CN211208804U - Unmanned aerial vehicle power inserts structure soon - Google Patents

Unmanned aerial vehicle power inserts structure soon Download PDF

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Publication number
CN211208804U
CN211208804U CN201922303218.5U CN201922303218U CN211208804U CN 211208804 U CN211208804 U CN 211208804U CN 201922303218 U CN201922303218 U CN 201922303218U CN 211208804 U CN211208804 U CN 211208804U
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CN
China
Prior art keywords
plug
aerial vehicle
unmanned aerial
gear
socket
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Fee Related
Application number
CN201922303218.5U
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Chinese (zh)
Inventor
陈曦
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Henan Guyi Automation Technology Co ltd
Original Assignee
Henan Guyi Automation Technology Co ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
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Publication date
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Priority to CN201922303218.5U priority Critical patent/CN211208804U/en
Application granted granted Critical
Publication of CN211208804U publication Critical patent/CN211208804U/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

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    • YGENERAL 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
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02EREDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
    • Y02E60/00Enabling technologies; Technologies with a potential or indirect contribution to GHG emissions mitigation
    • Y02E60/10Energy storage using batteries

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Abstract

The utility model discloses an unmanned aerial vehicle power supply quick-plug structure, which comprises a battery bin fixed on an unmanned aerial vehicle, wherein a rechargeable battery is fixed on one side in the battery bin, one side of the rechargeable battery is provided with a plurality of sockets, pluggable plugs are arranged in the sockets, and the sockets are provided with limiting devices capable of clamping the plugs; when guaranteeing rechargeable battery plug and socket high-speed joint, stop device on the socket can press from both sides tight plug, has guaranteed that plug and socket connection are reliable, firm, has avoided the plug to rock, the emergence of dropout phenomenon.

