CN207218335U - A kind of unmanned plane for being conveniently replaceable battery - Google Patents
A kind of unmanned plane for being conveniently replaceable battery Download PDFInfo
- Publication number
- CN207218335U CN207218335U CN201721290474.XU CN201721290474U CN207218335U CN 207218335 U CN207218335 U CN 207218335U CN 201721290474 U CN201721290474 U CN 201721290474U CN 207218335 U CN207218335 U CN 207218335U
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- China
- Prior art keywords
- battery
- fixedly connected
- protection shell
- sleeve
- movable plate
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Abstract
The utility model provides a kind of unmanned plane for being conveniently replaceable battery,Including body fuselage,Battery,Locking device and battery protection shell,The bottom of battery protection shell sets fluted,The ratcheting projection of groove,Projection is fixedly connected with moving member,Moving member is fixedly connected with movable plate,Roller is fixedly mounted on movable plate,Roller-coaster connects chute,Chute is fixedly mounted in the inner chamber of body fuselage,Movable plate contradicts the first sleeve,Buffer spring is fixedly mounted in the inside of first sleeve,Buffer spring is fixedly connected with second sleeve,Second sleeve is fixedly connected with the side wall of controller,Controller is electrically connected with power interface,The utility model is simple in construction,Battery can be fixed in the inner chamber of body fuselage well by locking device,Prevent battery from coming off,Realize stable power-supplying,And battery fast assembling-disassembling is realized by roller,Reduce replacing construction,It is easy to use,Securely and reliably.
Description
Technical field
Unmanned air vehicle technique field is the utility model is related to, specially a kind of unmanned plane for being conveniently replaceable battery.
Background technology
In recent years, with the development of science and technology, unmanned plane is extended to civil area from military field, especially extensive
Applied to the agricultural of civil area, forestry, electric power, security protection etc..While unmanned plane application is more and more wider, market
On also there is various unmanned plane species.
At present, unmanned plane on the market is mainly using lithium polymer battery as major impetus, and endurance is typically 20
Minute between 30 minutes, because of technical elements difference difference, but most of cruising time be all within 45 minutes, but
Charging interval has but been above one hour.Because unmanned plane needs to mitigate take-off weight as far as possible, so can not carry heavier
High capacity cell, after most of unmanned planes maintenance more than ten minutes to flight in 20 minutes, must just there are their artificial replacing electricity
Charging wire is plugged in pond, so the battery of unmanned plane needs to be conveniently replaceable.
Utility model content
The purpose of this utility model is to provide a kind of unmanned plane for being conveniently replaceable battery, to solve in above-mentioned background technology
The problem of proposition.
To achieve the above object, the utility model provides following technical scheme:A kind of unmanned plane for being conveniently replaceable battery, bag
Body fuselage and battery are included, the battery is wrapped with battery protection shell, and peace is fixed in the right side of the battery protection shell
Locking device is filled, the locking device includes hole slot, and the hole slot is fixedly connected with the right side of the battery protection shell, the hole
The inwall of groove is fixedly connected with adjustable spring, and the adjustable spring is fixedly connected with latch, and the latch is fixedly connected with sliding block, the machine
Body case is provided with pin hole at place relative with the snibbing position;
Battery interface is fixedly mounted in the left side center of the battery protection shell, and the bottom of the battery protection shell is provided with
Groove, the ratcheting projection of groove, the projection are fixedly connected with moving member, and the projection is in parallel with the moving member central shaft
Strip, the moving member is fixedly connected with movable plate, is fixedly mounted power interface on the movable plate, solid on the movable plate
Dingan County fills roller, and the roller-coaster connects chute, and the chute is fixedly mounted in the inner chamber of the body fuselage, the shifting
Dynamic plate contradicts the first sleeve, and buffer spring is fixedly mounted in the inside of first sleeve, and the buffer spring is fixedly connected with second
Sleeve, the second sleeve are fixedly connected with the side wall of controller, and the controller is electrically connected with power interface.
