CN216546704U - Anticollision formula fire control unmanned aerial vehicle - Google Patents
Anticollision formula fire control unmanned aerial vehicle Download PDFInfo
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- CN216546704U CN216546704U CN202123332403.0U CN202123332403U CN216546704U CN 216546704 U CN216546704 U CN 216546704U CN 202123332403 U CN202123332403 U CN 202123332403U CN 216546704 U CN216546704 U CN 216546704U
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Abstract
The utility model discloses an anti-collision fire-fighting unmanned aerial vehicle, which comprises a box body, a machine body and a connecting rod, wherein the top of the box body is provided with the machine body, one side of the machine body is provided with the connecting rod, one side of the connecting rod is provided with a wing, one side of the box body is provided with a connecting plate, one side of the connecting plate is provided with a damping air bag, one side of the damping air bag is connected with a protection plate, two sides of the box body are respectively provided with a conveying pipe, the bottom of the conveying pipe is provided with a spray head, the bottom of the box body is provided with a connecting plate, the anti-collision fire-fighting unmanned aerial vehicle passes through the connecting plate arranged at one side of the box body when the wing flies, one side of the connecting plate is provided with the damping air bag, one side of the damping air bag is connected with the protection plate, when an object is collided, the damping air bag and the protection plate protect the wing from being damaged and falling, the bottom of a supporting rod is connected with a butt joint plate through a damping bin, the butt plate is matched with a damping spring to relieve the descending impact force.
Description
Technical Field
The utility model relates to the technical field of unmanned aerial vehicles, in particular to an anti-collision type fire-fighting unmanned aerial vehicle.
Background
The pilotless plane is called unmanned plane for short, and is a unmanned aerial vehicle operated by radio remote control equipment and a self-contained program control device. The unmanned aerial vehicle is a general term of an unmanned aerial vehicle, and can be defined as follows from the technical point of view: unmanned fixed wing aircraft, unmanned VTOL aircraft, unmanned airship, unmanned helicopter, unmanned multi-rotor aircraft, unmanned paravane, etc. Compared with manned aircraft, it has the advantages of small volume, low cost, convenient use, low requirement on the operational environment, strong battlefield viability and the like. Since the unmanned aircraft has important significance for future air battles, the research and development work of the unmanned aircraft is carried out in all major military countries in the world.
Current unmanned aerial vehicle does not have buffer stop, leads to unmanned aerial vehicle to hit the object when the mistake flies very easily, when unmanned aerial vehicle receives the damage, can't carry out work, leads to falling, and the job schedule is unsmooth, for this reason we provide an anticollision formula fire control unmanned aerial vehicle to solve the problem among the prior art.
SUMMERY OF THE UTILITY MODEL
The utility model aims to provide an anti-collision fire-fighting unmanned aerial vehicle, which aims to solve the problems in the prior art.
In order to achieve the purpose, the utility model provides the following technical scheme: the utility model provides an anticollision formula fire control unmanned aerial vehicle, includes box, organism, connecting rod, the top of box sets up the organism, one side of organism is provided with the connecting rod, the wing is installed to one side of connecting rod, one side of box is provided with the connecting plate, one side of connecting plate is provided with the shock attenuation gasbag, one side of shock attenuation gasbag is connected with the guard plate, the both sides of box all are provided with the conveyer pipe, the shower nozzle is installed to the bottom of conveyer pipe, the bottom of box is provided with the linkage plate, the bottom of linkage plate is provided with the bracing piece, the bottom of bracing piece is connected with the butt joint plate through the shock attenuation storehouse, the bottom of butt joint plate is provided with damping spring, the support column is installed to the bottom in shock attenuation storehouse, the bottom of support column is provided with the walking wheel.
Preferably, damping plates are arranged at two ends of the damping spring.
Preferably, the bottom of connecting plate is provided with the backup pad, one side of backup pad is connected with the box, the both ends of backup pad all are provided with mounting panel A.
Preferably, the top of the box body is provided with a material injection pipe, and the material injection pipe is in threaded connection with a top cover.
Preferably, the inside of connecting plate, guard plate all seted up ventilative net.
Preferably, the top of the damping bin is provided with a notch, and a supporting rod is arranged inside the notch.
Preferably, the two sides of the shock absorption air bag are provided with fixing plates, and mounting bolts are arranged inside the fixing plates.
