CN216994861U - 24-hour mooring aerial device for unmanned aerial vehicle - Google Patents
24-hour mooring aerial device for unmanned aerial vehicle Download PDFInfo
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- CN216994861U CN216994861U CN202220800681.XU CN202220800681U CN216994861U CN 216994861 U CN216994861 U CN 216994861U CN 202220800681 U CN202220800681 U CN 202220800681U CN 216994861 U CN216994861 U CN 216994861U
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Abstract
The utility model discloses an aerial device for 24-hour mooring of an unmanned aerial vehicle, which belongs to the technical field of aerial devices, and aims to provide electric power support for the unmanned aerial vehicle, and damage can be caused when the aerial device is tied up in strong wind weather, because the traditional aerial device is not provided with a protection component; the motor drives the rack to move through the gear, when the convex sliding blocks slide along the convex sliding grooves, the second connecting rod enables the two cross sliding blocks to slide along the cross sliding grooves in the opposite direction, and therefore the first connecting rod drives the supporting legs to rotate along the guide plate, the supporting effect is achieved, and the battery box is effectively protected.
Description
Technical Field
The utility model relates to the technical field of air mooring devices, in particular to an air mooring device for an unmanned aerial vehicle in 24 hours.
Background
Carry out 24 hours through unmanned aerial vehicle and detain in the air to important field today, the important equipment that has progressively become reconnaissance and patrol and examine, however in the middle of still continuing research and development because of present unmanned aerial vehicle's development maturity, unmanned aerial vehicle's high power consumptive is the important influence factor that influences unmanned aerial vehicle and detain for a long time, consequently, need provide electric power for unmanned aerial vehicle through staying aerial device and support, additionally, because of environmental factor, run into strong wind weather, probably cause unmanned aerial vehicle to be forced to descend the phenomenon, it is not equipped with the protection component to stay aerial device in the past, can lead to damaging, for this we propose an unmanned aerial vehicle 24 hours and stay aerial device and be used for solving above-mentioned problem.
SUMMERY OF THE UTILITY MODEL
The utility model aims to provide a 24-hour air mooring device for an unmanned aerial vehicle, which aims to solve the problems in the background technology.
In order to achieve the purpose, the utility model provides the following technical scheme: the utility model provides an aerial device of unmanned aerial vehicle 24 hours mooring, includes the unmanned aerial vehicle bottom plate, surface clamping has the mounting panel on the unmanned aerial vehicle bottom plate, fixed surface is equipped with the mounting bracket on the mounting panel, the fixed support piece that is equipped with in mounting bracket both ends, mounting panel bottom end fixed mounting has power component, power component slidable mounting is in the mounting bracket bottom, power component and support piece fixed connection, mounting bracket upper end joint has the battery case.
According to the preferable technical scheme, clamping grooves are symmetrically formed in two ends of the upper surface of the bottom plate of the unmanned aerial vehicle, rectangular blocks are fixedly arranged on two ends of the upper surface of the bottom plate of the unmanned aerial vehicle, first rectangular grooves are formed in the rectangular blocks, and the first rectangular grooves and the clamping grooves are connected with mounting plates in a clamping mode.
According to a preferred technical scheme, the mounting plate is made of an elastic alloy plate, inclined plates are fixedly arranged at two ends of the mounting plate, clamping plates and clamping blocks are symmetrically and fixedly arranged at the bottom ends of the inclined plates, the clamping plates are clamped in the clamping grooves, the clamping blocks are clamped in the first rectangular grooves, and a plurality of first heat dissipation grooves are formed in the upper surface of the mounting plate.
According to a preferred technical scheme, the mounting frame comprises two transverse plates, two longitudinal plates are fixedly arranged between the transverse plates, a connecting plate is fixedly connected between the longitudinal plates, rectangular buckles are symmetrically and fixedly arranged on the upper surfaces of the transverse plates, battery boxes are clamped at the upper ends of the rectangular buckles, second rectangular grooves are symmetrically formed in the side surfaces of the longitudinal plates, the battery boxes are clamped in the second rectangular grooves, supporting pieces are fixedly connected to two ends of the connecting plate, a convex sliding groove is formed in the bottom surface of the connecting plate, and a power assembly is slidably mounted in the convex sliding groove.
