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CN107124906A - A battery holding component, drone and charger - Google Patents

A battery holding component, drone and charger
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Publication number
CN107124906A
CN107124906ACN201680002335.4ACN201680002335ACN107124906ACN 107124906 ACN107124906 ACN 107124906ACN 201680002335 ACN201680002335 ACN 201680002335ACN 107124906 ACN107124906 ACN 107124906A
Authority
CN
China
Prior art keywords
battery
holding section
button
fastening assembly
battery compartment
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.)
Granted
Application number
CN201680002335.4A
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Chinese (zh)
Other versions
CN107124906B (en
Inventor
熊荣明
唐尹
熊贤武
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.)
SZ DJI Technology Co Ltd
Original Assignee
SZ DJI 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.)
Filing date
Publication date
Application filed by SZ DJI Technology Co LtdfiledCriticalSZ DJI Technology Co Ltd
Publication of CN107124906ApublicationCriticalpatent/CN107124906A/en
Application grantedgrantedCritical
Publication of CN107124906BpublicationCriticalpatent/CN107124906B/en
Expired - Fee Relatedlegal-statusCriticalCurrent
Anticipated expirationlegal-statusCritical

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Abstract

The application discloses fixing subassembly, unmanned aerial vehicle and charger of battery, wherein, the fixing subassembly of battery includes: the battery compartment 12 is used for accommodating batteries, one end of the battery compartment 12 is provided with an electrical interface, and the other end of the battery compartment is provided with a first clamping part; an operating member 14a and an elastic member 16 provided on the battery compartment and engaged with the first engaging portion; when the battery is placed in the battery compartment 12, the electrical interface is connected with the electrical interface of the battery, and the elastic member 16 elastically drives the first clamping part and/or the battery to enable the battery to be in snap fit with the first clamping part, so that the battery is fixed to the battery compartment 12; when the operating member 14a is actuated, the operating member 14a drives the first engaging portion to relatively separate the first engaging portion from the battery, so as to unlock the battery from the battery compartment 12. Through the mode, the problem that the battery is hard to take and place in the process and needs to be operated by two hands simultaneously can be solved.

