CN205998147U - Battery and aircraft - Google Patents
Battery and aircraft Download PDFInfo
- Publication number
- CN205998147U CN205998147U CN201620836604.4U CN201620836604U CN205998147U CN 205998147 U CN205998147 U CN 205998147U CN 201620836604 U CN201620836604 U CN 201620836604U CN 205998147 U CN205998147 U CN 205998147U
- Authority
- CN
- China
- Prior art keywords
- battery
- aircraft
- buckle
- pedestal
- slide block
- 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.)
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- NJPPVKZQTLUDBO-UHFFFAOYSA-N novaluron Chemical compound C1=C(Cl)C(OC(F)(F)C(OC(F)(F)F)F)=CC=C1NC(=O)NC(=O)C1=C(F)C=CC=C1F NJPPVKZQTLUDBO-UHFFFAOYSA-N 0.000 claims abstract description 39
- 230000005611 electricity Effects 0.000 claims description 5
- 239000007787 solid Substances 0.000 claims 1
- 238000010586 diagram Methods 0.000 description 4
- 230000000694 effects Effects 0.000 description 4
- RZVHIXYEVGDQDX-UHFFFAOYSA-N 9,10-anthraquinone Chemical compound C1=CC=C2C(=O)C3=CC=CC=C3C(=O)C2=C1 RZVHIXYEVGDQDX-UHFFFAOYSA-N 0.000 description 2
- 239000000284 extract Substances 0.000 description 2
- 238000009434 installation Methods 0.000 description 2
- 238000010009 beating Methods 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000003139 buffering effect Effects 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 230000002787 reinforcement Effects 0.000 description 1
- 239000004576 sand Substances 0.000 description 1
Classifications
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01M—PROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSION OF CHEMICAL ENERGY INTO ELECTRICAL ENERGY
- H01M50/00—Constructional details or processes of manufacture of the non-active parts of electrochemical cells other than fuel cells, e.g. hybrid cells
- H01M50/20—Mountings; Secondary casings or frames; Racks, modules or packs; Suspension devices; Shock absorbers; Transport or carrying devices; Holders
- H01M50/249—Mountings; Secondary casings or frames; Racks, modules or packs; Suspension devices; Shock absorbers; Transport or carrying devices; Holders specially adapted for aircraft or vehicles, e.g. cars or trains
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C39/00—Aircraft not otherwise provided for
- B64C39/02—Aircraft not otherwise provided for characterised by special use
-
- 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
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Chemical Kinetics & Catalysis (AREA)
- Electrochemistry (AREA)
- General Chemical & Material Sciences (AREA)
- Battery Mounting, Suspending (AREA)
Abstract
The utility model discloses a kind of battery and aircraft, described battery includes battery unit, pedestal, buckle body and buckle slide block, described battery unit is connected with the first side of described pedestal, described buckle body includes transverse arm and the side arm being connected with described transverse arm, described side arm and described pedestal pivot joint, described side arm is provided with the clamping part that can be at open position or latched position, and when described buckle slide block acts on described transverse arm, described clamping part is in an open position.Described battery and aircraft, using lever principle, coordinate realization to snap connection by the clamping part of buckle body and the snap-fit being arranged in battery settling groove, be convenient to mount and dismount, be easy to the replacement of aircraft battery, and consolidate with the combination of aircraft, it is difficult in flight course to fall.
Description
Technical field
This utility model is related to vehicle technology field, more particularly, to a kind of battery and aircraft.
Background technology
Aircraft can fly by user's control and in the air, and user can control the flight side of aircraft as needed
To aircraft will realize normal work, needs to couple together battery it is ensured that battery is powered for aircraft with aircraft.Tradition
, battery is to be fixed by way of bandage on board the aircraft, needs to change or safeguards inconvenient during battery.And, adopt
Fixed with bandage type, built on the sand, during aircraft flight, battery easily skids off and falls for the combination of battery and aircraft.
Content of the invention
Based on this it is necessary to provide a kind of battery and aircraft, this battery is convenient to mount and dismount and the combination of aircraft consolidates；
The battery of this aircraft is convenient to mount and dismount, it is firm to install, and is difficult to fall in flight course.
