Small remote sensing monitoring unmanned aerial vehicle with anti-collision structure

Abstract

The small remote sensing monitoring unmanned aerial vehicle with the anti-collision structure comprises an unmanned aerial vehicle body, a first anti-collision shell is detachably installed at the front end of the unmanned aerial vehicle body, a second anti-collision shell is detachably installed at the rear end of the unmanned aerial vehicle body, and a pair of installation rods is fixedly connected to the rear end of the first anti-collision shell. The outer ends of the mounting rods are movably sleeved with sleeving plates, the ends, away from the mounting rods, of the sleeving plates are fixedly connected with the second anti-collision shell, the front end and the rear end of the unmanned aerial vehicle body are sleeved with the first anti-collision shell and the second anti-collision shell correspondingly, the unmanned aerial vehicle body is protected through the first anti-collision shell and the second anti-collision shell, and when the unmanned aerial vehicle body is impacted by external force, the unmanned aerial vehicle body is prevented from being damaged. External force is buffered, so that internal elements and a detection mechanism are not easy to damage, the unmanned aerial vehicle can return smoothly, the air crash phenomenon is not easy to generate, and the service life of the unmanned aerial vehicle body is prolonged.

Description

TECHNICAL FIELD

[0001] The utility model relates to unmanned plane protection field especially is concerned about a small -size remote sensing monitoring unmanned plane with anti -collision structure. BACKGROUND

[0002] Small -size remote sensing monitoring unmanned plane has flexible flight ability, can reach the place that human is difficult to touch or dangerous, realizes all -round, dead -angle -free monitoring, ensures the comprehensiveness and accuracy of monitoring, is equipped with advanced sensor and high -definition camera on it, can gather high -precision monitoring data, provides detailed monitoring report for industrial enterprise, helps enterprise to understand equipment operation state and environmental change situation in time, in dangerous industrial environment, unmanned plane can replace artificial monitoring, reduces personnel safety risk, simultaneously ensures the smooth completion of monitoring task, and unmanned plane has wide application in environmental protection field, such as air quality monitoring, water quality monitoring, forest fire monitoring etc., can monitor the pollutant concentration in environment in real time, provides accurate data support for environmental protection department, helps environmental protection work.

[0003] The small -size remote sensing monitoring unmanned plane on the market has the following shortcomings when in use:

[0004] The small -size remote sensing monitoring unmanned plane in the prior art protects the internal elements and detection mechanism of the small -size remote sensing monitoring unmanned plane mainly by the shell on the small -size remote sensing monitoring unmanned plane, and the shell has a poor protective effect on the internal elements of the small -size remote sensing monitoring unmanned plane, when the small -size remote sensing monitoring unmanned plane is hit by external objects, the internal elements and detection mechanism of the small -size remote sensing monitoring unmanned plane are easily damaged, when the internal elements and detection mechanism of the small -size remote sensing monitoring unmanned plane are damaged, the small -size remote sensing monitoring unmanned plane cannot return normally, and even the small -size remote sensing monitoring unmanned plane may crash.

[0005] When the small -size remote sensing monitoring unmanned plane detects the surrounding environment by using the detection head thereon, the positions of the detection probes on different types of small -size remote sensing monitoring unmanned planes are different, so it is necessary to customize a protective device matched with the detection probe according to the position of the detection probe, thereby increasing the production cost and being inconvenient for personnel to use. UTILITY MODEL CONTENT

[0006] In view of the above problems, the utility model provides a small -size remote sensing monitoring unmanned plane with anti -collision structure, which has the advantages of being capable of preventing the small -size remote sensing monitoring unmanned plane from colliding.