Description

A kind of fastening assembly of battery, unmanned plane and charger
Technical field
The application is related to a kind of fastening assembly of battery, unmanned plane and charger.
Background technology
In recent years, with the development of science and technology, unmanned plane is extended to civil area from military field, especially extensiveIn terms of the agricultural of civil area, forestry, electric power, security protection.
Unmanned plane generally requires setting battery and is powered, at present, it usually needs both hands are operated, to realize batteryPick and place.
The content of the invention
In order at least partly solve problem above, the application provides a kind of fastening assembly of battery, and this method includes:IncludingBattery compartment, for housing battery and being battery charging, one end of the battery compartment is provided with electric interfaces, the battery compartment it is anotherEnd is provided with the first holding section;Operating parts and elastic component, it is arranged on the battery compartment and coordinated with first holding section;ItsIn, when the battery is placed in the battery compartment, the electric interfaces are connected with the electric interfaces of the battery, the elastic componentFirst holding section described in flexible drive and/or the battery, make the battery be clasped with first holding section, and then willThe battery is fixed on the battery compartment;In operating parts described in start, the operating parts drives first holding section, makes instituteThe first holding section and the battery relative separation are stated, and then unlocks from the battery compartment battery.
In order at least partly solve problem above, the application provides a kind of unmanned plane, including:Including fuselage, it is placed in instituteThe battery in fuselage is stated, includes the fastening assembly of any of the above-described described battery, the fastening assembly of the battery is the fuselageA part or be installed on the fuselage.
In order at least partly solve problem above, the application provides a kind of charger, includes the fastening assembly of above-mentioned battery.
The beneficial effect of the application is:A kind of fastening assembly of battery, unmanned plane and charger are provided, by elastic component withBattery can be fixed on battery compartment by the interaction relation of the first holding section, one hand;And pass through operating parts and the connection of the first holding sectionDynamic relation, one hand can unlock battery from battery compartment, facilitate picking and placeing for battery.
Brief description of the drawings
Fig. 1 is a kind of dimensional structure diagram of the fastening assembly of battery of the embodiment of the present application;
Fig. 2 is the operating parts of the embodiment of the present application and the perspective exploded view of elastic component;
Fig. 3 is a kind of battery of the embodiment of the present application and the perspective exploded view of fastening assembly;
Fig. 4 is the schematic diagram of battery and fastening assembly assembling process in Fig. 3;
Fig. 5 is the schematic diagram after being completed in Fig. 4;
Fig. 6 is the schematic cross-section along Fig. 5 center lines III-III;
Fig. 7 is the enlarged diagram of a-quadrant in Fig. 6;
Fig. 8 is the dimensional structure diagram of the electric interfaces of the embodiment of the present application;
Fig. 9 is the enlarged diagram in B regions in Fig. 6;
Figure 10 is a kind of dimensional structure diagram of operating parts of the embodiment of the present application;
Figure 11 is the dimensional structure diagram of another operating parts of the embodiment of the present application;
Figure 12 is the dimensional structure diagram of another operating parts of the embodiment of the present application;
Figure 13 is the dimensional structure diagram of another operating parts of the embodiment of the present application;
Figure 14 is the dimensional structure diagram of another operating parts of the embodiment of the present application;
Figure 15 is a kind of schematic perspective view of unmanned plane of the embodiment of the present application;
Figure 16 is a kind of perspective exploded view of charger of the embodiment of the present application.
Embodiment
Below in conjunction with the accompanying drawing in the embodiment of the present application, the technical scheme in the embodiment of the present application is carried out clear, completeSite preparation is described, it is clear that described embodiment is only a part of embodiment of the application, rather than whole embodiments.It is based onEmbodiment in the application, it is every other that those of ordinary skill in the art are obtained under the premise of creative work is not madeEmbodiment, belongs to the scope of the application protection.
It will be appreciated that term " first ", " second ", " the 3rd " are only used for describing purpose, and it is not intended that indicate orImply relative importance or the implicit quantity for indicating indicated technical characteristic.Thus, " first ", " second ", " are definedAt least one this feature can be expressed or be implicitly included to three " feature.In the description of the present application, " multiple " be meant that toIt is few two, such as two, three etc., unless otherwise specifically defined.
Fig. 1 to Fig. 3 is referred to, Fig. 1 is a kind of dimensional structure diagram of the fastening assembly of battery of the embodiment of the present application,Fig. 2 is the operating parts of the embodiment of the present application and the perspective exploded view of elastic component, and Fig. 3 is a kind of battery of the embodiment of the present applicationAnd the perspective exploded view of fastening assembly.As illustrated, the fastening assembly in the present embodiment includes battery compartment 12, specifically,The battery compartment 12 includes body 122 and is formed at the storage tank 124 of body 122, and the storage tank 124 is specifically for housing battery20。
