CN210912904U - Scalable comprehensive protection device of unmanned aerial vehicle - Google Patents
Scalable comprehensive protection device of unmanned aerial vehicle Download PDFInfo
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- CN210912904U CN210912904U CN201922066411.1U CN201922066411U CN210912904U CN 210912904 U CN210912904 U CN 210912904U CN 201922066411 U CN201922066411 U CN 201922066411U CN 210912904 U CN210912904 U CN 210912904U
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- unmanned aerial
- sleeve
- aerial vehicle
- holding tank
- auxiliary rod
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Abstract
The utility model belongs to the technical field of the unmanned aerial vehicle protection technique and specifically relates to a scalable comprehensive protection device of unmanned aerial vehicle, the female joint comprises a sleeve, the staple bolt is installed at the sleeve top, the sleeve passes through the staple bolt and is connected with the unmanned aerial vehicle horn, sleeve and unmanned aerial vehicle horn parallel arrangement, and the sleeve interpolation is equipped with the mobile jib, the mobile jib top is equipped with first holding tank, the sleeve one end is kept away from to the mobile jib is equipped with the connecting plate, it is connected with the auxiliary rod to rotate between two connecting plates, the auxiliary rod holds to the mobile jib in, be equipped with locking mechanical system between auxiliary rod and the connecting plate, the auxiliary rod inboard is equipped with the second holding tank, second holding tank tip rotates and is connected with the connecting block, be equipped with the third holding tank in the connecting block, the third holding tank internal. The device simple structure, it is swift to use, can protect unmanned aerial vehicle's wing, avoids unmanned aerial vehicle to damage the problem because of the wing that the misoperation arouses.
Description
Technical Field
The utility model relates to an unmanned aerial vehicle protects technical field, especially relates to a scalable comprehensive protection device of unmanned aerial vehicle.
Background
Along with the development of the society and the improvement of the living standard of people, people have requirements on the living environment of the people, the flying development of the modern society enables people to learn the society more widely, people desire to explore the sky and want to soar the sky like birds, so that people have airplanes, but not everyone has the possibility of flying to the sky, and not everyone can drive the airplanes, but the unmanned aerial vehicle is an invention for people to fly to the sky and does not need to spend much money, but the existing unmanned aerial vehicle is not particularly expensive, but the people who are poor and people can not own, and the unmanned aerial vehicle flying to the sky also needs protection measures, if the unmanned aerial vehicle is not operated well, the unmanned aerial vehicle is easy to hit large buildings or birds, so that the unmanned aerial vehicle is damaged, but the existing unmanned aerial vehicle does not have corresponding protection measures, the thing that the striking damaged appears very easily takes place, consequently, we propose the scalable comprehensive protection device of unmanned aerial vehicle, protect unmanned aerial vehicle.
SUMMERY OF THE UTILITY MODEL
The utility model aims at solving the shortcoming that self damage appears easily in having unmanned aerial vehicle under the improper condition of operation among the prior art, and the scalable comprehensive protection device of unmanned aerial vehicle that provides.
In order to achieve the above purpose, the utility model adopts the following technical scheme:
the design is an unmanned aerial vehicle telescopic comprehensive protection device, which comprises a sleeve, wherein the top of the sleeve is provided with a hoop, the sleeve is connected with an unmanned aerial vehicle arm through the hoop, the sleeve is arranged in parallel with the unmanned aerial vehicle arm, the opening of the sleeve is outwards arranged, a main rod is inserted in the sleeve, the top of the main rod is provided with a first accommodating groove, one end of the main rod, which is far away from the sleeve, is provided with two connecting plates, the two connecting plates are symmetrically arranged, an auxiliary rod is rotatably connected between the two connecting plates and accommodated in the main rod, a locking mechanism is arranged between the auxiliary rod and the connecting plates, the inner side of the auxiliary rod is provided with a second accommodating groove, the end part of the second accommodating groove is rotatably connected with a connecting block, a third accommodating groove is arranged in the connecting block, the third accommodating groove is connected with two, and the connecting block and the protective support are accommodated in the second accommodating groove.
Preferably, the number of the hoops is two, and the two hoops are arranged at intervals.
