CN216375030U - Make things convenient for unmanned aerial vehicle of dismouting - Google Patents
Make things convenient for unmanned aerial vehicle of dismouting Download PDFInfo
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- CN216375030U CN216375030U CN202122570666.9U CN202122570666U CN216375030U CN 216375030 U CN216375030 U CN 216375030U CN 202122570666 U CN202122570666 U CN 202122570666U CN 216375030 U CN216375030 U CN 216375030U
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- unmanned aerial
- aerial vehicle
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- vehicle body
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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
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T10/00—Road transport of goods or passengers
- Y02T10/60—Other road transportation technologies with climate change mitigation effect
- Y02T10/70—Energy storage systems for electromobility, e.g. batteries
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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
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T10/00—Road transport of goods or passengers
- Y02T10/60—Other road transportation technologies with climate change mitigation effect
- Y02T10/7072—Electromobility specific charging systems or methods for batteries, ultracapacitors, supercapacitors or double-layer capacitors
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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
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
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Abstract
The utility model discloses an unmanned aerial vehicle convenient to disassemble and assemble, wherein a plurality of groups of mounting plates are fixedly connected with the bottom of an unmanned aerial vehicle body, and one or more of various application modules are arranged on the lower side of each group of mounting plates; the upper surface of the unmanned aerial vehicle body is provided with a threaded hole, a guide hole and a battery mounting groove, and an electrode socket is electrically connected in the battery mounting groove; the battery replacement mechanism includes: the protective cover is nested above the unmanned aerial vehicle body, the rotating seat is nested at the center of the protective cover, the screw rod is fixedly connected below the rotating seat and is screwed with the threaded hole, the guide post is fixedly connected to the lower surface of the protective cover and is nested and spliced with the guide hole, the multiple groups of supporting springs are fixedly connected around the screw rod, and the splicing seat is fixedly connected to the bottom end of the supporting spring; the top end of the storage battery is provided with a plug-in groove which is nested and plugged with the plug-in seat. The unmanned aerial vehicle battery replacement system can meet various use requirements according to different installation application modules, and can replace the storage battery quickly and stably so as to prolong the service life of the unmanned aerial vehicle.
Description
Technical Field
The utility model relates to the technical field of unmanned aerial vehicles, in particular to an unmanned aerial vehicle convenient to disassemble and assemble.
Background
With the rapid development of the current society, unmanned aerial vehicle equipment is widely applied to the production and the life of people. But traditional unmanned aerial vehicle often the structure is fixed, only can realize single function, has restricted unmanned aerial vehicle's application prospect greatly. And the used battery of traditional unmanned aerial vehicle installs inside unmanned aerial vehicle's shell, when no battery electric energy exhausts, need charge to the battery immediately and just can guarantee that unmanned aerial vehicle continues to use, leads to result in greatly reduced. Therefore, a need exists for a new modular unmanned aerial vehicle structure with a wide application range.
Disclosure of Invention
The utility model aims to provide an unmanned aerial vehicle convenient to disassemble and assemble, which can meet various use requirements according to different installation application modules, and can quickly and stably replace a storage battery so as to prolong the use time of the unmanned aerial vehicle.
In order to achieve the purpose, the utility model provides the following technical scheme: an unmanned aerial vehicle convenient to disassemble and assemble comprises an unmanned aerial vehicle body, a plurality of groups of storage batteries, mounting plates which are arranged on the lower side of the unmanned aerial vehicle body in a matched mode, and a battery replacing mechanism which is arranged on the upper side of the unmanned aerial vehicle body in a matched mode, wherein each mounting plate comprises a plurality of groups and is fixedly connected with the bottom of the unmanned aerial vehicle body through a fixing bolt, and one or more of a plurality of application modules are fixedly arranged on the lower side of each group of mounting plates;
the center of the upper surface of the unmanned aerial vehicle body is provided with a vertically-arranged threaded hole, a plurality of groups of vertically-arranged guide holes are formed around the threaded hole, a plurality of groups of uniformly-arranged battery mounting grooves are formed around the threaded hole, and each group of battery mounting grooves is electrically connected with an electrode socket; the battery replacement mechanism includes: the protective cover is nested and installed right above the unmanned aerial vehicle body, the rotating seat is nested and installed at the center of the protective cover in a relative rotating mode, the screw rod is fixedly connected to the lower side of the rotating seat and is screwed with the threaded hole, the guide post is fixedly connected to the lower surface of the protective cover and is nested and plugged with the guide hole, the plurality of groups of supporting springs are uniformly and fixedly connected to the periphery of the screw rod and are vertically and downwards arranged, and the plug-in seat is fixedly connected to the bottom end of each group of supporting springs and is vertically opposite to the battery installation groove; the top end of the storage battery is provided with a plug-in groove which is nested and plugged with the plug-in seat, and the bottom end of the storage battery is provided with an electrode slot which is electrically connected with the electrode socket.
