CN212529283U - Be applied to unmanned aerial vehicle's battery locking structure - Google Patents
Be applied to unmanned aerial vehicle's battery locking structure Download PDFInfo
- Publication number
- CN212529283U CN212529283U CN202020818601.4U CN202020818601U CN212529283U CN 212529283 U CN212529283 U CN 212529283U CN 202020818601 U CN202020818601 U CN 202020818601U CN 212529283 U CN212529283 U CN 212529283U
- Authority
- CN
- China
- Prior art keywords
- shell
- aerial vehicle
- left end
- unmanned aerial
- locking structure
- 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
Links
Images
Classifications
-
- 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
Landscapes
- Battery Mounting, Suspending (AREA)
Abstract
The utility model discloses a battery locking structure applied to an unmanned aerial vehicle, which comprises an installation shell, a metal sheet, a clamping plate, a pressure spring, a connecting ring, a fixing frame, a sliding chute, a sliding block, a cover plate, a supporting block, a limiting plate and a convenient installation device, wherein the convenient installation device is arranged at the left end of the installation shell, an inserted bar is driven by a hand-held block in a connecting mechanism to pass through the installation shell to be spliced with a connecting seat, then the rotating rod drives the push rod to rotate, the push rod is abutted against the roller, at the moment, the push rod pushes the rotating plates outwards through the roller, the two groups of rotating plates are rotatably connected around the rotating shaft, meanwhile, the rotating plates are slidably arranged with the sliding rod, the spring is compressed, then the rotor plate drives splint and presss from both sides tight inserted bar, has realized the effect of convenient installation, and it is comparatively troublesome when further having solved to lead to dismantling for the efficiency of installation and dismantlement reduces, has influenced staff's the problem of long-term during operation.
Description
Technical Field
The utility model relates to a locking structure field of being correlated with specifically is a be applied to unmanned aerial vehicle's battery locking structure.
Background
The unmanned aircraft is an unmanned aircraft operated by using a radio remote control device and a self-contained program control device, or is completely or intermittently and autonomously operated by an on-board computer, the battery is an important component of the unmanned aircraft, sufficient electric energy is provided for the unmanned aircraft, a locking structure is arranged outside the battery and used for fixing the battery, the locking structure improves the stability of the locking of the battery, and the phenomenon of pressure loss of the battery is avoided.
When the locking structure is in the use, because the connection between locking structure and the unmanned aerial vehicle is bolted connection, it is comparatively troublesome when leading to dismantling for the efficiency of installation and dismantlement reduces, has influenced staff's working duration.
SUMMERY OF THE UTILITY MODEL
Therefore, in order to solve the above insufficiency, the utility model provides a be applied to unmanned aerial vehicle's battery locking structure here.
The utility model discloses a realize like this, construct a battery locking structure who is applied to unmanned aerial vehicle, the device is including installation shell and convenient installation device, the inside left end of installation shell is fixed with the laminating of sheetmetal right-hand member to the inside bottom of installation shell is fixed with the laminating of fixed frame lower extreme, the sheetmetal right-hand member is provided with eight cardboards, and the sheetmetal middle part is provided with the clamping ring, cardboard front end 1cm department is provided with the pressure spring, the installation shell rear end is provided with the spout, and inside and the outside slidable mounting of slider of spout, the slider front end is fixed with the laminating of apron rear end, apron lower extreme left side is fixed with laminating on the piece, and the apron right-hand member is fixed with the laminating of spacing board left end, convenient installation device right-hand member is pegged graft with the installation shell left end, convenient installation device is by coupling mechanism, splint, rotor plate, roller, Shell, slide bar and spring component, coupling mechanism middle part upside is pegged graft with the installation shell left end, splint are inside to be hugged closely in coupling mechanism middle part downside, the rotor plate right-hand member is fixed with the laminating of splint left end downside, the roller middle part is fixed with rotor plate left end locking, the push rod left end is fixed with the laminating of rotary rod right-hand member, rotary rod middle part and shell left end interference fit, the shell is inside fixed with the slide bar front and back both ends laminating, the outside cover of slide bar is equipped with the spring.
Preferably, coupling mechanism comprises handheld piece, inserted bar and connecting seat, handheld piece lower extreme and the laminating of inserted bar upper end are fixed, the inserted bar outside passes the installation shell left end and pegs graft with the connecting seat is inside, the laminating of connecting seat left end and shell right-hand member is fixed.