Preferably, a locking bolt is installed at the bottom end of the opening of the sleeve.
Preferably, the locking mechanism comprises two clamping grooves and two clamping blocks, the clamping grooves are formed in the inner sides of the connecting plates, the two clamping grooves are arranged in an angle of 90 degrees by taking the auxiliary rod as an axis, the clamping blocks are arranged on the auxiliary rod, and the clamping blocks are matched with the clamping grooves.
Preferably, the two groups of torsion springs are arranged in opposite directions.
The utility model provides a scalable comprehensive protection device of unmanned aerial vehicle, beneficial effect lies in: the device simple structure, it is swift to use, can protect unmanned aerial vehicle's wing, avoids unmanned aerial vehicle to damage the problem because of the wing that the misoperation arouses, and the device has the elasticity simultaneously, can accomodate to the sleeve in, is connected simple to operate through staple bolt and unmanned aerial vehicle horn.
Drawings
Fig. 1 is a schematic structural view of a retractable comprehensive protection device for an unmanned aerial vehicle according to the present invention;
fig. 2 is a top view of the retractable overall protection device for an unmanned aerial vehicle according to the present invention;
fig. 3 is the utility model provides a scalable comprehensive protection device of unmanned aerial vehicle's cross-sectional view.
In the figure: unmanned aerial vehicle horn 1, sleeve 2, staple bolt 21, locking bolt 22, mobile jib 3, first holding tank 31, connecting plate 4, draw-in groove 41, fixture block 42, auxiliary rod 5, second holding tank 51, connecting block 6, third holding tank 61, torsional spring 62, protective bracket 7.
Detailed Description
The technical solutions in the embodiments of the present invention will be described clearly and completely with reference to the accompanying 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.
Referring to fig. 1-3, a scalable comprehensive protection device of unmanned aerial vehicle, including sleeve 2, staple bolt 21 is installed at 2 tops of sleeve, and staple bolt 21 quantity is two, and two staple bolt 21 intervals set up, and sleeve 2 is connected with unmanned aerial vehicle horn 1 through staple bolt 21, sleeve 2 and 1 parallel arrangement of unmanned aerial vehicle horn, staple bolt 21 and 1 zonulae occludens of unmanned aerial vehicle horn, and staple bolt 21 that the interval set up can make sleeve 2 install more stably, can not appear trembling.
The opening of the sleeve 2 is outwards arranged, a locking bolt 22 is installed at the bottom end of the opening of the sleeve 2, a main rod 3 is inserted into the sleeve 2, a first accommodating groove 31 is formed in the top of the main rod 3, connecting plates 4 are arranged at one end, away from the sleeve 2, of the main rod 3, the number of the connecting plates 4 is two, the two connecting plates 4 are symmetrically arranged, an auxiliary rod 5 is rotatably connected between the two connecting plates 4, the auxiliary rod 5 is accommodated into the main rod 3, a locking mechanism is arranged between the auxiliary rod 5 and the connecting plates 4 and comprises a clamping groove 41 and a clamping block 42, clamping grooves 41 are formed in the inner sides of the two connecting plates 4, the number of the clamping grooves 41 is two, the two clamping grooves 41 are arranged at 90 degrees by taking the auxiliary rod 5 as an axis, the clamping block 42 is arranged on the auxiliary rod 5, the clamping block 42 and the clamping groove 41 are matched with each other, when the secondary rod 5 is placed in the first accommodating groove 31, the fixture block 42 is clamped with one of the fixture grooves 41 to prevent loosening, and when the secondary rod 5 is vertical, the fixture block 42 is clamped with the other fixture groove 41 to lock the secondary rod 5.
The inner side of the auxiliary rod 5 is provided with a second holding groove 51, the end part of the second holding groove 51 is rotatably connected with a connecting block 6, a third holding groove 61 is arranged in the connecting block 6, the third holding groove 61 is rotatably connected with two groups of protective supports 7, the two groups of protective supports 7 are symmetrically arranged, a rotating shaft connecting the protective supports 7 and the connecting block 6 is provided with a torsion spring 62, the two groups of torsion springs 62 are reversely arranged, the connecting block 6 and the protective supports 7 are accommodated in the second holding groove 51, the two protective supports 7 are used for protecting the wings of the unmanned aerial vehicle, the connecting block 6 and the protective supports 7 are both accommodated through the second holding groove 51, when in use, the connecting block 6 is rotated out of the second holding groove 51, the protective wall plates 7 are outwards expanded under the action of the torsion spring 62 without the blocking of the auxiliary rod 5, meanwhile, the supports 7 are abutted against the edges of the auxiliary, protect unmanned aerial vehicle.
