CN107579186A - Unmanned aerial vehicle onboard intelligent battery bead fixed structure - Google Patents
Unmanned aerial vehicle onboard intelligent battery bead fixed structure Download PDFInfo
- Publication number
- CN107579186A CN107579186A CN201710976207.6A CN201710976207A CN107579186A CN 107579186 A CN107579186 A CN 107579186A CN 201710976207 A CN201710976207 A CN 201710976207A CN 107579186 A CN107579186 A CN 107579186A
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- bead
- battery
- plate
- aerial vehicle
- unmanned aerial
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- 239000011324 bead Substances 0.000 title claims abstract description 142
- 230000007246 mechanism Effects 0.000 claims abstract description 34
- 230000035939 shock Effects 0.000 claims abstract description 24
- 230000008676 import Effects 0.000 claims description 18
- 230000005611 electricity Effects 0.000 description 6
- 238000000034 method Methods 0.000 description 5
- 229910000838 Al alloy Inorganic materials 0.000 description 4
- 230000008569 process Effects 0.000 description 4
- 238000004891 communication Methods 0.000 description 3
- 239000011521 glass Substances 0.000 description 3
- 238000009434 installation Methods 0.000 description 3
- 238000012360 testing method Methods 0.000 description 3
- 206010020649 Hyperkeratosis Diseases 0.000 description 2
- 230000008859 change Effects 0.000 description 2
- 238000005516 engineering process Methods 0.000 description 2
- 238000003780 insertion Methods 0.000 description 2
- 230000037431 insertion Effects 0.000 description 2
- 238000007726 management method Methods 0.000 description 2
- 238000004806 packaging method and process Methods 0.000 description 2
- 229920000049 Carbon (fiber) Polymers 0.000 description 1
- 229920000742 Cotton Polymers 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000000903 blocking effect Effects 0.000 description 1
- 239000004917 carbon fiber Substances 0.000 description 1
- 230000023402 cell communication Effects 0.000 description 1
- 239000000306 component Substances 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 239000008358 core component Substances 0.000 description 1
- 230000007423 decrease Effects 0.000 description 1
- 230000007812 deficiency Effects 0.000 description 1
- 230000003111 delayed effect Effects 0.000 description 1
- 238000013461 design Methods 0.000 description 1
- 230000008034 disappearance Effects 0.000 description 1
- 238000002474 experimental method Methods 0.000 description 1
- 230000005484 gravity Effects 0.000 description 1
- 230000002452 interceptive effect Effects 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 230000035800 maturation Effects 0.000 description 1
- 238000010297 mechanical methods and process Methods 0.000 description 1
- VNWKTOKETHGBQD-UHFFFAOYSA-N methane Chemical compound C VNWKTOKETHGBQD-UHFFFAOYSA-N 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- IAIWVQXQOWNYOU-FPYGCLRLSA-N nitrofural Chemical compound NC(=O)N\N=C\C1=CC=C([N+]([O-])=O)O1 IAIWVQXQOWNYOU-FPYGCLRLSA-N 0.000 description 1
- 230000002093 peripheral effect Effects 0.000 description 1
- 239000000575 pesticide Substances 0.000 description 1
- 238000013439 planning Methods 0.000 description 1
- 230000010152 pollination Effects 0.000 description 1
- 238000003672 processing method Methods 0.000 description 1
- 230000001737 promoting effect Effects 0.000 description 1
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- 238000006467 substitution reaction Methods 0.000 description 1
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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
- Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
- Y02E60/00—Enabling technologies; Technologies with a potential or indirect contribution to GHG emissions mitigation
- Y02E60/10—Energy storage using batteries
Abstract
The invention discloses a kind of unmanned aerial vehicle onboard intelligent battery bead fixed structure, bead fixed seat including being provided with bead, bead introducing mechanism is provided with bead fixed seat, bead introducing mechanism can be mobile relative to bead fixed seat when battery loads and unloads and bead introducing mechanism can contact and fix with bead.The present invention realizes the convenience and accuracy of battery assembly and disassembly operations, realizes multipoint positioning, battery assembly and disassembly run along same track, improve efficiency while will not damage battery core by using wedge-shaped bead introducing mechanism；By setting the bead fixed seat with bumper and absorbing shock pad, it matches with wedge-shaped bead introducing mechanism and used, and slows down impact when realizing the fastness of battery fixation, while installing, protects the safety of battery；Rotated using bead and combine wedge-shaped approaching face, it is only necessary to which giving very little thrust just can be automatically mounted into position, be lifted up just can quickly and securely extracting battery, improve the convenience and efficiency of assembly and disassembly.