According to a preferred technical scheme of the utility model, the supporting piece comprises two convex sliding blocks and guide plates, the convex sliding blocks are slidably mounted in convex sliding grooves, the side surfaces of the convex sliding blocks are fixedly connected with a power assembly, the bottom surfaces of the convex sliding blocks are rotatably hinged with two second connecting rods, the upper surfaces of the other ends of the second connecting rods are rotatably connected with a cross sliding block, the two guide plates are fixedly arranged at two ends of a connecting plate, the surfaces of the guide plates are provided with cross sliding grooves, the cross sliding blocks are slidably arranged in the cross sliding grooves, the upper surfaces of the cross sliding blocks are rotatably hinged with first connecting rods, the other ends of the first connecting rods are rotatably hinged with supporting legs, and the bottom ends of the supporting legs are rotatably hinged to the end parts of the guide plates.
As a preferred technical scheme of the utility model, the power assembly comprises a motor, the motor is fixedly arranged on the bottom surface of the mounting plate, the output end of the motor movably penetrates through the mounting plate and is fixedly connected with a gear, the gear is engaged and connected with two racks, the racks are slidably arranged in the convex sliding groove, and the other end of each rack is fixedly connected with the side surface of the convex sliding block.
According to a preferred technical scheme, the battery box comprises a bottom shell and an upper shell, the bottom shell is detachably connected with the upper shell, concave blocks are symmetrically and fixedly arranged on two sides of the bottom shell, second heat dissipation grooves are formed in the other two sides of the bottom shell, the upper ends of rectangular buckles are clamped in the concave blocks, L-shaped buckles are symmetrically and fixedly arranged at two ends of the bottom surface of the bottom shell and clamped in the second rectangular grooves, heat dissipation fins are fixedly arranged on the upper surface of the upper shell, and a mooring cable connector is detachably mounted on one side of the upper shell.
Compared with the prior art, the utility model has the beneficial effects that:
1. the mounting plate is mounted on a base plate of the unmanned aerial vehicle through elastic clamping, the battery box is clamped in the rectangular buckle in the concave block, and the L-shaped buckle is clamped in the second rectangular groove, so that the battery box can be quickly and fixedly mounted, and the ground charging device is connected through the mooring cable connector to enable the unmanned aerial vehicle to be detained;
2. the motor drives the rack to move through the gear, when the convex sliding blocks slide in the convex sliding grooves, the second connecting rod enables the two cross sliding blocks to slide in the cross sliding grooves reversely, and therefore the first connecting rod drives the supporting legs to rotate along the guide plates, the supporting effect is achieved, and the battery box is effectively protected.
Drawings
FIG. 1 is a schematic structural view of the present invention,
FIG. 2 is a schematic view of a battery pack according to the present invention,
figure 3 is a schematic top view of a structural mount of the present invention,
figure 4 is a bottom schematic view of the structural mount of the present invention,
figure 5 is a schematic view of a structural support member of the present invention,
figure 6 is an enlarged schematic view of the utility model at a in figure 5,
fig. 7 is a schematic view of the bottom plate and mounting plate of the unmanned aerial vehicle with the structure of the utility model.
In the figure: 1. an unmanned aerial vehicle bottom plate; 11. a card slot; 12. a rectangular block; 121. a first rectangular groove; 2. mounting a plate; 21. a sloping plate; 211. clamping a plate; 212. a clamping block; 22. a first heat sink; 3. a battery case; 31. a bottom case; 32. an upper shell; 33. a heat dissipating fin; 34. mooring the cable joint; 35. a concave block; 36. an L-shaped buckle; 37. a second heat sink; 4. a mounting frame; 41. a transverse plate; 42. a rectangular buckle; 43. a connecting plate; 431. a convex chute; 44. a longitudinal plate; 441. a second rectangular groove; 5. a support member; 51. a guide plate; 511. a cross-shaped chute; 52. a crosshead shoe; 53. a first link; 54. supporting legs; 55. a male slider; 56. a second link; 6. a power assembly; 61. a motor; 62. a gear; 63. a rack.
Detailed Description
The technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only a part of the embodiments of the present invention, and not all of the embodiments. All other embodiments, which can be derived by a person skilled in the art from the embodiments given herein without making any creative effort, shall fall within the protection scope of the present invention.
