CN210258824U - Fire control is with electronic unmanned aerial vehicle of many rotors - Google Patents
Fire control is with electronic unmanned aerial vehicle of many rotors Download PDFInfo
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- CN210258824U CN210258824U CN201921205624.1U CN201921205624U CN210258824U CN 210258824 U CN210258824 U CN 210258824U CN 201921205624 U CN201921205624 U CN 201921205624U CN 210258824 U CN210258824 U CN 210258824U
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Abstract
The utility model provides a fire control is with many rotor electric unmanned aerial vehicle. Including unmanned aerial vehicle body, control mainboard, folding mechanism and heat dissipation mechanism, folding mechanism is located the lower extreme surface of unmanned aerial vehicle body, folding mechanism includes the telescopic link, one side surface sliding connection of telescopic link has the connecting block, one side surface fixed connection of connecting block has the rotation splint. The utility model provides a fire control is with many rotor electric unmanned aerial vehicle has telescopic link, connecting block, rotating splint, pivot, connecting rod, rotating panel, connecting rod No. two, rotating panel No. two, can fold and receive and release when no longer using the device, reduces occupation position, and the installation is simple, and convenient to use, the cost of manufacture is cheap; the installation panel, mounting screw, host computer, axis of rotation, the flabellum that set up can dispel the heat that the fuselage produced, increases radiating frequency, also is favorable to protecting unmanned aerial vehicle's normal work simultaneously, improves work efficiency.
Description
Technical Field
The utility model relates to an unmanned aerial vehicle field especially relates to a fire control is with many rotor electric unmanned aerial vehicle.
Background
An unmanned aircraft, abbreviated as "drone", and abbreviated in english as "UAV", is an unmanned aircraft that is operated by a radio remote control device and a self-contained program control device, or is operated autonomously, either completely or intermittently, by an onboard computer.
Like the utility model discloses a green type discharging device for dry-mixed mortar of utility model that the bulletin number is CN206046040U, it has realized through putting into in the hollow structure of horn pole and aerify the inside lining, realizes the effect of tracking the control for a long time, but occupation space also can not protect the telescopic link not receive wearing and tearing when not using the telescopic link, the inside heat that produces of long-time work of machine in addition can't the problem of scattering.
Therefore, it is necessary to provide a multi-rotor electric unmanned aerial vehicle for fire fighting to solve the above technical problems.
Disclosure of Invention
The utility model provides a fire control is with many rotors electric unmanned aerial vehicle has solved occupation space when not using the telescopic link and also can not protect the telescopic link not receive wearing and tearing, the problem that the heat that the machine long-time work inside produced can't be dispelled in addition.
For solving the technical problem, the utility model provides a pair of many rotors electric unmanned aerial vehicle are used in fire control, including unmanned aerial vehicle body, control mainboard, folding mechanism and heat dissipation mechanism, folding mechanism is located the lower extreme surface of unmanned aerial vehicle body, folding mechanism includes the telescopic link, one side surface sliding connection of telescopic link has the connecting block, one side surface fixed connection of connecting block rotates splint, one side middle part internal surface of rotating splint rotates and is connected with the pivot, one side surface of pivot rotates and is connected with a rotating panel, the opposite side surface of pivot rotates and is connected with No. two rotating panel, No. two one side surface fixed connection and a connecting rod of rotating panel, one side internal surface sliding connection of a connecting rod has No. two connecting rods.
Preferably, the heat dissipation mechanism is located the bottom surface of one side of control mainboard, the heat dissipation mechanism is including the installation panel, installation panel bottom middle part outer fixed surface is connected with the host computer, bottom surface one side surface threaded connection of installation panel has the mounting screw, the bottom internal surface of host computer rotates and is connected with the axis of rotation, the outer fixed surface of axis of rotation is connected with the flabellum.
Preferably, the two groups of mounting screws are arranged, the outer surfaces of the mounting screws are coated with a layer of conductive anti-poison paint, and the outer surfaces of the rotating shafts are coated with a layer of lubricating oil.
Preferably, one side of unmanned aerial vehicle body is equipped with the rotor, one side external surface fixedly connected with spliced pole of rotor, the top external surface fixedly connected with solid fixed splint of spliced pole.
Preferably, the inner surface of the middle part of the top end of the fixed clamping plate is rotatably connected with a rotator, and the outer surface of the bottom end of the connecting column is fixedly connected with an engine.
Preferably, the top surface of control mainboard external surface fixedly connected with backup pad, the bottom surface fixedly connected with fixed mounting frame of backup pad, the backup pad all scribbles one deck acrylic acid waterproof coating with fixed mounting frame's surface.
