CN211468755U - Unmanned aerial vehicle capable of lowering water falling surface - Google Patents
Unmanned aerial vehicle capable of lowering water falling surface Download PDFInfo
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- CN211468755U CN211468755U CN201921922492.4U CN201921922492U CN211468755U CN 211468755 U CN211468755 U CN 211468755U CN 201921922492 U CN201921922492 U CN 201921922492U CN 211468755 U CN211468755 U CN 211468755U
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- aerial vehicle
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Abstract
The utility model provides an unmanned aerial vehicle capable of landing on water surface, which comprises an unmanned aerial vehicle body, a lighting lamp, a camera, a battery cabin, a fixed plate, a driving part, wings, a foot rest rod, an inflator pump, a floating body, a foot rest and a buffer spring, wherein the unmanned aerial vehicle body is provided with a connecting rod, one side of the connecting rod is provided with the inflator pump, the inflator pump is communicated with the floating body, and the foot rest is arranged below the floating body; a buffer spring is arranged inside the foot rest; the side is equipped with a plurality of archs on the protective housing. The utility model discloses the body, the setting of foot rest and protecting crust, simple structure is favorable to realizing steadily descending to the surface of water, prevents to receive the restriction on ground and can't carry out the condition of descending, can realize the steady descending on surface of water and ground through foot rest and body, the marketing and the application of being convenient for.
Description
Technical Field
The utility model belongs to the technical field of unmanned aerial vehicle, especially, relate to an unmanned aerial vehicle of face can fall into water.
Background
The existing unmanned aerial vehicle is a flying device which can fly through remote control, the unmanned aerial vehicle can be divided into military use and civil use according to the application field, the unmanned aerial vehicle is divided into a reconnaissance plane and a target plane, the civil use aspect and the industrial application of the unmanned aerial vehicle are really just needed by the unmanned aerial vehicle, and the unmanned aerial vehicle is currently applied in the fields of aerial photography, agriculture, plant protection, micro self-timer, express transportation, disaster relief, wild animal observation, infectious disease monitoring, surveying and mapping, news reporting, electric power inspection, disaster relief, movie and television shooting, romantic manufacturing and the like, so that the use of the unmanned aerial vehicle is greatly expanded.
But current unmanned aerial vehicle can't guarantee to realize descending on ground and the surface of water, and especially unmanned aerial vehicle ground descending receives the restriction, can't carry out ground descending, and does not possess the problem of surface of water descending ability again.
Therefore, the unmanned aerial vehicle capable of lowering the water level is very necessary to be invented.
SUMMERY OF THE UTILITY MODEL
In order to solve the technical problem, the utility model provides an unmanned aerial vehicle of surface of water can descend to solve current unmanned aerial vehicle and can't guarantee to realize descending on ground and the surface of water, especially unmanned aerial vehicle ground descending receives the restriction, can't carry out ground descending, and does not possess the problem of surface of water descending ability again. An unmanned aerial vehicle capable of lowering a water falling surface comprises an unmanned aerial vehicle body, a lighting lamp, cameras, battery bins, a fixing plate, a driving part, wings, a foot rest rod, an inflator pump, a floating body, foot rests and buffer springs, wherein the lighting lamp is arranged above the unmanned aerial vehicle body, the cameras are arranged on the unmanned aerial vehicle body, and two battery bins are arranged on two sides of each camera; fixing plates are arranged on two sides of the unmanned aerial vehicle body, wherein a driving part is arranged on each fixing plate, and the driving part is connected with the wings; the unmanned aerial vehicle body is provided with a leg frame rod, wherein an inflator pump is arranged on one side of the leg frame rod and is communicated with the floating body, and a foot rest is arranged below the floating body; a buffer spring is arranged in the foot rest.
The body includes the protecting crust, and is protruding, protection rubber circle and gasbag, the protecting crust up side is equipped with a plurality of archs, and wherein the protecting crust is inside to be inlayed and to have the protection rubber circle, and this protection rubber encloses inside and is equipped with the gasbag.
The upper side surface of the protective shell is inclined to one side, and the lower side surface of the protective shell is in a horizontal plane; the protrusions are approximately in an isosceles trapezoid structure.
The foot rest is characterized in that a circular hollow bulge is arranged at the lower end of the foot rest rod, an internal thread is arranged inside the circular hollow bulge, a solid circular bulge is arranged at the upper end of the foot rest, and an external thread is arranged outside the solid circular bulge.
The floating body is of a square structure, wherein the lower end of the foot rest rod and the upper end of the foot rest penetrate through the floating body to fix the foot rest rod and the foot rest.
Compared with the prior art, the utility model discloses following beneficial effect has:
1. the utility model discloses the setting of body is favorable to realizing steadily descending to the surface of water, prevents to receive the unable condition of descending that carries out of restriction on ground, can realize the steady descending on surface of water and ground through foot rest and body.
2. The utility model discloses the setting of protecting crust is favorable to the inclined plane through side on one's body, avoids appearing body top storage river for the sunken condition of body guarantees the long-time safe descending of unmanned aerial vehicle on the surface of water.
3. The utility model discloses the setting of foot rest is favorable to the solid circular arch through self upper end, carries out the foot rest and the body that quick replacement damaged, can optimize and use experience.
Drawings
Fig. 1 is a schematic structural diagram of the present invention.
Fig. 2 is a schematic view of the foot stool of the present invention.
Fig. 3 is a schematic view of the floating body structure of the present invention.
Fig. 4 is a side view schematic diagram of the floating body of the present invention.