Preferably, the battery is lithium polymer battery.
Preferably, the locking device is provided with two, and on longitudinal center's axial symmetry peace of the battery protection shell
Dress.
Preferably, the projection is provided with two, and on the horizontal line installation substantially symmetrical about its central axis of the moving member.
Preferably, the roller is provided with four, and symmetrically pacifies on the transverse central axis ring of the movable plate
Dress.
Compared with prior art, the beneficial effects of the utility model are:
1st, the utility model is simple in construction, and battery can be fixed in body fuselage well by locking device
In chamber, prevent battery from coming off, realize stable power-supplying, and battery fast assembling-disassembling is realized by roller, reduce replacing construction, make
With facilitating, securely and reliably;
2nd, on the one hand the utility model is caused battery interface and power interface closely to contradict, realized steady by buffer spring
Fixed power supply, on the other hand stores elastic potential energy, facilitates battery to depart from the inner chamber of body fuselage, realizes fast assembling-disassembling;
3rd, the utility model reduces the frictional resistance between movable plate and chute, conveniently torn open by setting four groups of rollers
Holding storage battery.
Brief description of the drawings
Fig. 1 is the utility model structure diagram;
Fig. 2 is battery protection shell and mobile plate structure schematic diagram in the utility model;
Fig. 3 is locking device structure schematic diagram in the utility model.
In figure:1 body fuselage, 2 batteries, 201 battery protection shells, 202 battery interfaces, 203 grooves, 3 locking devices,
301 hole slots, 302 adjustable springs, 303 latches, 304 sliding blocks, 4 projections, 5 moving members, 6 movable plates, 7 power interfaces, 8 rollers, 9 are slided
Groove, 10 first sleeves, 11 buffer springs, 12 second sleeves, 13 controllers.
Embodiment
Below in conjunction with the accompanying drawing in the utility model embodiment, the technical scheme in the embodiment of the utility model is carried out
Clearly and completely describing, it is clear that described embodiment is only the utility model part of the embodiment, rather than whole
Embodiment.Based on the embodiment in the utility model, those of ordinary skill in the art are not under the premise of creative work is made
The every other embodiment obtained, belong to the scope of the utility model protection.
In description of the present utility model, it is to be understood that term " " center ", " transverse direction ", " longitudinal direction ", " interior ", " outer "
Orientation or position relationship Deng instruction are based on the orientation or position relationship shown in accompanying drawing 1, are for only for ease of and describe this practicality
It is new and simplify description, rather than instruction or imply signified device or particular orientation that structure must have, with specific side
Position construction and operation, therefore it is not intended that to limitation of the present utility model.In addition, term " first ", " second " etc. are only used for
Purpose is described, and it is not intended that instruction or hint relative importance or the implicit quantity for indicating indicated technical characteristic.
Fig. 1-3 are referred to, the utility model provides a kind of technical scheme:A kind of unmanned plane for being conveniently replaceable battery, including
Body fuselage 1 and battery 2, battery 2 are lithium polymer battery, and are electrically connected with battery interface 202.The outer wrapping of battery 2
There is a battery protection shell 201, the right side of battery protection shell 201 is fixedly mounted locking device 3, and locking device 3 is provided with two, and
Vertical central axis on battery protection shell 201 are symmetrically installed.Locking device 3 includes hole slot 301, and hole slot 301 is fixedly connected with electricity
The right side of pond containment vessel 201, the inwall of hole slot 301 are fixedly connected with adjustable spring 302, and adjustable spring 302 is fixedly connected with latch
303, latch 303 is fixedly connected with sliding block 304, and body fuselage 1 is provided with pin hole 202 at place relative with the position of latch 303.