Description
Technical field
The present invention relates to a kind of unmanned plane battery fixing structure, and in particular to a kind of unmanned aerial vehicle onboard intelligent battery bead is consolidated
Determine structure.
Background technology
With the increasingly maturation, and the popularization of modern agriculture theory of unmanned air vehicle technique so that unmanned plane is in modern agriculture
Substantial amounts of popularization has been obtained in production, such as：Pesticide spraying, fertilising, crop pollination etc. are carried out using unmanned plane.With traditional work
Mode is compared, and drastically increases operating efficiency.However, in the UAS used now, electrokinetic cell is used as nobody
One of core component of machine system, but there are many deficiencies, wherein what is protruded the most is the fixation and dismounting of electrokinetic cell.
Plant protection unmanned plane use power consumption it is big, the battery used can not it is excessive can not be too small, if battery is excessive, body
Product and weight it is excessive, cause UAV system dose to diminish, although too small volume and weight meet require, electricity not enough, it is necessary to
More frequently change, therefore, it is necessary to match unmanned plane scheme, select suitable battery；Nevertheless, plant protection unmanned plane is still
Need constantly to change battery to meet efficient job requirements, therefore, the replacing construction and efficiency of battery, which directly affect, plants
Protect the overall operating efficiency of unmanned plane.
The simple battery pack that the existing agricultural unmanned plane of major part all uses adds the power scheme being mechanically fixed, i.e., by battery core
After simple packaging, it is connected by straight cutting plug with unmanned plane, the battery core simply packed is by mechanical method, such as bolt, buckle
Or the fixture such as binding strap is fixed, or even some unmanned planes directly load naked battery core to get up to use, and use with top
Case, battery fix/detaching structure complexity, not only expend time and manpower, and during careless manipulation, easily battery core is caused to damage
Wound, causes to leak electricity, or even jeopardize the safety of operating personnel.
The content of the invention
The technical problems to be solved by the invention are that existing unmanned machine battery uses bolt, buckle or this machine of binding strap
Tool formula fixed form, assembling-disassembling structure is complicated, time and effort consuming, and easily causes the damage to battery core, and its object is to provide one
Kind unmanned aerial vehicle onboard intelligent battery bead fixed structure, realizes that unmanned machine battery can rapidly and accurately be pacified by bead fixed structure
Position is attached to, meets being accurately positioned when battery quickly loads and quickly splits out convenient, battery core will not be damaged.
The present invention is achieved through the following technical solutions：
Unmanned aerial vehicle onboard intelligent battery bead fixed structure, including the bead fixed seat of bead is provided with, the bead is consolidated
Bead introducing mechanism is provided with reservation, bead introducing mechanism being capable of and glass mobile relative to bead fixed seat when battery loads and unloads
Pearl introducing mechanism can be contacted and fixed with bead.For carrying out agricultural operation as the unmanned plane of power supply using battery,
Changing battery is most commonly seen and frequently operates, but existing machinery formula fixed form, such as bolt, buckle or colligation side
Formula, all extremely inconvenient, fixed too tight or too loose all easy generation problem, it is fixed can tightly cause very much battery into and out tired
Difficulty, it is fixed too loose and connection can be caused to loosen, trigger vibration, even result in battery packages fracture failure, and also it is this mechanical
Fixed structure is careless slightly because protruding parts itself is more, and its protruding parts will cause battery to scratch so that battery core by
Damage, and this programme is then to use bead fixed structure on the fixed structure of unmanned machine battery first, by battery wall
The upper multigroup bead introducing mechanism of installation carries out pairing use with the bead in bead fixed seat, in battery self gravitation or external force
Realize that battery is directed into luggage tears open using 360 ° of rotations of bead under promoting, bead fast and accurately can be imported into by this structure
Correct installation position, being accurately positioned when battery quickly loads can be met simultaneously and quickly split out convenient, and assembling and dissembling process
Due to being to slide in place, it will not produce and contact with battery core, so as to protect the integrality of battery core, extend service life and protection
The safety of operating personnel.