Its technical scheme is as follows：
A kind of battery, including battery unit, pedestal, buckle body and buckle slide block, described battery unit and described base
First side of seat connects, and described buckle body includes transverse arm and the side arm being connected with described transverse arm, described side arm and described pedestal
Pivot joint, described side arm is provided with the clamping part that can be at open position or latched position, when described buckle slide block act on described
During transverse arm, described clamping part is in an open position.
Wherein in an embodiment, described battery also includes clamping support, and described clamping support is arranged on described pedestal
On, described side arm and described clamping support pivot joint, so that described side arm rotates with respect to described clamping support.
Wherein in an embodiment, described battery also includes at least one resetting-mechanism, one end of described resetting-mechanism
It is connected with described transverse arm, the other end of described resetting-mechanism is connected with described pedestal.
Wherein in an embodiment, described buckle slide block includes peristome, and described peristome is in downward opening U-shaped knot
Structure, described peristome can transverse arm described in accommodating portion.
Wherein in an embodiment, the second side of described pedestal is provided with chute, so that described buckle slide block energy
Enough slide along direction defined in described chute.
Wherein in an embodiment, described battery unit includes accommodating the battery compartment of battery core, and described battery compartment outer wall sets
There is fixing hidden discount, coordinate and form interlocking for the hidden discount auxiliary section in the battery settling groove with aircraft.
Wherein in an embodiment, described battery compartment includes storehouse under storehouse and battery on the battery cooperating, described
On battery, the both sides in storehouse are equipped with described fixing hidden discount, and under described battery, the both sides in storehouse are equipped with described fixing hidden discount.
Wherein in an embodiment, under described battery, storehouse is provided with plug and buckles, for the attaching plug with aircraft even
Connect.
Wherein in an embodiment, described battery also includes cell rear cover and bonnet handle, and described bonnet handle is installed
On described cell rear cover, described cell rear cover is located at the second side of institute's pedestal and is connected with described pedestal, and described buckle is slided
The part of block stretches out described cell rear cover.
Wherein in an embodiment, described battery also includes buckle button, and described buckle button is arranged on described card
Button upper end of slide block, and partial denudation is outside described cell rear cover.
A kind of aircraft, including battery described above, aircraft body and flight control system, described aircraft body includes
There are the motor that propeller is connected and the battery settling groove for installing described battery with propeller, on described battery settling groove
It is provided with the snap-fit with described clamping part interlock fit, so that described battery is fixedly mounted on described battery settling groove, when
Described clamping part is in an open position, and described battery is in detachable state, when described clamping part is in the locked position, described electricity
Pond is in non-dismountable state.
Wherein in an embodiment, it is provided with described battery settling groove and the fixing hidden discount interlock fit of described battery
Hidden discount auxiliary section.
Wherein in an embodiment, described aircraft body also includes buckleing the electricity of interlock fit with the plug of described battery
Source plug.
The beneficial effects of the utility model are：
Above-mentioned battery, may be installed in the battery settling groove of aircraft, by the clamping part of buckle body be arranged on electricity
Snap-fit cooperation realization in the mounting groove of pond snaps connection.When carrying out disassembling section, by pressing down on buckle slide block, can
Promote buckle slide block to act on the transverse arm of buckle body, so that transverse arm is moved downward, and the side arm of buckle body is rotated even with pedestal
Connect, side arm can rotate along pedestal, so that the clamping part on side arm is lifted up by lever principle in an open position, buckle
Portion and the snap-fit unblock of aircraft, outwards extract pedestal and can achieve and aircraft disengaging；Likewise, carrying out installing behaviour
When making, by pressing buckle slide block, battery is pushed in aircraft, then decontrol buckle slide block, clamping part and snap-fit
Interlocking is fixed, you can realize the connection with aircraft.Described battery, using lever principle, real with aircraft by buckle body
Existing buckle-type connects, and is convenient to mount and dismount, is easy to the replacement of aircraft battery, and consolidates with the combination of aircraft.
Described aircraft, including battery described above, possesses the technique effect of described battery, being clasped of aircraft
Portion can realize interlock fit with the clamping part of buckle body, and battery is convenient to mount and dismount, it is firm to install, and is difficult to fall in flight course
Fall.
