CN211336428U - Unmanned aerial vehicle for environment detection - Google Patents
Unmanned aerial vehicle for environment detection Download PDFInfo
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- CN211336428U CN211336428U CN201922346789.7U CN201922346789U CN211336428U CN 211336428 U CN211336428 U CN 211336428U CN 201922346789 U CN201922346789 U CN 201922346789U CN 211336428 U CN211336428 U CN 211336428U
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- aerial vehicle
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Abstract
The utility model relates to an environmental detection uses unmanned aerial vehicle, including the unmanned aerial vehicle base, the gaseous collector of environmental protection, the wing, camera and unmanned aerial vehicle frame, elevating gear's top is provided with the gaseous collector of environmental protection, evenly be provided with a plurality of wing mounting bracket on the periphery in the unmanned aerial vehicle base outside, be provided with the wing on the wing mounting bracket, be provided with the camera mount pad on the periphery of unmanned aerial vehicle base between the adjacent wing mounting bracket, camera mount pad internal fixation is provided with the camera, the bottom of the unmanned aerial vehicle base between the adjacent wing mounting bracket is all connected and is provided with the enhancement connecting rod, the setting is in the bottom position of unmanned aerial vehicle base in the unmanned aerial vehicle frame connection, the bottom of unmanned aerial vehicle frame is connected. The utility model discloses an unmanned aerial vehicle base, unmanned aerial vehicle frame, the setting of strengthening connecting rod and reinforcement loop bar isotructure for unmanned aerial vehicle overall structure's fastness and stability are stronger.
Description
Technical Field
The utility model relates to an environmental detection correlation technique field especially relates to an environmental detection uses unmanned aerial vehicle.
Background
At present, the requirement of cities on the environment is higher and higher, the intensity of environment detection is increased, the original environment monitoring is a fixed point position relatively, and the covered point and surface are not complete. Utilize unmanned aerial vehicle to carry out environmental monitoring among the prior art, utilize unmanned aerial vehicle as the carrier, carry on small-size ambient gas check out test set, can be diversified, the nimble real-time supervision in no dead angle. However, the center of gravity of the airplane is correspondingly raised when the mounting position of the gas collector of the general unmanned aerial vehicle is higher than the wings, so that the wind resistance and the flight safety coefficient of the unmanned aerial vehicle are reduced; meanwhile, the general unmanned aerial vehicle has higher requirements on the weight of the carrying equipment, and the weight is large, so that the flight time of the unmanned aerial vehicle is greatly influenced.
In view of the above-mentioned drawbacks, the present designer has made active research and innovation to create an environment-inspecting unmanned aircraft with industrial utility.
SUMMERY OF THE UTILITY MODEL
In order to solve the technical problem, the utility model aims at providing an environment detects uses unmanned aerial vehicle.
In order to achieve the above purpose, the utility model adopts the following technical scheme:
an unmanned aerial vehicle for environmental detection comprises an unmanned aerial vehicle base, an environment-friendly gas collector, wings, a camera and an unmanned aerial vehicle frame, wherein the unmanned aerial vehicle base is of a cylindrical structure, a mounting hole is formed in the middle of the unmanned aerial vehicle base, a lifting device is arranged in the mounting hole, the environment-friendly gas collector is arranged at the top of the lifting device, a plurality of wing mounting frames are uniformly arranged on the circumferential surface of the outer side of the unmanned aerial vehicle base, the first ends of the wing mounting frames are connected with the unmanned aerial vehicle base, the second ends of the wing mounting frames are connected with the wing mounting seats, the wings are arranged on the wing mounting seats, the camera mounting seats are arranged on the circumferential surface of the unmanned aerial vehicle base between the adjacent wing mounting frames, the camera is fixedly arranged in the camera mounting seats, the bottoms of the unmanned aerial vehicle bases between the adjacent wing mounting, the bottom of unmanned aerial vehicle frame is connected with the descending sill bar through the connecting piece, and the both ends of descending sill bar all are provided with the shock attenuation lantern ring.
As a further improvement, the unmanned aerial vehicle frame is connected with the unmanned aerial vehicle base between and is provided with the reinforcement loop bar.
As a further improvement, the unmanned aerial vehicle base that corresponds wing mounting bracket top still is provided with the mounting, and the mounting passes unmanned aerial vehicle base and wing mounting bracket looks fixed connection.