Preferably, the outer fixed surface in the middle part of the bottom of control mainboard is connected with the telescopic link, the bottom of telescopic link is equipped with the mounting bar, fixed mounting groove has been seted up at the bottom middle part of mounting bar.
Preferably, the inner surface of the fixed mounting groove is connected with a mounting column in a threaded manner, the outer surface of the mounting column is provided with threads, and the outer surface of the bottom end of the mounting column is fixedly connected with a hook.
Compared with the prior art, the utility model provides a pair of fire control is with many rotor electric unmanned aerial vehicle has as follows
(1) The telescopic link, connecting block, rotation splint, pivot, a connecting rod, a rotation panel, No. two connecting rods, No. two rotation panels that set up can fold and receive and release when being convenient for no longer use the device, reduce occupation position, and the installation is simple, and convenient to use, the cost of manufacture is low-priced.
(2) The installation panel, mounting screw, host computer, axis of rotation, the flabellum that set up can dispel the heat that the fuselage produced, increases radiating frequency, also is favorable to protecting unmanned aerial vehicle's normal work simultaneously, improves work efficiency.
Drawings
Fig. 1 is a schematic structural view of a preferred embodiment of a fire-fighting multi-rotor electric unmanned aerial vehicle according to the present invention;
FIG. 2 is a schematic structural view of the telescoping rod shown in FIG. 1;
FIG. 3 is a schematic view of the first rotating panel shown in FIG. 2;
FIG. 4 is a schematic view of the mounting panel of FIG. 1;
fig. 5 is a schematic structural view of the mounting bar and the hook shown in fig. 1.
Reference numbers in the figures: 1. an unmanned aerial vehicle body; 2. a control main board; 3. a telescopic rod; 4. installing a panel; 5. fixing the mounting rack; 6. mounting a bar; 7. hooking; 8. a support plate; 9. an engine; 10. a rotor; 11. fixing the clamping plate; 12. a rotator; 13. connecting columns; 14. connecting blocks; 15. rotating the clamping plate; 16. a rotating shaft; 17. a first connecting rod; 18. a first rotating panel; 19. a second connecting rod; 20. a second rotating panel; 21. mounting screws; 22. a host; 23. a rotating shaft; 24. a fan blade; 25. fixing the mounting groove; 26. connecting columns; 27. and (4) threading.
Detailed Description
The present invention will be further described with reference to the accompanying drawings and embodiments.
Please refer to fig. 1, fig. 2, fig. 3, fig. 4 and fig. 5 in combination, wherein fig. 1 is a schematic structural diagram of a preferred embodiment of a fire-fighting multi-rotor electric drone; FIG. 2 is a schematic structural view of the telescoping rod shown in FIG. 1; FIG. 3 is a schematic view of the first rotating panel shown in FIG. 2; FIG. 4 is a schematic view of the mounting panel of FIG. 1; fig. 5 is a schematic structural view of the mounting bar and the hook shown in fig. 1. A multi-rotor electric unmanned aerial vehicle for fire fighting comprises an unmanned aerial vehicle body 1, a control main board 2, a folding mechanism and a heat dissipation mechanism, wherein the folding mechanism is positioned on the outer surface of the lower end of the unmanned aerial vehicle body 1, the folding mechanism comprises a telescopic rod 3, the outer surface of one side of the telescopic rod 3 is connected with a connecting block 14 in a sliding manner, the outer surface of one side of the connecting block 14 is fixedly connected with a rotating splint 15, the inner surface of the middle part of one side of the rotating splint 15 is connected with a rotating shaft 16 in a rotating manner, the outer surface of one side of the rotating shaft 16 is connected with a first rotating panel 18 in a rotating manner, the outer surface of the other side of the rotating shaft 16 is connected with a second rotating panel 20 in a rotating manner, the outer surface of one side of the second rotating panel 20 is fixedly connected, convenient use and low manufacturing cost.
The device can be folded and stored conveniently when not used, in the preferred embodiment, the heat dissipation mechanism is located on the outer surface of one side of the bottom of the control main board 2 and comprises an installation panel 4, the outer surface of the middle part of the bottom end of the installation panel 4 is fixedly connected with a host computer 22, the outer surface of one side of the bottom of the installation panel 4 is connected with an installation screw 21 in a threaded mode, the inner surface of the bottom of the host computer 22 rotates and is connected with a rotating shaft 23, and the outer surface of the rotating shaft 23 is fixedly connected with.