Preferably, the front end of the clamping plate is provided with a clamping pad, and the clamping plates are provided with two groups.
Preferably, the rotating plates are provided with two groups, and the middle parts of the two groups of rotating plates are rotatably connected with the inside of the shell through rotating shafts.
Preferably, the height of the rollers is 5cm, and two sets of rollers are provided.
Preferably, the push rod is conical, and the lower end of the push rod is 3cm away from the slide rod.
Preferably, the left end in the shell is provided with a groove, and the groove is inserted in the push rod.
Preferably, the middle part of the inserted bar is attached to the insides of the two groups of clamping plates, and the length of the inserted bar is 2cm less than the height of the shell.
Preferably, the connecting seat left end is provided with the connection piece to the connection piece left end is fixed with the laminating of shell right-hand member downside.
Preferably, the convenient installation devices are provided with three groups, and the three groups of convenient installation devices are all on the same horizontal plane.
Preferably, the spring is made of spring steel.
Preferably, the hand-held block is made of ABS plastic.
The utility model has the advantages of as follows: the utility model discloses an improve and provide a battery locking structure who is applied to unmanned aerial vehicle here, compare with equipment of the same type, have following improvement:
a be applied to unmanned aerial vehicle's battery locking structure, convenient installation device has been set up through the installation shell left end, the handheld piece by among the coupling mechanism drives the inserted bar and passes installation shell and connecting seat and peg graft, the rotary rod drives the push rod and rotates after that, the push rod offsets with the roller, this moment, the push rod passes through the roller and promotes the rotor plate to the outside, two sets of rotor plates rotate around the pivot and connect, and simultaneously, rotor plate and slide bar slidable mounting, the spring is compressed, then the rotor plate drives splint and presss from both sides tight inserted bar, the effect of convenient installation has been realized, it is comparatively troublesome when leading to dismantling further to solve, make the efficiency of installation and dismantlement reduce, the problem of staff's length of operation has been influenced.
Drawings
FIG. 1 is a schematic structural view of the present invention;
FIG. 2 is a schematic view of a partial structure of the present invention;
FIG. 3 is a schematic structural view of the portable mounting device of the present invention;
fig. 4 is a schematic view of the internal structure of the housing of the present invention;
fig. 5 is a schematic view of the structure of the connection mechanism of the present invention.
Wherein: the device comprises an installation shell-1, a metal sheet-2, a clamping plate-3, a pressure spring-4, a connecting ring-5, a fixed frame-6, a sliding groove-7, a sliding block-8, a cover plate-9, a resisting block-10, a limiting plate-11, a convenient installation device-12, a connecting mechanism-121, a clamping plate-122, a rotating plate-123, a roller-124, a push rod-125, a rotating rod-126, an outer shell-127, a sliding rod-128, a spring-129, a handheld block-1211, an inserting rod-1212, a connecting seat-1213, a clamping pad-1201, a rotating shaft-1202, a groove-1203 and a connecting piece-1204.
Detailed Description
The present invention will be described in detail with reference to the accompanying fig. 1-5, and the technical solutions in the embodiments of the present invention will be clearly and completely described, 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.
The first embodiment is as follows:
please refer to fig. 1-2, the utility model provides a be applied to unmanned aerial vehicle's battery locking structure here through the improvement, including installation shell 1 and convenient installation device 12, 1 inside left end of installation shell is fixed with the laminating of 2 right-hand members of sheetmetal, and 1 inside bottom of installation shell is fixed with the laminating of 6 lower extremes of fixed frame, 2 right-hand members of sheetmetal are provided with eight cardboard 3, and 2 middle parts of sheetmetal are provided with clamping ring 5, 1cm department of 3 front ends of cardboard is provided with pressure spring 4, 1 rear end of installation shell is provided with spout 7, and spout 7 is inside with 8 outside slidable mounting of slider, 8 front ends of slider are fixed with the laminating of 9 rear ends of apron, apron 9 lower extreme left sides are fixed with the laminating of 10 upper ends of piece, and apron 9 right-hand members are fixed with the laminating of 11 left ends of limiting plate, convenient installation device 12 right.