[0007] The technical scheme of the utility model is:

[0008] The utility model provides a kind of small remote sensing monitoring unmanned plane with anti-collision structure, including unmanned plane body, the front end of unmanned plane body is detachably installed with first anticollision shell, the rear end of unmanned plane body is detachably installed with second anticollision shell, the rear end of first anticollision shell is fixedly connected with a pair of installation rod, the outer end of installation rod is movably sleeved with sleeve plate, the end of a pair of sleeve plate away from installation rod is fixedly connected with second anticollision shell, the upper end of sleeve plate is threadedly connected with limiting tube, the upper end of installation rod is provided with a plurality of insertion slots movably inserted with limiting tube, the end of first anticollision shell and second anticollision shell away from each other is provided with installation slot, the inside of installation slot is movably inserted with insertion plate, detection hole is opened on insertion plate, the inner wall of first anticollision shell and second anticollision shell is in contact with the outer end of unmanned plane body, the inner wall of first anticollision shell and second anticollision shell is provided with side wall circular groove, reinforcing frame is fixedly connected in the inside of side wall circular groove, spring and rubber frame are movably sleeved with the outer end of reinforcing frame, the inner top wall and inner bottom wall of first anticollision shell and second anticollision shell are fixedly connected with rubber block.

[0009] The working principle of the above technical solution is as follows: in use, the first anticollision shell and the second anticollision shell are respectively sleeved on the front and rear ends of the unmanned plane body, so that the two ends of the unmanned plane body are tightly fitted with the inner walls of the first anticollision shell and the second anticollision shell, then the limiting tube is installed on the sleeve plate, and the lower end of the limiting tube is inserted into the insertion slot, so that the installation rod is fixed in the sleeve plate by the limiting tube, thereby improving the stability of the connection between the first anticollision shell and the second anticollision shell. After the first anticollision shell and the second anticollision shell are respectively sleeved on the front and rear ends of the unmanned plane body, the depth of the installation rod inserted into the sleeve plate is adjusted, thereby adjusting the distance between the first anticollision shell and the second anticollision shell, and then the unmanned plane body of different lengths is installed.

[0010] A pair of limiting blocks are fixedly connected to the side ends of the insertion plate, and a limiting groove is formed in the inner side wall of the installation slot.

[0011] When the insertion plate moves, the limiting blocks move together, and the limiting blocks solve the technical problem that the insertion plate moves forward and backward in the prior art.

[0012] In further technical solutions, after the limiting tube is installed on the sleeve plate, the lower end of the limiting tube is inserted into the inside of the insertion slot. A reinforcing block is fixedly connected to the side end of the installation rod, and a reinforcing groove is formed in the inner side wall of the sleeve plate.

[0013] When the installation rod moves, the reinforcing block moves together, and the reinforcing block solves the technical problem that the installation rod is easily rotated in the sleeve plate in the prior art.

[0014] In further technical solutions, after the limiting tube is installed on the sleeve plate, the upper end of the limiting tube extends a certain distance from the sleeve plate.

[0015] Since the upper end of the limiting tube extends out of the sleeve plate by a certain distance, the technical problem of inconvenient manual rotation of the limiting tube in the prior art is solved.

[0016] In a further technical solution, a plurality of circular grooves are formed in the insertion plate, a sealing block is movably inserted into the circular grooves, and a through hole is formed in the inner wall of the circular groove. The first anti-collision shell and the second anti-collision shell are both in communication with the through hole.

[0017] The sealing block can seal the circular groove and the through hole, and the technical problem of inconvenient monitoring of the probe at different positions in the prior art is solved by using the circular groove and the through hole.

[0018] In a further technical solution, a magnetic coating one is coated on the outer end of the sealing block, and a magnetic coating two is coated on the inner wall of the circular groove.

[0019] After the magnetic coating one and the magnetic coating two are adsorbed together, the stability of the sealing block in the circular groove can be improved.

[0020] In a further technical solution, after the sealing block is installed in the circular groove, the side end of the sealing block is flush with the side end of the circular groove, and a handle is fixedly connected to the end of the sealing block away from the circular groove.

[0021] When the handle is pulled, it will move the sealing block together, solving the technical problem of the sealing block in the prior art that is not easy to move.

[0022] The beneficial effects of the utility model are:

[0023] 1. When in use, the first anti-collision shell and the second anti-collision shell are respectively sleeved on the front and rear ends of the unmanned aerial vehicle body, the unmanned aerial vehicle body is protected by the first anti-collision shell and the second anti-collision shell, so that when the unmanned aerial vehicle body is impacted by external force, the external force is buffered, thereby the internal elements and the detection mechanism are not easily damaged, the unmanned aerial vehicle body can smoothly return, the phenomenon of crashing is not easy to occur, and the service life of the unmanned aerial vehicle body is improved.

