CN222380757U - An external power supply device for unmanned aerial vehicle - Google Patents
An external power supply device for unmanned aerial vehicle Download PDFInfo
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- CN222380757U CN222380757U CN202421074918.6U CN202421074918U CN222380757U CN 222380757 U CN222380757 U CN 222380757U CN 202421074918 U CN202421074918 U CN 202421074918U CN 222380757 U CN222380757 U CN 222380757U
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- 238000009434 installation Methods 0.000 claims abstract description 16
- 230000005611 electricity Effects 0.000 claims abstract description 15
- 230000001681 protective effect Effects 0.000 claims description 17
- 238000004891 communication Methods 0.000 claims description 6
- 230000000149 penetrating effect Effects 0.000 claims description 3
- 208000035473 Communicable disease Diseases 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 238000004146 energy storage Methods 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 230000017525 heat dissipation Effects 0.000 description 1
- 208000015181 infectious disease Diseases 0.000 description 1
- 238000007689 inspection Methods 0.000 description 1
- 238000010030 laminating Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000006467 substitution reaction Methods 0.000 description 1
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Abstract
The utility model discloses an external power supply electricity taking device of an unmanned aerial vehicle, which belongs to the technical field of external power supplies and comprises an unmanned aerial vehicle body, wherein an installation groove is formed in the bottom of the unmanned aerial vehicle body, two groups of support frames are symmetrically installed in the installation groove in a rotating mode, two groups of protection boxes are symmetrically installed at the bottom of the unmanned aerial vehicle body, elastic telescopic components capable of sliding in the support frames are installed in the protection boxes, the bottoms of the two groups of support frames are abutted to the external power supply body, and two groups of fixing blocks which are buckled to the inside of the support frames are symmetrically installed at the top of the external power supply body.
Description
Technical Field
The utility model relates to the technical field of external power supplies, in particular to an external power supply electricity taking device of an unmanned aerial vehicle.
Background
Along with the continuous development of unmanned aerial vehicle industry, unmanned aerial vehicle has started gradually and is taking photo by plane, agriculture, plant protection, little letter self-timer, express delivery transportation, disaster relief, observe wild animal, control infectious disease, survey, news report, electric power inspection, relief of disaster, video shooting expansion are used, because the battery energy storage of continuation of the current unmanned aerial vehicle self is limited, need be equipped with corresponding external power supply generally and get the electricity.
The current external power supply of unmanned aerial vehicle gets electric installation and installs directly laminating unmanned aerial vehicle usually, and external power supply gets electric installation can give off a large amount of heat and be unfavorable for self heat dissipation when using, and is used for installing external power supply and gets electric installation's support frame and be unfavorable for unmanned aerial vehicle's normal use, consequently, the technical staff provides an external power supply of unmanned aerial vehicle and gets electric installation to solve the problem that proposes among the above-mentioned background art.
Disclosure of utility model
The utility model aims to provide an external power supply electricity taking device of an unmanned aerial vehicle so as to solve the problems in the background technology.
The external power supply electricity taking device of the unmanned aerial vehicle comprises an unmanned aerial vehicle body, wherein the bottom of the unmanned aerial vehicle body is provided with a mounting groove, two groups of support frames are symmetrically rotatably arranged in the mounting groove, two groups of protection boxes are symmetrically arranged at the bottom of the unmanned aerial vehicle body, and elastic telescopic components capable of sliding in the support frames are arranged in the protection boxes;
The bottom butt of two sets of support frame has external power supply body, two sets of buckles to the inside fixed block of support frame are installed to external power supply body's top symmetry, and locking subassembly to the fixed block location is installed to one side of support frame bottom.
Preferably, the support frame comprises a U-shaped support rod rotatably arranged in the installation groove, two groups of communication grooves for sliding of the elastic telescopic components are symmetrically formed in the U-shaped support rod, and a fixing box for supporting the locking component is integrally formed at one side of the bottom end of the U-shaped support rod.