Referring to fig. 3-4, the present invention provides a battery locking structure for an unmanned aerial vehicle, wherein the portable mounting device 12 is formed by a connecting mechanism 121, a clamping plate 122, a rotating plate 123, a roller 124, a pushing rod 125, a rotating rod 126, a housing 127, a sliding rod 128 and a spring 129, the upper side of the middle portion of the connecting mechanism 121 is inserted into the left end of the mounting housing 1, the clamping plate 122 is closely attached to the lower side of the middle portion of the connecting mechanism 121 to clamp the connecting mechanism 121, so as to achieve the effect of convenient connection, the right end of the rotating plate 123 is attached to the lower side of the left end of the clamping plate 122 to be connected to the housing 127 through a rotating shaft 1202, so as to achieve the clamping effect, the middle portion of the roller 124 is locked and fixed to the left end of the rotating plate 123, the left end of the pushing rod 125 is attached to the right end of the rotating rod 126 to be fixed to be beneficial for pushing, the push rod 125 can be driven to move, so that the transmission function is realized, the inner part of the shell 127 is attached and fixed to the front end and the rear end of the sliding rod 128, and the spring 129 is sleeved outside the sliding rod 128, so that the stability of the device can be improved.
Please refer to fig. 5, the utility model provides a be applied to unmanned aerial vehicle's battery locking structure here through the improvement, coupling mechanism 121 is by handheld piece 1211, inserted bar 1212 and connecting seat 1213 are constituteed, handheld piece 1211 lower extreme is fixed with the laminating of inserted bar 1212 upper end, be favorable to driving inserted bar 1212 and pass installation shell 1, inserted bar 1212 outside passes installation shell 1 left end and the inside grafting that pegs graft of connecting seat 1213, be favorable to realizing the function of being connected with splint 122, the laminating of connecting seat 1213 left end and shell 127 right-hand member is fixed, be favorable to increasing the stability of device.
Example two:
the utility model discloses an improve and provide a be applied to unmanned aerial vehicle's battery locking structure here, the rotor plate 123 front end is fixed with the laminating of spring 129, is favorable to rotor plate 123 compression spring 129, the function of hoisting device stability, the outside counterbalance with roller 124 of push rod 125 is favorable to promoting rotor plate 123 to the outside, slide bar 128 middle part and rotor plate 123 middle part back side slip installation are favorable to rotor plate 123 at the outside slidable mounting of slide bar 128, realize gliding function.
The utility model provides a battery locking structure applied to an unmanned aerial vehicle through improvement, and the working principle is as follows;
firstly, before use, the mounting shell 1 is firstly mounted on an external unmanned aerial vehicle by using the convenient mounting device 12, a handheld block 1211 in the connecting mechanism 121 is firstly held by hand, and the handheld block 1211 drives an insertion rod 1212 to penetrate through the mounting shell 1 to be inserted into a connecting seat 1213;
secondly, then, the rotating rod 126 drives the pushing rod 125 to rotate, the pushing rod 125 abuts against the roller 124, at this time, the pushing rod 125 pushes the rotating plates 123 outwards through the roller 124, the two groups of rotating plates 123 are rotatably connected inside the shell 127 around the rotating shaft 1202, meanwhile, the rotating plates 123 and the sliding rod 128 are slidably mounted, the spring 129 is compressed, then the rotating plates 123 drive the clamping plates 122 and the clamping pads 1201 to clamp the inserting rods 1212, so that the convenient mounting effect is realized, wherein the groove 1203 and the connecting sheet 1204 play a role in connection, and the problems that the dismounting is troublesome, the mounting and dismounting efficiency is reduced, and the working time of workers is influenced are further solved;
thirdly, mounting the positive electrode and the negative electrode of the battery of the unmanned aerial vehicle respectively corresponding to the pressure spring 4 and the connecting ring 5, and clamping the battery at the upper ends of the clamping plate 3 and the fixing frame 6;
fourthly, finally, exert the effect of thrust to apron 9 for apron 9 passes through slider 8 and 7 inside slidable mounting of spout, when the limiting plate 11 left end face offsets with the right-hand member face of installation shell 1, stops to exert the force, and wherein, sheetmetal 2 has played the effect of connecting, supports piece 10 and has played the effect of blocking, thereby has realized the fixed effect of locking.