[0024] 2. When in use, by being provided with the rubber frame, the rubber plate and the spring, not only the stability of the anti-collision mechanism on the unmanned aerial vehicle body can be improved, but also the vibration felt by the unmanned aerial vehicle body can be buffered, so that the internal elements are not easily damaged, and the service life of the unmanned aerial vehicle body is further improved.

[0025] 3. A plurality of circular grooves and through holes are formed in the insertion plate, after the first anti-collision shell and the second anti-collision shell are installed on unmanned aerial vehicle bodies of different models for use, according to the positions of the monitoring probes thereon, the sealing block can be pulled out of the circular groove by using the handle, and the surrounding environment can be monitored by using the circular groove and the through hole corresponding to the probe, so that personnel can select the circular groove and the through hole according to the positions of the detection probes in actual use. BRIEF DESCRIPTION OF DRAWINGS

[0026] Figure 1 is the overall structure schematic diagram of the charger of the embodiment of the utility model;

[0027] Figure 2 is the split schematic diagram of the embodiment of the utility model;

[0028] Figure 3 is the first anti-collision shell schematic diagram of the embodiment of the utility model;

[0029] Figure 4 is the embodiment of the utility model Figure 3 A place local amplification schematic diagram in;

[0030] Figure 5 is the embodiment of the utility model Figure 3 B place local amplification schematic diagram in;

[0031] Figure 6 is the embodiment of the utility model Figure 2 C place local amplification schematic diagram in;

[0032] Figure 7 is the second anti-collision shell schematic diagram of the embodiment of the utility model.

[0033] Mark explanation:

[0034] 1, unmanned aerial vehicle body; 2, first anti-collision shell; 3, second anti-collision shell; 4, mounting rod; 5, sleeve plate; 6, limiting tube; 7, plug-in slot; 8, mounting groove; 9, detection hole; 10, limiting block; 11, limiting slot; 12, round groove; 13, sealing block; 14, through hole; 15, magnetic coating one; 16, magnetic coating two; 17, handle; 18, plug-in plate; 19, reinforcing block; 20, reinforcing groove; 21, side wall round groove; 22, reinforcing frame; 23, spring; 24, rubber block; 25, rubber frame. DETAILED DESCRIPTION

[0035] The embodiments of the utility model are further described below in combination with the drawings.

[0036] Embodiment:

[0037] As Figure 1 - Figure 7As shown, a small remote sensing monitoring drone with an anti-collision structure includes a drone body 1. A first anti-collision shell 2 is detachably installed at the front end of the drone body 1, and a second anti-collision shell 3 is detachably installed at the rear end of the drone body 1. A pair of mounting rods 4 are fixedly connected to the rear end of the first anti-collision shell 2. A connecting plate 5 is movably sleeved on the outer end of the mounting rod 4. The ends of the pair of connecting plates 5 away from the mounting rods 4 are fixedly connected to the second anti-collision shell 3. A limit tube 6 is threadedly connected to the upper end of the connecting plate 5. A plurality of insertion slots 7 are provided on the upper end of the mounting rod 4 for movably inserting into the limit tube 6. The first anti-collision shell 2 and... The second anti-collision shell 3 has a mounting groove 8 at one of its far ends. A plug plate 18 is movably inserted into the mounting groove 8. A detection hole 9 is provided on the plug plate 18. The inner walls of the first anti-collision shell 2 and the second anti-collision shell 3 are in contact with the outer end of the UAV body 1. The inner sidewalls of the first anti-collision shell 2 and the second anti-collision shell 3 are provided with sidewall circular grooves 21. A reinforcing frame 22 is fixedly connected inside the sidewall circular grooves 21. A spring 23 and a rubber frame 23 are movably sleeved on the outer end of the reinforcing frame 22. Rubber blocks 24 are fixedly connected to the inner top wall and inner bottom wall of the first anti-collision shell 2 and the second anti-collision shell 3.