The installation screws 21 are arranged to facilitate the fixed connection of the outer surface of one side of the installation panel 4 to the outer surface of the bottom of the mounting plate (2). in the embodiment, preferably, two sets of installation screws 21 are arranged, the outer surface of the installation screws 21 is coated with a layer of conductive anti-poison paint, and the outer surface of the rotating shaft 23 is coated with a layer of lubricating oil.
Through the rotor 10 that is equipped with, be convenient for unmanned aerial vehicle's taking off, this embodiment, it is preferred, one side of unmanned aerial vehicle body 1 is equipped with rotor 10, and one side external fixed surface of rotor 10 is connected with spliced pole 13, and the top external fixed surface of spliced pole 13 is connected with solid fixed splint 11.
The unmanned aerial vehicle's of being convenient for whole operation, this embodiment, it is preferred, the top middle part internal surface rotation of solid fixed splint 11 is connected with rotating ware 12, and the bottom external surface fixed connection of spliced pole 13 has engine 9.
Placing when being convenient for unmanned aerial vehicle does not use, this embodiment, it is preferred, the top external fixed surface of control mainboard 2 is connected with backup pad 8, the bottom external fixed surface of backup pad 8 is connected with fixed mounting bracket 5, backup pad 8 all scribbles one deck acrylic acid waterproof coating with fixed mounting bracket 5's surface.
Be convenient for support and connect, this embodiment, it is preferred, the bottom middle part external surface fixed connection of control mainboard 2 has telescopic link 3, and the bottom of telescopic link 3 is equipped with mounting bar 6, and fixed mounting groove 25 has been seted up at the bottom middle part of mounting bar 6.
The connection is more stable, in this embodiment, preferably, the inner surface of the fixing installation groove 25 is connected with the installation column 26 through screw threads, the outer surface of the installation column 26 is provided with screw threads 27, and the outer surface of the bottom end of the installation column 26 is fixedly connected with the hook 7.
The utility model provides a pair of fire control is with many rotor electric unmanned aerial vehicle's theory of operation as follows: firstly, the outer surface of one side of the telescopic rod 3 is connected to the inner surface of one side of the connecting block 14 in a sliding manner, then the outer surface of the other side of the connecting block 14 is fixedly connected to the outer surface of one side of the rotating clamp plate 15, then the outer surface of the rotating clamp plate 15 is connected to the outer surface of one side of the first rotating panel 18 in a rotating manner through the outer surface of the rotating shaft 16, then the outer surface of one side of the second rotating panel 20 is connected to the outer surface of one side of the rotating shaft 16 in a rotating manner, then the outer surface of one side of the first connecting rod 17 is connected to the outer surface of one side of the first rotating panel 18, and then the outer surface of one side of the second connecting rod 19 is connected to the inner surface of the other side of the; at first with one side surface fixed connection of host computer 22 at one side of installation panel 4 middle part outward appearance, again with one side surface swivelling joint of axis of rotation 23 at one side of host computer 22 middle part internal surface, then with one side surface of flabellum 24 fixed connection at axis of rotation 23, at last with one side surface threaded connection of installation panel 4's opposite side surface through mounting screw 21 in bottom one side surface of control mainboard 2 again, can go the heat that the fuselage produced, increase radiating frequency, also be favorable to protecting unmanned aerial vehicle's normal work simultaneously, and the work efficiency is improved.
Compared with the prior art, the utility model provides a pair of many rotors electric unmanned aerial vehicle for fire control has following beneficial effect:
1. the telescopic link 3, the connecting block 14, rotate splint 15, pivot 16, a connecting rod 17, a rotation panel 18, No. two connecting rods 19, No. two rotation panels 20 that set up, can fold when being convenient for no longer use the device and receive and release, reduce and occupy the position, the installation is simple, and convenient to use, the cost of manufacture is low-priced.
2. The installation panel 4, mounting screw 21, host computer 22, axis of rotation 23, flabellum 24 that set up can dispel the heat that the fuselage produced, increase the radiating frequency, also are favorable to protecting unmanned aerial vehicle's normal work simultaneously, improve work efficiency.
The above only is the embodiment of the present invention, not limiting the scope of the present invention, all the equivalent structures or equivalent processes of the present invention are used in the specification and the attached drawings, or directly or indirectly applied to other related technical fields, and the same principle is included in the protection scope of the present invention.
