CN220884870U - Unmanned aerial vehicle transfer device capable of protecting wings - Google Patents
Unmanned aerial vehicle transfer device capable of protecting wings Download PDFInfo
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- CN220884870U CN220884870U CN202321647435.6U CN202321647435U CN220884870U CN 220884870 U CN220884870 U CN 220884870U CN 202321647435 U CN202321647435 U CN 202321647435U CN 220884870 U CN220884870 U CN 220884870U
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- 238000012546 transfer Methods 0.000 title claims description 12
- 230000005540 biological transmission Effects 0.000 claims description 17
- 238000001125 extrusion Methods 0.000 claims description 15
- 230000001681 protective effect Effects 0.000 claims description 11
- 230000000149 penetrating effect Effects 0.000 claims description 7
- 230000000694 effects Effects 0.000 description 5
- 230000009471 action Effects 0.000 description 4
- 238000010030 laminating Methods 0.000 description 4
- 238000000034 method Methods 0.000 description 4
- 230000033228 biological regulation Effects 0.000 description 3
- 230000007423 decrease Effects 0.000 description 3
- 238000012545 processing Methods 0.000 description 3
- 238000009434 installation Methods 0.000 description 2
- 230000033001 locomotion Effects 0.000 description 2
- 230000007246 mechanism Effects 0.000 description 2
- 230000008569 process Effects 0.000 description 2
- 230000001012 protector Effects 0.000 description 2
- 230000002787 reinforcement Effects 0.000 description 2
- 230000003014 reinforcing effect Effects 0.000 description 2
- 238000012876 topography Methods 0.000 description 2
- 241000883990 Flabellum Species 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 238000002474 experimental method Methods 0.000 description 1
- 238000013508 migration Methods 0.000 description 1
- 230000005012 migration Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000011017 operating method Methods 0.000 description 1
- 230000001360 synchronised effect Effects 0.000 description 1
- 230000007723 transport mechanism Effects 0.000 description 1
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Abstract
The utility model relates to an unmanned aerial vehicle transferring device capable of protecting wings, and aims to solve the technical problem of current unmanned aerial vehicle transferring protection, wherein an extruding plate is slidably arranged at the top of the inner side of each positioning frame, first guide rods are fixedly arranged on the surfaces of the two ends of the inner side bottom of each positioning frame, pushing sleeves are slidably sleeved on the outer side surfaces of each first guide rods, and connecting blocks are fixedly arranged at the two ends of the side edges of the bottom of each extruding plate.
Description
Technical Field
The utility model relates to the field of unmanned aerial vehicle protection, in particular to an unmanned aerial vehicle transfer device capable of protecting wings.
Background
Unmanned aerial vehicle is modern technological's result, can survey topography and topography for people, also can record some fine time in some activities, also be one of modern children's favorite toy, unmanned aerial vehicle's flight is most take off through the wing fan, and the flabellum on the wing is extremely easily damaged in the in-process of using, and then in transporting the in-process to it, generally can use corresponding protection transport mechanism and carry out the protection to it.
According to chinese published patent (publication No. "CN 112027076B"), it is known that an unmanned aerial vehicle transfer device capable of protecting wings comprises an unmanned aerial vehicle body, an unmanned aerial vehicle arm, a connector, a locking lever and a protection frame, a fixed shaft is arranged above the outer side of the unmanned aerial vehicle body, a mounting hole is formed in the bottom of the outer side of the fixed shaft, a connecting rod is arranged in the connector, a locking lever is arranged in the connecting rod, a limiting block is arranged in the middle of the locking lever, a guide groove is formed in the outer side of the limiting block, a thimble is arranged below the guide groove, a driving rod is arranged on the inner side of the second connecting piece, and an extrusion column is connected to the outer side of the driving rod. This unmanned aerial vehicle transfer device that can protect the wing conveniently fold the wing fan and accomodate, conveniently protect the wing fan, and can accomodate the unmanned aerial vehicle arm in a rotating way, conveniently reduce unmanned aerial vehicle's volume, conveniently accomodate, and can dismantle protector, protector's use, in the course of realizing the utility model, the inventor finds that there is following problem not solved among the prior art at least, in the use, traditional unmanned aerial vehicle transfer device is when transporting the protection to unmanned aerial vehicle, generally can use corresponding positioning mechanism and carry out positioning process to unmanned aerial vehicle's wing, and in this process, need the operator to carry out manual regulation to the positioning mechanism that lies in unmanned aerial vehicle wing both sides, guarantee that it laminates in the wing outside and carry out the position reinforcement processing to it, but because unmanned aerial vehicle's wing quantity is more, lead to too loaded down with trivial details to adjust it, time and energy consuming, extremely easily influence the positioning protection stability to the wing because not in place. For this reason, new solutions need to be designed to solve.