Compared with the prior art, the utility model has the beneficial effects that:
1. according to the utility model, the organism is arranged at the top of the box body, the connecting rod is arranged on one side of the organism, the wing is arranged on one side of the connecting rod, the connecting plate is arranged on one side of the box body when the wing flies, the damping air bag is arranged on one side of the connecting plate, the protection plate is connected to one side of the damping air bag, and when an object is collided, the damping air bag and the protection plate protect the wing to prevent the wing from being damaged and falling.
2. The bottom of the supporting rod is connected with the butt plate through the damping bin, the butt plate is matched with the damping spring to relieve descending impact force, the bottom of the damping bin is provided with the supporting column, and the walking wheels are arranged at the bottom of the supporting column, so that when a machine body descends, the machine body is prevented from being damaged.
Drawings
The accompanying drawings, which are included to provide a further understanding of the utility model and are incorporated in and constitute a part of this specification, illustrate embodiments of the utility model and together with the description serve to explain the principles of the utility model and not to limit the utility model. In the drawings:
fig. 1 is a schematic view of the overall structure of the present invention.
Fig. 2 is a schematic overall perspective structure of the present invention.
Fig. 3 is a schematic diagram of a connecting plate structure according to the present invention.
In the figure: 1. a body; 2. a connecting rod; 3. an airfoil; 4. a connecting plate; 5. a protection plate; 6. a shock-absorbing air bag; 7. a support plate; 8. mounting a plate A; 9. a delivery pipe; 10. a spray head; 11. a connector tile; 12. a damping bin; 13. a support pillar; 14. a traveling wheel; 15. a damping plate; 16. a damping spring; 17. a butt plate; 18. a support bar; 19. a breathable net; 20. a material injection pipe; 21. mounting a plate B; 22. and (4) a box body.
Detailed Description
In order to make the objects, technical solutions and advantages of the embodiments of the present invention more apparent, the technical solutions of the embodiments of the present invention will be described clearly and completely with reference to the accompanying drawings of the embodiments of the present invention, and it is obvious that the described embodiments are some, but not all embodiments of the present invention. All other embodiments, which can be obtained by a person skilled in the art without any inventive step based on the embodiments of the present invention, are within the scope of the present invention. Thus, the following detailed description of the embodiments of the present invention, presented in the figures, is not intended to limit the scope of the utility model, as claimed, but is merely representative of selected embodiments of the utility model. All other embodiments, which can be obtained by a person skilled in the art without any inventive step based on the embodiments of the present invention, are within the scope of the present invention.
Referring to fig. 1, 2 and 3, in an embodiment of the present invention, an anti-collision fire-fighting unmanned aerial vehicle includes a box 22, a machine body 1 and a connecting rod 2, the machine body 1 is disposed on the top of the box 22, the connecting rod 2 is disposed on one side of the machine body 1, a wing 3 is mounted on one side of the connecting rod 2, a connecting plate 4 is disposed on one side of the box 22, a damping airbag 6 is disposed on one side of the connecting plate 4, a protection plate 5 is connected to one side of the damping airbag 6, delivery pipes 9 are disposed on both sides of the box 22, a nozzle 10 is mounted at the bottom of the delivery pipe 9, a connecting plate 11 is disposed at the bottom of the box 22, a support rod 18 is disposed at the bottom of the connecting plate 11, a butt plate 17 is connected to the bottom of the support rod 18 through a damping bin 12, a damping spring 16 is disposed at the bottom of the butt plate 17, the butt plate 17 cooperates with the damping spring 16, alleviate the impact force that descends, support column 13 is installed to the bottom of surge bin 12, the bottom of support column 13 is provided with walking wheel 14, damping spring 16's both ends all are provided with damping plate 15, prevent to kick-back, the bottom of connecting plate 4 is provided with backup pad 7, one side of backup pad 7 is connected with box 22, the both ends of backup pad 7 all are provided with mounting panel A8, notes material pipe 20 has been seted up at the top of box 22, notes material pipe 20 threaded connection has the top cap, ventilative net 19 has all been seted up to the inside of connecting plate 4, guard plate 5, avoids increasing the windage, the notch has been seted up at the top of surge bin 12, the inside of notch is provided with bracing piece 18, the both sides of shock attenuation gasbag 6 are provided with the fixed plate, the inside of fixed plate is provided with mounting bolt, is convenient for installation shock attenuation gasbag 6.