Please refer to Fig. 2, Fig. 3 and Fig. 5, wherein, Fig. 5 is the schematic diagram after being completed in Fig. 4.In the present embodimentIn, one end of battery compartment 12 is provided with the first holding section 128, and the other end of battery compartment 12 engages provided with electric interfaces 126 and secondPortion 123.Wherein, the first holding section 128 is dead bolt, and the free end of dead bolt is lozenges, the bottom of lozenges dorsad battery compartment 12Face is set.Specifically, battery compartment 12 includes two relative side, and the first holding section 128 is disposed therein one side, electric interfaces126 and second holding section 123 be arranged at another side.And the side of the first holding section 128 of correspondence is provided with operating cavity 125, operationChamber 125 stores the first holding section 128.
Further, the fastening assembly also includes the operation for being arranged on battery compartment 12 and coordinating with the first holding section 128Part 14a and elastic component 16.
Further, battery 20 includes electric interfaces 22, the 3rd holding section 26, the 4th holding section 24, and the 3rd cardConjunction portion 26 is correspondingly arranged with the first holding section 128, and the 4th holding section 24 is correspondingly arranged with the second holding section 123.
Fig. 4, Fig. 6, Fig. 7 and Fig. 8 are referred to, wherein, Fig. 4 is the schematic diagram of battery and fastening assembly assembling process in Fig. 3,Fig. 7 is the enlarged diagram of a-quadrant in the schematic cross-section along Fig. 5 center lines III-III, Fig. 7, and Fig. 8 is the embodiment of the present applicationThe dimensional structure diagram of electric interfaces.In the present embodiment, when battery 20 is placed in battery compartment 12, electric interfaces 126 can be madeIt is that holding section and the electric interfaces 22 of battery 20 are clasped, and the electric interfaces 126 of battery compartment 12 and electrically connecing for battery 20What mouth 22 was clasped is oriented parallel to Pin pin., can on the electric interfaces 22 of battery 20 in the application scenarios of the applicationTo open up L-shaped hole.Alternatively, larger-size bar hole can be opened up in other embodiments, so as to avoid working as battery compartment 12On the terminal of electric interfaces 126 when being inserted into inclined battery 20, collide or bend.
Further, during battery 20 is placed in battery compartment 12, the electric interfaces 22 of electric interfaces 126 and battery 20At least electrically connect, and be at least electrically insulated when battery 20 screws out battery compartment 12 completely when battery 20 is completely screwed into battery compartment 12.
In addition, an accessory ID 121 is provided with close to the side of electric interfaces 126 on battery compartment 12, specifically, in battery20 when being placed in during battery compartment 12, and battery compartment 12 is first inserted in the one end of battery 20 with electric interfaces 22, and then battery 20 enclosesRotated around the sideline of the accessory ID 121.
In above-described embodiment, the electric interfaces 126 on battery compartment 12 are regard as the electric interfaces on holding section and battery 2022 are clasped, and the one end of battery 20 is fixed on into battery compartment 12 using the frictional force patched between electric interfaces 126,22In, the fixation of battery 20 can be facilitated without additionally setting other snap-in structures again at the end of battery 20.
Simultaneously refering to Fig. 3 into Fig. 7, with previous embodiment using the frictional force patched between electric interfaces 126,22 by electricityThe one end of pond 20 is fixed on unlike battery compartment 12, in other embodiments, utilizes the 4th holding section 24, the second holding sectionBattery compartment 12 is fixed in the one end of battery 20 by 123.Specifically, the 4th holding section 24 is the first of one end end face of battery 20Flange, correspondingly, the second holding section 123 are disposed on the second flange of the side of the first flange of correspondence of battery compartment 12.Meanwhile, theOne flange 24 from be less than with a distance from bottom surface the second flange 123 from bottom surface with a distance from.
During practical operation, during battery 20 is placed in battery compartment 12, battery 20 has one end of the first flange 24 firstIt is placed in battery compartment 12, the first flange 24 is embedded under the second flange 123, battery 20 is with the second flange 123 or the first flange 24Rotated for axle, the other end screws in the battery compartment 12.
In above-described embodiment, the first flange 24 on the second flange 123 or battery 20 on battery compartment 12 is regard as engagingPortion, facilitates being fixed for battery 20.
In addition, being provided with bullet adjacent to the position of the first holding section 128 in the bottom surface of the battery compartment 12 or the bottom surface of battery 20Piece 18, alternatively it is also possible to be set to cushion.Battery 20 is supported in the one end of shell fragment 18, and other end supports battery compartment 12, withBattery 20 is at least partly ejected into battery compartment 12 after unblock battery 20.Such as, battery acts on lower tail in the elastic force that shell fragment 18 is providedEject in portion.And when battery 20 is completely disposed at battery compartment, i.e., the first holding section 128 supports lower snap lock battery in elastic component 1620 are in compressive state in battery compartment 12, shell fragment 18.At the same time, battery 20 is exposed to the one side in air and the side of battery compartment 12Side top surface is complementary and round and smooth connects.
Fig. 2, Fig. 3, Fig. 5, Fig. 6 and Fig. 9 are referred to, in a particular embodiment, operating parts 14a includes button 142a and slide bar144a.Wherein, button 142a is arranged at the top surface of body 122.Specifically, chute 127 is set on the top surface of body 122, usedIn collecting button 142a.Alternatively, button 142a can also be arranged on the side of body 122, i.e., set in the side of body 122Chute 127 houses button 142a.