Disclosure of utility model
The utility model aims to overcome the defects of the prior art, adapt to the actual needs, and provide an unmanned aerial vehicle transferring device capable of protecting wings so as to solve the technical problem of transferring protection of the current unmanned aerial vehicle.
In order to achieve the purpose of the utility model, the technical scheme adopted by the utility model is as follows: the unmanned aerial vehicle transferring device capable of protecting the wing comprises a placing box, wherein a placing frame is fixedly arranged on the inner side of the placing box, and positioning frames are fixedly arranged on the surfaces of two ends of the outer side of the placing frame;
The top of the inner side of each positioning frame is slidably provided with an extrusion plate, the surfaces of the two ends of the bottom of the inner side of each positioning frame are fixedly provided with first guide rods, the outer side surfaces of the first guide rods are slidably sleeved with pushing sleeves, the two ends of the side edge of the bottom of each extrusion plate are fixedly provided with connecting blocks, the top of each connecting block is hinged with a pushing rod through a rotating shaft, the bottom of each pushing rod is hinged with the outer side surface of the top of each pushing sleeve through a rotating shaft, the surfaces of the two ends of the outer side of each pushing sleeve are fixedly provided with a pushing rod, the pushing rods penetrate through the side edge of each positioning frame and are slidably arranged in the side edge of each two groups of pushing rods, and pushing blocks are fixedly arranged between the outer side tops of the pushing rods;
The locating frame is characterized in that mounting plates are fixedly mounted on the surfaces of two ends of the outer side of the locating frame, each two groups of mounting plates are internally provided with an I-shaped rod in a penetrating and sliding mode, the surfaces of the middle ends of the I-shaped rods are fixedly sleeved with transmission plates, the surfaces of the bottoms of the transmission plates are fixedly mounted with mounting blocks, and the tops of the side edges of the mounting blocks are hinged to the outer side surfaces of the transmission plates through rotating shafts.
Preferably, the top of the placement box is hinged with a protective cover plate through a rotating shaft, a laminating soft cushion is fixedly adhered to the bottom surface of the protective cover plate, and the laminating soft cushion is positioned inside the placement frame.
Preferably, each of the two end surfaces of the outer side of the positioning frame is fixedly provided with a connecting rod, and a protection arc plate is fixedly arranged between one side, far away from the positioning frame, of each two groups of connecting rods.
Preferably, a placement groove is formed in the middle end of the placement frame.
Preferably, the guide grooves are formed in the two ends of the side edge of the bottom of each positioning frame, and the pushing rod penetrates through the guide grooves to be installed in a sliding mode.
Preferably, a hollow pipe is fixedly installed on the surface of the middle end of the inner bottom of each placement frame, a second guide rod is installed on the top of the inner side of each hollow pipe in a penetrating and sliding mode, and the top of the second guide rod is fixedly connected with the surface of the bottom of the extrusion plate.
Preferably, the inner side surface of the top end of each transmission plate is fixedly provided with a fitting arc plate.