Preferably, the elastic telescopic assembly comprises two groups of sliding rods which are slidably arranged in the protective box, one ends of the two groups of sliding rods extending to the interior of the protective box are connected with push-pull rods which can slide in the interior of the communication groove, one ends of the two groups of sliding rods positioned in the interior of the protective box are connected with the same movable plate, and a telescopic spring sleeved on the outer ring of the sliding rod is connected between the movable plate and the interior of the protective box.
Preferably, two groups of fixed rods penetrating through the movable plates are symmetrically arranged in the protective box, and the movable plates can slide on the surfaces of the fixed rods.
Preferably, the locking assembly comprises an adjusting screw rod in threaded connection with the fixed box, one end of the adjusting screw rod is rotationally connected with a positioning plate, a plurality of groups of inserting rods capable of being buckled into the fixed block are fixedly arranged on one side of the positioning plate away from the adjusting screw rod, and an auxiliary piece for limiting the moving direction of the positioning plate is fixedly arranged on one side of the positioning plate connected with the adjusting screw rod.
Preferably, the auxiliary piece comprises two groups of auxiliary rods fixedly connected with the positioning plate, the two groups of auxiliary rods are symmetrically arranged on two sides of the adjusting screw rod, and the two groups of auxiliary rods are slidably arranged in the fixed box.
Preferably, one end of the adjusting screw, which is far away from the positioning plate, is welded with a turntable, and a plurality of groups of anti-skid grooves are formed in the outer ring of the turntable.
Compared with the prior art, the utility model has the beneficial effects that:
1. According to the utility model, the U-shaped support rod is arranged to mount the external power supply electricity taking device at the bottom far away from the unmanned aerial vehicle body, so that the external power supply body can conveniently dissipate heat of the external power supply body during use, the top of the external power supply body is provided with the fixing block which is buckled to the bottom of the U-shaped support rod, and the positioning plate, the inserting rod and the auxiliary rod moving rod are driven by the adjusting screw rod, so that the external power supply body can be conveniently assembled and disassembled rapidly.
2. According to the utility model, the push-pull rod is arranged to move the U-shaped support rod, the push-pull rod drives the slide rod and the movable plate to move, and the movable plate drives the telescopic spring to move, so that elastic support positioning can be provided for the U-shaped support rod, after the external power supply power taking device is disassembled, the U-shaped support rod is automatically reset through resetting of the telescopic spring, folding and storage of the installation structure can be facilitated, normal use of the unmanned aerial vehicle body at ordinary times is facilitated, and other equipment and the like can be assembled at the bottom of the unmanned aerial vehicle body.
Drawings
FIG. 1 is a schematic diagram of the overall structure of the present utility model;
FIG. 2 is a bottom view of the overall structure of the present utility model;
FIG. 3 is an enlarged view of FIG. 1A in accordance with the present utility model;
Fig. 4 is an enlarged view of B of fig. 2 in accordance with the present utility model.
In the figure, 1, an unmanned aerial vehicle body; 2, an installation groove, 3, a protective box, 4, an external power supply body, 5, a fixed block, 6, a U-shaped supporting rod, 7, a communicating groove, 8, a fixed box, 9, a sliding rod, 10, a push-pull rod, 11, a movable plate, 12, a telescopic spring, 13, a fixed rod, 14, an adjusting screw rod, 15, a positioning plate, 16, an inserting rod, 17, an auxiliary rod, 18 and a rotary table.
Detailed Description
The following description of the embodiments of the present utility model will be made clearly and completely with reference to the accompanying drawings, in which it is apparent that the embodiments described are only some embodiments of the present utility model, but not all embodiments. 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. 1-4, in the embodiment of the utility model, an external power supply electricity taking device for an unmanned aerial vehicle comprises an unmanned aerial vehicle body 1, wherein an installation groove 2 is formed in the bottom of the unmanned aerial vehicle body 1, two groups of supporting frames are symmetrically installed in the installation groove 2 in a rotating mode, two groups of protection boxes 3 are symmetrically installed at the bottom of the unmanned aerial vehicle body 1, elastic telescopic components capable of sliding in the supporting frames are installed in the protection boxes 3, the bottoms of the two groups of supporting frames are abutted to an external power supply body 4, two groups of fixing blocks 5 which are buckled to the inside of the supporting frames are symmetrically installed at the top of the external power supply body 4, locking components for positioning the fixing blocks 5 are installed on one side of the bottom of the supporting frames, and the unmanned aerial vehicle body 1 and the external power supply body 4 can be connected through inserted connection wires.