Further, the side of slide bar 144a dorsad dead bolts 128 is provided with cylinder 1444a, and dead bolt is from slide bar 144a directionsThe direction of battery 20 is extended.
Please continue to refer to Fig. 2 and Fig. 9, elastic component 16 is spring, and its one end is sheathed on cylinder 1444a, and other end is supportedIn in battery compartment 12.
Specifically, elastic component 16 is contained in operating cavity 125, and elastic component 16 is located at the first holding section 128 back to battery 20 1Side, one end is resisted against slide bar 144a, and then supports the first holding section 128 indirectly, and other end is directly resisted against operating cavity 125Cavity wall.
In non-actuation button 142a, elastic component 16 passes through the first holding section of slide bar 144a flexible drives in a free state128 namely dead bolt moved towards battery 20, make dead bolt stretch out operating cavity 125 engage with battery 20;Also, dead bolt is in elastic component 16Continue support it is lower continue snap lock battery 20 in battery compartment 12.
Certainly, in turn, elastic component 16 can also flexible drive battery 20 to be clasped with the first holding section 128, enterAnd battery 20 is fixed on battery compartment 12.
In actuation button 142a, button 142a drives the first holding section 128 namely dead bolt, makes dead bolt relative with battery 20Separation, and then the 12 unblock battery 20 from battery compartment.Dead bolt departs from after battery 20, retraction operating cavity 125.
In the embodiment of the present application, there is plurality of optional fits kind in button 142a and slide bar 144a, to cause actuation buttonDuring 142a, button 142a can drive the first holding section 128:
1) first kind
In actuation button 142a, button 142a bands moving slide-bar 144a is moved in the same direction, i.e., moved towards the direction away from battery 20Move and dead bolt is separated with battery 20, and then the unblock battery 20 from battery compartment 12.
Such as shown in Fig. 2 button 142 towards slide bar 144a one side are provided with projection 1422a, alternatively, otherIn embodiment, button 142a towards slide bar 144a one side it can also be provided that depression.Correspondingly, slide bar 144a is towards button142a one side is provided with the depression 1442a coordinated with projection 1422a.Certainly, when button 142a towards slide bar 144a one side are setWhen being set to depression, slide bar 144a towards button 142a one side are set to projection and coordinated with it accordingly, and then make the projection1422a is embedded in the depression 1442a, so that button 142a is connected to slide bar 144a.
Correspondence above-described embodiment, actuation button 142a is referred specifically to:Button is promoted or stirs along the top surface or side of body 122142a。
There is provided a kind of operating parts and elastic component in above-described embodiment, when battery is fixed on battery compartment, operating parts, which drives, to be slidedBar is moved in the same direction, battery is unlocked from battery compartment, and by shell fragment by battery ejection, battery taking and placing, solution can be achieved in one handDetermine the problem of battery taking and placing is laborious in the prior art.
Alternatively, in other embodiments, the matching relationship of button and slide bar can also be as shown in Figure 10.Figure 10 is thisApply for a kind of dimensional structure diagram of operating parts of embodiment.Specifically, button 142b towards slide bar 144b one side are setHave the first projection 1422b, slide bar 144b towards button 142b one side provided with the second projection 1442b, the first projection 1422b is located atBetween battery and the second projection 1442b.Because the first projection 1422b is located between battery and the second projection 1442b, therefore, startWhen button 142b makes it away from battery direction, the first projection 1422b promotes the second projection 1442b to move in the same direction, and then drives cunningBar 144b, dead bolt 128 are mobile in the same direction.
Further, the first projection 1422b towards the second projection 1442b one side are provided with the first inclined-plane (not identifying), theTwo projections 1442 towards the first projection 1422b one side are provided with the second inclined-plane (not identifying), in button 142b band moving slide-bars 144bFirst inclined-plane is fitted with the second inclined-plane and keeps being relatively fixed in moving process in the same direction.Because of the first projection 1422b and the second projection1442b uses inclined-plane laminating type, therefore in the first projection 1422b promotes the second projection 1442b moving process in the same direction, it is stableProperty is higher.
Alternatively, in other embodiments, the matching relationship of button and slide bar can also be as shown in figure 11.Please join in the lumpFigure 11 is read, Figure 11 is the dimensional structure diagram of another operating parts of the embodiment of the present application, is with Figure 10 differences, pressesButton 142c is not provided with the first inclined-plane towards the first projection 1422c of slide bar 144c one side, accordingly, and slide bar 144c directions are pressedSecond projection 1442c of button 142c one side is not provided with the second inclined-plane.
There is provided a kind of operating parts in above-described embodiment, when battery is fixed on battery compartment, one hand can start operating parts,And then moved in the same direction with moving slide-bar, battery is unlocked from battery compartment, and by shell fragment by battery ejection, solve prior artThe problem of middle battery taking and placing is laborious.
2) Second Type
In actuation button 142d, the button 142d band incorgruous movements of moving slide-bar 144d move towards the direction away from batteryAnd dead bolt is separated with battery, and then unlock from battery compartment battery.