Description

Unmanned aerial vehicle power inserts structure soon
Technical Field
The utility model belongs to the technical field of unmanned aerial vehicle, especially, relate to an unmanned aerial vehicle power inserts structure soon.
Background
The battery of the unmanned aerial vehicle is positioned on the body of the unmanned aerial vehicle, and mainly provides power for the aircraft to ensure that the aircraft can effectively complete flight tasks, the battery connector needs to be reliably connected in the process of executing the tasks by the aircraft, and if the battery of the aircraft can be well fastened, great hidden danger is caused on the safety of the aircraft in flight; at present, in order to guarantee the rapidity of battery plug connection, the connector is set to be a quick-insertion structure, the use is convenient, but the quick-insertion structure is not provided with an anti-loosening and shedding structure, the connector is easy to shake and shed, poor contact is caused, and the normal flight of the unmanned aerial vehicle is influenced.
SUMMERY OF THE UTILITY MODEL
To the above problem, the utility model provides a structure is inserted soon to unmanned aerial vehicle power, fine solution the problem that the unmanned aerial vehicle plug easily rocked, drops.
In order to realize the purpose, the utility model discloses a technical scheme as follows: the utility model provides an unmanned aerial vehicle power is structure of inserting soon, is fixed with rechargeable battery in one side in the battery compartment including being fixed in the battery compartment on the unmanned aerial vehicle, and one side of rechargeable battery is provided with a plurality of sockets, is provided with pluggable plug in the socket, but be provided with the stop device who presss from both sides tight plug on the socket.
Furthermore, the cross-sectional areas of the socket and the plug are rectangular, and at least one side surface of the plug is an elastic plate.
Further, stop device is including setting up the gear on the socket, and the elastic plate is provided with the rack with gear engagement on the side towards the socket inner wall, sets up the spacing hole along gear axis circumference equipartition on the gear side, gear one side is provided with the fixed block, but wear to be provided with the spacing pole that can reciprocate to slide and can insert in the spacing hole in the fixed block.
Furthermore, set up in the fixed block and supply the gliding through-hole of gag lever post, the both ends of through-hole all are provided with detachable fender ring, and one side that the gag lever post is close to the gear is provided with the flange, and the flange is provided with the spring with keeping away from between the fender ring of gear one side, and the both ends of spring contact with flange and fender ring respectively.
Furthermore, a contact pin is arranged in the socket, and a jack is arranged on the plug.
Furthermore, the upper side face and the lower side face of the plug are both elastic plates, and two groups of limiting devices and two groups of sockets are arranged on the limiting devices and the sockets.
Furthermore, the ends, far away from the gear, of the limiting rods of the two groups of limiting devices are integrally connected.
Compared with the prior art, the utility model discloses following beneficial effect has: when guaranteeing rechargeable battery plug and socket high-speed joint, stop device on the socket can press from both sides tight plug, has guaranteed that plug and socket connection are reliable, firm, has avoided the plug to rock, the emergence of dropout phenomenon.
Drawings
FIG. 1 is a schematic view of the overall structure of the present invention;
FIG. 2 is a cross-sectional view A-A of FIG. 1;
fig. 3 is a sectional view B-B of fig. 2.
In the figure: 1. a battery compartment; 2. a rechargeable battery; 3. a socket; 4. a plug; 5. a gear; 6. a rack; 7. a limiting hole; 8. a fixed block; 9. a limiting rod; 10. a through hole; 11. a baffle ring; 12. a flange; 13. a spring; 14. inserting a pin; 15. and (4) inserting the jack.
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. Based on the embodiments in the present invention, all other embodiments obtained by a person skilled in the art without creative work belong to the protection scope of the present invention.
As shown in fig. 1-3, an unmanned aerial vehicle power structure of inserting soon, including being fixed in unmanned aerial vehicle's last battery compartment 1, one side is fixed with rechargeable battery 2 in the battery compartment 1, and one side of rechargeable battery 2 is provided with a plurality of sockets 3, is provided with pluggable plug 4 in the socket 3, be provided with the stop device that can press from both sides tight plug 4 on the socket 3.
In this embodiment, the cross-sectional area of socket 3 and plug 4 all is the rectangle, and at least one side is the elastic plate on the plug 4, elastic plate and 4 a body coupling of plug, and the whole polypropylene material that can use of plug 4, polypropylene have stronger toughness, so have fine elasticity to polypropylene has fine fire resistance, has improved the utility model discloses a security.
In the embodiment, the limiting device comprises a gear 5 arranged on the socket 3, a rack 6 meshed with the gear 5 is arranged on the side surface of the elastic plate facing the inner wall of the socket 3, limiting holes 7 evenly distributed along the circumference of the axis of the gear 5 are formed in the side surface of the gear 5, a fixed block 8 is arranged on one side of the gear 5, and a limiting rod 9 capable of sliding in a reciprocating manner and capable of being inserted into the limiting holes 7 is arranged in the fixed block 8 in a penetrating manner; and the gear 5 is connected to the socket 3 through a gear shaft, and the limit rod 9 is inserted into the limit hole 7 to prevent the gear 5 from rotating so as to fix the position of the plug 4.
In this embodiment, a through hole 10 for the limiting rod 9 to slide is formed in the fixing block 8, two ends of the through hole 10 are respectively provided with a detachable stop ring 11, one side of the limiting rod 9, which is close to the gear 5, is provided with a flange 12, a spring 13 is arranged between the flange 12 and the stop ring 11, which is far away from the gear 5, and two ends of the spring 13 are respectively contacted with the flange 12 and the stop ring 11; the limiting rod 9 can automatically reset under the action of the elastic force of the spring 13 and slides to one side of the gear 5, so that the use is convenient.
In this embodiment, the socket 3 is provided with pins 14, and the plug 4 is provided with sockets 15.
In this embodiment, the upper and lower side surfaces of the plug 14 are both elastic plates, and two sets of limiting devices and the socket 3 are arranged; further improve the 3 clamping-force to plug 4 of socket, improved the utility model discloses a reliability.
In this embodiment, the gear 5 is kept away from to two sets of stop device's gag lever post 9 one end body coupling, and the two sets of stop device's gag lever post 9 of simultaneous operation simplifies the operating procedure, and it is more convenient to use, has improved operating efficiency.
Use the utility model discloses in the time, earlier insert socket 3 with plug 4 to the direction pulling of keeping away from gear 5 with gag lever post 9, jack 15 cup joints on contact pin 14, gear 5 and rack 6 meshing, and extrude the elastic plate on the plug 4 to the direction that is close to contact pin 14, when guaranteeing that plug 4 inserts tightly, relieve gag lever post 9, during gag lever post 9 inserts spacing hole 7 on the gear 5, prevent gear 5 and rotate, thereby gear 5 blocks plug 4 and steps up, the utility model discloses simple structure when guaranteeing rechargeable battery 2 plug 4 and socket 3 high-speed joint, plug 4 can be pressed from both sides to the stop device of 3 on the socket, has guaranteed that plug 4 and socket 3 connect reliably, firmly, has avoided plug 4 to rock, the emergence of obscission.
Although the present invention has been described in detail with reference to the foregoing embodiments, it will be apparent to those skilled in the art that modifications may be made to the embodiments or portions thereof without departing from the spirit and scope of the invention.