In order to carry out the positioning of battery in the circumferential so that it assembles and disassembles the face progress for being along vertical direction, so also
Circumferentially positioned plate is provided with, bead introducing mechanism is arranged on circumferentially positioned plate.Determined in the circumferential when so battery is fixed
Position, and prevent battery double swerve or rotation from causing to misplace.
By test of many times, automatic clamping function can be realized after battery insertion by finding the structure of wedge shape, so bead
Introducing mechanism preferably uses wedge-shaped bead introducing mechanism, i.e. bead introducing mechanism includes wedge shape importing plate, and wedge shape imports plate as week
Face to location-plate towards bead is recessed, and is provided with circumferentially positioned plate on the face of wedge shape importing plate and is provided with shaft shoulder positioning
Platform and the bead hole matched with bead size, while shaft shoulder positioning table is arranged on above bead hole, bead hole is arranged on wedge shape and led
Enter directly over plate and import plate with wedge shape to be connected.It is recessed and bead fixed seat imports the relative face of plate with wedge shape and is recessed groove
Bumper and absorbing shock pad is provided with groove, and bumper and absorbing shock pad is fixed on the most bottom surface of groove, bead is arranged on bead fixed seat and wedge
Shape is imported on the relative face of plate, and bead is located at below groove, and shaft shoulder positioning table is fixed in bead introducing mechanism relative to bead
Seat is inserted into groove contacting with bumper and absorbing shock pad when mobile, while the glass when shaft shoulder positioning table contacts with bumper and absorbing shock pad
Pearl is located in bead hole, is contacted by shaft shoulder positioning table with bumper and absorbing shock pad and realizes axially position, and circumferentially positioned plate is consolidated with bead
The contact of reservation side wall is realized circumferentially positioned, and bead is fixed in bead hole and realizes that battery is eventually assembled into position, and this 3 points are made simultaneously
With, realize battery fixation fastness.
The bead fixed seat that dottle pin is fixed with bumper and absorbing shock is enclosed in this programme, on unmanned plane, the structure is in fixation
While bead, also constitute a part for unmanned plane rigid support, the structure can meet battery quickly into and out,
Even a certain degree of impact can be met, for battery it is whole into and out process for, only stationary plane connects, bead
The process of importing needs certain strength, during remaining, the motion of battery is influenceed without spare part, therefore very save
Power.
Still further, after entering the segment distance of installation position one when battery bottom, lift-pull handle can be directly unclamped, electricity
Pond falls under gravity, and the bumper and absorbing shock pad in fixed seat can absorb impulsive force, and bead and wedge-shaped introducing mechanism
It can complete to be accurately positioned, the convenience that the assembling of such battery will be extremely.
In order to which bead fixed seat is fixed, several mounting holes are also provided with bead fixed seat and are used for and nobody
Machine is fixed, and ensures fixed fastness.
