CN216624444U - Durable unmanned aerial vehicle battery compartment - Google Patents
Durable unmanned aerial vehicle battery compartment Download PDFInfo
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- CN216624444U CN216624444U CN202123095210.8U CN202123095210U CN216624444U CN 216624444 U CN216624444 U CN 216624444U CN 202123095210 U CN202123095210 U CN 202123095210U CN 216624444 U CN216624444 U CN 216624444U
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- unmanned aerial
- aerial vehicle
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Abstract
The utility model discloses a durable unmanned aerial vehicle battery compartment, which comprises a body; the body is internally provided with an installation cavity with an opening at the front end, a shock absorption layer covers the inner wall of the installation cavity, the side wall of the body is provided with heat dissipation holes communicated with the outside and the inside of the installation cavity, 4 support arms which are distributed at equal angles extend outwards integrally from the periphery of the body, and each support arm is connected with a first reinforcing rib with the side wall of the body; the upper surface of body has a plurality of shock attenuation stopper. Have the buffer layer through the installation cavity inner wall covering to and the upper surface of body has a plurality of shock attenuation stopper, unmanned aerial vehicle's shock attenuation performance has effectively been increased, unmanned aerial vehicle's durability has been strengthened, and each support arm of cooperation all is connected with first strengthening rib with the body lateral wall, the structural strength of support arm can effectively be strengthened to first strengthening rib, prevent that the support arm from taking place to warp at the flight in-process, change the position of screw even, thereby unmanned aerial vehicle flight in-process stability has been guaranteed.
Description
Technical Field
The utility model relates to the field of unmanned aerial vehicles, in particular to a durable unmanned aerial vehicle battery compartment.
Background
An unmanned aircraft, abbreviated as "drone", and abbreviated in english as "UAV", is an unmanned aircraft that is operated by a radio remote control device and a self-contained program control device, or is operated autonomously, either completely or intermittently, by an onboard computer. Drones tend to be more suitable for tasks that are too "fool, dirty, or dangerous" than are manned aircraft. Unmanned aerial vehicles can be classified into military and civil applications according to the application field. For military use, unmanned aerial vehicles divide into reconnaissance aircraft and target drone. In the civil aspect, the unmanned aerial vehicle + the industry application is really just needed by the unmanned aerial vehicle; the unmanned aerial vehicle is applied to the fields of aerial photography, agriculture, plant protection, miniature self-timer, express transportation, disaster relief, wild animal observation, infectious disease monitoring, surveying and mapping, news reporting, power inspection, disaster relief, film and television shooting, romantic manufacturing and the like, the application of the unmanned aerial vehicle is greatly expanded, and developed countries actively expand the industrial application and develop the unmanned aerial vehicle technology.
The support arm on the current unmanned aerial vehicle battery compartment generally directly extends from the body, and the general structural strength of support arm is not high enough, when careless bumps, take place to warp easily, can change the screw position after taking place to warp, thereby influence unmanned aerial vehicle's flight stability, the whole shock attenuation performance in unmanned aerial vehicle battery compartment is not good simultaneously, damage the inside components and parts of battery compartment easily after the bump, make unmanned aerial vehicle's durability relatively poor, therefore, it is necessary to make further improvement to current unmanned aerial vehicle battery compartment structure.
SUMMERY OF THE UTILITY MODEL
In view of the above, the present invention is directed to the defects in the prior art, and a main object of the present invention is to provide a durable battery compartment for unmanned aerial vehicles, which can effectively solve the problems of insufficient structural strength of the support arm, easy influence on flight stability, poor damping performance, and poor durability of the support arm in the conventional battery compartment for unmanned aerial vehicles.
In order to achieve the purpose, the utility model adopts the following technical scheme:
a durable unmanned aerial vehicle battery compartment comprises a body; the body is internally provided with an installation cavity with an opening at the front end, the inner wall of the installation cavity is covered with a damping layer, the side wall of the body is provided with heat dissipation holes communicated with the outside and the inside of the installation cavity, the periphery of the body integrally extends outwards to form 4 supporting arms arranged at equal angles, the outer end of each supporting arm integrally extends upwards to form a connecting rod, and each supporting arm is connected with the side wall of the body through a first reinforcing rib; the upper surface of body has a plurality of shock attenuation stopper, and the shock attenuation stopper sets up with vertical extension.
Preferably, the body is made of polyethylene.
Preferably, the shock absorbing layer is made of rubber.
