CN220577528U - Unmanned aerial vehicle convenient to change battery - Google Patents
Unmanned aerial vehicle convenient to change battery Download PDFInfo
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- CN220577528U CN220577528U CN202321711057.3U CN202321711057U CN220577528U CN 220577528 U CN220577528 U CN 220577528U CN 202321711057 U CN202321711057 U CN 202321711057U CN 220577528 U CN220577528 U CN 220577528U
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- 238000003466 welding Methods 0.000 claims description 35
- 238000012544 monitoring process Methods 0.000 description 4
- 238000012986 modification Methods 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 208000035473 Communicable disease Diseases 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 238000005286 illumination Methods 0.000 description 1
- 208000015181 infectious disease Diseases 0.000 description 1
- 238000007689 inspection Methods 0.000 description 1
- 238000012423 maintenance Methods 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 238000013507 mapping Methods 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 230000000149 penetrating effect Effects 0.000 description 1
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Abstract
The utility model discloses an unmanned aerial vehicle convenient to replace a battery, and relates to the field of unmanned aerial vehicles. According to the utility model, the battery main body, the placing rack and the fixing plate are pushed to move through the box cover, the fixing plate is limited through the connecting block, the second spring and the first limiting rod, the positions of the fixing plate and the placing rack are limited, and an operator can conveniently and quickly replace the battery main body of the unmanned aerial vehicle through arranging the power supply structure and the pushing mechanism, so that the replacement of the battery main body of the unmanned aerial vehicle does not need to depend on a screwdriver, and the battery main body of the unmanned aerial vehicle is convenient to replace.
Description
Technical Field
The utility model relates to the technical field of unmanned aerial vehicles, in particular to an unmanned aerial vehicle with a battery convenient to replace.
Background
Unmanned plane is unmanned plane controlled by radio remote control equipment and self-contained program control device, or is operated by vehicle-mounted computer completely or intermittently and autonomously, and unmanned plane can be classified into military and civil according to application field. For military purposes, unmanned aerial vehicles are classified into reconnaissance and drones. In civil aspect, the unmanned aerial vehicle industry application is the real just-needed unmanned aerial vehicle; the method is applied to the fields of aerial photography, agriculture, plant protection, miniature self-timer shooting, express delivery transportation, disaster relief, wild animal observation, infectious disease monitoring, mapping, news reporting, power inspection, disaster relief, film and television shooting, romantic manufacturing and the like.
When current unmanned aerial vehicle needs to cruise the monitoring, supply power to the controller through the power, the controller controls unmanned aerial vehicle and flies, carry out real-time video recording to the monitoring position through controller control camera and light, current unmanned aerial vehicle need use the screwdriver to dismantle the bolt that the battery was covered when changing the battery, thereby dismantle and change the battery cover, because the battery of unmanned aerial vehicle need use the screwdriver to dismantle the bolt that the battery was covered when changing, just can change the battery, and the bolt volume on the battery cover is less, lose easily, and need use the screwdriver just can change unmanned aerial vehicle's battery, make unmanned aerial vehicle's battery be difficult for changing.
Disclosure of Invention
The utility model aims to provide an unmanned aerial vehicle with a battery convenient to replace, so as to solve the problem that the battery of the unmanned aerial vehicle in the current market is not easy to replace, which is proposed by the background technology.
In order to achieve the above purpose, the present utility model provides the following technical solutions: the utility model provides an unmanned aerial vehicle convenient to change battery, includes organism, base, power supply structure, pushing mechanism, support column and go-between, there is the base the bottom of organism through bolted connection, the inside of organism is provided with the power supply structure that extends to the organism outside, the bottom of power supply structure is provided with pushing mechanism, the top welding of organism has the support column, the outer wall cover of support column is equipped with the go-between, the inside of support column is provided with stop gear, pushing mechanism is including connecting box, first dead lever, first spring, guard plate, mount, torsion spring, connecting block, second spring, first gag lever post, connecting rod and turning block, the inside welding of organism has the connecting box that extends to the organism outside, the inside welding of connecting box has first dead lever, the outer wall cover of first dead lever is equipped with first spring, the outer wall welding of connecting box has the mount, the welding of the inside bottom of connecting box has the torsion spring, one side welding that the mount was kept away from to torsion spring has the connecting block, the inside of connecting block is provided with the second spring.
Preferably, the inside of connecting block is located the top of second spring and is provided with first gag lever post, one side welding that torsion spring was kept away from to the connecting block has the connecting rod that extends to the guard plate inboard, the one end welding of connecting rod has the turning block.