The present invention compared with prior art, has the following advantages and advantages：
1st, the present invention realizes the convenience and accuracy of battery assembly and disassembly operations by using wedge-shaped bead introducing mechanism,
Multipoint positioning is realized, battery assembly and disassembly run along same track, improve efficiency while will not damage battery core, and then anti-leak-stopping
Electricity, it ensure that the safety of operating personnel；
2nd, by setting the bead fixed seat with bumper and absorbing shock pad, it makes the present invention with the pairing of wedge-shaped bead introducing mechanism
With, the fastness of battery fixation is realized, while slow down impact when installing, protect the safety of battery；
3rd, the present invention uses laborsaving, is rotated using bead and combines wedge-shaped approaching face, it is only necessary to which giving very little thrust just can be automatically
It is installed in place, is lifted up just battery can quickly and securely being extracted, improves the convenience and efficiency of assembly and disassembly.
Brief description of the drawings
Accompanying drawing described herein is used for providing further understanding the embodiment of the present invention, forms one of the application
Point, do not form the restriction to the embodiment of the present invention.In the accompanying drawings：
Fig. 1 is the structural representation of battery；
Sectional view when Fig. 2 is fixing assembling；
Fig. 3 is the front view of bead introducing mechanism；
Fig. 4 is the structural representation of bead fixed seat；
Mark and corresponding parts title in accompanying drawing：
1- handles, cover on 2-, 3- bead introducing mechanisms, 4- framework pillars, 5- shock callus, 6- shells, 7- quick plugs,
8- control panels, 9- bead fixed seats, 10- bumper and absorbing shock pads, 11- beads, 12- shaft shoulder positioning tables, 13- wedge shapes import plate, 14-
Framework column face, the circumferentially positioned plates of 15-, 16- beads hole, 17- mounting holes, 18- locating faces, 19- axial locating surfaces.
Embodiment
For the object, technical solutions and advantages of the present invention are more clearly understood, with reference to embodiment and accompanying drawing, to this
Invention is described in further detail, and exemplary embodiment of the invention and its explanation are only used for explaining the present invention, do not make
For limitation of the invention.
Embodiment：
As shown in Figures 1 to 4, for agricultural plant protection unmanned plane, battery is arranged to use electricity is installed in the inner chamber of shell 6
The structures such as Chi Xin, circuit components, control chip group, plug, it uses full packaging type structure, and shell 6 is made up of carbon fiber board,
Wrap up, energy shatter-resistant, waterproof and dustproof, in order to increase the fastness of structure, be provided with below shell 6 in conjunction with elastic cotton liner
Framework made of aluminium alloy, frame roof are protruded to form framework pillar 4 made of some aluminium alloys, and shell 6 is arranged on framework
In the region that pillar 4 is formed, and the wall of shell 6 is bonded with the inwall of framework pillar 4, and bead introducing mechanism 3 is arranged on corresponding frame
On the outer wall of pillar body 4, base of frame is provided with shock callus 5, and the top of shell 6 is provided with lid 2, upper lid 2 is passed through with shell 6
Screw is fixed, and battery and other electrical parts are arranged in the seal cavity that lid 2 and shell 6 are formed, and are provided with upper lid 2 fast
Fast plug 7 and handle 1, handle 1, which is easy for operating personnel, to be held and takes, and quick plug 7 includes quick plug shell, quick plug shell
Fixed with upper lid 2, accessory power outlet and limit switch (being not drawn into figure) are provided with quick plug shell, and limit switch is set
Below accessory power outlet, accessory power outlet and limit switch are connected through upper lid 2 with battery.By increasing at quick plug 7
Add limit switch, limit switch is a flexible member, and it is when being squeezed to inside battery retraction and cell communication, extruding
Power disappearance automatic rebounding departs from the connection with battery, and when normally insertion equipment, the ledge meeting physics on relevant device touches
Send out limit switch, now could normally-open battery, realize powered operation, otherwise battery not supplying power for outside, is so avoided
Hot plugging sparking, it is moreover, spacing to open situations such as extracted by force during supplying power for outside when battery is by improper operation
Close automatic spring and form power-off, battery can be detected by the break-make of limit switch immediately, after automatic alarm and progress
Operating personnel are protected, prevent from getting an electric shock by continuous operation.
