first battery with the second battery symmetry set up in the main part.

2. The unmanned aerial vehicle battery arrangement of claim 1, comprising a number of the first batteries, the number of the second batteries being equal to the number of the first batteries.

3. The unmanned aerial vehicle battery arrangement of claim 2, wherein the first battery is connected in parallel with the second battery.

4. The unmanned aerial vehicle battery arrangement of claim 1, wherein a hollow cavity is provided in a middle portion of the main body.

5. The unmanned aerial vehicle battery arrangement of any of claims 1-4, wherein a front portion of the main body is provided with a first battery compartment for housing the first battery.

6. The unmanned aerial vehicle battery arrangement of claim 5, wherein the first battery compartment comprises a first bearing surface, a first blocking surface and a first guide surface, the first bearing surface is located at the bottom of the first battery, the first blocking surface is located at the front side and the rear side of the first battery, the first blocking surface is located at the upper portion of the first battery, the first guide surface is located at the left side and the right side of the first battery, and the distance between the two first guide surfaces located at the left side and the right side of the first battery is gradually reduced from top to bottom.

7. The unmanned aerial vehicle battery arrangement of claim 6, wherein the first carrying surface is provided with a first positioning claw, and the first positioning claw is provided on a front side and a rear side of the first battery.

8. The unmanned aerial vehicle battery arrangement of any of claims 1-4, wherein a rear portion of the main body is provided with a second battery compartment for housing the second battery.

9. The unmanned aerial vehicle battery arrangement of claim 8, wherein the second battery compartment includes a second bearing surface, a second retaining surface and a second guide surface, the second bearing surface is located at a bottom of the second battery, the second retaining surface is located at front and rear sides of the second battery, the second retaining surface is located at an upper portion of the second battery, the second guide surface is located at left and right sides of the second battery, and a distance between two of the second guide surfaces located at left and right sides of the second battery is gradually reduced from top to bottom.

10. The unmanned aerial vehicle battery arrangement of claim 9, wherein a second positioning claw is disposed on the second bearing surface, and the second positioning claw is disposed on a front side and a rear side of the second battery.