Preferably, the power supply structure is including battery case, rack, battery main part, lid, electric wire, sliding tray and fixed plate, the top welding of connection box has the battery case, the inside of battery case is provided with the rack, the internally mounted of rack has the battery main part.
Preferably, the one end welding of rack has the lid that extends to the battery case outside, the inside of battery case is provided with the electric wire that extends to the organism inside, the sliding tray that extends to the connection box inside is seted up to the bottom of battery case, the bottom welding of rack has the fixed plate that extends to first dead lever outer wall.
Preferably, the inside of organism is installed with electric wire connection's controller, the camera that extends to the organism outside is installed to the one end of controller, the light is installed on the top of camera.
Preferably, the outer wall welding of go-between has the support frame, the inboard welding of support frame has the link, the internally mounted of link has the fan blade.
Preferably, the stop gear is including threaded rod, first conical gear, second gag lever post, spacing balladeur train, slide bar, second conical gear, second dead lever and interior hexagonal groove piece, the inside of support column is provided with the threaded rod, the outer wall welding of threaded rod has first conical gear, the outer wall at threaded rod both ends all overlaps and is equipped with the second gag lever post, the inner wall welding of support column has spacing balladeur train, the outer wall welding of second gag lever post has the slide bar that runs through spacing balladeur train.
Preferably, one side at the top end of the first conical gear is provided with a second conical gear, a second fixing rod is welded at the top end of the second conical gear, and an inner hexagonal groove block is welded at the top end of the second fixing rod.
Compared with the prior art, the utility model has the beneficial effects that:
1. this unmanned aerial vehicle needs when changing the battery, make first gag lever post can't carry out spacingly to the fixed plate through rotating the piece, the connecting rod, the connecting block, first gag lever post and torsion spring, first spring promotes rack through the fixed plate, battery body and lid remove, make the battery body remove to the outside of battery case, after changing the battery body, promote battery body through the lid, rack and fixed plate remove, it is spacing to the fixed plate through the connecting block, second spring and first gag lever post, make the position of fixed plate and rack carry out spacingly, be convenient for operating personnel carry out quick replacement to unmanned aerial vehicle's battery body through setting up power supply structure and pushing mechanism, make unmanned aerial vehicle's battery body change need not rely on the screwdriver, make unmanned aerial vehicle's battery body be convenient for change.
2. When this unmanned aerial vehicle's fan blade needs to be changed, drive interior hexagonal groove piece, second dead lever and second bevel gear through outer hexagonal wrench and rotate, second bevel gear drives first bevel gear and threaded rod and rotates, drives two sets of second gag levers post through the threaded rod and remove for the second gag lever post can't carry out spacingly to the go-between, makes go-between, support frame, link and wind leaf be convenient for dismantle fast, makes unmanned aerial vehicle's support frame, link and wind leaf be convenient for dismouting and maintenance.
Drawings
FIG. 1 is a front view of the present utility model;
FIG. 2 is a front cut-away view of the present utility model;
FIG. 3 is a top view of the connecting ring of the present utility model;
FIG. 4 is a front cut-away view of the spacing mechanism of the present utility model;
fig. 5 is a front cut-away view of the power supply structure and the pushing mechanism of the present utility model.
In the figure: 1. a body; 101. a controller; 102. a camera; 103. a lighting lamp; 2. a base; 3. a power supply structure; 301. a battery case; 302. a placing rack; 303. a battery main body; 304. a box cover; 305. an electric wire; 306. a sliding groove; 307. a fixing plate; 4. a pushing mechanism; 401. a connection box; 402. a first fixing rod; 403. a first spring; 404. a protection plate; 405. a fixing frame; 406. a torsion spring; 407. a connecting block; 408. a second spring; 409. a first stop lever; 410. a connecting rod; 411. a rotating block; 5. a support column; 6. a connecting ring; 601. a support frame; 602. a connecting frame; 603. a fan blade; 7. a limiting mechanism; 701. a threaded rod; 702. a first bevel gear; 703. a second limit rod; 704. limiting sliding frame; 705. a slide bar; 706. a second bevel gear; 707. a second fixing rod; 708. and an inner hexagonal groove block.