As an optimal scheme, the lateral wall of body set up with unmanned aerial vehicle support frame fixed connection's first connecting hole, this first connecting hole is for 4 that the equal angle was arranged, and each first connecting hole all is located corresponding the support arm under.
As an optimal scheme, all set up on each support arm with unmanned aerial vehicle processing tool cooperation location's locating hole.
As a preferable scheme, a second connecting hole matched with an unmanned aerial vehicle accessory for fixed installation is formed in the connecting rod.
Preferably, the side wall of the connecting rod is integrally extended with a second reinforcing rib connected with the surface of the corresponding supporting arm.
Preferably, the damping plugs are arranged on the left side and the right side of the upper surface of the body in a left-right symmetry mode.
Compared with the prior art, the utility model has obvious advantages and beneficial effects, and specifically, the technical scheme includes that:
it has the buffer layer to cover through the installation cavity inner wall, and the upper surface of body has a plurality of shock attenuation stopper, the buffer layer can effectively reduce the external collision stress to the inside components and parts of unmanned aerial vehicle battery storehouse after the collision, avoid the collision to cause the damage to the inside components and parts of unmanned aerial vehicle, simultaneously the shock attenuation stopper can weaken the external impact to the unmanned aerial vehicle body, unmanned aerial vehicle's shock attenuation performance has effectively been increased, unmanned aerial vehicle's durability has been strengthened, and each support arm of cooperation all is connected with first strengthening rib with the body lateral wall, the structural strength of support arm can effectively be strengthened to first strengthening rib, prevent that the support arm from taking place to warp at the flight in-process, change the position of screw even, thereby unmanned aerial vehicle flight in-process stability has been guaranteed.
To more clearly illustrate the structural features and effects of the present invention, the present invention will be described in detail below with reference to the accompanying drawings and specific embodiments.
Drawings
FIG. 1 is a schematic perspective view of a preferred embodiment of the present invention;
FIG. 2 is a schematic cross-sectional view of a preferred embodiment of the present invention.
The attached drawings indicate the following:
10. body 101 and mounting cavity
102. Heat dissipation hole 103 and first connection hole
104. Positioning hole 105, second connecting hole
11. Shock-absorbing layer 12 and supporting arm
13. Connecting rod 14 and first reinforcing rib
15. Damping plug 16, second strengthening rib.
Detailed Description
Referring to fig. 1 to 2, a specific structure of a preferred embodiment of the present invention is shown, which includes a body 10.
The unmanned aerial vehicle battery box comprises a body 10, wherein the body 10 is internally provided with an installation cavity 101 with an opening at the front end, the installation cavity 101 is used for installing an unmanned aerial vehicle battery, the inner wall of the installation cavity 101 is covered with a shock-absorbing layer 11, the shock-absorbing layer is used for reducing the collision stress of the external world on accessories such as internal batteries and the like when the unmanned aerial vehicle collides, the accessories inside of the unmanned aerial vehicle are effectively protected, the durability is improved, the side wall of the body 10 is provided with heat dissipation holes 102 communicating the external world with the inside of the installation cavity 101, the heat dissipation function of the unmanned aerial vehicle battery box is enhanced, the problem that the heat generated by the batteries cannot be timely discharged when the unmanned aerial vehicle flies is avoided, so that the internal components of the unmanned aerial vehicle are damaged is solved, meanwhile, the overall quality of the unmanned aerial vehicle battery box can be reduced by the heat dissipation holes 102, the cost of raw materials is reduced, 4 support arms 12 which are arranged at equal angles are integrally and outwards extended from the periphery of the body 10, the outer end of each support arm 12 is integrally extended upwards with a connecting rod 13, and each support arm 12 is connected with the side wall of the body 10 with a first reinforcing rib 14, the first reinforcing ribs 14 are used for enhancing the structural stability of the supporting arms 12 and preventing the supporting arms 12 from deforming when collision occurs, so that the flight attitude of the unmanned aerial vehicle is influenced; the upper surface of the body 10 is provided with a plurality of shock absorption plugs 15, and the shock absorption plugs 15 are arranged in a vertically extending manner; the shock attenuation stopper can reduce external impulsive force to body 10, further strengthens unmanned aerial vehicle's durability.