The working principle of the utility model is as follows: the airplane wing protection device is characterized in that a machine body 1 is arranged on the top of a box body 22, a connecting rod 2 is arranged on one side of the machine body 1, a wing 3 is installed on one side of the connecting rod 2, a connecting plate 4 is arranged on one side of the box body 22 when the wing 3 flies, a damping airbag 6 is arranged on one side of the connecting plate 4, a protection plate 5 is connected to one side of the damping airbag 6, when an object is collided, the damping airbag 6 and the protection plate 5 protect the wing 3 and prevent the wing 3 from being damaged and falling, conveying pipes 9 are arranged on two sides of the box body 22, a spray head 10 is installed at the bottom of each conveying pipe 9 and sprays fire extinguishing dry powder, a supporting rod 18 is arranged at the bottom of a connecting plate 11, the bottom of each supporting rod 18 is connected with a butt plate 17 through a damping bin 12, the butt plates 17 are matched with damping springs 16 to relieve descending impact force, supporting columns 13 are installed at the bottom of the damping bins 12, and walking wheels 14 are arranged at the bottoms of the supporting columns 13, when the machine body 1 descends, the damage to the machine body 1 is avoided.
Finally, it should be noted that: although the present invention has been described in detail with reference to the foregoing embodiments, it will be apparent to those skilled in the art that changes may be made in the embodiments and/or equivalents thereof without departing from the spirit and scope of the utility model. Any modification, equivalent replacement, or improvement made within the spirit and principle of the present invention should be included in the protection scope of the present invention.
Claims (7)
1. The utility model provides an anticollision formula fire control unmanned aerial vehicle, includes box (22), organism (1), connecting rod (2), its characterized in that: the aircraft is characterized in that a machine body (1) is arranged at the top of the box body (22), a connecting rod (2) is arranged on one side of the machine body (1), a wing (3) is installed on one side of the connecting rod (2), a connecting plate (4) is arranged on one side of the box body (22), a damping air bag (6) is arranged on one side of the connecting plate (4), a protection plate (5) is connected to one side of the damping air bag (6), conveying pipes (9) are arranged on two sides of the box body (22), a spray head (10) is installed at the bottom of each conveying pipe (9), a connecting plate (11) is arranged at the bottom of the box body (22), a supporting rod (18) is arranged at the bottom of the connecting plate (11), a butt plate (17) is connected to the bottom of the supporting rod (18) through a damping bin (12), a damping spring (16) is arranged at the bottom of the butt plate (17), and a supporting column (13) is installed at the bottom of the damping bin (12), and a travelling wheel (14) is arranged at the bottom of the supporting column (13).
2. The anti-collision fire-fighting unmanned aerial vehicle of claim 1, wherein: damping plates (15) are arranged at two ends of the damping spring (16).
3. The anti-collision fire-fighting unmanned aerial vehicle of claim 1, wherein: the bottom of connecting plate (4) is provided with backup pad (7), one side of backup pad (7) is connected with box (22), the both ends of backup pad (7) all are provided with mounting panel A (8).
4. The anti-collision fire-fighting unmanned aerial vehicle of claim 1, wherein: the top of the box body (22) is provided with a material injection pipe (20), and the material injection pipe (20) is in threaded connection with a top cover.
5. The anti-collision fire-fighting unmanned aerial vehicle of claim 1, wherein: the connecting plate (4) and the protection plate (5) are both internally provided with a breathable net (19).
6. The anti-collision fire-fighting unmanned aerial vehicle of claim 1, wherein: the top of the damping bin (12) is provided with a notch, and a supporting rod (18) is arranged inside the notch.
7. The anti-collision fire-fighting unmanned aerial vehicle of claim 1, wherein: and fixing plates are arranged on two sides of the damping air bag (6), and mounting bolts are arranged in the fixing plates.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202123332403.0U CN216546704U (en) | 2021-12-28 | 2021-12-28 | Anticollision formula fire control unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202123332403.0U CN216546704U (en) | 2021-12-28 | 2021-12-28 | Anticollision formula fire control unmanned aerial vehicle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN216546704U true CN216546704U (en) | 2022-05-17 |
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ID=81559446
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202123332403.0U Active CN216546704U (en) | 2021-12-28 | 2021-12-28 | Anticollision formula fire control unmanned aerial vehicle |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN216546704U (en) |
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2021
- 2021-12-28 CN CN202123332403.0U patent/CN216546704U/en active Active
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