Battery interface 202 is fixedly mounted in the left side center of battery protection shell 201, and the bottom of battery protection shell 201 is set
Fluted 203, the ratcheting projection 4 of groove 203, projection 4 is fixedly connected with moving member 5, and projection 4 is provided with two, and on moving member 5
Horizontal line installation substantially symmetrical about its central axis.Projection 4 is in the strip parallel with the central shaft of moving member 5, and moving member 5 is fixedly connected with movable plate
6, power interface 7 is fixedly mounted on movable plate 6, roller 8 is fixedly mounted on movable plate 6, roller 8 is provided with four, and on moving
The transverse central axis ring of dynamic plate 6 is symmetrically installed.Roller 8 is slidably connected chute 9, and chute 9 is fixedly mounted on body fuselage 1
Inner chamber in.Movable plate 6 contradicts the first sleeve 10, and buffer spring 11, buffer spring 11 is fixedly mounted in the inside of the first sleeve 10
Second sleeve 12 is fixedly connected with, second sleeve 12 is fixedly connected with the side wall of controller 13, and controller 13 is electrically connected with power interface
7, realize battery 2 to the continued power of controller 13.
Operation principle:By in the horizontal push-in body fuselage 1 in direction of the groove 203 of battery protection shell 201 along projection 4
In chamber, battery protection shell 201 promotes movable plate 6 to move horizontally, and movable plate 6 promotes the first sleeve 10, the first sleeve 10 and second
Sleeve 12 compresses buffer spring 11, and buffer spring 11 stores elastic potential energy, now between battery interface 202 and power interface 7
Circuit pathways, the power supply circuit path of unmanned plane.To pull back again sliding block 304, sliding block 304 drives latch 303 to return in hole slot 301,
When the end face of battery protection shell 201 and body fuselage 1 overlaps, sliding block 304 is unclamped, latch 303 inserts pin hole 202, limitation
Battery protection shell 201 departs from body fuselage 1, realizes that battery protection shell 201 and body fuselage 1 are stably connected with.
When that need to change battery 2, sliding block 304 of pulling back, battery protection shell 201 releases the limitation ot it of latch 303, buffering
Spring 11 discharges elastic potential energy, and in the presence of buffer spring 11 and roller 8, battery protection shell 201 automatically disengages body fuselage
1, realize quick-replaceable.
While there has been shown and described that embodiment of the present utility model, for the ordinary skill in the art,
It is appreciated that these embodiments can be carried out with a variety of changes in the case where not departing from principle of the present utility model and spirit, repaiied
Change, replace and modification, the scope of the utility model are defined by the appended claims and the equivalents thereof.
Claims (5)
1. a kind of unmanned plane for being conveniently replaceable battery, including body fuselage (1) and battery (2), it is characterised in that:The electric power storage
Pond (2) is wrapped with battery protection shell (201), and locking device (3) is fixedly mounted in the right side of the battery protection shell (201),
The locking device (3) includes hole slot (301), and the hole slot (301) is fixedly connected with the right-hand member of the battery protection shell (201)
Face, the inwall of the hole slot (301) are fixedly connected with adjustable spring (302), and the adjustable spring (302) is fixedly connected with latch
(303), the latch (303) is fixedly connected with sliding block (304), and the body fuselage (1) is relative with the latch (303) position
Place is provided with pin hole;
Battery interface (202), the battery protection shell (201) is fixedly mounted in the left side center of the battery protection shell (201)
Bottom fluted (203) are set, the ratcheting projection of the groove (203) (4), the projection (4) is fixedly connected with moving member (5),
The projection (4) is in the strip parallel with the moving member (5) central shaft, and the moving member (5) is fixedly connected with movable plate
(6) power interface (7), is fixedly mounted on the movable plate (6), roller (8), the rolling is fixedly mounted on the movable plate (6)
Wheel (8) is slidably connected chute (9), and the chute (9) is fixedly mounted in the inner chamber of the body fuselage (1), the movable plate
(6) the first sleeve (10) is contradicted, buffer spring (11), the buffer spring is fixedly mounted in the inside of first sleeve (10)
(11) second sleeve (12) is fixedly connected with, the second sleeve (12) is fixedly connected with the side wall of controller (13), the controller
(13) it is electrically connected with power interface (7).