Example (b): as shown in fig. 1-7, the utility model provides an unmanned aerial vehicle 24-hour mooring aerial device, which comprises an unmanned aerial vehicle base plate 1, wherein a mounting plate 2 is clamped on the upper surface of the unmanned aerial vehicle base plate 1, the mounting plate 2 is elastically clamped and mounted on the unmanned aerial vehicle base plate 1, a mounting frame 4 is fixedly arranged on the upper surface of the mounting plate 2, support members 5 are fixedly arranged at two ends of the mounting frame 4, a power assembly 6 is fixedly arranged at the bottom end of the mounting plate 2, the power assembly 6 is slidably mounted in the bottom end of the mounting frame 4, the power assembly 6 is fixedly connected with the support members 5, and a battery box 3 is clamped at the upper end of the mounting frame 4, so that the support members 5 can stretch out and draw back through the power assembly 6, and the battery box 3 and an unmanned aerial vehicle body which are clamped and fixed by the mounting frame 4 can be effectively protected.
Further, draw-in groove 11 has been seted up to 1 upper surface both ends symmetry of unmanned aerial vehicle bottom plate, 1 upper surface both ends of unmanned aerial vehicle bottom plate are fixed and are equipped with rectangular block 12, first rectangular channel 121 has been seted up in rectangular block 12, joint mounting panel 2 in first rectangular channel 121 and the draw-in groove 11 to unmanned aerial vehicle bottom plate 1 and mounting panel 2 can quick fixed mounting.
Further, 2 materials of mounting panel are the elastic alloy board, 2 fixed swash plates 21 that are equipped with in both ends of mounting panel, 21 bottom symmetries of swash plate are fixed and are equipped with cardboard 211, fixture block 212, cardboard 211 joint is in draw-in groove 11, fixture block 212 joint is in first rectangular channel 121, a plurality of first radiating grooves 22 have been seted up to 2 upper surfaces of mounting panel to when extruding mounting panel 2, make mounting panel 2 produce certain deformation, then through cardboard 211 joint in draw-in groove 11, and fixture block 212 joint is in first rectangular channel 121, thereby make mounting panel 2 install unmanned aerial vehicle bottom plate 1 fast on.
Further, mounting bracket 4 is including two diaphragm 41, the fixed two vertical plates 44 that are equipped with between diaphragm 41, fixedly connected with connecting plate 43 between the vertical plate 44, diaphragm 41 upper surface symmetry is fixed and is equipped with rectangle buckle 42, rectangle buckle 42 upper end joint battery case 3, second rectangular channel 441 has been seted up to vertical plate 44 side symmetry, joint battery case 3 in the second rectangular channel 441 to through diaphragm 41 and vertical plate 44 fixed mounting battery case 3, connecting plate 43 both ends fixed connection support piece 5, convex spout 431 has been seted up to connecting plate 43 bottom surface, slidable mounting power component 6 in the convex spout 431, thereby power component 6 can make support piece 5 work.
Further, the supporting member 5 includes two convex sliding blocks 55 and guide plates 51, the convex sliding blocks 55 are slidably mounted in the convex sliding grooves 431, the side surfaces of the convex sliding blocks 55 are fixedly connected with the power assembly 6, the bottom surfaces of the convex sliding blocks 55 are rotatably hinged with two second connecting rods 56, the upper surfaces of the other ends of the second connecting rods 56 are rotatably connected with the cross sliding blocks 52, the two guide plates 51 are fixedly arranged at the two ends of the connecting plate 43, the surface of the guide plate 51 is provided with the cross sliding grooves 511, the cross sliding blocks 52 are slidably arranged in the cross sliding grooves 511, the upper surfaces of the cross sliding blocks 52 are rotatably hinged with the first connecting rods 53, the other ends of the first connecting rods 53 are rotatably hinged with the supporting feet 54, the bottom ends of the supporting feet 54 are rotatably hinged to the end portions of the guide plates 51, so that when the convex sliding blocks 55 slide along the convex sliding grooves 431, the two second connecting rods 56 can be moved, and the two cross sliding blocks 52 can slide along the cross sliding grooves 511 reversely, so that the first link 53 drives the supporting leg 54 to rotate along the guide plate 51, thereby playing a supporting role and effectively protecting the battery box 3.