The control panel 8 being connected with battery management module is also installed on upper lid 2 simultaneously, this control panel 8 also can
It is enough directly to buy on the market, cell switch is provided with control panel 8, LED lamplight is shown and buzzer, battery can pass through
Different light status and buzzer combination, to complete different condition prompting or warning function.In battery management module
The communication module for carrying out real-time communication is provided with, communication module is also existing and can directly bought on the market, is led to
Cross battery delivery outlet with the external world to be connected, in time by data output, especially for aircraft, ground handling operator can be accurate in real time
Grasp battery status, and then more rational planning uses.
In order to realize the fixation to battery, the bead fixed seat 9 being mutually matched and bead introducing mechanism 3 are provided with, in glass
It is provided with several mounting holes 17 in pearl fixed seat 9 to be used to be fixed with unmanned plane, bead introducing mechanism 3 is arranged on circumferential fixed
On the plate 15 of position, now circumferentially positioned plate 15 is framework pillar 4, and the outside wall surface of framework pillar 4 is named as framework column face 14,
The outside wall surface of as circumferentially positioned plate 15, bead introducing mechanism 3 are arranged on framework column face 14, and bead introducing mechanism 3 includes
Wedge shape imports plate 13, and actually wedge shape imports plate 13 and is recessed for the face of circumferentially positioned plate 15 towards bead 11, circumferentially fixed
Position plate 15 is provided with the face of wedge shape importing plate 13 and is provided with shaft shoulder positioning table 12 and the bead hole 16 matched with the size of bead 11,
Shaft shoulder positioning table 12 is arranged on the top of bead hole 16, and bead hole 16 is arranged on wedge shape and imports directly over plate 13 and import plate with wedge shape
13 connections, so import under the guiding of plate 13 in wedge shape and bead 11 can be introduced into bead hole 16, middle without pause and clamping stagnation.
In order to there are enough space shaft shoulder positioning tables 12 and prevent from interfering, plate is imported in bead fixed seat 9 and wedge shape
13 relative faces are recessed groove, and groove moves and in fact in a groove through the top of bead fixed seat 9, shaft shoulder positioning table 12
Existing axially position, while bumper and absorbing shock pad 10 is also provided with a groove, and bumper and absorbing shock pad 10 is fixed on the most bottom surface of groove,
Shaft shoulder positioning table 12 is inserted into groove and bumper and absorbing shock pad when bead introducing mechanism moves relative to bead fixed seat 9
10 contacts, because bead 11 is arranged on the face relative with wedge shape importing plate 13 of bead fixed seat 9, in order to prevent that bead 11 from being delayed
Rushing beam 10 and blocking influences the contact that bead 11 imports plate 13 with wedge shape, and bead 11 will be located at below groove, be positioned in the shaft shoulder
Bead 11 is located in bead hole 16 when platform 12 contacts with bumper and absorbing shock pad 10.
When battery is fixed, bumper and absorbing shock pad 10 is named as axial locating surface 19 with the face that shaft shoulder positioning table 12 contacts, its
Realize axially position.And setting the face of bead 11 to be named as locating face 18, locating face 18 is determined with circumferential when mounted
Axially position is realized in the outside wall surface contact of position plate 15, and bead 11, which can slip into bead hole 11 under the guiding of introducing mechanism and realize, to be determined
Position, coordinate by axial locating surface, locating face coordinate and bead structure three coordinate degree of completing battery quick fixation,
Battery assembly and disassembly are run along same track, are improved efficiency while will not be damaged battery core, and then prevent from leaking electricity, and ensure that operator
The safety of member.
When carrying out installing fixed, after bead 11 slips into the approaching face of wedge shape importing plate 13, if there is less position to offset,
It is recessed because wedge shape imports plate 13 for the face of circumferentially positioned plate 15 towards bead 11, it has certain difference in height, wedge shape
The peripheral wall surfaces of approaching face four can push bead 11 to correct moving direction, be directed to bead in the moving process of bead 11
Positioned in hole 16.