In some of these implementations, the application modules include at least a landing gear, a shelf, and a camera.
In some of them implementation, the upper surface rigid coupling of unmanned aerial vehicle body has sealed nested ring, the battery mounting groove sets up at sealed nested ring inboard, the outer fringe and the nested joint of sealed nested ring of protection casing.
In some implementations, a sunken groove is formed in the center of the upper surface of the protective cover, the top end of the rotating seat is exposed in the sunken groove, and the top end of the rotating seat is in the shape of a bolt head.
In some implementations, the open end of the insertion seat faces the outer side of the protective cover, the top end of the storage battery is fixedly connected with a nesting seat which is nested and matched with the battery installation groove, and the top end of the nesting seat is provided with the insertion groove.
Compared with the prior art, the utility model has the following beneficial effects: through the mounting panel fixed mounting that will be equipped with different application module in the bottom of unmanned aerial vehicle body to realize different work through the unmanned aerial vehicle body. Rotate the seat through revolving to revolve to the combination and the separation of control protection casing and unmanned aerial vehicle body, the convenience is changed the battery, and is long when the use of improvement unmanned aerial vehicle body. The setting of plug socket, nested seat simultaneously can guarantee the battery of new change stable installation in the battery mounting groove and guarantee with unmanned aerial vehicle body electric connection, and supporting spring's setting can make the battery of installing in the battery mounting groove have certain antidetonation effect simultaneously.
Drawings
FIG. 1 is a schematic diagram of the assembled battery of the present invention;
FIG. 2 is a schematic structural view of the disassembled battery of the present invention;
FIG. 3 is a schematic view of the present invention after the landing gear is added;
FIG. 4 is a schematic structural view of the present invention after being installed with a shelf;
fig. 5 is a schematic structural diagram of the present invention after a camera and a landing gear are added.
In the figure: 1 unmanned aerial vehicle body, 2 batteries, 3 mounting panels, 4 screw holes, 5 guide holes, 6 battery mounting grooves, 7 electrode socket, 8 protection casings, 9 rotation seats, 10 screw rods, 11 guide pillars, 12 supporting spring, 13 plug sockets, 14 undercarriage, 15 goods shelves, 16 cameras, 17 sealed nested rings, 18 heavy groove, 19 nested seats.
Detailed Description
The technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only a part of the embodiments of the present invention, and not all of the embodiments. All other embodiments, which can be derived by a person skilled in the art from the embodiments given herein without making any creative effort, shall fall within the protection scope of the present invention.