Description of the embodiments
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, 2, 3, 4 and 5, the present utility model provides a technical solution: the utility model provides an unmanned aerial vehicle convenient to change battery, including organism 1, the base 2, power supply structure 3, pushing mechanism 4, support column 5 and go-between 6, there is base 2 bottom of organism 1 through bolted connection, the inside of organism 1 is provided with the power supply structure 3 that extends to the organism 1 outside, the bottom of power supply structure 3 is provided with pushing mechanism 4, the top welding of organism 1 has support column 5, the outer wall cover of support column 5 is equipped with go-between 6, the inside of support column 5 is provided with stop gear 7, pushing mechanism 4 is including the junction box 401, first dead lever 402, first spring 403, guard plate 404, mount 405, torsion spring 406, connecting block 407, second spring 408, first gag lever post 409, connecting rod 410 and rotating block 411, the inside welding of organism 1 has the junction box 401 that extends to the organism 1 outside, the inside welding of junction box 401 has first dead lever 402, the outer wall cover of first dead lever 402 is equipped with first spring 403, the outer wall welding of junction box 401 has guard plate 404, the inside bottom welding of junction box 405 has mount 405, one side welding of mount 405 has torsion spring 406, one side welding of torsion spring 406 has mount 405, the inside of junction box 408 is provided with second connecting block 408.
Referring to fig. 1, 2 and 5, a first limit lever 409 is disposed at the top end of the second spring 408 in the connecting block 407, a connecting rod 410 extending to the inner side of the protection plate 404 is welded at one side of the connecting block 407 away from the torsion spring 406, a rotating block 411 is welded at one end of the connecting rod 410, and the outer wall at the bottom end of the first limit lever 409 is slidably connected with the inner wall of the connecting block 407.
In specific implementation, when the battery of the unmanned aerial vehicle needs to be replaced, the rotating block 411 rotates to drive the connecting rod 410, the connecting block 407 and the first limiting rod 409 to rotate, the first limiting rod 409 rotates to drive the torsion spring 406 to twist and deform, the first limiting rod 409 rotates to enable the first limiting rod 409 to be incapable of limiting the fixed plate 307, the first spring 403 loses limit to reset, the first spring 403 pushes the fixed plate 307, the placing frame 302, the battery body 303 and the box cover 304 to move, the fixed plate 307 slides on the inner wall of the sliding groove 306 to enable the placing frame 302 to drive the battery body 303 to move to the outer side of the battery box 301, the rotating block 411 is released, the torsion spring 406 loses limit to drive the connecting block 407, the first limiting rod 409, the connecting rod 410 and the rotating block 411 to reset, after the battery main body 303 is replaced by an operator, the box cover 304 is pushed to the inside of the battery box 301, the box cover 304 pushes the placing frame 302 and the fixing plate 307 to move, the fixing plate 307 pushes the first spring 403 to compress and deform, one side of the bottom end of the fixing plate 307 contacts with one side of the top end of the first limiting rod 409, the fixing plate 307 pushes the first limiting rod 409 to descend, the first limiting rod 409 descends to push the second spring 408 to compress and deform, after the fixing plate 307 moves to one side of the first limiting rod 409, the second spring 408 loses limit to reset, the second spring 408 pushes the first limiting rod 409 to limit the fixing plate 307, the battery main body 303 of the unmanned aerial vehicle is convenient to replace quickly by arranging the power supply structure 3 and the pushing mechanism 4, the battery replacing efficiency is effectively improved, and the battery replacing operation of the operator is convenient to conduct.
Referring to fig. 1, 2 and 5, the power supply structure 3 includes a battery case 301, a placement frame 302, a battery main body 303, a case cover 304, an electric wire 305, a sliding groove 306 and a fixing plate 307, wherein the top end of the connection case 401 is welded with the battery case 301, the placement frame 302 is disposed in the battery case 301, the battery main body 303 is mounted in the placement frame 302, the case cover 304 extending to the outer side of the battery case 301 is welded at one end of the placement frame 302, the electric wire 305 extending to the inner side of the machine body 1 is disposed in the battery case 301, the sliding groove 306 extending to the inner side of the connection case 401 is disposed at the bottom end of the battery case 301, the fixing plate 307 extending to the outer wall of the first fixing rod 402 is welded at the bottom end of the placement frame 302, the inner wall of the fixing plate 307 is slidably connected with the outer wall of the first fixing rod 402, and the outer wall of the placement frame 302 is slidably connected with the inner wall of the battery case 301.
In specific implementation, the battery main body 303 of the unmanned aerial vehicle is limited by the placement frame 302.
Referring to fig. 1 and 2, a controller 101 connected with an electric wire 305 is installed inside the machine body 1, a camera 102 extending to the outside of the machine body 1 is installed at one end of the controller 101, a lighting lamp 103 is installed at the top end of the camera 102, and the controller 101 is electrically connected with the camera 102 and the lighting lamp 103.