Claims (8)
1. The utility model provides a fire control is with electronic unmanned aerial vehicle of many rotors, its characterized in that includes: an unmanned aerial vehicle body (1), a control main board (2), a folding mechanism and a heat dissipation mechanism, the folding mechanism is positioned on the outer surface of the lower end of the unmanned aerial vehicle body (1), the folding mechanism comprises a telescopic rod (3), the outer surface of one side of the telescopic rod (3) is connected with a connecting block (14) in a sliding way, the outer surface of one side of the connecting block (14) is fixedly connected with a rotating clamping plate (15), the inner surface of the middle part of one side of the rotating splint (15) is rotationally connected with a rotating shaft (16), the outer surface of one side of the rotating shaft (16) is rotationally connected with a first rotating panel (18), the outer surface of the other side of the rotating shaft (16) is rotatably connected with a second rotating panel (20), the outer surface of one side of the second rotating panel (20) is fixedly connected with a first connecting rod (17), the inner surface of one side of the first connecting rod (17) is connected with a second connecting rod (19) in a sliding manner.
2. The fire-fighting multi-rotor electric unmanned aerial vehicle as claimed in claim 1, wherein the heat dissipation mechanism is located on the outer surface of one side of the bottom of the control main board (2), the heat dissipation mechanism comprises a mounting panel (4), a main machine (22) is fixedly connected to the outer surface of the middle portion of the bottom end of the mounting panel (4), a mounting screw (21) is connected to the outer surface of one side of the bottom of the mounting panel (4) in a threaded manner, a rotating shaft (23) is rotatably connected to the inner surface of the bottom of the main machine (22), and fan blades (24) are fixedly connected to the outer surface of the rotating shaft (.
3. A fire fighting multi-rotor electric drone according to claim 2, characterized in that there are two sets of mounting screws (21), the outer surface of the mounting screws (21) is coated with a layer of conductive anti-toxic paint, and the outer surface of the rotating shaft (23) is coated with a layer of lubricating oil.
4. A fire-fighting multi-rotor electric unmanned aerial vehicle as claimed in claim 1, wherein one side of the unmanned aerial vehicle body (1) is provided with a rotor (10), a connecting column (13) is fixedly connected to the outer surface of one side of the rotor (10), and a fixing splint (11) is fixedly connected to the outer surface of the top end of the connecting column (13).
5. A fire fighting multi-rotor electric unmanned aerial vehicle according to claim 4, characterized in that a rotator (12) is rotatably connected to the inner surface of the top middle part of the fixing splint (11), and an engine (9) is fixedly connected to the outer surface of the bottom end of the connecting column (13).
6. A fire-fighting multi-rotor electric unmanned aerial vehicle as claimed in claim 1, wherein the top outer surface of the control main board (2) is fixedly connected with a support plate (8), the bottom outer surface of the support plate (8) is fixedly connected with a fixed mounting frame (5), and the outer surfaces of the support plate (8) and the fixed mounting frame (5) are coated with a layer of acrylic waterproof paint.
7. The fire-fighting multi-rotor electric unmanned aerial vehicle as claimed in claim 1, wherein the outer surface of the middle portion of the bottom end of the control main board (2) is fixedly connected with a telescopic rod (3), a mounting bar (6) is arranged at the bottom of the telescopic rod (3), and a fixing mounting groove (25) is formed in the middle portion of the bottom end of the mounting bar (6).
8. A fire-fighting multi-rotor electric unmanned aerial vehicle as claimed in claim 7, wherein the inner surface of the fixing installation groove (25) is connected with an installation column (26) through screw threads, the outer surface of the installation column (26) is provided with screw threads (27), and the outer surface of the bottom end of the installation column (26) is fixedly connected with a hook (7).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201921205624.1U CN210258824U (en) | 2019-07-29 | 2019-07-29 | Fire control is with electronic unmanned aerial vehicle of many rotors |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201921205624.1U CN210258824U (en) | 2019-07-29 | 2019-07-29 | Fire control is with electronic unmanned aerial vehicle of many rotors |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN210258824U true CN210258824U (en) | 2020-04-07 |
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ID=70014865
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201921205624.1U Active CN210258824U (en) | 2019-07-29 | 2019-07-29 | Fire control is with electronic unmanned aerial vehicle of many rotors |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN210258824U (en) |
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2019
- 2019-07-29 CN CN201921205624.1U patent/CN210258824U/en active Active
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| Date | Code | Title | Description |
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| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CP01 | Change in the name or title of a patent holder |
Address after: 610000 No. 1, 1st floor, 2nd building, 26 Xinwen Road, Chengdu High-tech Zone, Sichuan Province Patentee after: Dewiver Intelligent Equipment Group Co., Ltd Address before: 610000 No. 1, 1st floor, 2nd building, 26 Xinwen Road, Chengdu High-tech Zone, Sichuan Province Patentee before: Sichuan diweifu Intelligent Equipment Co.,Ltd. |
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| CP01 | Change in the name or title of a patent holder |