Such as, the matching relationship of button and slide bar can be as shown in figure 12, and Figure 12 is another of the embodiment of the present applicationThe dimensional structure diagram of operating parts.Specifically, button 142d towards slide bar 144d one side are provided with the first projection 1422d,Slide bar 144d towards button 142d one side are provided with the second projection 1442d, the first projection 1422d towards the second projection 1442d'sThe first inclined-plane (not identifying) simultaneously is provided with, the second projection 1442d towards the first projection 1422d one side are provided with the second inclined-plane (notMark), the first inclined-plane is located between battery and the second inclined-plane.
Using Figure 12 view directions as reference, when pressing button 142d downwards, distance is protected between the first projection 1422d and batteryHold constant, now, the first inclined-plane is fitted with the second inclined-plane, the first inclined-plane produces the thrust component of horizontal direction to the second inclined-plane,Both are relative to slide, and then causes slide bar 144d to drive dead bolt 128 to be moved towards the direction away from battery.
Alternatively, in other embodiments, the matching relationship of button and slide bar can also be as shown in figure 13.Please join in the lumpRead Figure 13, be with Figure 12 differences, the first inclined-plane is not between battery and the second inclined-plane, but both with battery itBetween distance it is suitable;In addition, button 142e flowing mode of making not is pressed down on, but the distance between holding and battery 20Level is slided on the premise of constant.Under this matching relationship, the first inclined-plane produces water to the second inclined-plane during sliding button 142eSquare to thrust component, both are relative to slide, and then causes slide bar 144e to drive dead bolt 128 to be moved towards the direction away from batteryIt is dynamic.
Above-described embodiment is there is provided a kind of operating parts, when battery is fixed on battery compartment, and operating parts band moving slide-bar is incorgruous to be movedDynamic, one-handed performance can be such that battery is unlocked from battery compartment, and by shell fragment by battery ejection, solve battery in the prior artThe problem of picking and placeing laborious.
Certainly, the matching relationship of button and slide bar is not limited to above two type, such as button is knob, refers to figure14, Figure 14 be the dimensional structure diagram of another operating parts of the embodiment of the present application.As schemed, the knob 142f peripheries are provided withFirst teeth 1422f, slide bar 144f towards button 142f one side provided with the second teeth 1442f, the first teeth 1422f and1442f is engaged.During rotational button 142f, button 142f keeps constant with the distance between battery, passes through teeth band moving slide-bar144f, and then cause slide bar 144f to drive dead bolt 128 to be moved towards the direction away from battery.
Refering to Figure 15, Figure 15 is a kind of dimensional structure diagram of unmanned plane of the embodiment of the present application.The unmanned plane 30 is wrappedInclude fuselage 32, be placed in fuselage 32 battery, include the fastening assembly of battery, and the fastening assembly is the one of fuselage 32Part is installed on fuselage 32, and the structure of the wherein fastening assembly of battery sees above described, and it is no longer repeated herein.
Also referring to Fig. 2, Fig. 3, Fig. 6 and Fig. 7, battery compartment 12 is further provided with the second holding section 123, battery 20It is provided with electric interfaces 22, the 3rd holding section 26, the 4th holding section 24.Wherein, 128 pairs of the 3rd holding section 26 and the first holding sectionIt should set, the 4th holding section 24 is correspondingly arranged with the second holding section 123.
Wherein, the 4th holding section 24 is the first flange of one end end face of battery 20, and the second holding section 123 is disposed on batteryStorehouse 12 correspondence the first flange 24 side the second flange, the first flange from a distance from 24 bottom surfaces be less than the second flange 123 bottom of fromThe distance in face.
Further, the 3rd holding section 26 is the pit of one end end face of battery 20, and the first holding section 128 is entered into pit 26And battery 20 is fixed on battery compartment 12, pit 26 and then the 12 unblock battery 20 from battery compartment are left in the first holding section 128.
In a particular embodiment, when battery 20 is placed in battery compartment 12, the 4th holding section 24 and the buckle of the second holding section 123Coordinate, the first holding section of flexible drive 128 of elastic component 16 is clasped with the 3rd holding section 26, and then battery 20 is fixed on into electricityPond storehouse 12.
Further, it is specially to promote or stir button along the top surface or side of body 122 in start operating parts 14a142a, makes the button 142a drive the first holding section 128 and the relative separation of battery 20, and then unlock battery from battery compartment 1220。
There is provided a kind of fastening assembly of battery in above-described embodiment, by the way that holding section and elastic component layout are arrived into battery compartmentTwo ends, battery can be improved laborious in fetching process and need both hands while the problem of operating.
Refering to Figure 16, Figure 16 is a kind of structural representation of charger of the embodiment of the present application.As illustrated, the charger40 include the fastening assembly and charging plug 42 of battery.Wherein, described in the structure of the fastening assembly of the battery is seen above, thisIt is no longer repeated at place.
The application provides a kind of fastening assembly of battery, unmanned plane and charger, can improve battery in fetching processIt is laborious and need both hands while the problem of operating.
Presently filed embodiment is the foregoing is only, the scope of the claims of the application is not thereby limited, it is every to utilize thisEquivalent structure or equivalent flow conversion that application specification and accompanying drawing content are made, or directly or indirectly it is used in other correlationsTechnical field, is similarly included in the scope of patent protection of the application.