In specific implementation, the controller 101 controls the camera 102 and the lighting lamp 103 to be started and closed.
Referring to fig. 1, 2, 3 and 4, a supporting frame 601 is welded on the outer wall of the connecting ring 6, a connecting frame 602 is welded on the inner side of the supporting frame 601, a fan blade 603 is mounted in the connecting frame 602, the fan blade 603 is electrically connected with the controller 101, and the fan blade 603 is connected with the electric wire 305 through a buckle.
In specific implementation, the controller 101 controls the fan blade 603 to operate, the battery main body 303 supplies power to the fan blade 603 through the electric wire 305, so that the fan blade 603 operates, and the unmanned aerial vehicle is driven to fly through the fan blade 603.
Referring to fig. 2, 3 and 4, the limiting mechanism 7 includes a threaded rod 701, a first conical gear 702, a second limiting rod 703, a limiting carriage 704, a sliding rod 705, a second conical gear 706, a second fixing rod 707 and an inner hexagonal groove 708, wherein the threaded rod 701 is disposed inside the supporting column 5, the first conical gear 702 is welded on the outer wall of the threaded rod 701, the second limiting rod 703 is sleeved on the outer walls of the two ends of the threaded rod 701, the limiting carriage 704 is welded on the inner wall of the supporting column 5, the sliding rod 705 penetrating through the limiting carriage 704 is welded on the outer wall of the second limiting rod 703, a second conical gear 706 is disposed on one side of the top end of the first conical gear 702, a second fixing rod 707 is welded on the top end of the second conical gear 706, inner hexagonal groove 708 is welded on the outer wall of the two ends of the threaded rod 701, the outer wall of the threaded rod 701 is in threaded connection with the inner wall of the second limiting rod 703, the outer wall of the sliding rod 705 is in sliding connection with the inner wall of the limiting carriage 704, the outer wall of the bottom end of the second conical gear 706 is in engagement with the outer wall of the first conical gear 702, and the two ends of the second conical gear 702 are engaged with the inner wall of the limiting ring 6.
In specific implementation, when the fan blade 603 of the unmanned aerial vehicle needs to be overhauled, the output end of the outer hexagonal wrench is inserted into the inner hexagonal groove block 708, the second fixing rod 707 and the second bevel gear 706 are driven by the outer hexagonal wrench to rotate reversely, the second bevel gear 706 rotates reversely to drive the first bevel gear 702 meshed with the second bevel gear 706 to rotate positively, the first bevel gear 702 rotates positively to drive the threaded rod 701 to rotate positively, the threaded rod 701 rotates positively to drive the two groups of second limiting rods 703 connected with the threaded rod 701 to move, the second limiting rods 703 drive the sliding rods 705 to slide on the inner sides of the limiting carriages 704, the distance between the two groups of second limiting rods 703 is gradually shortened, two ends of the second limiting rods 703 cannot limit the connecting ring 6, the connecting ring 6 is detached from the outer wall of the supporting column 5, and the connecting ring 6, the supporting frame 601, the connecting frames 602 and 603 are convenient to detach, overhaul and replace the fan blade.
To sum up: when the unmanned aerial vehicle is used, the battery body 303 supplies power to the camera 102, the illuminating lamp 103 and the fan blade 603, the controller 101 controls the unmanned aerial vehicle to fly through the fan blade 603, and the camera 102 and the illuminating lamp 103 are used for illumination and shooting monitoring.
Although the present utility model has been described with reference to the foregoing embodiments, it will be apparent to those skilled in the art that modifications may be made to the embodiments described, or equivalents may be substituted for elements thereof, and any modifications, equivalents, improvements and changes may be made without departing from the spirit and principles of the present utility model.
Claims (8)
1. Unmanned aerial vehicle convenient to change battery, including organism (1), base (2), power supply structure (3), pushing mechanism (4), support column (5) and go-between (6), its characterized in that: the utility model discloses a machine body, including support column (1), support column (5) are provided with bottom through bolted connection, there is base (2) bottom of organism (1), the inside of organism (1) is provided with power supply structure (3) that extend to the organism (1) outside, the bottom of power supply structure (3) is provided with pushing mechanism (4), the top welding of organism (1) has support column (5), the outer wall cover of support column (5) is equipped with go-between (6), the inside of support column (5) is provided with stop gear (7), pushing mechanism (4) are including connecting box (401), first dead lever (402), first spring (403), guard plate (404), mount (405), torsion spring (406), connecting block (407), second spring (408), first stop lever (409), connecting rod (410) and rotating block (411), the inside welding of organism (1) has connecting box (401) that extends to the organism (1) outside, the inside welding of connecting box (401) has first dead lever (402), the outer wall cover of first dead lever (402) is equipped with first spring (403), the inside of connecting box (401), one side welding of mount (405) has torsion spring (406), one side welding that torsion spring (406) kept away from mount (405) has connecting block (407), the inside of connecting block (407) is provided with second spring (408).