Referring to fig. 1-5, an unmanned aerial vehicle convenient to disassemble and assemble comprises an unmanned aerial vehicle body 1, a plurality of groups of storage batteries 2, a mounting plate 3 which is arranged on the lower side of the unmanned aerial vehicle body 1 in a matching way, and a battery replacing mechanism which is arranged on the upper side of the unmanned aerial vehicle body 1 in a matching way, wherein the mounting plate 3 comprises a plurality of groups and is fixedly connected with the bottom of the unmanned aerial vehicle body 1 through fixing bolts, and one or more of various application modules are fixedly arranged on the lower side of each group of mounting plate 3;
the center of the upper surface of the unmanned aerial vehicle body 1 is provided with a vertically-arranged threaded hole 4, a plurality of groups of vertically-arranged guide holes 5 are formed around the threaded hole 4, a plurality of groups of uniformly-arranged battery mounting grooves 6 are formed around the threaded hole 4, and each group of battery mounting grooves 6 is electrically connected with an electrode socket 7; the battery replacement mechanism includes: the protective cover 8 is nested and installed right above the unmanned aerial vehicle body 1, the rotating seat 9 is nested and installed at the center of the protective cover 8 in a relative rotating mode, the screw rod 10 is fixedly connected to the position right below the rotating seat 9 and is screwed with the threaded hole 4, the guide post 11 is fixedly connected to the lower surface of the protective cover 8 and is nested and inserted with the guide hole 5, the plurality of groups of supporting springs 12 are uniformly and fixedly connected to the periphery of the screw rod 10 and are vertically and downwards arranged, and the inserting seat 13 is fixedly connected to the bottom end of each group of supporting springs 12 and is vertically opposite to the battery installing groove 6; the top end of the storage battery 2 is provided with a plug-in groove which is nested and plugged with the plug-in seat 13, and the bottom end of the storage battery 2 is provided with an electrode slot which is electrically connected with the electrode socket 7.
In some of them implementation, the application module includes undercarriage 14, goods shelves 15, camera 16 at least, and when installation undercarriage 14, can make things convenient for unmanned aerial vehicle body 1 to take off and land in the place of topography unevenness, when installation goods shelves 15, can transport the goods through unmanned aerial vehicle body 1, when installation undercarriage 14, camera 16, conveniently take photo by plane through unmanned aerial vehicle body 1.
In some of them implementation, the upper surface rigid coupling of unmanned aerial vehicle body 1 has sealed nested ring 17, and battery mounting groove 6 sets up in sealed nested ring 17 inboard, and the sealed joint of protection casing 8 and sealed nested ring 17 is guaranteed to the outer fringe of protection casing 8, can avoid external moisture, dust to get into battery mounting groove 6 and influence the stable power supply of battery 2.
In some of them implementation, protection casing 8 upper surface center department has seted up heavy groove 18, rotates the seat 9 top and exposes in heavy groove 18, and rotates the seat 9 top and set up to the bolt head shape, conveniently revolves to rotating seat 9 and revolve to make protection casing 8 stable installation in unmanned aerial vehicle body 1 top side.
In some of these implementations, the open end of bayonet socket 13 is arranged towards the protection casing 8 outside, conveniently hangs battery 2 on bayonet socket 13, and then installs downwards to battery mounting groove 6 in, and battery 2 top rigid coupling has the nested seat 19 that is inosculated with battery mounting groove 6 nestification, guarantees that battery 2 can stable installation in battery mounting groove 6, and nested seat 19 top has seted up the bayonet socket
The working principle of the unmanned aerial vehicle is that the mounting plate 3 provided with different application modules is fixedly mounted at the bottom of the unmanned aerial vehicle body 1, so that different work can be realized through the unmanned aerial vehicle body 1. Rotate the seat 9 through revolving to revolve wrong and drive screw rod 10 and rotate to control protection casing 8 and unmanned aerial vehicle body 1's combination and separation, the convenience is changed battery 2, and is long when improving unmanned aerial vehicle body 1's use. Simultaneously the setting of bayonet socket 13, nested seat 19 can guarantee the battery 2 of new change stable installation in battery mounting groove 6 and guarantee with unmanned aerial vehicle body 1 electric connection, and the setting of supporting spring 12 can make the battery 2 of installing in battery mounting groove 6 have certain antidetonation effect simultaneously.
Although embodiments of the present invention have been shown and described, it will be appreciated by those skilled in the art that changes, modifications, substitutions and alterations can be made in these embodiments without departing from the principles and spirit of the utility model, the scope of which is defined in the appended claims and their equivalents.