As a further improvement, the bottom of the unmanned aerial vehicle base is provided with power supply unit, and power supply unit is connected with the environmental protection gas collector.
As a further improvement of the utility model, the connecting piece is a convex connecting sleeve.
As a further improvement, the lifting device is a lifting cylinder, and the telescopic rod of the lifting cylinder is in driving connection with the environment-friendly gas collector.
As a further improvement, the damping sleeve ring is a rubber damping sleeve ring.
As a further improvement, the unmanned aerial vehicle frame is an ultralight aviation aluminum material frame structure.
As a further improvement, the number of the wing mounting frames is 4-8.
As a further improvement of the utility model, the number of the wing installation frames is 6.
Borrow by above-mentioned scheme, the utility model discloses at least, have following advantage:
the utility model relates to an environment measuring uses unmanned aerial vehicle, through the setting of unmanned aerial vehicle base, unmanned aerial vehicle frame, enhancement connecting rod and reinforcement loop bar isotructure, make the fastness and the stability of unmanned aerial vehicle overall structure stronger; the lifting device is arranged at the bottom of the environment-friendly gas collector, so that the aircraft can be closely attached to the aircraft roof when the unmanned aerial vehicle flies normally, and when the aircraft reaches a gas collection area, the lifting device is controlled by the ground remote controller to lift the environment-friendly gas collector so as to accurately collect gas, so that the wind resistance and the flying safety coefficient of the unmanned aerial vehicle are improved; the power supply device in the base of the unmanned aerial vehicle is used for supplying power to the environment-friendly gas collector, so that the weight of the power supply of the environment-friendly gas collector is reduced, and the whole structure weight of the unmanned aerial vehicle is greatly reduced due to the fact that the frame of the unmanned aerial vehicle is of an ultra-light aviation aluminum frame structure; through the shock attenuation lantern ring that the both ends of descending sill bar and descending sill bar all set up, take certain shock attenuation to the vibrations that produce when descending unmanned aerial vehicle and handle, prevent to cause certain damage to unmanned aerial vehicle inner assembly because the vibrations that the descending produced.
The above description is only an overview of the technical solution of the present invention, and in order to make the technical means of the present invention clearer and can be implemented according to the content of the description, the following detailed description is made with reference to the preferred embodiments of the present invention and accompanying drawings.
Drawings
In order to more clearly illustrate the technical solutions of the embodiments of the present invention, the drawings that are required to be used in the embodiments will be briefly described below, it should be understood that the following drawings only illustrate some embodiments of the present invention, and therefore should not be considered as limiting the scope, and for those skilled in the art, other related drawings can be obtained according to the drawings without inventive efforts.
Fig. 1 is a schematic structural view of the unmanned aerial vehicle for environmental monitoring during landing for collecting environmental gas;
FIG. 2 is an enlarged view of a portion of the base of the drone of FIG. 1;
fig. 3 is a schematic structural diagram of the unmanned aerial vehicle for environment detection during flight.
In the drawings, the meanings of the reference numerals are as follows.
1 unmanned aerial vehicle base 2 mounting holes
3 lifting device 4 environmental protection gas collector
5-camera mounting seat 6 wing
7 wing mount pad 8 wing mounting bracket
9 camera 10 strengthening loop bar
11 unmanned aerial vehicle frame 12 descends sill bar
13 connecting piece 14 shock-absorbing collar
15 fixing piece 16 reinforced connecting rod
Detailed Description
The following detailed description of the embodiments of the present invention is provided with reference to the accompanying drawings and examples. The following examples are intended to illustrate the invention, but are not intended to limit the scope of the invention.
In order to make the technical solution of the present invention better understood, the technical solution 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 some embodiments of the present invention, not all embodiments. The components of embodiments of the present invention, as generally described and illustrated in the figures herein, may be arranged and designed in a wide variety of different configurations. Thus, the following detailed description of the embodiments of the present invention, presented in the accompanying drawings, is not intended to limit the scope of the invention, as claimed, but is merely representative of selected embodiments of the invention. Based on the embodiment of the present invention, all other embodiments obtained by the person skilled in the art without creative work belong to the protection scope of the present invention.