Compared with the prior art, the utility model has the beneficial effects that:
1. According to the utility model, the extruding plate is arranged in the positioning frame, so that when the unmanned aerial vehicle is arranged in the positioning frame, and after the wing of the unmanned aerial vehicle is arranged in the positioning frame, the extruding plate can be driven to synchronously descend in the positioning frame only by continuously pressing down the positioning frame, the two ends of the pushing rod are arranged below the extruding plate and above the pushing sleeve by combining the rotating shafts, when the extruding plate descends, the pushing sleeve can provide corresponding pushing force for the pushing sleeve under the pushing action of the pushing rod, the pushing sleeve can horizontally move relatively outside the guiding rod, and then the driving plate can rotate by taking the working rod as the center of a circle, so that the bottom of the driving plate is driven to synchronously rotate in opposite directions at the top of the positioning frame, the distance between the two groups of the bonding arc plates is ensured, the inner side of the bonding arc plates can be subjected to bonding and reinforcing treatment by the pushing and reinforcing of the pushing sleeve after the wing of the unmanned aerial vehicle, and the required protection and transportation operation of the operator is reduced, and the labor consumption of the operator for adjusting and the installation is reduced.
2. According to the utility model, the guide rod is inserted into the hollow pipe in a sliding manner, and under the guide sliding effect of the hollow pipe on the guide rod, when the extrusion plate is extruded by the wing and descends in the positioning frame, the extrusion plate cannot arbitrarily laterally move in the positioning frame to influence the transmission effect on the transmission plate, so that the position adjustment transmission rationality of the joint arc plate is ensured.
Drawings
FIG. 1 is a schematic top view of the overall cross-sectional structure of the present utility model;
FIG. 2 is a schematic diagram of an overall partial cross-sectional elevation view of the present utility model;
FIG. 3 is an enlarged view of the structure of the portion A of the present utility model;
FIG. 4 is a schematic perspective view of a positioning frame according to the present utility model;
In the figure: 1. placing a box; 11. a protective cover plate; 12. attaching a soft cushion; 13. placing a frame; 14. a placement groove;
2. A positioning frame; 21. an extrusion plate; 22. a first guide bar; 23. pushing the sleeve; 24. a connecting block; 25. a push rod; 26. a pushing rod; 27. a pushing block; 28. a mounting block;
3. a mounting plate; 31. an I-shaped rod; 32. a drive plate; 33. attaching an arc plate; 34. a guide groove;
4. a hollow tube; 41. a second guide bar; 42. a connecting rod; 43. and (5) protecting the arc plate.
Detailed Description
The utility model is further illustrated by the following examples in conjunction with the accompanying drawings:
Example 1: referring to fig. 1 to 4, a placing frame 13 is fixedly installed on the inner side of a placing box 1, a placing groove 14 is formed in the middle end of the placing frame 13, positioning frames 2 are fixedly installed on the surfaces of the two ends of the outer side of the placing frame 13, an extrusion plate 21 is slidably installed on the top of the inner side of each positioning frame 2, a first guide rod 22 is fixedly installed on the surfaces of the two ends of the bottom of the inner side of each positioning frame 2, a push sleeve 23 is slidably sleeved on the outer surface of each first guide rod 22, a connecting block 24 is fixedly installed on the two ends of the side edge of the bottom of each extrusion plate 21, a push rod 25 is hinged to the outer surface of the top of the push sleeve 23 through a rotating shaft, an abutting rod 26 is fixedly installed on the surfaces of the two ends of the outer side of each push sleeve 23 through the rotating shaft, an abutting rod 26 penetrates through the inner side edge of the positioning frames 2, an abutting block 27 is fixedly installed between the outer sides of each abutting rod 26, a pair of abutting rods 2 is fixedly installed on the top end face of each abutting rod 31, a transmission plate 32 is fixedly sleeved on the inner side face of each side face of the corresponding fixing plate 32 through the corresponding side of the corresponding fixing plate 31, a transmission plate 32 is fixedly installed on the top of each transmission plate 32 in a synchronous manner, and the transmission plate 32 is fixedly sleeved on the top face of each transmission plate 32 through the transmission plate 32, adjust the interval between two sets of laminating arc plates 33, guarantee that laminating arc plate 33 inboard can laminate in unmanned aerial vehicle's wing outside after, move the reinforcement to it and handle and realize transporting the protectiveness to it, reduce the operator and consolidate the required operating procedure of regulation to the protection, reduce the operator and to transport the required labour consumption of regulation installation.