When needs are installed to external power supply get electric installation, pull open two sets of support frames of mounting groove 2 inside relatively, after the support frame moved to suitable position, with the fixed block 5 buckle at external power supply body 4 top to the support frame on, operating personnel rotates locking subassembly and can be fixed to the bottom of support frame with external power supply body 4, can drive the flexible subassembly and remove when the support frame rotates, after the external power supply body 4 of bottom is dismantled, can accomodate the support frame to the below of mounting groove 2 through the reset of flexible subassembly, prevent unmanned aerial vehicle body 1 when normal use and accomodate, support frame, locking subassembly etc. occupy great space.
In one embodiment, specifically, the support frame includes a U-shaped support rod 6 rotatably installed in the installation groove 2, two sets of communication grooves 7 for sliding the elastic telescopic component are symmetrically formed in the U-shaped support rod 6, and a fixing box 8 for supporting the locking component is integrally formed at one side of the bottom end of the U-shaped support rod 6.
The elastic telescopic assembly comprises two groups of sliding rods 9 which are slidably mounted in the protective box 3, one ends of the two groups of sliding rods 9 extending to the interior of the protective box 3 are connected with push-pull rods 10 which can slide in the interior of the communication groove 7, one ends of the two groups of sliding rods 9 located in the interior of the protective box 3 are connected with the same movable plate 11, and telescopic springs 12 sleeved on the outer rings of the sliding rods 9 are connected between the movable plate 11 and the interior of the protective box 3.
The U-shaped supporting rod 6 is pulled to rotate, the U-shaped supporting rod 6 drives the fixed box 8 to rotate, the U-shaped supporting rod 6 simultaneously drives the push-pull rod 10 to slide in the communicating groove 7 when moving, the push-pull rod 10 drives the slide rod 9 to move, the slide rod 9 drives the movable plate 11 to move in the protective box 3, the movable plate 11 drives the telescopic spring 12 to stretch out and draw back, the U-shaped supporting rod 6 can be restored to be stored by utilizing the restoration of the telescopic spring 12 after the external force on the U-shaped supporting rod 6 is withdrawn, further, two groups of fixed rods 13 penetrating through the movable plate 11 are symmetrically arranged in the protective box 3, the movable plate 11 can slide on the surface of the fixed rod 13, and the movable plate 11, the slide rod 9 and the telescopic spring 12 can move more stably.
In one embodiment, the locking assembly comprises an adjusting screw 14 in threaded connection with the fixing box 8, one end of the adjusting screw 14 is rotationally connected with a positioning plate 15, one side of the positioning plate 15 away from the adjusting screw 14 is fixedly provided with a plurality of groups of inserting rods 16 which can be buckled inside the fixing block 5, one side of the positioning plate 15 connected with the adjusting screw 14 is fixedly provided with auxiliary pieces for limiting the moving direction of the positioning plate 15, the auxiliary pieces comprise two groups of auxiliary rods 17 fixedly connected with the positioning plate 15, the two groups of auxiliary rods 17 are symmetrically arranged on two sides of the adjusting screw 14, and the two groups of auxiliary rods 17 are slidably arranged inside the fixing box 8.
Two sets of fixed blocks 5 at the top of the external power supply body 4 are respectively buckled to the interiors of the two sets of U-shaped supporting rods 6, an operator rotates the adjusting screw 14, the adjusting screw 14 drives the positioning plate 15 to move, the positioning plate 15 drives the auxiliary rod 17 to slide in the interior of the fixed box 8, the positioning plate 15 simultaneously drives the inserting rod 16 to move, the inserting rod 16 is buckled to the interiors of the fixed blocks 5, the fixed blocks 5 and the external power supply body 4 can be fixed, further, one end of the adjusting screw 14, which is far away from the positioning plate 15, is welded with the turntable 18, a plurality of groups of anti-skid grooves are formed in the outer ring of the turntable 18, and the operator can conveniently rotate the adjusting screw 14.