Brief description
Fig. 1 is the structural representation one of the battery described in this utility model embodiment；
Fig. 2 is the configuration schematic diagram of the battery described in this utility model embodiment；
Fig. 3 is the inner mounting structure schematic diagram of the battery described in this utility model embodiment；
Fig. 4 is the mplifying structure schematic diagram at A in Fig. 3；
Fig. 5 is the structural representation two of the battery described in this utility model embodiment；
Fig. 6 is the mounting structure schematic diagram of the battery described in this utility model embodiment.
Description of reference numerals：
10th, battery unit, 110, battery core, 120, battery compartment, 122, storehouse on battery, 124, storehouse under battery, 130, fixing dark
Button, 140, plug button, 20, pedestal, 210, through hole, 220, chute, 30, buckle body, 310, transverse arm, 320, side arm, 330, card
Buckle, 40, buckle slide block, 50, clamping support, 60, cell rear cover, 70, bonnet handle, 80, buckle button, 1, battery installs
Groove, 2, snap-fit.
Specific embodiment
Below embodiment of the present utility model is described in detail：
As shown in Figure 1, Figure 2, Figure 3 shows, a kind of battery, slides including battery unit 10, pedestal 20, buckle body 30 and buckle
Block 40, described battery unit 10 is connected with the first side of described pedestal 20, described buckle body 30 include transverse arm 310 and with institute
State the side arm 320 of transverse arm 310 connection, described side arm 320 and the pivot joint of described pedestal 20, described side arm 320 is provided with and can be at beating
The clamping part 330 of open position or latched position, when described buckle slide block 40 acts on described transverse arm 310, described clamping part 330
In an open position.In the present embodiment, described pedestal 20 includes pedestal mounting plate, the first side of described pedestal mounting plate and battery
Unit 10 connects, and the second side of described pedestal mounting plate is provided with convex closure, and described pedestal mounting plate two ends in transverse direction are provided with
Through hole 210, the both sides of described transverse arm 310 are equipped with side arm 320, and described clamping part 330 is located at described side arm 320 away from transverse arm
310 side, described buckle body 30 is stretched out by described through hole 210 across described convex closure, described side arm 320, makes described card
Buckle 330 stretches out the first side of pedestal 20.
Above-mentioned battery, may be installed in the battery settling groove 1 of aircraft, by the clamping part 330 of buckle body 30 with set
Put the cooperation realization of the snap-fit 2 in battery settling groove 1 to snap connection.When carrying out disassembling section, by pressing down on card
Button slide block 40, can promote buckle slide block 40 to act on the transverse arm 310 of buckle body 30, so that transverse arm 310 is moved downward, and buckle is originally
The side arm 320 of body 30 is rotated with pedestal 20 and is connected, and side arm 320 can rotate along pedestal 20, is made on side arm 320 by lever principle
Clamping part 330 be lifted up in an open position, clamping part 330 is unlocked with the snap-fit 2 of aircraft, outwards extracts base
Seat 20 be can achieve and departed from aircraft；Likewise, when carrying out installation operation, making clamping part 330 by pressing buckle slide block 40
In an open position, battery is pushed in aircraft, then decontrols buckle slide block 40, clamping part 330 is in the locked position and card
The interlocking of button auxiliary section 2 is fixed, you can realize the connection with aircraft.Described battery, using lever principle, by buckle body 30
Realize buckle-type with aircraft to be connected, be convenient to mount and dismount, be easy to the replacement of aircraft battery, and consolidate with the combination of aircraft.
In the present embodiment, described battery also includes clamping support 50, and described clamping support 50 is arranged on described pedestal 20,
Described side arm 320 and the pivot joint of described clamping support 50, so that described side arm 320 rotates with respect to described clamping support 50.Adopt
With said structure, buckle body 30 is passed through clamping support 50 and realizes being connected with the rotation of pedestal 20, connects reliable, conveniently.Buckle
The two ends of support 50 can provide, for the side arm of buckle body 30, the fulcrum rotating, and buckle body 30 can be with respect to clamping support 50
Rotation, and then realize opening or lock operation using lever principle.In the present embodiment, described battery also includes at least one reset
Mechanism's (not shown), one end of described resetting-mechanism is connected with described transverse arm 310, the other end of described resetting-mechanism and institute
State pedestal 20 to connect.By arranging resetting-mechanism, can prevent buckle body 30 during aircraft flight from rocking and clamping part occurs
330 phenomenons getting loose, play reinforcement, buffering and the effect resetting, increase the lock of buckle body 30 further to buckle body 30
Tight ability.In the present embodiment, described resetting-mechanism can be spring, flexure strip etc., and resetting-mechanism is two, is separately positioned on card
The both sides of button slide block 40.