A kind of 2. unmanned plane for being conveniently replaceable battery according to claim 1, it is characterised in that:The battery (2) is
Lithium polymer battery.
A kind of 3. unmanned plane for being conveniently replaceable battery according to claim 1, it is characterised in that:The locking device (3)
Two are provided with, and is symmetrically installed on the vertical central axis of the battery protection shell (201).
A kind of 4. unmanned plane for being conveniently replaceable battery according to claim 1, it is characterised in that:The projection (4) is set
There are two, and on the horizontal line installation substantially symmetrical about its central axis of the moving member (5).
A kind of 5. unmanned plane for being conveniently replaceable battery according to claim 1, it is characterised in that:The roller (8) is set
There are four, and symmetrically installed on the transverse central axis ring of the movable plate (6).
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
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CN201721290474.XU CN207218335U (en) | 2017-09-24 | 2017-09-24 | A kind of unmanned plane for being conveniently replaceable battery |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
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CN201721290474.XU CN207218335U (en) | 2017-09-24 | 2017-09-24 | A kind of unmanned plane for being conveniently replaceable battery |
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Publication Number | Publication Date |
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CN207218335U true CN207218335U (en) | 2018-04-10 |
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CN201721290474.XU Expired - Fee Related CN207218335U (en) | 2017-09-24 | 2017-09-24 | A kind of unmanned plane for being conveniently replaceable battery |
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Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN108394309A (en) * | 2018-06-06 | 2018-08-14 | 深圳草莓创新技术有限公司 | A kind of unmanned machine battery positioning and locking device and its method |
CN108860626A (en) * | 2018-06-12 | 2018-11-23 | 天津天喜科技有限公司 | Battery installation device for civil unmanned aircraft |
CN109920947A (en) * | 2019-01-23 | 2019-06-21 | 广东工业大学 | A kind of battery ejection protective device of high temperature-proof and anticollision |
CN110391376A (en) * | 2019-07-19 | 2019-10-29 | 广西南宁一键智农科技有限公司 | The locking device of single rotor unmanned plane battery cover |
CN110549997A (en) * | 2019-10-14 | 2019-12-10 | 博众精工科技股份有限公司 | Clean system is changed to power station battery |
CN114291148A (en) * | 2021-12-09 | 2022-04-08 | 南阳理工学院 | Commodity self-settlement shopping cart based on artificial intelligence |
-
2017
- 2017-09-24 CN CN201721290474.XU patent/CN207218335U/en not_active Expired - Fee Related
Cited By (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN108394309A (en) * | 2018-06-06 | 2018-08-14 | 深圳草莓创新技术有限公司 | A kind of unmanned machine battery positioning and locking device and its method |
CN108860626A (en) * | 2018-06-12 | 2018-11-23 | 天津天喜科技有限公司 | Battery installation device for civil unmanned aircraft |
CN109920947A (en) * | 2019-01-23 | 2019-06-21 | 广东工业大学 | A kind of battery ejection protective device of high temperature-proof and anticollision |
CN110391376A (en) * | 2019-07-19 | 2019-10-29 | 广西南宁一键智农科技有限公司 | The locking device of single rotor unmanned plane battery cover |
CN110549997A (en) * | 2019-10-14 | 2019-12-10 | 博众精工科技股份有限公司 | Clean system is changed to power station battery |
CN110549997B (en) * | 2019-10-14 | 2021-07-09 | 博众精工科技股份有限公司 | Clean system is changed to power station battery |
CN114291148A (en) * | 2021-12-09 | 2022-04-08 | 南阳理工学院 | Commodity self-settlement shopping cart based on artificial intelligence |
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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: 20180410 Termination date: 20200924 |
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CF01 | Termination of patent right due to non-payment of annual fee |