Specifically, referring to fig. 1 to 4, the top of the placement box 1 is hinged with a protective cover plate 11 through a rotating shaft, a bonding soft cushion 12 is fixedly adhered to the bottom surface of the protective cover plate 11, the bonding soft cushion 12 is positioned inside the placement frame 13, and the position limiting stability of the unmanned aerial vehicle is improved by abutting the protection quality of the bonding soft cushion 12 and the top of the unmanned aerial vehicle.
Further, referring to fig. 1 to 4, connecting rods 42 are fixedly mounted on two end surfaces of the outer side of each positioning frame 2, a protective arc plate 43 is fixedly mounted between one sides of each two groups of connecting rods 42 far away from the positioning frames 2, and the protective quality of the outer side of the wing is improved through the structure of the protective arc plate 43.
It should be noted that, referring to fig. 1 to 4, the two ends of the bottom side edge of each positioning frame 2 are provided with guide grooves 34, and the moving resisting rod 26 is installed inside the guide grooves 34 in a penetrating and sliding manner, so that the driving rationality of the whole device is ensured under the guiding and sliding action of the moving resisting rod 26 by the guide grooves 34.
It should be noted that, referring to fig. 1 to 4, the hollow tube 4 is fixedly mounted on the surface of the middle end of the inner bottom of each placement frame 13, the second guide rod 41 is slidably mounted on the top of the inner side of each hollow tube 4, and the top of the second guide rod 41 is fixedly connected with the bottom surface of the extrusion plate 21, and the extrusion plate 21 is prevented from arbitrary tilting movement when being pushed by the guiding sliding action of the hollow tube 4 on the second guide rod 41, so as to affect the driving rationality of the whole device.
It should be noted that, referring to fig. 1 to 4, the inner surface of the top end of each driving plate 32 is fixedly provided with a bonding arc plate 33, and the bonding arc plate 33 is ensured to be bonded to the outer side of the wing and then is subjected to the resisting limiting treatment through the structural effect of the bonding arc plate 33.
During operation, outside pulling protective cover 11, place the unmanned aerial vehicle that will transport the processing in placing frame 13 inside, place unmanned aerial vehicle wing in positioning frame 2 inside thereupon, it pushes down the processing to last to unmanned aerial vehicle, make unmanned aerial vehicle in placing frame 13 inside decline and drive the wing in step in positioning frame 2 inside decline after, cause the extrusion to stripper plate 21 and make it in positioning frame 2 inside decline after, combine the pivot and be connected with push sleeve 23 and stripper plate 21 below respectively with the upper and lower both ends of push rod 25, make push rod 25 can provide the corresponding driving force of push sleeve 23 and make it at first guide bar 22 outside surface horizontal migration, then under the action of supporting movable rod 26, provide the corresponding outside driving force of actuator plate 32 bottom, make actuator plate 32 rotate as the centre of a circle, make actuator plate 32 bottom under the effect of receiving outside driving its top laminate arc plate 33 rotate in positioning frame 2 top synchronization, the interval between two sets of laminate arc 33 plates is guaranteed, guarantee that laminate plate 33 can be in the outside of the unmanned aerial vehicle, can be carried out the outside the motion of unmanned aerial vehicle and the unmanned aerial vehicle is placed in the outside, can guarantee that unmanned aerial vehicle is placed the unmanned aerial vehicle is stable in the outside, the unmanned aerial vehicle can be carried out the safety and is placed in the outside the surface of the safety of unmanned aerial vehicle, the unmanned aerial vehicle is placed in the outside the face of the safety of the aircraft is guaranteed, the unmanned aerial vehicle is placed in the face place 13, the unmanned aerial vehicle is placed in the face of the safety of the back of the top is not is guaranteed to the face down.
In addition, the components designed by the utility model are all universal standard components or components known by the person skilled in the art, the structures and principles of the components are all known by the person skilled in the art through technical manuals or known by routine experimental methods, and the utility model can be completely realized by the person skilled in the art.
The embodiments of the present utility model are disclosed as preferred embodiments, but not limited thereto, and those skilled in the art will readily appreciate from the foregoing description that various modifications and variations can be made without departing from the spirit of the present utility model.