Claims (25)

CN201680002335.4A2016-09-262016-09-26 A battery holding component, drone and chargerExpired - Fee RelatedCN107124906B (en)

Applications Claiming Priority (1)

Application NumberPriority DateFiling DateTitle
PCT/CN2016/100177WO2018053858A1 (en)2016-09-262016-09-26Battery fixing assembly, unmanned aerial vehicle, and charger

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Publication NumberPublication Date
CN107124906Atrue CN107124906A (en)2017-09-01
CN107124906B CN107124906B (en)2019-01-29

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CN108860626A (en)*2018-06-122018-11-23天津天喜科技有限公司Battery installation device for civil unmanned aircraft
WO2019140642A1 (en)*2018-01-192019-07-25深圳市大疆创新科技有限公司Battery safety alert system
CN110383524A (en)*2017-09-302019-10-25深圳市大疆创新科技有限公司Battery module and unmanned plane
WO2020087284A1 (en)*2018-10-302020-05-07深圳市大疆创新科技有限公司Battery control circuit, battery and unmanned aerial vehicle
CN111661345A (en)*2020-06-102020-09-15安阳全丰航空植保科技股份有限公司Unmanned aerial vehicle battery compartment structure
CN111806618A (en)*2019-04-112020-10-23太普动力新能源(常熟)股份有限公司 Locking structure and electric bicycle frame with the same
CN113131557A (en)*2020-01-142021-07-16华广生技股份有限公司Charging device for physiological signal sensor and charging method thereof
CN113540679A (en)*2020-04-202021-10-22成都鼎桥通信技术有限公司Mobile terminal
CN114644123A (en)*2020-12-182022-06-21东友科技股份有限公司 UAV and its battery replacement system

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CN108321622B (en)*2018-04-062025-01-07深圳市宝尔爱迪科技有限公司 A self-locking and unlocking structure for a charger and a battery assembly
CN108725245B (en)*2018-05-302023-06-23西安工业大学Battery replacement system and replacement method of aircraft
CN113471613A (en)*2020-03-122021-10-01比亚迪股份有限公司Vehicle battery box and vehicle
CN111358347A (en)*2020-05-062020-07-03苏州海力电器有限公司Rotary type locking structure of dust collector battery pack
EP4556380A1 (en)*2023-11-172025-05-21"Rogoz" Spolka z Ograniczona Odpowiedzialnoscia- A-Spolka Komandytowo-AkcyjnaA frame for unmanned aerial vehicle and a method of replacing battery

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CN110383524A (en)*2017-09-302019-10-25深圳市大疆创新科技有限公司Battery module and unmanned plane
CN110383524B (en)*2017-09-302022-03-15深圳市大疆创新科技有限公司Battery module and unmanned aerial vehicle
WO2019140642A1 (en)*2018-01-192019-07-25深圳市大疆创新科技有限公司Battery safety alert system
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WO2020087284A1 (en)*2018-10-302020-05-07深圳市大疆创新科技有限公司Battery control circuit, battery and unmanned aerial vehicle
CN111806618A (en)*2019-04-112020-10-23太普动力新能源(常熟)股份有限公司 Locking structure and electric bicycle frame with the same
CN113131557A (en)*2020-01-142021-07-16华广生技股份有限公司Charging device for physiological signal sensor and charging method thereof
CN113540679A (en)*2020-04-202021-10-22成都鼎桥通信技术有限公司Mobile terminal
CN113540679B (en)*2020-04-202023-06-20成都鼎桥通信技术有限公司Mobile terminal
CN111661345A (en)*2020-06-102020-09-15安阳全丰航空植保科技股份有限公司Unmanned aerial vehicle battery compartment structure
CN114644123A (en)*2020-12-182022-06-21东友科技股份有限公司 UAV and its battery replacement system

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