In the present embodiment, described buckle slide block 40 includes peristome, and described peristome is in downward opening U-shape structure, institute
Stating peristome can transverse arm 310 described in accommodating portion.By arranging the peristome of U-shaped structure, the peristome energy of buckle slide block 40
Transverse arm 310 described in enough accommodating portions, and then can reliably promote the transverse arm 310 of buckle body 30 downward by buckle slide block 40
Mobile.The second side of described pedestal 20 is provided with chute 220, so that described buckle slide block 40 can be along described chute 220
Slide in defined direction.In the present embodiment, direction defined in described chute 220 is to instigate transverse arm 310 to move up and down, and then
Make clamping part 330 realize open or locking state direction.By arranging chute 220, described buckle slide block 40 can be relatively
Move up and down in pedestal 20, structure is simple.
As shown in Figure 2, Figure 3, Figure 4, described battery unit 10 includes accommodating the battery compartment 120 of battery core 110, described battery compartment
120 outer walls are provided with fixing hidden discount 130, coordinate and form interlocking for the hidden discount auxiliary section in the battery settling groove 1 with aircraft.
By fixing hidden discount 130 is arranged on battery compartment 120, after the battery of the present embodiment inserts battery settling groove 1 of aircraft, Gu
Determine hidden discount 130 and can realize interlock fit with the hidden discount auxiliary section in battery settling groove 1, thus fixing described battery further,
The battery of the present embodiment and aircraft fix stably, difficult for drop-off.In the present embodiment, described battery compartment 120 includes phase interworking
Storehouse 124 under storehouse 122 and battery on the battery closing, on described battery, the both sides in storehouse 122 are equipped with described fixing hidden discount 130, described
Under battery, the both sides in storehouse 124 are equipped with described fixing hidden discount 130.Using said structure, the battery of the present embodiment is arranged on battery
When in mounting groove 1, fixing hidden discount 130 can be in whole circumferential direction and hidden discount auxiliary section interlock fit, fix stably, reliability.
In the present embodiment, as shown in Fig. 2, Fig. 5, under described battery, storehouse 124 is provided with plug and buckles 140, inserts for the power supply with aircraft
Head connects.By setting plug button 140, after the battery of the present embodiment is installed on board the aircraft, this plug button 140 and aircraft
Attaching plug connects, and can further function as the effect of fixing described battery.
In the present embodiment, as shown in Figure 1 and Figure 2, described battery also includes cell rear cover 60 and bonnet handle 70, described after
Lid handle 70 is arranged on described cell rear cover 60, described cell rear cover 60 be located at institute's pedestal 20 the second side and with described base
Seat 20 connection, the part of described buckle slide block 40 stretches out described cell rear cover 60.By arranging cell rear cover 60 and bonnet handle
70, the battery of the present embodiment is actual when being installed or removed, and can be operated by holding bonnet handle 70, structure is attractive in appearance,
Easy to operate.In the present embodiment, described battery also includes buckle button 80, and described buckle button is arranged on described buckle and slides
Block 40 upper end, and partial denudation is outside described cell rear cover 60.Pressed by arranging buckle in the upper end of described buckle slide block 40
Button 80, is easy to press buckle slide block 40, meets human engineering, easy to operate.
Battery described in the present embodiment, realizes buckle-type by buckle body 30 and aircraft and is connected, and so that battery is fixed on
In aircraft, it is convenient to mount and dismount, is easy to the replacement of aircraft battery.Buckle body 30 is realized opening or locking using lever principle,
Battery is consolidated with the combination of aircraft.By using fixing hidden discount 130 and plug button 140, can self-contained battery further, make battery
More firm with the combination of aircraft.The battery of the present embodiment, is convenient to mount and dismount, is easy to the replacement of aircraft battery, with aircraft
Combination consolidate, difficult for drop-off during aircraft flight.
