CN211182296U - Unmanned aerial vehicle battery heat preservation device - Google Patents
Unmanned aerial vehicle battery heat preservation device Download PDFInfo
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- CN211182296U CN211182296U CN201922236846.6U CN201922236846U CN211182296U CN 211182296 U CN211182296 U CN 211182296U CN 201922236846 U CN201922236846 U CN 201922236846U CN 211182296 U CN211182296 U CN 211182296U
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- battery
- aerial vehicle
- unmanned aerial
- ejector pin
- pole
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
- Y02E60/00—Enabling technologies; Technologies with a potential or indirect contribution to GHG emissions mitigation
- Y02E60/10—Energy storage using batteries
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Abstract
The utility model belongs to the field of unmanned aerial vehicle batteries, in particular to an unmanned aerial vehicle battery heat preservation device, aiming at the problem that the prior unmanned aerial vehicle can generate larger vibration in the flying or descending process, the contact failure can be caused by the huge vibration, the current can be overlarge during the vibration, the overcurrent protection critical point of a protection plate is reached, and the long-time influence on the cruising ability and the service life of the battery is generated, the utility model provides a scheme which comprises a machine body, a battery box is arranged above the machine body, a battery body is arranged in the battery box, and a warmer is arranged around the battery body, the utility model has simple structure, the battery box generates the vibration to extrude a first spring, the vibration generated by the battery box is effectively slowed down, when the vibration is larger, a movable rod moves to drive a top plate to move, the top plate moves to effectively block the downward vibration generated by the battery box, thereby the, the battery body endurance is improved, the service life is prolonged, and the use is convenient.
Description
Technical Field
The utility model relates to an unmanned aerial vehicle battery technology field especially relates to an unmanned aerial vehicle battery heat preservation device.
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.
The patent that publication number is CN204216106U discloses an unmanned aerial vehicle battery heat preservation device, the shell upper end is provided with the connection wing, it is porose on the connection wing, the shell inboard is fixed with warm baby, be provided with warm baby charging hole on the shell lateral wall, warm baby upper end is provided with the zip fastener, the fixed band board passes through bolt and shell fixed connection, unmanned aerial vehicle is flying or descends the in-process, can produce great vibrations, huge vibrations probably lead to contact failure, the shake opens circuit, the electric current can be too big in the time of vibrations, the overcurrent protection critical point of protection shield has been reached, long-time duration and the life-span to the battery produce the influence, consequently, need a neotype unmanned aerial vehicle battery heat preservation device to satisfy people's demand.
SUMMERY OF THE UTILITY MODEL
The utility model aims at solving and having unmanned aerial vehicle among the prior art at flight or decline in-process, probably producing great vibrations, huge vibrations probably lead to contact failure, and the shake opens circuit, and the current can be too big in the time of vibrations, has reached the overcurrent protection critical point of protection shield, and the shortcoming that produces the influence to the duration and the life-span of battery for a long time, and the unmanned aerial vehicle battery heat preservation device that provides.
In order to achieve the above purpose, the utility model adopts the following technical scheme:
unmanned aerial vehicle battery heat preservation device, which comprises a bod, the top of fuselage is equipped with the battery case, is equipped with battery body in the battery case, and battery body all is equipped with warm baby all around, the bottom side of battery case rotates installs two squeeze bars, has seted up on the fuselage and has placed the chamber, places and has seted up the through-hole on the top side inner wall in chamber, and two through-holes and equal movable mounting have been run through respectively to the bottom of two squeeze bars, and two installation poles are installed to one side fixed mounting of a movable bar, and one side fixed mounting of another movable bar has two telescopic links, and flexible groove has all been seted up to the one end of two installation poles, and the one end of two telescopic links extends to two flexible inslots respectively and the one end of equal fixed mounting has first spring, and the other end fixed.
Preferably, place and seted up the ejector pin hole on the top side inner wall in chamber, the downthehole movable mounting of ejector pin has the ejector pin, outside the both ends of ejector pin all extended to the ejector pin hole, the top fixed mounting of ejector pin has the roof, and the both sides of ejector pin all rotate and install the push rod, and the one end of two push rods all rotates to be installed and moves the pole, moves one side of pole and one side looks adaptation of movable rod, can effectively block the vibrations that the battery case produced downwards.
Preferably, place and seted up on the top side inner wall in chamber and move the groove, move the one end slidable mounting of pole and move the inslot, move one side fixed mounting of pole and have the one end of second spring, the other end fixed mounting of second spring moves on the one side inner wall in groove, moves the pole and removes the back and be convenient for reset.