Bumper and absorbing shock pad 10 and Al-alloy parts plane fit structure are employed carrying out locating face cooperation, by calculating
And experiment, suitable decrement is reserved, ensures enough combination tightnesses.Moreover, wedge shape imports the height that plate 13 is recessed, warp
Tight calculating and multiple comparison test are crossed, more lower slightly than locating face, this processing method not only ensure that bead is appropriate
Decrement, and reduce circumferentially fixed face and frictional force during relative slide, make assembling more laborsaving and convenient.
Axially position equally employs bumper and absorbing shock pad 10 and Al-alloy parts plane fit structure, by calculating and testing,
Reserved enough thickness, ensures that the impulsive force that battery decline is brought can be buffered fully.
The bead 11 that the present invention uses is national standard finished parts, the type selecting after calculating, then is adjusted through overtesting, is ensured enough
Intensity, life-span and precision, bead fixed seat 9 also constitutes the one of unmanned plane rigid support while fixed bead 11
Part.Wedge-shaped bead introducing mechanism is a part for battery frame pillar body, constitutes the framework of battery.
Bead fixed seat 9 uses the direct-connected design of non-boltization with bead 11 and bumper and absorbing shock pad 10, and assembly technology is simple,
Reliability is high, and the fixed structure of this bead formula is used on unmanned plane, is not applied only in the fixation of battery first, while can
For Quick Release medicine-chest etc. Quick-dismantling structure.
Above-described embodiment, the purpose of the present invention, technical scheme and beneficial effect are carried out further
Describe in detail, should be understood that the embodiment that the foregoing is only the present invention, be not intended to limit the present invention
Protection domain, within the spirit and principles of the invention, any modification, equivalent substitution and improvements done etc., all should include
Within protection scope of the present invention.
Claims (8)
1. unmanned aerial vehicle onboard intelligent battery bead fixed structure, it is characterised in that the bead including being provided with bead (11) is fixed
Seat (9), bead introducing mechanism (3), bead introducing mechanism (3) energy when battery loads and unloads are provided with the bead fixed seat (9)
Enough and bead introducing mechanisms (3) mobile relative to bead fixed seat (9) can be contacted and fixed with bead (11).
2. unmanned aerial vehicle onboard intelligent battery bead fixed structure according to claim 1, it is characterised in that also include circumferential
Location-plate (15), the bead introducing mechanism (3) are arranged on circumferentially positioned plate (15).
3. unmanned aerial vehicle onboard intelligent battery bead fixed structure according to claim 2, it is characterised in that the bead is led
Enter mechanism (3) and include wedge shape to import plate (13), it is circumferentially positioned plate (15) towards in the face of bead (11) that wedge shape, which imports plate (13),
Spill into, circumferentially positioned plate (15) be provided with wedge shape import plate (13) face on be provided with shaft shoulder positioning table (12) and and bead
(11) the bead hole (16) of size matching.
4. unmanned aerial vehicle onboard intelligent battery bead fixed structure according to claim 3, it is characterised in that the shaft shoulder is determined
Position platform (12) is arranged on above bead hole (16), and bead hole (16) are arranged on wedge shape and import directly over plate (13) and imported with wedge shape
Plate (13) connects.
5. unmanned aerial vehicle onboard intelligent battery bead fixed structure according to claim 3, it is characterised in that the bead is consolidated
Reservation (9) imports the relative face of plate (13) with wedge shape and is recessed groove, and shaft shoulder positioning table (12) is relative in bead introducing mechanism
It is inserted into when bead fixed seat (9) is mobile in groove.
6. unmanned aerial vehicle onboard intelligent battery bead fixed structure according to claim 5, it is characterised in that in the groove
Bumper and absorbing shock pad (10) is provided with, and bumper and absorbing shock pad (10) is fixed on the most bottom surface of groove, shaft shoulder positioning table (12) is in bead
It is inserted into groove contacting with bumper and absorbing shock pad (10) when introducing mechanism is relative to bead fixed seat (9) movement.