As shown in fig. 6, a kind of aircraft, including battery described above, aircraft body and flight control system, described flight
Device main body includes motor and the battery settling groove 1 for installing described battery that propeller is connected, described electricity with propeller
Pond mounting groove 1 is provided with the snap-fit 2 with described clamping part 330 interlock fit, so that described battery is fixedly mounted on described
On battery settling groove 1, when described clamping part 330 is in an open position, described battery is in detachable state, when described clamping part
330 are in the locked position, and described battery is in non-dismountable state.For the ease of schematically illustrate, in Fig. 6, aircraft body is hidden
Hide, only illustrate the structure of battery settling groove 1.Described aircraft, including battery described above, possesses the skill of described battery
Art effect, the battery settling groove 1 of aircraft is used for installing described battery, and the snap-fit 2 of aircraft can be with clamping part 330
Realize buckle-type connected mode.Aircraft described in the present embodiment, is assembled with battery by arranging battery settling groove 1, interior
Portion space is fully used, and battery is convenient to mount and dismount, installs firm, is difficult to fall in flight course.
In the present embodiment, in described battery settling groove 1, it is provided with the hidden discount with fixing hidden discount 130 interlock fit of described battery
Auxiliary section.When described battery is arranged in battery settling groove 1, the hidden discount auxiliary section of described aircraft can also with battery on consolidate
Determine hidden discount 130 to lock further, to the installation reliability of battery, fix stably.Further, described aircraft body is also wrapped
Include the attaching plug buckleing interlock fit with the plug of described battery.The attaching plug of aircraft can buckle 140 with the plug of battery
Lock further, to battery fix stably, during this aircraft flight, battery is fixing reliable, is difficult to fall.
Each technical characteristic of embodiment described above can arbitrarily be combined, for making description succinct, not to above-mentioned reality
The all possible combination of each technical characteristic applied in example is all described, as long as however, the combination of these technical characteristics is not deposited
In contradiction, all it is considered to be the scope of this specification record.
Embodiment described above only have expressed several embodiments of the present utility model, and its description is more concrete and detailed,
But therefore can not be interpreted as the restriction to utility model patent scope.It should be pointed out that the common skill for this area
For art personnel, without departing from the concept of the premise utility, some deformation can also be made and improve, these broadly fall into
Protection domain of the present utility model.Therefore, the protection domain of this utility model patent should be defined by claims.
Claims (13)
1. a kind of battery is it is characterised in that include battery unit, pedestal, buckle body and buckle slide block, described battery unit
Be connected with the first side of described pedestal, described buckle body includes transverse arm and the side arm being connected with described transverse arm, described side arm with
Described pedestal pivot joint, described side arm is provided with the clamping part that can be at open position or latched position, when described buckle slide block is made
During for described transverse arm, described clamping part is in an open position.
2. it is characterised in that also including clamping support, described clamping support is arranged on institute to battery according to claim 1
State on pedestal, described side arm and described clamping support pivot joint, so that described side arm rotates with respect to described clamping support.
3. battery according to claim 1 is it is characterised in that also include at least one resetting-mechanism, described resetting-mechanism
One end be connected with described transverse arm, the other end of described resetting-mechanism is connected with described pedestal.
4. it is characterised in that described buckle slide block includes peristome, described peristome is in battery according to claim 1
Downward opening U-shape structure, described peristome can transverse arm described in accommodating portion.
5. battery according to claim 1 is it is characterised in that the second side of described pedestal is provided with chute, so that
Described buckle slide block can slide along direction defined in described chute.
6. battery according to claim 1 is it is characterised in that described battery unit includes accommodating the battery compartment of battery core, institute
State battery compartment outer wall and be provided with fixing hidden discount, coordinate for the hidden discount auxiliary section in the battery settling groove with aircraft and formed mutually
Lock.
7. battery according to claim 6 it is characterised in that described battery compartment include on the battery cooperating storehouse and
Storehouse under battery, on described battery, the both sides in storehouse are equipped with described fixing hidden discount, under described battery the both sides in storehouse be equipped with described solid
Determine hidden discount.
8. battery according to claim 7 it is characterised in that under described battery storehouse be provided with plug buckle, for flight
The attaching plug of device connects.