In the figure:
the unmanned aerial vehicle comprises an unmanned aerial vehicle body, 2-a lighting lamp, 3-a camera, 4-a battery cabin, 5-a fixing plate, 6-a driving part, 7-a wing, 8-a scaffold rod, 9-an inflator pump, 10-a floating body, 101-a protective shell, 102-a bulge, 103-a protective rubber ring, 104-an air bag, 11-a foot rest and 12-a buffer spring.
Detailed Description
In order to make the technical solution of the present invention better understood, the technical solution of the embodiments of the present invention will be clearly and completely described below, and it is obvious that the described embodiments are only some embodiments of the present invention, not all embodiments. Based on the embodiments in the present invention, all other embodiments obtained by a person skilled in the art without creative efforts shall belong to the protection scope of the present invention.
As shown in figures 1 to 4
The utility model provides an unmanned aerial vehicle of surface of water can descend, including unmanned aerial vehicle body 1, light 2, camera 3, battery compartment 4, fixed plate 5, drive division 6, wing 7, foot rest pole 8, inflator pump 9, body 10, foot rest 11 and buffer spring 12, when unmanned aerial vehicle ground descending receives the restriction, when needing to descend the surface of water, body 10 with the unmanned aerial vehicle below carries out and the surface of water contact, because the inside gas that is full of body 10, so make body 10 form a small-size raft body, support unmanned aerial vehicle and descend to the surface of water, when river falls on body 10, because the side is an inclined plane on protective housing 101, so make river can't carry out and save above body 10, river can carry out the body through the recess between protruding 102 and the protruding 102 and flow down 10.
When the foot rest 11 or the floating body 10 needs to be replaced, the floating body 10 is detached from the inflator pump 9 after being screwed out from the lower end of the foot rest bar 8 through the bulge above the foot rest 11, then the prepared foot rest 11 and the floating body 10 are replaced, the floating body 10 is sleeved at the bulge at the lower end of the foot rest bar 8, then the connection is carried out through the bulge above the foot rest 11, then the foot rest 11 is connected with the foot rest bar 8, and the floating body 10 can be fixed when the foot rest 11 is connected with the foot rest bar 8.
Utilize technical scheme, or technical personnel in the field are in the utility model discloses under technical scheme's the inspiration, design similar technical scheme, and reach above-mentioned technological effect, all fall into the utility model discloses a protection scope.
Claims (5)
1. The utility model provides an unmanned aerial vehicle of surface falls into water which characterized in that: the unmanned aerial vehicle comprises an unmanned aerial vehicle body (1), a lighting lamp (2), a camera (3), battery bins (4), a fixing plate (5), a driving part (6), wings (7), a leg frame rod (8), an inflator pump (9), a floating body (10), foot frames (11) and buffer springs (12), wherein the lighting lamp (2) is arranged above the unmanned aerial vehicle body (1), the camera (3) is arranged on the unmanned aerial vehicle body (1), and two battery bins (4) are arranged on two sides of the camera (3); fixing plates (5) are arranged on two sides of the unmanned aerial vehicle body (1), wherein a driving part (6) is arranged on each fixing plate (5), and the driving part (6) is connected with the wings (7); the unmanned aerial vehicle body (1) is provided with a leg frame rod (8), wherein one side of the leg frame rod (8) is provided with an inflator pump (9), the inflator pump (9) is communicated with a floating body (10), and a foot rest (11) is arranged below the floating body (10); a buffer spring (12) is arranged in the foot rest (11).
2. A surface-mountable drone according to claim 1, characterised in that: the floating body (10) comprises a protective shell (101), protrusions (102), a protective rubber ring (103) and an air bag (104), wherein the plurality of protrusions (102) are arranged on the upper side face of the protective shell (101), the protective rubber ring (103) is embedded in the protective shell (101), and the air bag (104) is arranged in the protective rubber ring (103).
3. The unmanned aerial vehicle capable of lowering water level of claim 2, wherein: the upper side surface of the protective shell (101) inclines towards one side, wherein the lower side surface of the protective shell (101) is in a horizontal plane; the protrusions (102) are approximately in an isosceles trapezoid structure.
4. A surface-mountable drone according to claim 1, characterised in that: the lower end of the foot rest rod (8) is provided with a circular hollow bulge, wherein an internal thread is arranged inside the circular hollow bulge, the upper end of the foot rest (11) is provided with a solid circular bulge, and an external thread is arranged outside the solid circular bulge.
5. A surface-mountable drone according to claim 1, characterised in that: the floating body (10) adopts a square structure, wherein the lower end of the foot rest rod (8) and the upper end of the foot rest (11) penetrate through the floating body (10) to fix the same.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201921922492.4U CN211468755U (en) | 2019-11-08 | 2019-11-08 | Unmanned aerial vehicle capable of lowering water falling surface |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201921922492.4U CN211468755U (en) | 2019-11-08 | 2019-11-08 | Unmanned aerial vehicle capable of lowering water falling surface |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN211468755U true CN211468755U (en) | 2020-09-11 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201921922492.4U Active CN211468755U (en) | 2019-11-08 | 2019-11-08 | Unmanned aerial vehicle capable of lowering water falling surface |
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| CN (1) | CN211468755U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112918694A (en) * | 2021-04-02 | 2021-06-08 | 北京博观寰宇科技有限公司 | Equipment of unmanned aerial vehicle protection of saving oneself of falling into water is exclusively used in |
-
2019
- 2019-11-08 CN CN201921922492.4U patent/CN211468755U/en active Active
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112918694A (en) * | 2021-04-02 | 2021-06-08 | 北京博观寰宇科技有限公司 | Equipment of unmanned aerial vehicle protection of saving oneself of falling into water is exclusively used in |
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