[0038] Limiting blocks 10 are fixedly connected to a pair of side ends of the plug-in plate 18. A limiting groove 11 is provided on the inner side wall of the mounting groove 8, which is movably inserted into the limiting block 10. After the limiting tube 6 is installed on the socket plate 5, its lower end will be inserted into the inside of the plug-in groove 7. A reinforcing block 19 is fixedly connected to a pair of side ends of the mounting rod 4. A pair of reinforcing grooves 20 are provided on the inner side wall of the socket plate 5, which are slidably connected to the reinforcing block 19. After the limiting tube 6 is installed on the socket plate 5, its upper end will extend a certain distance from inside the socket plate 5.

[0039] The working principle of the above technical solution is as follows:

[0040] Step 1: When in use, the first anti-collision shell 2 and the second anti-collision shell 3 are respectively fitted onto the front and rear ends of the drone body 1, so that the two ends of the drone body 1 are tightly fitted with the inner sidewalls of the first anti-collision shell 2 and the second anti-collision shell 3. The first anti-collision shell 2 and the second anti-collision shell 3 protect the drone body 1, so that when it is subjected to external impact, it will buffer the external force, thereby making its internal components and detection mechanism less likely to be damaged, thus enabling it to return smoothly, reducing the risk of crashing, and improving the service life of the drone body 1.

[0041] Step 2: After the first anti-collision shell 2 and the second anti-collision shell 3 are respectively fitted onto the front and rear ends of the UAV body 1, the mounting rod 4 is inserted into the socket plate 5. Then, the limiting tube 6 is installed on the socket plate 5, so that the lower end of the limiting tube 6 is inserted into the insertion groove 7. The mounting rod 4 is fixed in the socket plate 5 by the limiting tube 6, thereby improving the stability of the connection between the first anti-collision shell 2 and the second anti-collision shell 3, and thus improving the stability of the first anti-collision shell 2 and the second anti-collision shell 3 on the UAV body 1.

[0042] After the first anti-collision shell 2 and the second anti-collision shell 3 are installed on the drone body 1, the spring 23 will push the rubber frame 25 under the action of the spring force, so that it will clamp the drone body 1, thereby improving the stability of the first anti-collision shell 2 and the second anti-collision shell 3 on the drone body 1. On the other hand, when the drone body 1 collides with a foreign object, the rubber frame 25 and the rubber block 24 can buffer the shock received by the outside of the drone body 1, further protecting the drone body 1 and making its internal components less likely to be damaged by shock.

[0043] In summary, when in use, the first anti-collision shell 2 and the second anti-collision shell 3 can protect the drone body 1, making it less susceptible to damage and improving its service life. Furthermore, the first anti-collision shell 2 and the second anti-collision shell 3 are detachable, making it easy for personnel to replace them.

[0044] In another embodiment, such as Figure 3 as well as Figure 5 As shown, the plug plate 18 has multiple circular slots 12, and a sealing block 13 is movably inserted into the inside of the circular slot 12. A through hole 14 is provided on the inner wall of the circular slot 12. Both the first anti-collision shell 2 and the second anti-collision shell 3 are connected to the through hole 14. The outer end of the sealing block 13 is coated with a magnetic coating 15, and the inner wall of the circular slot 12 is coated with a magnetic coating 16. After the sealing block 13 is installed in the circular slot 12, its side end is flush with the side end of the circular slot 12. A handle 17 is fixedly connected to the end of the sealing block 13 away from the circular slot 12.

[0045] In use, the probe on the drone body 1 monitors the external environment through the circular groove 12, through hole 14 and detection hole 9. The plug-in plate 18 has multiple circular grooves 12 and through holes 14. After the first anti-collision shell 2 and the second anti-collision shell 3 are installed on different models of drone bodies 1, the sealing block 13 can be pulled by the handle 17 according to the position of the monitoring probe. The sealing block 13 can be removed from the circular groove 12. The surrounding environment can be monitored by using the circular groove 12 and through hole 14 corresponding to the probe. This makes it convenient for personnel to select the corresponding circular groove 12 and through hole 14 according to the actual probe position.

