CN215475789U - Geological survey is with unmanned aerial vehicle auxiliary lighting device - Google Patents
Geological survey is with unmanned aerial vehicle auxiliary lighting device Download PDFInfo
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- CN215475789U CN215475789U CN202023046850.5U CN202023046850U CN215475789U CN 215475789 U CN215475789 U CN 215475789U CN 202023046850 U CN202023046850 U CN 202023046850U CN 215475789 U CN215475789 U CN 215475789U
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- 230000017525 heat dissipation Effects 0.000 description 5
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Abstract
The utility model discloses an unmanned aerial vehicle auxiliary lighting device for geological exploration, belongs to the technical field of unmanned aerial vehicle auxiliary equipment, solves the problem that the existing unmanned aerial vehicle for geological exploration is poor in lighting effect, and is technically characterized in that: including the unmanned aerial vehicle main part, be provided with the camera in the unmanned aerial vehicle main part, unmanned aerial vehicle main part below symmetry is provided with electric telescopic handle, electric telescopic handle keeps away from the one end fixed connection installation pole of unmanned aerial vehicle main part, be provided with the light on the installation pole, the symmetry is provided with the recess on the installation pole, the symmetry is provided with reset spring in the recess, reset spring's one end fixed connection recess, reset spring's other end fixed connection card ball, the card ball sets up on the recess, camera bilateral symmetry is provided with the ball groove, ball groove and card ball mutually support, have the good advantage of illuminating effect.
Description
Technical Field
The utility model relates to the technical field of unmanned aerial vehicle auxiliary equipment, in particular to an unmanned aerial vehicle auxiliary lighting device for geological exploration.
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; at present, 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 reports, power inspection, disaster relief, film and television shooting, romantic manufacturing and the like, the application of the unmanned aerial vehicle is greatly expanded, the developed countries also actively expand industrial application and develop unmanned aerial vehicle technology, and the 62 nd meeting of the world customs organization coordination system committee (HSC) decides in 2018 to classify the unmanned aerial vehicle into a camera which can fly.
The unmanned aerial vehicle for geological survey of current has and in the use, has the night and uses or when the local use that light is not enough, leads to the not good problem of effect of shooing, is difficult to obtain popularization and application.
Therefore, it is desirable to provide an auxiliary lighting device for unmanned aerial vehicle for geological survey, aiming at solving the above problems.
SUMMERY OF THE UTILITY MODEL
Aiming at the defects in the prior art, the embodiment of the utility model aims to provide an unmanned aerial vehicle auxiliary lighting device for geological exploration, so as to solve the problems in the background technology.
In order to achieve the purpose, the utility model provides the following technical scheme:
an unmanned aerial vehicle auxiliary lighting device for geological exploration comprises an unmanned aerial vehicle main body, wherein a camera is arranged on the unmanned aerial vehicle main body, electric telescopic rods are symmetrically arranged below the unmanned aerial vehicle main body, one end of each electric telescopic rod, far away from the unmanned aerial vehicle main body, is fixedly connected with a mounting rod, the mounting rod is provided with a lighting lamp, the mounting rod is symmetrically provided with grooves, the grooves are symmetrically provided with return springs, one end of the return spring is fixedly connected with the groove, the other end of the return spring is fixedly connected with the clamping ball, the ball clamping device is arranged on the groove, ball grooves are symmetrically arranged on two sides of the illuminating lamp, the ball grooves and the ball clamping device are matched with each other, the ball clamping device is extruded by pushing the illuminating lamp, get into the recess under reset spring's effect, when reacing the ball groove, reset spring pops out the card ball for the card ball connects the ball groove, makes can the effectual fixed of light and take out.
As a further scheme of the utility model, the mounting rod is symmetrically provided with lower buffer plates, the lower buffer plates are provided with outer sleeves, inner loop bars are arranged in the outer sleeves, the lower parts of the inner loop bars are fixedly connected with the connecting plate, the connecting plate is movably connected with the inner parts of the outer sleeves, one ends of the inner loop bars, far away from the connecting plate, are fixedly connected with the upper buffer plate, the upper buffer plate is fixedly connected with the unmanned aerial vehicle main body, and the distance between the upper buffer plate and the lower buffer plate is changed by adjusting the connection between the outer sleeves and the inner loop bars, so that the upper buffer plate and the lower buffer plate are matched with each other, and a better supporting device can be realized.