Examples
As shown in figures 1 to 3 of the drawings,
an unmanned aerial vehicle for environmental detection comprises an unmanned aerial vehicle base 1, an environmental protection gas collector 4, wings 6, a camera 9 and an unmanned aerial vehicle frame 11, wherein the unmanned aerial vehicle base 1 is of a cylindrical structure, a mounting hole 2 is formed in the middle of the unmanned aerial vehicle base 1, a lifting device 3 is arranged in the mounting hole 2, the environmental protection gas collector 4 is arranged at the top of the lifting device 3, a plurality of wing mounting frames 8 are uniformly arranged on the circumferential surface of the outer side of the unmanned aerial vehicle base 1, the first ends of the wing mounting frames 8 are connected with the unmanned aerial vehicle base 1, the second ends of the wing mounting frames 8 are connected with wing mounting seats 7, the wings 6 are arranged on the wing mounting seats 7, camera mounting seats 5 are arranged on the circumferential surface of the unmanned aerial vehicle base 1 between the adjacent wing mounting frames 8, the camera 9 is fixedly arranged in the camera mounting seats 5, and reinforcing connecting rods 16 are connected with, unmanned aerial vehicle frame 11 is connected and is set up the bottom position at unmanned aerial vehicle base 1, and the bottom of unmanned aerial vehicle frame 11 is connected with descending sill bar 12 through connecting piece 13, and the both ends of descending sill bar 12 all are provided with the shock attenuation lantern ring 14.
The environmental protection gas collector 4 includes a plurality of environmental gas sensors, and the environmental protection gas collector 4 is a conventional technical means in the field, and is not specifically limited herein.
Wherein the camera 9 may be an optical high power zoom camera.
Preferably, a reinforcing sleeve rod 10 is further connected and arranged between the unmanned aerial vehicle frame 11 and the unmanned aerial vehicle base 1.
Preferably, the unmanned aerial vehicle base 1 above the corresponding wing mounting rack 8 is further provided with a fixing piece 15, and the fixing piece 15 penetrates through the unmanned aerial vehicle base 1 and is fixedly connected with the wing mounting rack 8. The strength of the connection between the wing mounting frame 8 and the unmanned aerial vehicle base 1 can be further strengthened through the fixing piece 15.
Preferably, the bottom of the unmanned aerial vehicle base 1 is provided with a power supply device (not shown in the figure), and the power supply device is connected with the environmental protection gas collector 4. Wherein the power supply means may be a rechargeable lithium battery.
Preferably, the connecting piece 13 is a male connecting sleeve.
Preferably, the lifting device 3 is a lifting cylinder, and a telescopic rod of the lifting cylinder is in driving connection with the environment-friendly gas collector 4.
Preferably, the cushion collar 14 is a rubber cushion collar.
Preferably, the unmanned aerial vehicle frame 11 is an ultralight aviation aluminum frame structure.
Preferably, the number of the wing mounting frames 8 is 4-8.
Preferably, the number of wing mounts 8 is 6.
The utility model relates to an environment measuring uses unmanned aerial vehicle, through the setting of unmanned aerial vehicle base 1, unmanned aerial vehicle frame 11, strengthen connecting rod 16 and strengthen loop bar 10 isotructure, make the fastness and the stability of unmanned aerial vehicle overall structure stronger; the lifting device 3 arranged at the bottom of the environment-friendly gas collector 4 can be used for tightly attaching to a machine top when the unmanned aerial vehicle flies normally, and when the unmanned aerial vehicle reaches a gas collection area, the lifting device 3 is controlled by a ground remote controller to lift the environment-friendly gas collector 4 so as to achieve the purpose of accurately collecting gas, so that the wind resistance and the flight safety coefficient of the unmanned aerial vehicle are improved; the power supply device in the unmanned aerial vehicle base 1 is used for supplying power to the environment-friendly gas collector 4, so that the weight of the power supply of the environment-friendly gas collector 4 is reduced, and the unmanned aerial vehicle frame 11 is an ultra-light aviation aluminum frame structure, so that the overall structural weight of the unmanned aerial vehicle is greatly reduced; through the shock attenuation lantern ring 14 that the both ends of descending sill bar 12 and descending sill bar 12 all set up, take certain shock attenuation to the vibrations that produce when descending unmanned aerial vehicle and handle, prevent to cause certain damage to unmanned aerial vehicle internal component because the vibrations that the descending produced.
The above description is only a preferred embodiment of the present invention, and is not intended to limit the present invention, and it should be noted that, for those skilled in the art, a plurality of modifications and variations can be made without departing from the technical principle of the present invention, and these modifications and variations should also be regarded as the protection scope of the present invention.