Claims (7)
1. The unmanned aerial vehicle transferring device capable of protecting the wing comprises a placing box (1), and is characterized in that a placing frame (13) is fixedly arranged on the inner side of the placing box (1), and positioning frames (2) are fixedly arranged on the surfaces of two ends of the outer side of the placing frame (13);
The device comprises a positioning frame (2), wherein an extrusion plate (21) is slidably arranged at the top of the inner side of the positioning frame (2), first guide rods (22) are fixedly arranged at the surfaces of the two ends of the inner side bottom of the positioning frame (2), push sleeves (23) are slidably sleeved on the outer side surfaces of the first guide rods (22), connecting blocks (24) are fixedly arranged at the two ends of the side edges of the bottom of each extrusion plate (21), push rods (25) are hinged to the top of each connecting block (24) through a rotating shaft, the bottoms of the push rods (25) are hinged to the outer side surfaces of the tops of the push sleeves (23) through rotating shafts, abutting rods (26) are fixedly arranged at the surfaces of the two ends of the outer side of each push sleeve (23), and abutting blocks (27) are fixedly arranged between the outer side tops of each two groups of abutting rods (26) in a penetrating and sliding manner;
The locating frame is characterized in that mounting plates (3) are fixedly mounted on the surfaces of two ends of the outer side of the locating frame (2), each two groups of mounting plates (3) are internally and slidably mounted with an I-shaped rod (31) in a penetrating mode, the surfaces of the middle ends of the I-shaped rods (31) are fixedly sleeved with transmission plates (32), mounting blocks (28) are fixedly mounted on the surfaces of the bottoms of the transmission plates (32), and the tops of the side edges of the mounting blocks (28) are hinged to the outer side surfaces of the transmission plates (32) through rotating shafts.
2. The unmanned aerial vehicle transfer device capable of protecting wings according to claim 1, wherein the top of the placement box (1) is hinged with a protective cover plate (11) through a rotating shaft, an attaching cushion (12) is fixedly adhered to the bottom surface of the protective cover plate (11), and the attaching cushion (12) is located inside the placement frame (13).
3. An unmanned aerial vehicle transfer device capable of protecting wings according to claim 1, wherein connecting rods (42) are fixedly arranged on the surfaces of the two ends of the outer side of each positioning frame (2), and a protection arc plate (43) is fixedly arranged between one side, far away from the positioning frame (2), of each two groups of connecting rods (42).
4. An unmanned aerial vehicle transfer device capable of protecting wings as claimed in claim 1, wherein a placement groove (14) is formed in the middle end of the placement frame (13).
5. An unmanned aerial vehicle transfer device capable of protecting wings according to claim 1, wherein guide grooves (34) are formed in two ends of the side edge of the bottom of each positioning frame (2), and the pushing rod (26) is installed in the guide grooves (34) in a penetrating and sliding manner.
6. An unmanned aerial vehicle transfer device capable of protecting wings according to claim 1, wherein a hollow pipe (4) is fixedly arranged on the surface of the middle end of the inner bottom of each placement frame (13), a second guide rod (41) is arranged on the inner top of each hollow pipe (4) in a penetrating and sliding manner, and the top of the second guide rod (41) is fixedly connected with the surface of the bottom of the extrusion plate (21).
7. An unmanned aerial vehicle transfer device capable of protecting a wing according to claim 1, wherein a fitting arc plate (33) is fixedly arranged on the inner surface of the top end of each transmission plate (32).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202321647435.6U CN220884870U (en) | 2023-06-27 | 2023-06-27 | Unmanned aerial vehicle transfer device capable of protecting wings |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202321647435.6U CN220884870U (en) | 2023-06-27 | 2023-06-27 | Unmanned aerial vehicle transfer device capable of protecting wings |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN220884870U true CN220884870U (en) | 2024-05-03 |
Family
ID=90879270
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202321647435.6U Active CN220884870U (en) | 2023-06-27 | 2023-06-27 | Unmanned aerial vehicle transfer device capable of protecting wings |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN220884870U (en) |
-
2023
- 2023-06-27 CN CN202321647435.6U patent/CN220884870U/en active Active
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