Preferably, a sliding groove is formed in one side of the movable rod, a sliding block is movably mounted in the sliding groove, an adjusting rod is rotatably mounted on one side of the sliding block, one end of the adjusting rod is rotatably mounted on the inner wall of one side of the placing cavity, one end of the extrusion rod is rotatably mounted on one side of the sliding block, and the extrusion rod moves to drive the movable rod to move.
Preferably, the inner wall of the bottom side of the placing cavity is provided with a sliding groove, the bottom ends of the two movable rods are fixedly provided with sliding blocks, and the bottom sides of the two sliding blocks are slidably mounted in the sliding groove to limit the movement of the movable rods.
The utility model discloses in, unmanned aerial vehicle battery heat preservation device, owing to set up the ejector pin, the movable rod, adjust the pole, the installation pole, the telescopic link, move the pole, the push rod, the ejector pin, it can extrude the ejector pin to have realized that the battery case vibrations, the ejector pin removes and drives the sliding block and remove in the sliding tray, the sliding block removes and drives the movable rod removal under the effect of adjusting the pole, the movable rod removes and drives the slider and remove in the spout, two movable rods remove and drive installation pole and telescopic link removal and extrude the first spring, can effectively slow down the vibrations that the battery case produced, when vibrations are great, can continue to extrude the movable rod removal, the movable rod removal drives and moves the pole and removes in moving the groove, it drives the push rod removal to move the push rod, the push rod removal drives the ejector pin;
the utility model discloses simple structure, thereby the battery case produces vibrations and drives the stripper bar removal, thereby the stripper bar removes the first spring of extrusion, effectively slows down the vibrations that the battery case produced, when vibrations are great, thereby the movable rod removes and drives the roof and remove, and the roof removes and can effectively block the vibrations that the battery case produced downwards to reach and effectively slow down the battery case vibrations, improved battery body duration and life-span, convenient to use.
Drawings
Fig. 1 is a schematic structural view of an unmanned aerial vehicle battery heat preservation device in front view;
fig. 2 is a schematic structural view of the inside of a battery box of the battery heat preservation device of the unmanned aerial vehicle provided by the utility model;
fig. 3 is the utility model provides a structure schematic diagram of a part in unmanned aerial vehicle battery heat preservation device figure 1.
In the figure: the battery comprises a machine body 1, a battery box 2, a warmer 3, a battery body 4, a placing cavity 5, an extrusion rod 6, a movable rod 7, a sliding groove 8, a sliding block 9, an adjusting rod 10, an installation rod 11, a telescopic rod 12, a sliding groove 13, a sliding block 14, a through hole 15, a moving groove 16, a moving rod 17, a push rod 18, a push rod 19, a push rod hole 20 and a top plate 21.
Detailed Description
The technical solutions in the embodiments of the present invention will be described clearly and completely with reference to the accompanying drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only some embodiments of the present invention, not all embodiments.
Example one
Referring to fig. 1-3, unmanned aerial vehicle battery heat preservation device, including fuselage 1, the top of fuselage 1 is equipped with battery case 2, be equipped with battery body 4 in the battery case 2, all be equipped with warm baby 3 around battery body 4, the bottom side of battery case 2 is rotated and is installed two squeeze bars 6, place chamber 5 has been seted up on the fuselage 1, through-hole 15 has been seted up on the top side inner wall of placing chamber 5, two through-holes 15 and equal movable mounting have movable rod 7 are run through respectively to the bottom of two squeeze bars 6, one side fixed mounting of a movable rod 7 has two installation poles 11, one side fixed mounting of another movable rod 7 has two telescopic links 12, the flexible groove has all been seted up to the one end of two installation poles 11, the one end of two telescopic links 12 extends to two flexible inslots respectively and the one end of equal fixed mounting first spring, the other end fixed mounting of first spring is on one.
The utility model discloses in, place and seted up ejector pin hole 20 on the top side inner wall of chamber 5, movable mounting has ejector pin 19 in the ejector pin hole 20, outside ejector pin hole 20 was all extended to at 19's both ends, ejector pin 19's top fixed mounting has roof 21, ejector pin 19's both sides were all rotated and are installed push rod 18, the one end of two push rod 18 is all rotated and is installed and move pole 17, move one side of pole 17 and one side looks adaptation of movable rod 7, can effectively block the vibrations of battery case 2 production downwards.
The utility model discloses in, place and seted up on the top side inner wall of chamber 5 and moved groove 16, move the one end slidable mounting of pole 17 and move the groove 16 in, move one side fixed mounting of pole 17 and have the one end of second spring, the other end fixed mounting of second spring is on moving one side inner wall of groove 16, moves the pole 17 and removes the back and is convenient for reset.