The above, only be the concrete implementation of the preferred embodiment of the present invention, but the protection scope of the present invention is not limited thereto, and any person skilled in the art is in the technical scope of the present invention, according to the technical solution of the present invention and the utility model, the concept of which is equivalent to replace or change, should be covered within the protection scope of the present invention.
Claims (5)
1. The telescopic comprehensive protection device for the unmanned aerial vehicle comprises a sleeve (2) and is characterized in that a hoop (21) is installed at the top of the sleeve (2), the sleeve (2) is connected with an unmanned aerial vehicle arm (1) through the hoop (21), the sleeve (2) is arranged in parallel with the unmanned aerial vehicle arm (1), the opening of the sleeve (2) is arranged outwards, a main rod (3) is inserted into the sleeve (2), a first accommodating groove (31) is formed in the top of the main rod (3), a connecting plate (4) is arranged at one end, away from the sleeve (2), of the main rod (3), the number of the connecting plates (4) is two, the two connecting plates (4) are symmetrically arranged, an auxiliary rod (5) is rotatably connected between the two connecting plates (4), the auxiliary rod (5) is accommodated into the main rod (3), and a locking mechanism is arranged between the auxiliary rod (5) and the connecting plates (4), auxiliary rod (5) inboard is equipped with second holding tank (51), second holding tank (51) tip rotates and is connected with connecting block (6), be equipped with third holding tank (61) in connecting block (6), third holding tank (61) internal rotation is connected with two sets of protection support (7), and is two sets of protection support (7) symmetry sets up, connects be equipped with torsional spring (62) in the pivot of protection support (7) and connecting block (6), connecting block (6) and protection support (7) hold to second holding tank (51) in.
2. The scalable comprehensive protection device of unmanned aerial vehicle of claim 1, characterized in that, staple bolt (21) quantity is two, and two staple bolt (21) interval sets up.
3. The telescopic full protection device for unmanned aerial vehicles according to claim 1, wherein a locking bolt (22) is installed at the bottom end of the opening of the sleeve (2).
4. The telescopic comprehensive protection device for the unmanned aerial vehicle as claimed in claim 1, wherein the locking mechanism comprises two clamping grooves (41) and two clamping blocks (42), the clamping grooves (41) are formed in the inner sides of the two connecting plates (4), the two clamping grooves (41) are arranged at 90 degrees by taking the auxiliary rod (5) as an axis, the clamping blocks (42) are arranged on the auxiliary rod (5), and the clamping blocks (42) and the clamping grooves (41) are matched with each other.
5. The telescopic full protection device for unmanned aerial vehicles according to claim 1, wherein the two sets of torsion springs (62) are arranged in opposite directions.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201922066411.1U CN210912904U (en) | 2019-11-26 | 2019-11-26 | Scalable comprehensive protection device of unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201922066411.1U CN210912904U (en) | 2019-11-26 | 2019-11-26 | Scalable comprehensive protection device of unmanned aerial vehicle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN210912904U true CN210912904U (en) | 2020-07-03 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201922066411.1U Active CN210912904U (en) | 2019-11-26 | 2019-11-26 | Scalable comprehensive protection device of unmanned aerial vehicle |
Country Status (1)
| Country | Link |
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| CN (1) | CN210912904U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112027076A (en) * | 2020-08-24 | 2020-12-04 | 王呼呼 | Unmanned aerial vehicle transfer device capable of protecting wings |
-
2019
- 2019-11-26 CN CN201922066411.1U patent/CN210912904U/en active Active
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112027076A (en) * | 2020-08-24 | 2020-12-04 | 王呼呼 | Unmanned aerial vehicle transfer device capable of protecting wings |
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