The foregoing is only a preferred embodiment of the present utility model, but the scope of the present utility model is not limited thereto, and any person skilled in the art, who is within the scope of the present utility model, should make equivalent substitutions or modifications according to the technical scheme of the present utility model and the inventive concept thereof, and should be covered by the scope of the present utility model.
Claims (7)
1. The unmanned aerial vehicle external power supply electricity taking device comprises an unmanned aerial vehicle body (1) and is characterized in that an installation groove (2) is formed in the bottom of the unmanned aerial vehicle body (1), two groups of support frames are symmetrically installed in the installation groove (2) in a rotating mode, two groups of protection boxes (3) are symmetrically installed at the bottom of the unmanned aerial vehicle body (1), and elastic telescopic components capable of sliding in the support frames are installed in the protection boxes (3);
Two sets of bottom butt of support frame has external power source body (4), two sets of buckle to inside fixed block (5) of support frame are installed to the top symmetry of external power source body (4), and locking subassembly to fixed block (5) location is installed to one side of support frame bottom.
2. The external power supply electricity taking device of the unmanned aerial vehicle according to claim 1, wherein the supporting frame comprises a U-shaped supporting rod (6) rotatably installed in the installation groove (2), two groups of communication grooves (7) for sliding the elastic telescopic components are symmetrically formed in the U-shaped supporting rod (6), and a fixing box (8) for supporting the locking component is integrally formed on one side of the bottom end of the U-shaped supporting rod (6).
3. The external power supply electricity taking device of the unmanned aerial vehicle is characterized in that the elastic telescopic assembly comprises two groups of sliding rods (9) which are slidably mounted in the protective box (3), one ends of the two groups of sliding rods (9) extending to the interior of the protective box (3) are connected with push-pull rods (10) which can slide in the interior of the communication groove (7), one ends of the two groups of sliding rods (9) located in the interior of the protective box (3) are connected with the same movable plate (11), and telescopic springs (12) sleeved on the outer ring of the sliding rods (9) are connected between the movable plate (11) and the interior of the protective box (3).
4. The external power supply electricity taking device of the unmanned aerial vehicle according to claim 3, wherein two groups of fixed rods (13) penetrating through the movable plate (11) are symmetrically arranged in the protective box (3), and the movable plate (11) can slide on the surface of the fixed rods (13).
5. The external power supply electricity taking device of the unmanned aerial vehicle according to claim 2, wherein the locking assembly comprises an adjusting screw (14) in threaded connection with the fixed box (8), one end of the adjusting screw (14) is rotatably connected with a positioning plate (15), one side, far away from the adjusting screw (14), of the positioning plate (15) is fixedly provided with a plurality of groups of inserting rods (16) which can be buckled into the fixed block (5), and one side, connected with the adjusting screw (14), of the positioning plate (15) is fixedly provided with an auxiliary part for limiting the moving direction of the positioning plate (15).
6. The external power supply electricity taking device for the unmanned aerial vehicle according to claim 5, wherein the auxiliary parts comprise two groups of auxiliary rods (17) fixedly connected with the positioning plate (15), the two groups of auxiliary rods (17) are symmetrically arranged on two sides of the adjusting screw (14), and the two groups of auxiliary rods (17) are slidably arranged in the fixed box (8).
7. The external power supply electricity taking device for the unmanned aerial vehicle according to claim 5, wherein one end, far away from the positioning plate (15), of the adjusting screw (14) is welded with a rotary disc (18), and a plurality of groups of anti-skid grooves are formed in the outer ring of the rotary disc (18).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202421074918.6U CN222380757U (en) | 2024-05-17 | 2024-05-17 | An external power supply device for unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202421074918.6U CN222380757U (en) | 2024-05-17 | 2024-05-17 | An external power supply device for unmanned aerial vehicle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN222380757U true CN222380757U (en) | 2025-01-21 |
Family
ID=94247043
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202421074918.6U Active CN222380757U (en) | 2024-05-17 | 2024-05-17 | An external power supply device for unmanned aerial vehicle |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN222380757U (en) |
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2024
- 2024-05-17 CN CN202421074918.6U patent/CN222380757U/en active Active
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