Claims (7)

1. The utility model provides an unmanned aerial vehicle power inserts structure soon, its characterized in that: including being fixed in battery compartment (1) on the unmanned aerial vehicle, one side is fixed with rechargeable battery (2) in battery compartment (1), and one side of rechargeable battery (2) is provided with a plurality of sockets (3), is provided with pluggable plug (4) in socket (3), be provided with the stop device that can press from both sides tight plug (4) on socket (3).
2. The unmanned aerial vehicle power supply fast plug structure of claim 1, characterized in that: the cross-sectional areas of the socket (3) and the plug (4) are rectangular, and at least one side surface of the plug (4) is an elastic plate.
3. The unmanned aerial vehicle power supply fast plug structure of claim 2, characterized in that: stop device is including setting up gear (5) on socket (3), and the elastic plate is provided with rack (6) with gear (5) meshing on the side towards socket (3) inner wall, offers spacing hole (7) along gear (5) axis circumference equipartition on gear (5) side, gear (5) one side is provided with fixed block (8), wear to be provided with in fixed block (8) and can reciprocate to slide gag lever post (9) that can insert in spacing hole (7).
4. The unmanned aerial vehicle power supply fast plug structure of claim 3, characterized in that: the limiting device is characterized in that a through hole (10) for the limiting rod (9) to slide is formed in the fixing block (8), detachable retaining rings (11) are arranged at two ends of the through hole (10), a flange (12) is arranged on one side, close to the gear (5), of the limiting rod (9), a spring (13) is arranged between the flange (12) and the retaining ring (11) far away from one side of the gear (5), and two ends of the spring (13) are respectively in contact with the flange (12) and the retaining ring (11).
5. The unmanned aerial vehicle power supply fast plug structure of claim 1, characterized in that: and a contact pin (14) is arranged in the socket (3), and a jack (15) is arranged on the plug (4).
6. The unmanned aerial vehicle power supply fast plug structure of claim 3, characterized in that: the upper side face and the lower side face of the plug (4) are both elastic plates, and two groups of limiting devices and two groups of sockets (3) are arranged on the limiting devices.
7. The unmanned aerial vehicle power supply fast plug structure of claim 6, characterized in that: the ends, far away from the gear (5), of the limiting rods (9) of the two groups of limiting devices are integrally connected.
CN201922303218.5U 2019-12-19 2019-12-19 Unmanned aerial vehicle power inserts structure soon Expired - Fee Related CN211208804U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201922303218.5U CN211208804U (en) 2019-12-19 2019-12-19 Unmanned aerial vehicle power inserts structure soon

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201922303218.5U CN211208804U (en) 2019-12-19 2019-12-19 Unmanned aerial vehicle power inserts structure soon

Publications (1)

Publication Number Publication Date
CN211208804U true CN211208804U (en) 2020-08-07

Family

ID=71853863

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201922303218.5U Expired - Fee Related CN211208804U (en) 2019-12-19 2019-12-19 Unmanned aerial vehicle power inserts structure soon

Country Status (1)

Country Link
CN (1) CN211208804U (en)

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GR01 Patent grant
GR01 Patent grant
CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20200807

Termination date: 20211219

CF01 Termination of patent right due to non-payment of annual fee