2. The unmanned aerial vehicle for facilitating battery replacement according to claim 1, wherein: the inside of connecting block (407) is located the top of second spring (408) and is provided with first gag lever post (409), connecting block (407) are kept away from one side welding of torsion spring (406) and are had connecting rod (410) that extend to guard plate (404) inboard, one end welding of connecting rod (410) has rotating block (411).
3. The unmanned aerial vehicle for facilitating battery replacement according to claim 1, wherein: the power supply structure (3) comprises a battery box (301), a placing frame (302), a battery main body (303), a box cover (304), an electric wire (305), a sliding groove (306) and a fixing plate (307), wherein the battery box (301) is welded at the top end of the connecting box (401), the placing frame (302) is arranged in the battery box (301), and the battery main body (303) is arranged in the placing frame (302).
4. A drone for facilitating battery replacement according to claim 3, wherein: the battery box comprises a box body (1), wherein a box cover (304) extending to the outer side of the battery box (301) is welded at one end of a placing frame (302), an electric wire (305) extending to the inner side of the machine body (1) is arranged in the battery box (301), a sliding groove (306) extending to the inner side of a connecting box (401) is formed in the bottom end of the battery box (301), and a fixing plate (307) extending to the outer wall of a first fixing rod (402) is welded at the bottom end of the placing frame (302).
5. The unmanned aerial vehicle for facilitating battery replacement of claim 4, wherein: the intelligent camera is characterized in that a controller (101) connected with an electric wire (305) is arranged in the machine body (1), a camera (102) extending to the outer side of the machine body (1) is arranged at one end of the controller (101), and an illuminating lamp (103) is arranged at the top end of the camera (102).
6. The unmanned aerial vehicle for facilitating battery replacement according to claim 1, wherein: the outer wall welding of go-between (6) has support frame (601), the inboard welding of support frame (601) has link (602), the internally mounted of link (602) has fan blade (603).
7. The unmanned aerial vehicle for facilitating battery replacement according to claim 1, wherein: stop gear (7) are including threaded rod (701), first conical gear (702), second gag lever post (703), limit carriage (704), slide bar (705), second conical gear (706), second dead lever (707) and interior hexagonal groove block (708), the inside of support column (5) is provided with threaded rod (701), the outer wall welding of threaded rod (701) has first conical gear (702), the outer wall at threaded rod (701) both ends all overlaps and is equipped with second gag lever post (703), the inner wall welding of support column (5) has limit carriage (704), the outer wall welding of second gag lever post (703) has slide bar (705) that runs through limit carriage (704).
8. The unmanned aerial vehicle for facilitating battery replacement of claim 7, wherein: one side at first bevel gear (702) top is provided with second bevel gear (706), second dead lever (707) are welded on the top of second bevel gear (706), interior hexagonal groove block (708) are welded on the top of second dead lever (707).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202321711057.3U CN220577528U (en) | 2023-07-03 | 2023-07-03 | Unmanned aerial vehicle convenient to change battery |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202321711057.3U CN220577528U (en) | 2023-07-03 | 2023-07-03 | Unmanned aerial vehicle convenient to change battery |
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| Publication Number | Publication Date |
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| CN220577528U true CN220577528U (en) | 2024-03-12 |
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| Application Number | Title | Priority Date | Filing Date |
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| CN202321711057.3U Active CN220577528U (en) | 2023-07-03 | 2023-07-03 | Unmanned aerial vehicle convenient to change battery |
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| CN (1) | CN220577528U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN118651451A (en) * | 2024-08-19 | 2024-09-17 | 吉林农业科技学院 | A data collection device for investigating intensive use of agricultural land |
-
2023
- 2023-07-03 CN CN202321711057.3U patent/CN220577528U/en active Active
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN118651451A (en) * | 2024-08-19 | 2024-09-17 | 吉林农业科技学院 | A data collection device for investigating intensive use of agricultural land |
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