Further, the power assembly 6 includes a motor 61, the motor 61 is fixedly installed on the bottom surface of the mounting plate 2, the output end of the motor 61 movably penetrates through the mounting plate 2 and is fixedly connected with a gear 62, the gear 62 is engaged with two racks 63, the racks 63 are slidably arranged in the convex sliding groove 431, the other end of the rack 63 is fixedly connected with the side surface of the convex sliding block 55, so that the motor 61 drives the two racks 63 to reversely slide along the convex sliding groove 431 through the gear 62, the two convex sliding blocks 55 reversely move, and the moving directions of the four supporting feet 54 relative to the battery box 3 can be unified.
Further, the battery box 3 includes a bottom shell 31 and an upper shell 32, the bottom shell 31 is detachably connected with the upper shell 32, batteries are arranged in the bottom shell 31 and the upper shell 32, concave blocks 35 are symmetrically and fixedly arranged on two sides of the bottom shell 31, second heat dissipation grooves 37 are formed in the other two sides of the bottom shell 31, the upper ends of rectangular buckles 42 are clamped in the concave blocks 35, L-shaped buckles 36 are symmetrically and fixedly arranged at two ends of the bottom surface of the bottom shell 31, the L-shaped buckles 36 are clamped in the second rectangular grooves 441, the bottom shell 31 is connected with the transverse plate 41 and the longitudinal plate 44 in a clamping mode, heat dissipation fins 33 are fixedly arranged on the upper surface of the upper shell 32, a mooring cable connector 34 is detachably mounted on one side of the upper shell 32, and the mooring cable connector 34 is connected with the ground charging device.
The working principle is as follows: the mounting plate 2 is mounted on the unmanned aerial vehicle base plate 1, the battery box 3 and the unmanned aerial vehicle body can be effectively protected, the mounting plate 2 is manually extruded to enable the mounting plate 2 to generate certain deformation, then the mounting plate is clamped in the clamping groove 11 through the clamping plate 211, the clamping block 212 is clamped in the first rectangular groove 121, so that the mounting plate 2 is quickly mounted on the unmanned aerial vehicle base plate 1, the inclined plate 21 and the mounting plate 2 are in a ladder shape and have a buffering effect, when the battery box 3 is mounted, the concave blocks 35 on two sides of the bottom shell 31 are clamped at the upper end of the rectangular buckle 42 on the transverse plate 41, the L-shaped buckle 36 is clamped in the second rectangular groove 441 of the longitudinal plate 44, so that the bottom shell 31 can be quickly clamped and connected with the transverse plate 41 and the longitudinal plate 44, when the battery box 3 is used, the motor 61 drives the two racks 63 to reversely slide along the convex sliding grooves 431 through the gear 62, so that the two convex sliding blocks 55 reversely move, and therefore the moving directions of the four supporting legs 54 relative to the battery box 3 can be unified, when the convex slider 55 slides in the convex chute 431, two second connecting rods 56 can be moved, and two cross sliders 52 are pushed to slide in the cross chute 511 reversely, so that the first connecting rod 53 drives the supporting leg 54 to rotate along the guide plate 51, thereby playing a supporting role, effectively protecting the battery box 3, providing a battery in the bottom shell 31 and the upper shell 32, connecting the battery in the ground charging device through the mooring cable joint 34, and realizing the aerial detention of the unmanned aerial vehicle.
Although embodiments of the present invention have been shown and described, it will be appreciated by those skilled in the art that changes, modifications, substitutions and alterations can be made in these embodiments without departing from the principles and spirit of the utility model, the scope of which is defined in the appended claims and their equivalents.
Claims (7)
1. The utility model provides an unmanned aerial vehicle 24 hours is moored aerial device, includes unmanned aerial vehicle bottom plate (1), its characterized in that: unmanned aerial vehicle bottom plate (1) upper surface joint has mounting panel (2), fixed surface is equipped with mounting bracket (4) on mounting panel (2), fixed support piece (5) that are equipped with in mounting bracket (4) both ends, mounting panel (2) bottom fixed mounting has power component (6), power component (6) slidable mounting is in mounting bracket (4) bottom, power component (6) and support piece (5) fixed connection, mounting bracket (4) upper end joint has battery case (3).
2. The unmanned aerial vehicle 24-hour mooring aerial device of claim 1, wherein: draw-in groove (11) have been seted up to unmanned aerial vehicle bottom plate (1) upper surface both ends symmetry, unmanned aerial vehicle bottom plate (1) upper surface both ends are fixed to be equipped with rectangular block (12), first rectangular channel (121) have been seted up in rectangular block (12), joint mounting panel (2) in first rectangular channel (121) and draw-in groove (11).