As a further scheme of the utility model, the outer sleeve is provided with a plurality of positioning holes, the positioning holes are uniformly distributed on the outer sleeve, the inner sleeve rod is internally provided with a fixing groove, the fixing groove and the positioning holes are matched with each other, the fixing bolt is arranged in the fixing groove, the fixing bolt penetrates through the positioning holes, and the outer sleeve rod and the inner sleeve rod can be fixed after the adjustment is finished through the mutual matching of the positioning holes, the fixing groove and the fixing bolt, so that the inner sleeve rod can be effectively prevented from sliding downwards.
According to a further scheme of the utility model, electric rotating shafts are symmetrically arranged on two sides of the unmanned aerial vehicle main body and movably connected with the light supplementing plate, a plurality of light supplementing lamps are arranged on the light supplementing plate and uniformly distributed on the light supplementing plate, and the position of the light supplementing plate can be adjusted through the electric rotating shafts, so that the light supplementing lamps supplement light, and a better lighting effect is ensured.
As a further scheme of the utility model, the unmanned aerial vehicle main body is provided with a solar panel.
According to the further scheme of the utility model, the radiating fans are symmetrically arranged on the main body of the unmanned aerial vehicle, the radiating fan is connected with the solar cell panel through a circuit, and heat generated by light emitting of the illuminating lamp and the light supplementing lamp can be reduced through the radiating fans, so that the working effect of the device is ensured.
In summary, compared with the prior art, the embodiment of the utility model has the following beneficial effects:
according to the utility model, the illuminating lamp is pushed in, the clamping ball is extruded and enters the groove under the action of the reset spring, when the illuminating lamp reaches the ball groove, the reset spring ejects the clamping ball, so that the clamping ball is connected with the ball groove, the illuminating lamp can be effectively fixed and taken out, the distance between the upper buffer plate and the lower buffer plate is changed by adjusting the connection of the outer sleeve and the inner sleeve, the upper buffer plate and the lower buffer plate are mutually matched, a better supporting device can be realized, the position of the light supplementing plate can be adjusted through the electric rotating shaft, the light supplementing lamp is supplemented, and the better illuminating effect is ensured.
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 structural diagram of an embodiment of the present invention.
Fig. 2 is a schematic structural diagram of a view in an embodiment of the present invention.
Fig. 3 is a schematic structural diagram of a view B in the embodiment of the present invention.
Fig. 4 is a schematic structural diagram of an embodiment of the present invention after improvement.
Reference numerals: the unmanned aerial vehicle comprises a main body 1, a solar panel 2, a camera 3, an electric telescopic rod 4, a mounting rod 5, a lighting lamp 6, a groove 7, a reset spring 8, a ball 9, a ball groove 10, an electric rotating shaft 11, a light supplementing plate 12, a light supplementing lamp 13, an upper buffer plate 14, a lower buffer plate 15, an outer sleeve 16, an inner sleeve rod 17, a connecting plate 18, a positioning hole 19, a fixing groove 20, a fixing bolt 21 and a heat dissipation fan 22.
Detailed Description
In the description of the present invention, it is to be understood that the terms "longitudinal," "lateral," "upper," "lower," "top," "bottom," "inner," "outer," and the like are used in the orientations and positional relationships indicated in the drawings for convenience in describing the present invention and simplicity in description, and do not indicate or imply that the referenced devices or elements must have a particular orientation, be constructed in a particular orientation, and be operated in a particular manner, and thus are not to be construed as limiting the present invention.
Furthermore, the terms "first", "second" and "first" are used for descriptive purposes only and are not to be construed as indicating or implying relative importance or implicitly indicating the number of technical features indicated. Thus, a feature defined as "first" or "second" may explicitly or implicitly include one or more of that feature. In the description of the present invention, "a plurality" means two or more unless specifically defined otherwise.
In the present invention, unless otherwise expressly stated or limited, the terms "mounted," "connected," "secured," and the like are to be construed broadly and can, for example, be fixedly connected, detachably connected, or integrally formed; can be mechanically or electrically connected; either directly or indirectly through intervening media, either internally or in any other relationship. The specific meanings of the above terms in the present invention can be understood by those skilled in the art according to specific situations.
In order to make the objects, technical solutions and advantages of the present invention more apparent, the present invention is described in further detail below with reference to the accompanying drawings and embodiments. It should be understood that the specific embodiments described herein are merely illustrative of the utility model and are not intended to limit the utility model.
Specific implementations of the present invention are described in detail below with reference to specific embodiments.
Example 1
Referring to fig. 1-3, an unmanned aerial vehicle auxiliary lighting device for geological exploration comprises an unmanned aerial vehicle main body 1, a camera 3 is arranged on the unmanned aerial vehicle main body 1, electric telescopic rods 4 are symmetrically arranged below the unmanned aerial vehicle main body 1, one ends of the electric telescopic rods 4 far away from the unmanned aerial vehicle main body 1 are fixedly connected with mounting rods 5, lighting lamps 6 are arranged on the mounting rods 5, grooves 7 are symmetrically arranged on the mounting rods 5, return springs 8 are symmetrically arranged in the grooves 7, one ends of the return springs 8 are fixedly connected with the grooves 7, the other ends of the return springs 8 are fixedly connected with clamping balls 9, the clamping balls 9 are arranged on the grooves 7, ball grooves 10 are symmetrically arranged on two sides of the lighting lamps 6, the ball grooves 10 and the clamping balls 9 are matched with each other, the lighting lamps 6 are pushed in to extrude the clamping balls 9, and the clamping balls 9 enter the grooves 7 under the action of the return springs 8, when the lamp reaches the ball groove 10, the return spring 8 ejects the clamping ball 9, so that the clamping ball 9 is connected with the ball groove 10, and the lamp 6 can be effectively fixed and taken out.
The symmetry is provided with down buffer board 15 on the installation pole 5, be provided with outer tube 16 on the buffer board 15 down, be provided with interior loop bar 17 in the outer tube 16, interior loop bar 17 below fixed connection connecting plate 18, inside 18 swing joint outer tube 16 of connecting plate, the one end fixed connection that connecting plate 18 was kept away from to interior loop bar 17 connects up buffer board 14, go up 14 fixed connection unmanned aerial vehicle main part 1 of buffer board, through the connection of adjusting outer tube 16 and interior loop bar 17, change the distance of buffer board 14 and lower buffer board 15 for go up buffer board 14 and lower buffer board 15 and mutually support, strutting arrangement that can be better.
The outer sleeve 16 is provided with a plurality of positioning holes 19, the positioning holes 19 are evenly distributed on the outer sleeve 16, a fixing groove 20 is formed in the inner sleeve rod 17, the fixing groove 20 and the positioning holes 16 are matched with each other, a fixing bolt 21 is arranged in the fixing groove 20, the fixing bolt 21 penetrates through the positioning holes 19, and the outer sleeve 16 and the inner sleeve rod 17 can be fixed after adjustment is completed through mutual matching of the positioning holes 19, the fixing bolt 20 and the fixing bolt 21, so that the inner sleeve rod 17 can be effectively prevented from sliding downwards.
1 bilateral symmetry of unmanned aerial vehicle main part is provided with electronic pivot 11, 11 swing joint of electronic pivot mends worn-out fur 12, be provided with a plurality of light filling lamp 13 on mending worn-out fur 12, light filling lamp 13 evenly distributed can adjust the position of mending worn-out fur 12 through electronic pivot 11 on light filling board 12 for light filling lamp 13 carries out the light filling, and it is better to guarantee the illuminating effect.
Preferably, in this embodiment, the main body 1 of the unmanned aerial vehicle is provided with a solar panel 2.
Example 2
Referring to fig. 1 to 4, an auxiliary lighting device of an unmanned aerial vehicle for geological exploration comprises an unmanned aerial vehicle main body 1 and a heat dissipation fan 22, wherein a camera 3 is arranged on the unmanned aerial vehicle main body 1, electric telescopic rods 4 are symmetrically arranged below the unmanned aerial vehicle main body 1, one ends of the electric telescopic rods 4 far away from the unmanned aerial vehicle main body 1 are fixedly connected with mounting rods 5, illuminating lamps 6 are arranged on the mounting rods 5, grooves 7 are symmetrically arranged on the mounting rods 5, return springs 8 are symmetrically arranged in the grooves 7, one ends of the return springs 8 are fixedly connected with the grooves 7, the other ends of the return springs 8 are fixedly connected with clamping balls 9, the clamping balls 9 are arranged on the grooves 7, ball grooves 10 are symmetrically arranged on two sides of the illuminating lamps 6, the ball grooves 10 and the clamping balls 9 are matched with each other, the clamping balls 9 are pressed by pushing in the illuminating lamps 6, and enter the grooves 7 under the action of the return springs 8, when the lamp reaches the ball groove 10, the return spring 8 ejects the clamping ball 9, so that the clamping ball 9 is connected with the ball groove 10, and the lamp 6 can be effectively fixed and taken out.
The symmetry is provided with down buffer board 15 on the installation pole 5, be provided with outer tube 16 on the buffer board 15 down, be provided with interior loop bar 17 in the outer tube 16, interior loop bar 17 below fixed connection connecting plate 18, inside 18 swing joint outer tube 16 of connecting plate, the one end fixed connection that connecting plate 18 was kept away from to interior loop bar 17 connects up buffer board 14, go up 14 fixed connection unmanned aerial vehicle main part 1 of buffer board, through the connection of adjusting outer tube 16 and interior loop bar 17, change the distance of buffer board 14 and lower buffer board 15 for go up buffer board 14 and lower buffer board 15 and mutually support, strutting arrangement that can be better.
The outer sleeve 16 is provided with a plurality of positioning holes 19, the positioning holes 19 are evenly distributed on the outer sleeve 16, a fixing groove 20 is formed in the inner sleeve rod 17, the fixing groove 20 and the positioning holes 16 are matched with each other, a fixing bolt 21 is arranged in the fixing groove 20, the fixing bolt 21 penetrates through the positioning holes 19, and the outer sleeve 16 and the inner sleeve rod 17 can be fixed after adjustment is completed through mutual matching of the positioning holes 19, the fixing bolt 20 and the fixing bolt 21, so that the inner sleeve rod 17 can be effectively prevented from sliding downwards.
1 bilateral symmetry of unmanned aerial vehicle main part is provided with electronic pivot 11, 11 swing joint of electronic pivot mends worn-out fur 12, be provided with a plurality of light filling lamp 13 on mending worn-out fur 12, light filling lamp 13 evenly distributed can adjust the position of mending worn-out fur 12 through electronic pivot 11 on light filling board 12 for light filling lamp 13 carries out the light filling, and it is better to guarantee the illuminating effect.
What differs from embodiment 1, the symmetry is provided with heat dissipation fan 22 in the unmanned aerial vehicle main part 1, heat dissipation fan 22 circuit connection solar cell panel 2 can reduce the luminous heat that produces of light 6 and light filling lamp 13 through heat dissipation fan 22, guarantees the working effect of device.
The rest of the structure of this example is the same as example 1.
It needs to explain specially, through propelling into light 6 in this application, extrude card ball 9, get into recess 7 under reset spring 8's effect, when arriving ball groove 10, reset spring 8 pops out card ball 9, make card ball 9 connect ball groove 10, make can 6 effectual fixed with take out of light, through the connection of adjusting outer tube 16 and interior loop bar 17, buffer board 14 and lower buffer board 15's distance in the change, make and go up buffer board 14 and lower buffer board 15 and mutually support, strutting arrangement that can be better, can adjust the position of light supplementation board 12 through electronic pivot 11, make light supplementation lamp 13 carry out the light filling, guarantee that the illuminating effect is better.