The utility model discloses in, sliding tray 8 has been seted up to one side of movable rod 7, and movable mounting has sliding block 9 in the sliding tray 8, and one side of sliding block 9 is rotated and is installed regulation pole 10, and the one end of adjusting pole 10 is rotated and is installed on placing one side inner wall of chamber 5, and the one end of extrusion stem 6 is rotated and is installed on one side of sliding block 9, and extrusion stem 6 removes to be convenient for drive movable rod 7 and removes.
The utility model discloses in, place and seted up spout 13 on the bottom side inner wall in chamber 5, the equal fixed mounting in bottom of two movable rods 7 has slider 14, and the equal slidable mounting in bottom side of two sliders 14 carries on spacingly to movable rod 7 removal in spout 13.
Example two
Referring to fig. 1-3, unmanned aerial vehicle battery heat preservation device, including fuselage 1, the top of fuselage 1 is equipped with battery case 2, be equipped with battery body 4 in the battery case 2, all be equipped with warm baby 3 around battery body 4, two stripper bars 6 are installed through the round pin axle rotation to the bottom side of battery case 2, place chamber 5 has been seted up on the fuselage 1, through-hole 15 has been seted up on the top side inner wall of placing chamber 5, two through-hole 15 and equal movable mounting have a movable rod 7 are run through respectively to the bottom of two stripper bars 6, there are two installation poles 11 one side of a movable rod 7 through welded fastening installation, there are two telescopic links 12 one side of another movable rod 7 through welded fastening installation, flexible groove has all been seted up to the one end of two installation poles 11, the one end of two telescopic links 12 extends to two flexible inslot respectively and all has the one end of first spring through welded fastening installation, the other end of first spring passes through.
The utility model discloses in, place and seted up ejector pin hole 20 on the top side inner wall of chamber 5, movable mounting has ejector pin 19 in the ejector pin hole 20, outside ejector pin hole 20 was all extended to at the both ends of ejector pin 19, there is roof 21 on the top of ejector pin 19 through welded fastening, push rod 18 is all installed through the round pin axle rotation in the both sides of ejector pin 19, the one end of two push rods 18 is all installed through the round pin axle rotation and is moved pole 17, move one side of pole 17 and one side looks adaptation of movable rod 7, can effectively block the vibrations of battery case 2 production downwards.
The utility model discloses in, place and seted up on the top side inner wall of chamber 5 and moved groove 16, move the one end slidable mounting of pole 17 and move the inslot 16, move one side of pole 17 and install the one end of second spring through welded fastening, the other end of second spring passes through welded fastening and installs on moving one side inner wall of groove 16, moves pole 17 and is convenient for reset after removing.
The utility model discloses in, sliding tray 8 has been seted up to one side of movable rod 7, and movable mounting has sliding block 9 in the sliding tray 8, and one side of sliding block 9 is rotated through the round pin axle and is installed regulation pole 10, and the one end of adjusting pole 10 is rotated through the round pin axle and is installed on placing one side inner wall of chamber 5, and the one end of extrusion stem 6 is rotated through the round pin axle and is installed on one side of sliding block 9, and extrusion stem 6 removes and is convenient for drive movable rod 7 and remove.
The utility model discloses in, place and seted up spout 13 on the bottom side inner wall in chamber 5, the bottom of two movable rods 7 all has slider 14 through welded fixed mounting, and the equal slidable mounting in spout 13 of bottom side of two sliders 14 moves movable rod 7 and carries on spacingly.
In the utility model, when the unmanned aerial vehicle is working or landing, a large vibration is generated, the battery box 2 vibrates to extrude the extrusion rod 6, the extrusion rod 6 moves to drive the sliding block 9 to move in the sliding groove 8, the sliding block 9 moves to drive the movable rod 7 to move under the action of the adjusting rod 10, the movable rod 7 moves to drive the sliding block 14 to move in the sliding groove 13, the two movable rods 7 move to drive the mounting rod 11 and the telescopic rod 12 to move and extrude the first spring, the vibration generated by the battery box 2 can be effectively reduced, when the vibration is large, the movable rod 7 can continue to be extruded to move, the movable rod 7 moves to drive the movable rod 17 to move in the movable groove 16, the movable rod 17 moves to drive the push rod 18 to move, the push rod 18 moves to drive the ejector rod 19 to move, the ejector rod 19 moves to drive the top plate 21 to move, the top plate 21 moves to effectively block the vibration generated downwards by, is convenient to use.