3. The unmanned aerial vehicle 24-hour mooring aerial device of claim 2, wherein: mounting panel (2) material is the elastic alloy board, mounting panel (2) both ends are fixed and are equipped with swash plate (21), swash plate (21) bottom symmetry is fixed and is equipped with cardboard (211), fixture block (212), cardboard (211) joint is in draw-in groove (11), fixture block (212) joint is in first rectangular channel (121), a plurality of first radiating grooves (22) have been seted up to mounting panel (2) upper surface.
4. The unmanned aerial vehicle 24-hour mooring aerial device of claim 1, wherein: mounting bracket (4) is including two diaphragm (41), fixed two longitudinal plates (44) that are equipped with between diaphragm (41), fixedly connected with connecting plate (43) between longitudinal plate (44), diaphragm (41) upper surface symmetry is fixed and is equipped with rectangle buckle (42), rectangle buckle (42) upper end joint battery case (3), second rectangular channel (441) have been seted up to longitudinal plate (44) side symmetry, joint battery case (3) in second rectangular channel (441), connecting plate (43) both ends fixed connection support piece (5), convex spout (431) have been seted up to connecting plate (43) bottom surface, slidable mounting power component (6) in convex spout (431).
5. The unmanned aerial vehicle 24-hour mooring aerial device of claim 4, wherein: the supporting piece (5) comprises two convex sliding blocks (55) and a guide plate (51), the convex sliding block (55) is arranged in the convex sliding groove (431) in a sliding way, the lateral surface of the convex sliding block (55) is fixedly connected with the power assembly (6), the bottom surface of the convex sliding block (55) is rotatably hinged with two second connecting rods (56), the upper surface of the other end of each second connecting rod (56) is rotatably connected with a cross sliding block (52), the two guide plates (51) are fixedly arranged at the two ends of the connecting plate (43), the surface of the guide plate (51) is provided with a cross sliding groove (511), the cross sliding block (52) is arranged in the cross sliding groove (511) in a sliding way, the upper surface of the crosshead shoe (52) is hinged with a first connecting rod (53) in a rotating way, the other end of the first connecting rod (53) is hinged with a supporting leg (54) in a rotating mode, and the bottom end of the supporting leg (54) is hinged to the end portion of the guide plate (51) in a rotating mode.
6. The unmanned aerial vehicle 24-hour mooring aerial device of claim 5, wherein: the power assembly (6) comprises a motor (61), the motor (61) is fixedly installed on the bottom surface of the mounting plate (2), the output end of the motor (61) movably penetrates through the mounting plate (2) and is fixedly connected with a gear (62), the gear (62) is meshed and connected with two racks (63), the racks (63) are slidably arranged in the convex sliding groove (431), and the other end of each rack (63) is fixedly connected with the side surface of the convex sliding block (55).
7. The unmanned aerial vehicle 24-hour mooring aerial device according to claim 4, characterized in that: the battery box (3) comprises a bottom shell (31) and an upper shell (32), the bottom shell (31) is detachably connected with the upper shell (32), concave blocks (35) are symmetrically and fixedly arranged on two sides of the bottom shell (31), second heat dissipation grooves (37) are formed in the other two sides of the bottom shell (31), the upper ends of rectangular buckles (42) are clamped in the concave blocks (35), L-shaped buckles (36) are symmetrically and fixedly arranged at two ends of the bottom surface of the bottom shell (31), the L-shaped buckles (36) are clamped in the second rectangular grooves (441), heat dissipation fins (33) are fixedly arranged on the upper surface of the upper shell (32), and mooring cable connectors (34) are detachably mounted on one side of the upper shell (32).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202220800681.XU CN216994861U (en) | 2022-04-07 | 2022-04-07 | 24-hour mooring aerial device for unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202220800681.XU CN216994861U (en) | 2022-04-07 | 2022-04-07 | 24-hour mooring aerial device for unmanned aerial vehicle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN216994861U true CN216994861U (en) | 2022-07-19 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202220800681.XU Active CN216994861U (en) | 2022-04-07 | 2022-04-07 | 24-hour mooring aerial device for unmanned aerial vehicle |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN216994861U (en) |
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- 2022-04-07 CN CN202220800681.XU patent/CN216994861U/en active Active
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