The utility model discloses an improvement provides a be applied to unmanned aerial vehicle's battery locking structure, it passes installation shell 1 and pegs graft with connecting seat 1213 to drive inserted bar 1212 by handheld piece 1211 in coupling mechanism 121, rotary rod 126 drives push rod 125 and rotates after that, push rod 125 offsets with roller 124, at this moment, push rod 125 promotes rotor plate 123 to the outside through roller 124, two sets of rotor plates 123 rotate around pivot 1202 and connect, and simultaneously, rotor plate 123 and slide bar 128 slidable mounting, spring 129 is compressed, then rotor plate 123 drives splint 122 and presss from both sides tight inserted bar 1212 of clamp, the effect of convenient installation has been realized, it is comparatively troublesome when leading to dismantling further to have solved, make the efficiency of installation and dismantlement reduce, staff's the problem of length of operation has been influenced.
The basic principle and the main characteristics of the utility model and the advantages of the utility model have been shown and described above, and the utility model discloses the standard part that uses all can purchase from the market, and dysmorphism piece all can be customized according to the record of the description with the drawing, and the concrete connection mode of each part all adopts conventional means such as ripe bolt rivet among the prior art, welding, and machinery, part and equipment all adopt prior art, conventional model, and conventional connection mode in the prior art is adopted in addition to circuit connection, and the details are not repeated here.
The previous description of the disclosed embodiments is provided to enable any person skilled in the art to make or use the present invention. Various modifications to these embodiments will be readily apparent to those skilled in the art, and the generic principles defined herein may be applied to other embodiments without departing from the spirit or scope of the invention. Thus, the present invention is not intended to be limited to the embodiments shown herein but is to be accorded the widest scope consistent with the principles and novel features disclosed herein.
Claims (10)
1. The battery locking structure applied to the unmanned aerial vehicle comprises an installation shell (1), wherein the left end inside the installation shell (1) is fixedly attached to the right end of a metal sheet (2), the bottom end inside the installation shell (1) is fixedly attached to the lower end of a fixed frame (6), eight clamping plates (3) are arranged at the right end of the metal sheet (2), a connecting ring (5) is arranged in the middle of the metal sheet (2), a pressure spring (4) is arranged at a position 1cm away from the front end of each clamping plate (3), a sliding groove (7) is formed in the rear end of the installation shell (1), the inside of each sliding groove (7) is slidably mounted with the outside of a sliding block (8), the front end of each sliding block (8) is fixedly attached to the rear end of a cover plate (9), the left side of the lower end of the cover plate (9) is fixedly attached to the upper end of a supporting block (10);
the method is characterized in that: still include convenient installation device (12), convenient installation device (12) right-hand member is pegged graft with installation shell (1) left end, convenient installation device (12) comprises coupling mechanism (121), splint (122), rotor plate (123), roller (124), push rod (125), rotary rod (126), shell (127), slide bar (128) and spring (129), coupling mechanism (121) middle part upside is pegged graft with installation shell (1) left end, splint (122) inside hugs closely in coupling mechanism (121) middle part downside, rotor plate (123) right-hand member is fixed with splint (122) left end downside laminating, roller (124) middle part and rotor plate (123) left end locking are fixed, push rod (125) left end and rotary rod (126) right-hand member laminating are fixed, rotary rod (126) middle part and shell (127) left end cooperation, shell (127) inside and slide rod (128) front and back both ends laminating are fixed, the sliding rod (128) is sleeved with a spring (129).
2. The battery locking structure applied to the unmanned aerial vehicle as claimed in claim 1, wherein: coupling mechanism (121) comprise handheld piece (1211), inserted bar (1212) and connecting seat (1213), handheld piece (1211) lower extreme is fixed with the laminating of inserted bar (1212) upper end, inserted bar (1212) outside is passed installation shell (1) left end and is pegged graft with connecting seat (1213) inside, connecting seat (1213) left end is fixed with the laminating of shell (127) right-hand member.
3. The battery locking structure applied to the unmanned aerial vehicle as claimed in claim 1, wherein: the front end of the clamping plate (122) is provided with a clamping pad (1201), and the clamping plate (122) is provided with two groups.
4. The battery locking structure applied to the unmanned aerial vehicle as claimed in claim 1, wherein: the rotating plates (123) are provided with two groups, and the middle parts of the two groups of rotating plates (123) are rotatably connected with the inside of the shell (127) through rotating shafts (1202).
5. The battery locking structure applied to the unmanned aerial vehicle as claimed in claim 1, wherein: the height of the rollers (124) is 5cm, and two groups of rollers (124) are provided.
6. The battery locking structure applied to the unmanned aerial vehicle as claimed in claim 1, wherein: the push rod (125) is conical, and the distance between the lower end of the push rod (125) and the slide rod (128) is 3 cm.