[0046] The embodiments described above merely illustrate specific implementations of this utility model, and while the descriptions are detailed, they should not be construed as limiting the scope of this utility model patent. It should be noted that those skilled in the art can make various modifications and improvements without departing from the concept of this utility model, and these modifications and improvements all fall within the protection scope of this utility model.

Claims

1. A small remote sensing monitoring unmanned aerial vehicle with anti-collision structure, comprising an unmanned aerial vehicle body (1), characterized in that, The front end of the unmanned aerial vehicle body (1) is detachably installed with a first anti-collision shell (2), the rear end of the unmanned aerial vehicle body (1) is detachably installed with a second anti-collision shell (3), the rear end of the first anti-collision shell (2) is fixedly connected with a pair of mounting rods (4), the outer end of the mounting rod (4) is movably sleeved with a sleeve plate (5), the end of the sleeve plate (5) away from the mounting rod (4) is fixedly connected with the second anti-collision shell (3), the upper end of the sleeve plate (5) is threadedly connected with a limiting tube (6), the upper end of the mounting rod (4) is provided with a plurality of plug-in grooves (7) movably inserted with the limiting tube (6), the end of the first anti-collision shell (2) and the second anti-collision shell (3) away from each other is provided with a mounting groove (8), the inside of the mounting groove (8) is movably inserted with a plug-in plate (18), the plug-in plate (18) is provided with a detection hole (9), the inner wall of the first anti-collision shell (2) and the second anti-collision shell (3) is in contact with the outer end of the unmanned aerial vehicle body (1); The inner side wall of the first anti-collision shell (2) and the second anti-collision shell (3) is provided with a side wall circular groove (21), the inside of the side wall circular groove (21) is fixedly connected with a reinforcing frame (22), the outer end of the reinforcing frame (22) is movably sleeved with a spring (23) and a rubber frame (25), the inner top wall and the inner bottom wall of the first anti-collision shell (2) and the second anti-collision shell (3) are fixedly connected with a rubber block (24).

2. The small remote sensing monitoring unmanned aerial vehicle with anti-collision structure according to claim 1, characterized in that, The pair of side ends of the plug-in plate (18) are fixedly connected with a limiting block (10), the inner side wall of the mounting groove (8) is provided with a limiting groove (11) movably inserted with the limiting block (10).

3. The small remote sensing monitoring unmanned aerial vehicle with anti-collision structure according to claim 2, characterized in that, After the limiting tube (6) is installed on the sleeve plate (5), the lower end thereof is inserted into the inside of the plug-in groove (7), the pair of side ends of the mounting rod (4) are fixedly connected with a reinforcing block (19), the inner side wall of the sleeve plate (5) is provided with a pair of reinforcing grooves (20) slidably connected with the reinforcing block (19).

4. The small remote sensing monitoring unmanned aerial vehicle with anti-collision structure according to claim 3, characterized in that, After the limiting tube (6) is installed on the sleeve plate (5), the upper end thereof is stretched out from the sleeve plate (5) by a certain distance.

5. The small remote sensing monitoring unmanned aerial vehicle with anti-collision structure according to claim 4, characterized in that, The plug-in plate (18) is provided with a plurality of circular grooves (12), the inside of the circular groove (12) is movably inserted with a sealing block (13), the inner wall of the circular groove (12) is provided with a through hole (14), the first anti-collision shell (2) and the second anti-collision shell (3) are communicated with the through hole (14).

6. The small remote sensing monitoring unmanned aerial vehicle with anti-collision structure according to claim 5, characterized in that, The outer end of the sealing block (13) is coated with a magnetic coating one (15), the inner wall of the circular groove (12) is coated with a magnetic coating two (16).

7. The small remote sensing monitoring unmanned aerial vehicle with anti-collision structure according to claim 6, characterized in that, After the sealing block (13) is installed in the circular groove (12), the side end thereof is flush with the side end of the circular groove (12), the end of the sealing block (13) away from the circular groove (12) is fixedly connected with a handle (17).

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