In this embodiment, the body 10 is made of polyethylene; the shock absorption layer 11 is made of rubber; the side wall of the main body 10 is provided with 4 first connection holes 103 fixedly connected with the unmanned aerial vehicle support frame, the first connection holes 103 are arranged at equal angles, and each first connection hole 103 is located right below the corresponding support arm 12; each supporting arm 12 is provided with a positioning hole 104 matched and positioned with the unmanned aerial vehicle processing jig, so that the main body 10 can be conveniently matched and positioned with the clamps during processing; a second connecting hole 105 matched with an unmanned aerial vehicle accessory for fixed installation is formed in the connecting rod 13; a second reinforcing rib 16 connected with the surface of the corresponding support arm 12 is integrally extended from the side wall of the connecting rod 13, and the second reinforcing rib 16 can prevent the connecting rod 13 from deforming in flight, so that the stability of the overall structure of the unmanned aerial vehicle is enhanced; the damper plugs 15 are disposed on left and right sides of the upper surface of the body 10 in left-right symmetry.
The design of the utility model is characterized in that: it has the buffer layer to cover through the installation cavity inner wall, and the upper surface of body has a plurality of shock attenuation stopper, the buffer layer can effectively reduce the external collision stress to the inside components and parts of unmanned aerial vehicle battery storehouse after the collision, avoid the collision to cause the damage to the inside components and parts of unmanned aerial vehicle, simultaneously the shock attenuation stopper can weaken the external impact to the unmanned aerial vehicle body, unmanned aerial vehicle's shock attenuation performance has effectively been increased, unmanned aerial vehicle's durability has been strengthened, and each support arm of cooperation all is connected with first strengthening rib with the body lateral wall, the structural strength of support arm can effectively be strengthened to first strengthening rib, prevent that the support arm from taking place to warp at the flight in-process, change the position of screw even, thereby unmanned aerial vehicle flight in-process stability has been guaranteed.
The above description is only a preferred embodiment of the present invention, and is not intended to limit the technical scope of the present invention, so that any minor modifications, equivalent changes and modifications made to the above embodiment according to the technical spirit of the present invention are within the technical scope of the present invention.
Claims (8)
1. The utility model provides a durable type unmanned aerial vehicle battery compartment which characterized in that: comprises a body; the body is internally provided with an installation cavity with an opening at the front end, the inner wall of the installation cavity is covered with a damping layer, the side wall of the body is provided with heat dissipation holes communicated with the outside and the inside of the installation cavity, the periphery of the body integrally extends outwards to form 4 supporting arms arranged at equal angles, the outer end of each supporting arm integrally extends upwards to form a connecting rod, and each supporting arm is connected with the side wall of the body through a first reinforcing rib; the upper surface of body has a plurality of shock attenuation stopper, and the shock attenuation stopper sets up with vertical extension.
2. The durable unmanned aerial vehicle battery compartment of claim 1, wherein: the body is made of polyethylene.
3. The durable unmanned aerial vehicle battery compartment of claim 1, wherein: the shock-absorbing layer is made of rubber.
4. The durable unmanned aerial vehicle battery compartment of claim 1, wherein: the lateral wall of body set up with unmanned aerial vehicle support frame fixed connection's first connecting hole, this first connecting hole is for 4 that the equal angle was arranged, and each first connecting hole all is located corresponding the support arm under.
5. The durable unmanned aerial vehicle battery compartment of claim 1, wherein: all set up on each support arm with unmanned aerial vehicle processing tool cooperation location's locating hole.
6. The durable unmanned aerial vehicle battery compartment of claim 1, wherein: and a second connecting hole matched with the unmanned aerial vehicle accessory for fixed installation is formed in the connecting rod.
7. The durable unmanned aerial vehicle battery compartment of claim 1, wherein: and a second reinforcing rib connected with the surface of the corresponding support arm extends out of the side wall of the connecting rod integrally.
8. The durable unmanned aerial vehicle battery compartment of claim 1, wherein: the shock absorption plugs are arranged on the left side and the right side of the upper surface of the body in a bilateral symmetry mode.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
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CN202123095210.8U CN216624444U (en) | 2021-12-10 | 2021-12-10 | Durable unmanned aerial vehicle battery compartment |
Applications Claiming Priority (1)
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CN202123095210.8U CN216624444U (en) | 2021-12-10 | 2021-12-10 | Durable unmanned aerial vehicle battery compartment |
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CN216624444U true CN216624444U (en) | 2022-05-27 |
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CN202123095210.8U Active CN216624444U (en) | 2021-12-10 | 2021-12-10 | Durable unmanned aerial vehicle battery compartment |
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2021
- 2021-12-10 CN CN202123095210.8U patent/CN216624444U/en active Active
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