The above, only be the concrete implementation of the preferred embodiment of the present invention, but the protection scope of the present invention is not limited thereto, and any person skilled in the art is in the technical scope of the present invention, according to the technical solution of the present invention and the utility model, the concept of which is equivalent to replace or change, should be covered within the protection scope of the present invention.
Claims (5)
1. The heat preservation device for the battery of the unmanned aerial vehicle comprises a machine body (1), wherein a battery box (2) is arranged above the machine body (1), a battery body (4) is arranged in the battery box (2), and a heater (3) is arranged around the battery body (4), and is characterized in that two extrusion rods (6) are rotatably arranged at the bottom side of the battery box (2), a placing cavity (5) is formed in the machine body (1), through holes (15) are formed in the inner wall of the top side of the placing cavity (5), the bottom ends of the two extrusion rods (6) respectively penetrate through the two through holes (15) and are respectively and movably provided with a movable rod (7), two mounting rods (11) are fixedly arranged at one side of one movable rod (7), two telescopic rods (12) are fixedly arranged at one side of the other movable rod (7), telescopic grooves are respectively formed at one ends of the two mounting rods (11), one ends of the two telescopic rods (12) respectively extend into the two telescopic grooves and are respectively, the other end of the first spring is fixedly arranged on the inner wall of one side of the telescopic groove.
2. The unmanned aerial vehicle battery heat preservation device of claim 1, characterized in that, place and seted up ejector pin hole (20) on the top side inner wall of chamber (5), movable mounting has ejector pin (19) in ejector pin hole (20), outside the both ends of ejector pin (19) all extended to ejector pin hole (20), the top fixed mounting of ejector pin (19) has roof (21), push rod (18) are all installed in the both sides of ejector pin (19) rotation, the one end of two push rods (18) is all installed and is moved pole (17), move one side of pole (17) and one side looks adaptation of movable rod (7).
3. The unmanned aerial vehicle battery heat preservation device of claim 1, characterized in that place and seted up on the top side inner wall of chamber (5) and move groove (16), move the one end slidable mounting of pole (17) and move in groove (16), move one side fixed mounting of pole (17) and have the one end of second spring, the other end fixed mounting of second spring moves on the one side inner wall of groove (16).
4. The unmanned aerial vehicle battery heat preservation device of claim 1, characterized in that, sliding groove (8) have been seted up to one side of movable rod (7), and movable mounting has sliding block (9) in sliding groove (8), and one side of sliding block (9) is rotated and is installed adjusting pole (10), and the one end of adjusting pole (10) is rotated and is installed on placing the one side inner wall of chamber (5), and the one end of extrusion pole (6) is rotated and is installed on one side of sliding block (9).
5. The unmanned aerial vehicle battery heat preservation device of claim 1, characterized in that, place and offer spout (13) on the bottom side inner wall of chamber (5), the bottom of two movable rods (7) is all fixed with slider (14), the bottom side of two slider (14) is all slidable mounting in spout (13).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201922236846.6U CN211182296U (en) | 2019-12-13 | 2019-12-13 | Unmanned aerial vehicle battery heat preservation device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201922236846.6U CN211182296U (en) | 2019-12-13 | 2019-12-13 | Unmanned aerial vehicle battery heat preservation device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN211182296U true CN211182296U (en) | 2020-08-04 |
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ID=71827149
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201922236846.6U Active CN211182296U (en) | 2019-12-13 | 2019-12-13 | Unmanned aerial vehicle battery heat preservation device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN211182296U (en) |
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2019
- 2019-12-13 CN CN201922236846.6U patent/CN211182296U/en active Active
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20210325 Address after: 313100 no.358-1, Chizhou Avenue, Huaxi street, Changxing County, Huzhou City, Zhejiang Province Patentee after: Mingchuang Jialian (Zhejiang) New Energy Technology Co.,Ltd. Address before: 313200 4-13 / F, venture building, kechuangyuan, Deqing County, 345 Changhong East Street, Fuxi street, Deqing County, Huzhou City, Zhejiang Province Patentee before: Huzhou Heming Machinery Technology Co.,Ltd. |
|
| TR01 | Transfer of patent right | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20210527 Address after: Ruizhida company service center, phase II, Wickham reef, tortorarod City, vg1110, British Virgin Islands Patentee after: Guanlei battery Holding Co.,Ltd. Address before: 313100 no.358-1, Chizhou Avenue, Huaxi street, Changxing County, Huzhou City, Zhejiang Province Patentee before: Mingchuang Jialian (Zhejiang) New Energy Technology Co.,Ltd. |
|
| TR01 | Transfer of patent right |