Claims (5)
1. The utility model provides a make things convenient for unmanned aerial vehicle of dismouting which characterized in that: the battery replacement mechanism comprises an unmanned aerial vehicle body (1), a plurality of groups of storage batteries (2), mounting plates (3) which are arranged on the lower side of the unmanned aerial vehicle body (1) in a matching way, and a battery replacement mechanism which is arranged on the upper side of the unmanned aerial vehicle body (1) in a matching way, wherein the mounting plates (3) comprise a plurality of groups and are fixedly connected with the bottom of the unmanned aerial vehicle body (1) through fixing bolts, and one or more of a plurality of application modules are fixedly arranged on the lower side of each group of mounting plates (3);
the unmanned aerial vehicle comprises an unmanned aerial vehicle body (1), wherein a vertically-arranged threaded hole (4) is formed in the center of the upper surface of the unmanned aerial vehicle body (1), a plurality of groups of vertically-arranged guide holes (5) are formed around the threaded hole (4), a plurality of groups of uniformly-arranged battery mounting grooves (6) are formed around the threaded hole (4), and an electrode socket (7) is electrically connected in each group of battery mounting grooves (6); the battery replacement mechanism includes: the protective cover (8) is nested and installed right above the unmanned aerial vehicle body (1), the rotating seat (9) is nested and installed at the center of the protective cover (8) in a relative rotating mode, a screw rod (10) is fixedly connected to the right lower side of the rotating seat (9) and is screwed with the threaded hole (4), a guide post (11) is fixedly connected to the lower surface of the protective cover (8) and is nested and plugged with the guide hole (5), a plurality of groups of supporting springs (12) are uniformly and fixedly connected to the periphery of the screw rod (10) and are vertically and downwards arranged, and a plug-in seat (13) is fixedly connected to the bottom end of each group of supporting springs (12) and is vertically opposite to the battery installation groove (6); the top end of the storage battery (2) is provided with a plug-in groove which is nested and plugged with the plug-in seat (13), and the bottom end of the storage battery (2) is provided with an electrode slot which is electrically connected with the electrode socket (7).
2. The unmanned aerial vehicle of claim 1, wherein the unmanned aerial vehicle comprises: the application module at least comprises a landing gear (14), a goods shelf (15) and a camera (16).
3. The unmanned aerial vehicle of claim 1, wherein the unmanned aerial vehicle comprises: the upper surface rigid coupling of unmanned aerial vehicle body (1) has sealed nested ring (17), battery mounting groove (6) set up in sealed nested ring (17) inboard, the outer fringe and the nested joint of sealed nested ring (17) of protection casing (8).
4. The unmanned aerial vehicle of claim 1, wherein the unmanned aerial vehicle comprises: the protection cover (8) is characterized in that a sunk groove (18) is formed in the center of the upper surface of the protection cover (8), the top end of the rotating seat (9) is exposed in the sunk groove (18), and the top end of the rotating seat (9) is in a bolt head shape.
5. The unmanned aerial vehicle of claim 1, wherein the unmanned aerial vehicle comprises: the open end of the inserting seat (13) is arranged towards the outer side of the protective cover (8), the top end of the storage battery (2) is fixedly connected with an embedding seat (19) which is matched with the battery mounting groove (6) in an embedding way, and the top end of the embedding seat (19) is provided with the inserting groove.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
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CN202122570666.9U CN216375030U (en) | 2021-10-25 | 2021-10-25 | Make things convenient for unmanned aerial vehicle of dismouting |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
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CN202122570666.9U CN216375030U (en) | 2021-10-25 | 2021-10-25 | Make things convenient for unmanned aerial vehicle of dismouting |
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CN216375030U true CN216375030U (en) | 2022-04-26 |
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CN202122570666.9U Active CN216375030U (en) | 2021-10-25 | 2021-10-25 | Make things convenient for unmanned aerial vehicle of dismouting |
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CN (1) | CN216375030U (en) |
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2021
- 2021-10-25 CN CN202122570666.9U patent/CN216375030U/en active Active
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Effective date of registration: 20220629 Address after: 455000 4th floor, West Building of Hua'an machinery plant, 500m east of the intersection of Zhonghua Road and Chuangye Avenue, Beiguan District, Anyang City, Henan Province Patentee after: Anyang Hongan Aviation Technology Co.,Ltd. Address before: 543000 No. 3, Xinxing Second Road, Changzhou District, Wuzhou City, Guangxi Zhuang Autonomous Region Patentee before: Liu Yining |