Claims (10)
1. The unmanned aerial vehicle for environmental detection is characterized by comprising an unmanned aerial vehicle base (1), an environment-friendly gas collector (4), wings (6), a camera (9) and an unmanned aerial vehicle frame (11), wherein the unmanned aerial vehicle base (1) is of a cylindrical structure, a mounting hole (2) is formed in the middle of the unmanned aerial vehicle base (1), a lifting device (3) is arranged in the mounting hole (2), the environment-friendly gas collector (4) is arranged at the top of the lifting device (3), a plurality of wing mounting frames (8) are uniformly arranged on the circumferential surface of the outer side of the unmanned aerial vehicle base (1), the first ends of the wing mounting frames (8) are connected with the unmanned aerial vehicle base (1), the second ends of the wings (8) of the mounting frames are connected with the wing mounting seats (7), the wings (6) are arranged on the wing mounting seats (7), adjacent be provided with camera mount pad (5) on the periphery of unmanned aerial vehicle base (1) between wing mounting bracket (8), camera mount pad (5) internal fixation is provided with camera (9), and is adjacent the bottom of unmanned aerial vehicle base (1) between wing mounting bracket (8) is all connected and is provided with and strengthens connecting rod (16), the bottom position that sets up at unmanned aerial vehicle base (1) is connected in unmanned aerial vehicle frame (11), the bottom of unmanned aerial vehicle frame (11) is connected with descending sill bar (12) through connecting piece (13), the both ends of descending sill bar (12) all are provided with the shock attenuation lantern ring (14).
2. The unmanned aerial vehicle for environmental monitoring of claim 1, characterized in that still connect between unmanned aerial vehicle frame (11) and unmanned aerial vehicle base (1) and be provided with reinforcing loop bar (10).
3. The unmanned aerial vehicle for environmental monitoring of claim 1, wherein a fixing member (15) is further disposed on the unmanned aerial vehicle base (1) above the wing mounting bracket (8), and the fixing member (15) penetrates through the unmanned aerial vehicle base (1) and is fixedly connected with the wing mounting bracket (8).
4. The unmanned aerial vehicle for environment detection of claim 1, wherein the bottom of the unmanned aerial vehicle base (1) is provided with a power supply device, and the power supply device is connected with the environmental protection gas collector (4).
5. The unmanned aerial vehicle for environment sensing as claimed in claim 1, wherein the connecting member (13) is a convex-shaped connecting sleeve.
6. The unmanned aerial vehicle for environment detection as claimed in claim 1, wherein the lifting device (3) is a lifting cylinder, and an expansion link of the lifting cylinder is in driving connection with the environment-friendly gas collector (4).
7. The unmanned aerial vehicle for environment detection as claimed in claim 1, wherein the shock-absorbing collar (14) is a rubber shock-absorbing collar.
8. The unmanned aerial vehicle for environmental monitoring as claimed in claim 1, wherein the unmanned aerial vehicle frame (11) is an ultra-light aviation aluminum frame structure.
9. The unmanned aerial vehicle for environment inspection as claimed in claim 1, wherein the number of the wing mounts (8) is 4-8.
10. An environmental testing drone according to claim 9, characterised in that the number of wing mounts (8) is 6.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201922346789.7U CN211336428U (en) | 2019-12-24 | 2019-12-24 | Unmanned aerial vehicle for environment detection |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201922346789.7U CN211336428U (en) | 2019-12-24 | 2019-12-24 | Unmanned aerial vehicle for environment detection |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN211336428U true CN211336428U (en) | 2020-08-25 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201922346789.7U Expired - Fee Related CN211336428U (en) | 2019-12-24 | 2019-12-24 | Unmanned aerial vehicle for environment detection |
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| CN (1) | CN211336428U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN114384606A (en) * | 2020-10-19 | 2022-04-22 | 丰翼科技(深圳)有限公司 | Unmanned aerial vehicle environmental parameter acquisition device, unmanned aerial vehicle equipment and system |
-
2019
- 2019-12-24 CN CN201922346789.7U patent/CN211336428U/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN114384606A (en) * | 2020-10-19 | 2022-04-22 | 丰翼科技(深圳)有限公司 | Unmanned aerial vehicle environmental parameter acquisition device, unmanned aerial vehicle equipment and system |
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| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20200825 Termination date: 20211224 |