9. the battery according to any one of claim 1-8 is it is characterised in that also include cell rear cover and bonnet handle, institute
State bonnet handle to be arranged on described cell rear cover, described cell rear cover is located at the second side of institute's pedestal and is connected with described pedestal
Connect, the part of described buckle slide block stretches out described cell rear cover.
10. it is characterised in that also including buckle button, described buckle button is arranged on battery according to claim 9
Described buckle slide block upper end, and partial denudation is outside described cell rear cover.
A kind of 11. aircraft it is characterised in that include any one of claim 1-10 described in battery, aircraft body and fly
Control system, described aircraft body includes motor and the electricity for installing described battery that propeller is connected with propeller
Pond mounting groove, described battery settling groove is provided with the snap-fit with described clamping part interlock fit, so that described battery is fixed
It is arranged on described battery settling groove, when described clamping part is in an open position, described battery is in detachable state, when described
Clamping part is in the locked position, and described battery is in non-dismountable state.
12. aircraft according to claim 11 are it is characterised in that be provided with described battery settling groove and described battery
The hidden discount auxiliary section of fixing hidden discount interlock fit.
13. aircraft according to claim 11 are it is characterised in that described aircraft body also includes and described battery
The attaching plug of plug button interlock fit.
Priority Applications (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620836604.4U CN205998147U (en) | 2016-08-01 | 2016-08-01 | Battery and aircraft |
| PCT/CN2017/092791 WO2018024086A1 (en) | 2016-08-01 | 2017-07-13 | Battery and aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620836604.4U CN205998147U (en) | 2016-08-01 | 2016-08-01 | Battery and aircraft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205998147U true CN205998147U (en) | 2017-03-08 |
Family
ID=58200125
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201620836604.4U Active CN205998147U (en) | 2016-08-01 | 2016-08-01 | Battery and aircraft |
Country Status (2)
| Country | Link |
|---|---|
| CN (1) | CN205998147U (en) |
| WO (1) | WO2018024086A1 (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2018024086A1 (en) * | 2016-08-01 | 2018-02-08 | 亿航智能设备（广州）有限公司 | Battery and aircraft |
| CN111017230A (en) * | 2019-11-28 | 2020-04-17 | 成都智巡科技有限责任公司 | Novel unmanned aerial vehicle intelligent battery assembly structure |
Families Citing this family (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110155312B (en) * | 2019-05-13 | 2024-04-09 | 之江实验室 | Battery compartment of multi-rotor manned aircraft and manned aircraft comprising battery compartment |
| CN114602192B (en) * | 2022-04-02 | 2022-12-27 | 深圳市昱晟通讯设备有限公司 | Take aircraft of integral type installation element |
Family Cites Families (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US9586684B2 (en) * | 2014-02-27 | 2017-03-07 | David W. Carroll | Rotary propeller drone with integrated power storage |
| CN204223172U (en) * | 2014-10-27 | 2015-03-25 | 广州极飞电子科技有限公司 | Rotor craft battery fastening structure |
| CN204279915U (en) * | 2014-10-31 | 2015-04-22 | 深圳一电科技有限公司 | Rotor craft |
| CN205194757U (en) * | 2015-11-27 | 2016-04-27 | 深圳飞马机器人科技有限公司 | Unmanned aerial vehicle is with intelligent battery fast -assembling module |
| CN205376594U (en) * | 2015-12-17 | 2016-07-06 | 深圳曼塔智能科技有限公司 | Unmanned aerial vehicle battery lock decides structure, unmanned aerial vehicle battery pack and unmanned aerial vehicle |
| CN205998147U (en) * | 2016-08-01 | 2017-03-08 | 亿航智能设备（广州）有限公司 | Battery and aircraft |
-
2016
- 2016-08-01 CN CN201620836604.4U patent/CN205998147U/en active Active
-
2017
- 2017-07-13 WO PCT/CN2017/092791 patent/WO2018024086A1/en active Application Filing
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2018024086A1 (en) * | 2016-08-01 | 2018-02-08 | 亿航智能设备（广州）有限公司 | Battery and aircraft |
| CN111017230A (en) * | 2019-11-28 | 2020-04-17 | 成都智巡科技有限责任公司 | Novel unmanned aerial vehicle intelligent battery assembly structure |
Also Published As
| Publication number | Publication date |
|---|---|
| WO2018024086A1 (en) | 2018-02-08 |
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