7. The battery locking structure applied to the unmanned aerial vehicle as claimed in claim 1, wherein: a groove 1203 is formed in the left end of the interior of the shell 127, and the interior of the groove 1203 is spliced with the exterior of the push rod 125.
8. The battery locking structure applied to the unmanned aerial vehicle as claimed in claim 2, wherein: the middle part of the insertion rod (1212) is attached to the inner parts of the two groups of clamping plates (122), and the length of the insertion rod (1212) is 2cm less than the height of the shell (127).
9. The battery locking structure applied to the unmanned aerial vehicle as claimed in claim 2, wherein: connecting piece (1204) are provided with in connecting seat (1213) left end to connecting piece (1204) left end and shell (127) right-hand member downside laminating are fixed.
10. The battery locking structure applied to the unmanned aerial vehicle as claimed in claim 1, wherein: convenient installation device (12) are provided with three groups to convenient installation device (12) of three groups all are on same horizontal plane.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202020818601.4U CN212529283U (en) | 2020-05-15 | 2020-05-15 | Be applied to unmanned aerial vehicle's battery locking structure |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202020818601.4U CN212529283U (en) | 2020-05-15 | 2020-05-15 | Be applied to unmanned aerial vehicle's battery locking structure |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN212529283U true CN212529283U (en) | 2021-02-12 |
Family
ID=74542439
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202020818601.4U Expired - Fee Related CN212529283U (en) | 2020-05-15 | 2020-05-15 | Be applied to unmanned aerial vehicle's battery locking structure |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN212529283U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN114101172A (en) * | 2021-11-16 | 2022-03-01 | 徐州日托光伏科技有限公司 | New forms of energy solar panel belt cleaning device |
-
2020
- 2020-05-15 CN CN202020818601.4U patent/CN212529283U/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN114101172A (en) * | 2021-11-16 | 2022-03-01 | 徐州日托光伏科技有限公司 | New forms of energy solar panel belt cleaning device |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN212529283U (en) | Be applied to unmanned aerial vehicle's battery locking structure | |
| CN220106616U (en) | Battery module heating, pressurizing and standing equipment | |
| CN215245581U (en) | Photovoltaic board dust detection device based on many rotor unmanned aerial vehicle | |
| CN111905984B (en) | Power battery module turning device | |
| CN216072170U (en) | Transmission device for battery production | |
| CN213718019U (en) | Pressing clutch type three-clamping-arm mobile phone support | |
| CN213304266U (en) | Storage battery convenient to move | |
| CN212258947U (en) | Full duplex communication device for wireless transmission | |
| CN211496251U (en) | A shell coiling device for producing lithium sulphur battery | |
| CN216890019U (en) | Round frame type door turning machine | |
| CN217889935U (en) | Welding device for optical module production | |
| CN220759644U (en) | Anti-drop's cell-phone draw-in groove spraying tool | |
| CN218227065U (en) | Practical timber concatenation anchor clamps | |
| CN219499451U (en) | Law enforcement record appearance | |
| CN212355482U (en) | Modular extensible mobile platform connecting piece | |
| CN108500955A (en) | A kind of round part mounter hand | |
| CN219466045U (en) | Efficient helmet assembly line | |
| CN215159721U (en) | RFID fragmentation and buckle integrated device | |
| CN212747791U (en) | High-reliability level gauge for building construction | |
| CN218539722U (en) | Basketball leather cutting device | |
| CN216399480U (en) | Optical device module press-fitting device | |
| CN217667636U (en) | A change gear mechanism for hiding track processing | |
| CN211375649U (en) | Parking lot system management device adopting RFID | |
| CN218866484U (en) | RFID commodity identification puts thing device | |
| CN218200557U (en) | A pile up transfer device for new energy automobile battery is retrieved |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20210226 Address after: 308a6, North block, CLP lighting R & D center, 010 Keji South 12th Road, high tech community, Yuehai street, Nanshan District, Shenzhen, Guangdong 518000 Patentee after: Shenzhen Aohua Desai Industrial Co.,Ltd. Address before: No. 26, Meiren village, Zishan Town, Hui'an County, Quanzhou City, Fujian Province, 362100 Patentee before: HUIAN XIANFENG MACHINERY Co.,Ltd. |
|
| TR01 | Transfer of patent right | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20210212 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |