CN220518602U - Unmanned aerial vehicle wing protection casing convenient to installation - Google Patents
Unmanned aerial vehicle wing protection casing convenient to installation Download PDFInfo
- Publication number
- CN220518602U CN220518602U CN202321516596.1U CN202321516596U CN220518602U CN 220518602 U CN220518602 U CN 220518602U CN 202321516596 U CN202321516596 U CN 202321516596U CN 220518602 U CN220518602 U CN 220518602U
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- CN
- China
- Prior art keywords
- protection casing
- unmanned aerial
- aerial vehicle
- swivel
- fixedly connected
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- 238000009434 installation Methods 0.000 title claims description 7
- 230000007246 mechanism Effects 0.000 claims description 3
- 230000001681 protective effect Effects 0.000 abstract description 9
- 230000000694 effects Effects 0.000 description 9
- 238000000926 separation method Methods 0.000 description 5
- 230000007547 defect Effects 0.000 description 2
- 230000005484 gravity Effects 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
- 230000009471 action Effects 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 239000000428 dust Substances 0.000 description 1
- 230000006872 improvement Effects 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 230000008569 process Effects 0.000 description 1
- 238000005406 washing Methods 0.000 description 1
Classifications
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/40—Weight reduction
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- Forklifts And Lifting Vehicles (AREA)
Abstract
The utility model discloses an unmanned aerial vehicle wing protection cover convenient to install, which comprises a machine body and a plurality of upper protection covers, wherein a plurality of wing bodies are arranged on the outer side of the machine body, a lower protection cover is clamped at the bottom of the upper protection cover, the wing bodies are positioned in the upper protection cover, a swivel is rotatably connected to the top of the upper protection cover, two guide rods are inserted into the upper protection cover, the guide rods are fixed with the lower protection cover, limit rings are fixedly connected to the top ends of the two guide rods, clamping grooves are formed in one side of each guide rod, and the clamping grooves are clamped with the swivel. The utility model not only can facilitate the staff to detach and clean the protective cover and improve the convenience of the device, but also can limit the moving height of the lower protective cover through the limiting ring, and can guide the lower protective cover through the guide rod so as to stably move.
Description
Technical Field
The utility model relates to the technical field of unmanned aerial vehicles, in particular to an unmanned aerial vehicle wing protective cover convenient to install.
Background
Unmanned aerial vehicle is a unmanned aerial vehicle that utilizes radio remote control equipment, and unmanned aerial vehicle mostly has the wing, in order to avoid the wing to hurt the people, usually will be equipped with the protection casing to prevent touching the wing.
Through searching, publication number CN208947589U discloses an unmanned aerial vehicle wing protection cover convenient to install, and in the background art, it is proposed that dust is easily accumulated on a net structure at the outer end of a wing due to electrostatic action in the rotation process of the unmanned aerial vehicle wing, and the defects of the above-mentioned patent are: the net structure of outer end is inconvenient the user dismantles the washing, influences unmanned aerial vehicle's normal operating's problem, proposes a protection casing of new construction first and solves above-mentioned problem.
Disclosure of Invention
The utility model aims to solve the defects in the prior art, and provides an unmanned aerial vehicle wing protective cover convenient to install.
In order to achieve the above purpose, the present utility model adopts the following technical scheme:
the utility model provides an unmanned aerial vehicle wing protection casing convenient to installation, includes organism and a plurality of last protection casing, the outside of organism is equipped with a plurality of wing bodies, the bottom joint of going up the protection casing has lower protection casing, and the wing body is located the inside of going up the protection casing, the top of going up the protection casing rotates and is connected with the swivel, the inside of going up the protection casing is pegged graft there are two guide bars, and the guide bar is fixed mutually with lower protection casing, two the top fixedly connected with spacing ring of guide bar, the draw-in groove has been seted up to one side of guide bar, and draw-in groove and swivel looks joint, a plurality of keep away the position groove has been seted up to the circumference inner wall of swivel, be equipped with fixed establishment between swivel and the last protection casing.
As a still further scheme of the utility model, the fixing mechanism comprises a fixing block, the fixing block is fixed on the outer wall of one side of the upper protective cover through bolts, a slot is formed in the fixing block, a baffle is fixedly connected to the outer wall of one side of the swivel, a plugboard is fixedly connected to one side of the baffle, and the plugboard is spliced with the slot.
As a still further scheme of the utility model, one side of the baffle is fixedly connected with a second magnetic block.
As a still further scheme of the utility model, one side of the fixed block is fixedly connected with a first magnetic block, and the first magnetic block is contacted with a second magnetic block.
As a still further scheme of the utility model, a stop block is fixedly connected with the outer wall of one side of the upper protective cover.
As a still further scheme of the utility model, one side of the swivel is fixedly connected with a swivel handle.
As a still further scheme of the utility model, a plurality of anti-skid patterns are arranged on one side of the rotating handle, and the anti-skid patterns are uniformly distributed.
The beneficial effects of the utility model are as follows:
1. through the cooperation of last protection casing and lower protection casing use, rotate the swivel, make the picture peg shift out the slot, the guide bar is located keeps away the position inslot simultaneously, and lower protection casing down moves under the effect of gravity this moment, makes last protection casing and lower protection casing separation, then the staff shifts out the wing body with the protection casing, and then makes things convenient for the staff to dismantle the clearance to the protection casing, has improved the convenience of device.
2. Through the setting of dog, the dog can be limited the distance that the handle moved, when rotating the handle and making it contact with the dog, the guide bar is located keeps away the position inslot, reaches assistance-localization real-time's effect.
3. Through the setting of spacing ring, the spacing ring can restrict the height that the lower protection casing removed, avoids the guide bar to shift out the result of use that upper protection casing influences the device, has improved the restriction effect of device.
Drawings
Fig. 1 is a schematic perspective view of an unmanned aerial vehicle wing shield for easy installation;
FIG. 2 is a schematic view of a partially cut-away structure of an unmanned aerial vehicle wing shield according to the present utility model for easy installation;
fig. 3 is a schematic diagram of a local enlarged structure of an unmanned aerial vehicle wing shield provided by the utility model, which is convenient to install.
In the figure: 1. a body; 2. an upper protective cover; 3. a stop block; 4. a swivel; 5. a clearance groove; 6. a clamping groove; 7. a wing body; 8. a lower protective cover; 9. a rotating handle; 10. anti-skid lines; 11. a guide rod; 12. a limiting ring; 13. a fixed block; 14. a slot; 15. inserting plate; 16. a first magnetic block; 17. a second magnetic block; 18. and a baffle.
Detailed Description
The following description of the embodiments of the present utility model will be made with reference to the accompanying drawings, in which embodiments of the present utility model are shown, and in which embodiments are shown, by way of illustration, only, and not all embodiments of the utility model. All other embodiments, which can be made by those skilled in the art based on the embodiments of the utility model without making any inventive effort, are intended to be within the scope of the utility model.
Referring to fig. 1-3, an unmanned aerial vehicle wing protection casing convenient to installation, including organism 1 and a plurality of protection casing 2 of going up, the outside of organism 1 is equipped with a plurality of wing bodies 7, the bottom joint of going up protection casing 2 has lower protection casing 8, and wing body 7 is located the inside of going up protection casing 2, the top rotation of going up protection casing 2 is connected with swivel 4, the inside grafting of going up protection casing 2 has two guide bars 11, and guide bar 11 is fixed with lower protection casing 8 mutually, guide bar 11 can lead to lower protection casing 8, make it can be stable remove, the top of two guide bars 11 is through the bolt fastening limiting ring 12, limiting ring 12 can restrict the height that lower protection casing 8 removed, avoid guide bar 11 to shift out the result of use of protection casing 2 influence device, draw-in groove 6 has been seted up to one side of guide bar 11, and draw-in groove 6 and swivel 4 looks joint, a plurality of keeping away position grooves 5 have been seted up to the circumference inner wall of swivel 4 and go up between protection casing 2, rotate swivel 4, make guide bar 11 and its separation protection casing 8, and the effect that keeps away position groove 5 makes the guide bar 11 and keep away from the protection casing 8, and then make the effect that the guide bar is moved down by the guide bar 8, and then make the work personnel remove down, and make the lower protection casing 8 remove down, and then make things convenient for the person to detach under the effect of the guide bar, and the effect of moving down, and the protection casing 8, and then remove down the people.
In the utility model, it is to be noted that the fixing mechanism comprises a fixing block 13, the fixing block 13 is fixed on one side outer wall of the upper protection cover 2 through a bolt, a slot 14 is formed in the fixing block 13, a baffle 18 is welded on one side outer wall of the rotating handle 4, a plugboard 15 is fixed on one side of the baffle 18 through a bolt, the plugboard 15 is spliced with the slot 14, a second magnetic block 17 is fixed on one side of the baffle 18 through a bolt, a first magnetic block 16 is fixed on one side of the fixing block 13 through a bolt, the first magnetic block 16 is contacted with the second magnetic block 17, the rotating handle 4 is rotated to enable the plugboard 15 to move out of the slot 14, the first magnetic block 16 is separated from the second magnetic block 17, a stop 3 is fixed on one side outer wall of the upper protection cover 2 through a bolt, the stop 3 can limit the moving distance of the rotating handle 9, when the rotating handle 9 is contacted with the stop 3, a guide rod 11 is positioned in the slot 5 to achieve the effect of auxiliary positioning, the rotating handle 9 is fixed on one side of the rotating handle 4 through a bolt, the rotating handle 9 is convenient for a worker to rotate the rotating handle 4, a plurality of anti-skidding patterns 10 are distributed uniformly.
Working principle: when the protection casing needs to be dismantled, at first rotate swivel 4, make picture peg 15 shift out slot 14, first magnetic path 16 and second magnetic path 17 separation, swivel 4 removes simultaneously and makes guide bar 11 rather than the separation, keep away the position groove 5 and keep away the position to guide bar 11, lower protection casing 8 moves down under the effect of gravity this moment, thereby make guide bar 11 drive spacing ring 12 and move down, and then make protection casing 2 and lower protection casing 8 separation, then the staff shifts out wing body 7 with the protection casing, and then the convenience staff dismantles the clearance to the protection casing.
Finally, it should be noted that: modifications of the embodiments described in the foregoing will be readily apparent to those skilled in the art, and equivalents may be substituted for elements thereof. Any modification, equivalent replacement, improvement, etc. made within the spirit and principle of the present utility model should be included in the protection scope of the present utility model.
Claims (7)
1. Unmanned aerial vehicle wing protection casing convenient to installation, including organism (1) and a plurality of last protection casing (2), the outside of organism (1) is equipped with a plurality of wing bodies (7), a serial communication port, the bottom joint of going up protection casing (2) has lower protection casing (8), and wing body (7) are located the inside of going up protection casing (2), the top rotation of going up protection casing (2) is connected with swivel (4), the inside grafting of going up protection casing (2) has two guide bars (11), and guide bars (11) are fixed mutually with lower protection casing (8), two the top fixedly connected with spacing ring (12) of guide bar (11), draw-in groove (6) have been seted up to one side of guide bar (11), and draw-in groove (6) and swivel (4) looks joint, a plurality of keep away position groove (5) have been seted up to the circumference inner wall of swivel (4), be equipped with fixed establishment between swivel (4) and the last protection casing (2).
2. The unmanned aerial vehicle wing protection cover convenient to install according to claim 1, wherein the fixing mechanism comprises a fixing block (13), the fixing block (13) is fixed on one side outer wall of the upper protection cover (2) through a bolt, a slot (14) is formed in the fixing block (13), a baffle plate (18) is fixedly connected to one side outer wall of the swivel (4), a plugboard (15) is fixedly connected to one side of the baffle plate (18), and the plugboard (15) is spliced with the slot (14).
3. An unmanned aerial vehicle wing shield according to claim 2, wherein a second magnet (17) is fixedly connected to one side of the shield (18).
4. An unmanned aerial vehicle wing protection cover convenient to install according to claim 3, wherein a first magnetic block (16) is fixedly connected to one side of the fixed block (13), and the first magnetic block (16) is in contact with a second magnetic block (17).
5. The unmanned aerial vehicle wing protection cover convenient to install according to claim 1, wherein a stop block (3) is fixedly connected to the outer wall of one side of the upper protection cover (2).
6. An unmanned aerial vehicle wing shield according to claim 1, wherein the swivel (4) is fixedly connected with a handle (9) on one side.
7. The unmanned aerial vehicle wing protection cover convenient to install according to claim 6, wherein a plurality of anti-skidding lines (10) are formed on one side of the rotating handle (9), and the anti-skidding lines (10) are uniformly distributed.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN202321516596.1U CN220518602U (en) | 2023-06-14 | 2023-06-14 | Unmanned aerial vehicle wing protection casing convenient to installation |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN202321516596.1U CN220518602U (en) | 2023-06-14 | 2023-06-14 | Unmanned aerial vehicle wing protection casing convenient to installation |
Publications (1)
Publication Number | Publication Date |
---|---|
CN220518602U true CN220518602U (en) | 2024-02-23 |
Family
ID=89931076
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN202321516596.1U Active CN220518602U (en) | 2023-06-14 | 2023-06-14 | Unmanned aerial vehicle wing protection casing convenient to installation |
Country Status (1)
Country | Link |
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CN (1) | CN220518602U (en) |
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2023
- 2023-06-14 CN CN202321516596.1U patent/CN220518602U/en active Active
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