The above description is only for the purpose of illustrating the preferred embodiments of the present invention and is not to be construed as limiting the utility model, and any modifications, equivalents and improvements made within the spirit and principle of the present invention are intended to be included within the scope of the present invention.
Claims (6)
1. An unmanned aerial vehicle auxiliary lighting device for geological exploration comprises an unmanned aerial vehicle main body (1) and is characterized in that a camera (3) is arranged on the unmanned aerial vehicle main body (1), electric telescopic rods (4) are symmetrically arranged below the unmanned aerial vehicle main body (1), one ends, far away from the unmanned aerial vehicle main body (1), of the electric telescopic rods (4) are fixedly connected with mounting rods (5), illuminating lamps (6) are arranged on the mounting rods (5), grooves (7) are symmetrically arranged on the mounting rods (5), reset springs (8) are symmetrically arranged in the grooves (7), one ends of the reset springs (8) are fixedly connected with grooves (7), the other ends of the reset springs (8) are fixedly connected with clamping balls (9), the clamping balls (9) are arranged on the grooves (7), ball grooves (10) are symmetrically arranged on two sides of the illuminating lamps (6), the ball groove (10) and the clamping ball (9) are matched with each other.
2. The auxiliary lighting device of the unmanned aerial vehicle for geological exploration according to claim 1, wherein the mounting rod (5) is symmetrically provided with a lower buffer plate (15), the lower buffer plate (15) is provided with an outer sleeve (16), the outer sleeve (16) is internally provided with an inner sleeve rod (17), the inner sleeve rod (17) is fixedly connected with a connecting plate (18) below, the connecting plate (18) is movably connected with the inside of the outer sleeve (16), one end of the inner sleeve rod (17) far away from the connecting plate (18) is fixedly connected with an upper buffer plate (14), and the upper buffer plate (14) is fixedly connected with the unmanned aerial vehicle main body (1).
3. The unmanned aerial vehicle auxiliary lighting device for geological survey of claim 2, wherein the outer sleeve (16) is provided with a plurality of positioning holes (19), the positioning holes (19) are evenly distributed on the outer sleeve (16), the inner sleeve rod (17) is provided with a fixing groove (20), the fixing groove (20) and the positioning holes (19) are matched with each other, the fixing bolt (21) is arranged in the fixing groove (20), and the fixing bolt (21) penetrates through the positioning holes (19).
4. The auxiliary lighting device of the unmanned aerial vehicle for geological exploration according to claim 3, wherein the unmanned aerial vehicle main body (1) is symmetrically provided with an electric rotating shaft (11) at two sides, the electric rotating shaft (11) is movably connected with a light supplement plate (12), the light supplement plate (12) is provided with a plurality of light supplement lamps (13), and the light supplement lamps (13) are uniformly distributed on the light supplement plate (12).
5. Unmanned aerial vehicle auxiliary lighting device for geological survey according to claim 4, characterized in that the unmanned aerial vehicle body (1) is provided with a solar panel (2).
6. The auxiliary lighting device of unmanned aerial vehicle for geological survey as claimed in claim 1, wherein the unmanned aerial vehicle main body (1) is symmetrically provided with heat dissipating fans (22), and the heat dissipating fans (22) are electrically connected with the solar panel (2).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202023046850.5U CN215475789U (en) | 2020-12-16 | 2020-12-16 | Geological survey is with unmanned aerial vehicle auxiliary lighting device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202023046850.5U CN215475789U (en) | 2020-12-16 | 2020-12-16 | Geological survey is with unmanned aerial vehicle auxiliary lighting device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN215475789U true CN215475789U (en) | 2022-01-11 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202023046850.5U Expired - Fee Related CN215475789U (en) | 2020-12-16 | 2020-12-16 | Geological survey is with unmanned aerial vehicle auxiliary lighting device |
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| Country | Link |
|---|---|
| CN (1) | CN215475789U (en) |
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2020
- 2020-12-16 CN CN202023046850.5U patent/CN215475789U/en not_active Expired - Fee Related
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Granted publication date: 20220111 |