7. unmanned aerial vehicle onboard intelligent battery bead fixed structure according to claim 6, it is characterised in that the bead
(11) bead fixed seat (9) is arranged on to import on the relative face of plate (13) with wedge shape, and bead (11) is located at below groove, in axle
Bead (11) is located in bead hole (16) when shoulder positioning table (12) contacts with bumper and absorbing shock pad (10).
8. unmanned aerial vehicle onboard intelligent battery bead fixed structure according to claim 1, it is characterised in that the bead is consolidated
Several mounting holes (17) are provided with reservation (9).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710976207.6A CN107579186A (en) | 2017-10-19 | 2017-10-19 | Unmanned aerial vehicle onboard intelligent battery bead fixed structure |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710976207.6A CN107579186A (en) | 2017-10-19 | 2017-10-19 | Unmanned aerial vehicle onboard intelligent battery bead fixed structure |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN107579186A true CN107579186A (en) | 2018-01-12 |
Family
ID=61036551
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201710976207.6A Pending CN107579186A (en) | 2017-10-19 | 2017-10-19 | Unmanned aerial vehicle onboard intelligent battery bead fixed structure |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN107579186A (en) |
Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2005322894A (en) * | 2004-04-05 | 2005-11-17 | Iguchi Kiko Seisakusho:Kk | Positioning table for substrate, positioning equipment for the substrate, and positioning method of the substrate |
| DE102007027326A1 (en) * | 2007-06-14 | 2008-12-18 | Diehl Bgt Defence Gmbh & Co. Kg | Gas collecting device for collecting gaseous sample for analysis of sample, has gas collecting module with diaphragm pump that is effectively connected with controller and power supply e.g. battery, of flying apparatus i.e. micro drone |
| CN205113940U (en) * | 2015-10-08 | 2016-03-30 | 贵定县富茗茶业有限公司 | Can change tealeaves box of volume |
| CN205203401U (en) * | 2015-12-15 | 2016-05-04 | 杭州米为科技有限公司 | Protection architecture of unmanned aerial vehicle battery |
| CN205944189U (en) * | 2016-08-17 | 2017-02-08 | 深圳零度智能飞行器有限公司 | Quick detach formula battery lock detains structure and unmanned aerial vehicle |
| CN207233838U (en) * | 2017-10-19 | 2018-04-13 | 四川雷神空天科技有限公司 | Unmanned aerial vehicle onboard intelligent battery bead fixed structure |
-
2017
- 2017-10-19 CN CN201710976207.6A patent/CN107579186A/en active Pending
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2005322894A (en) * | 2004-04-05 | 2005-11-17 | Iguchi Kiko Seisakusho:Kk | Positioning table for substrate, positioning equipment for the substrate, and positioning method of the substrate |
| DE102007027326A1 (en) * | 2007-06-14 | 2008-12-18 | Diehl Bgt Defence Gmbh & Co. Kg | Gas collecting device for collecting gaseous sample for analysis of sample, has gas collecting module with diaphragm pump that is effectively connected with controller and power supply e.g. battery, of flying apparatus i.e. micro drone |
| CN205113940U (en) * | 2015-10-08 | 2016-03-30 | 贵定县富茗茶业有限公司 | Can change tealeaves box of volume |
| CN205203401U (en) * | 2015-12-15 | 2016-05-04 | 杭州米为科技有限公司 | Protection architecture of unmanned aerial vehicle battery |
| CN205944189U (en) * | 2016-08-17 | 2017-02-08 | 深圳零度智能飞行器有限公司 | Quick detach formula battery lock detains structure and unmanned aerial vehicle |
| CN207233838U (en) * | 2017-10-19 | 2018-04-13 | 四川雷神空天科技有限公司 | Unmanned aerial vehicle onboard intelligent battery bead fixed structure |
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