CN207773491U - Unmanned plane - Google Patents
Unmanned plane Download PDFInfo
- Publication number
- CN207773491U CN207773491U CN201820028597.4U CN201820028597U CN207773491U CN 207773491 U CN207773491 U CN 207773491U CN 201820028597 U CN201820028597 U CN 201820028597U CN 207773491 U CN207773491 U CN 207773491U
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- battery
- unmanned plane
- main body
- accommodating chamber
- frame main
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- 230000013011 mating Effects 0.000 claims description 8
- 230000000694 effects Effects 0.000 claims description 7
- 230000004308 accommodation Effects 0.000 claims description 3
- 238000000465 moulding Methods 0.000 claims 1
- 230000006978 adaptation Effects 0.000 description 4
- 230000005611 electricity Effects 0.000 description 4
- 238000000034 method Methods 0.000 description 4
- 238000010586 diagram Methods 0.000 description 3
- 238000005516 engineering process Methods 0.000 description 2
- 238000009434 installation Methods 0.000 description 2
- 238000007796 conventional method Methods 0.000 description 1
- 230000007812 deficiency Effects 0.000 description 1
- 238000013461 design Methods 0.000 description 1
- 238000011161 development Methods 0.000 description 1
- 239000000284 extract Substances 0.000 description 1
- 238000007689 inspection Methods 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 238000013507 mapping Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000003825 pressing Methods 0.000 description 1
- 230000009466 transformation Effects 0.000 description 1
- 230000000007 visual effect Effects 0.000 description 1
Classifications
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- 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
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U20/00—Constructional aspects of UAVs
- B64U20/70—Constructional aspects of the UAV body
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U20/00—Constructional aspects of UAVs
- B64U20/80—Arrangement of on-board electronics, e.g. avionics systems or wiring
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U50/00—Propulsion; Power supply
- B64U50/30—Supply or distribution of electrical power
- B64U50/39—Battery swapping
-
- 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
- H01M50/202—Casings or frames around the primary casing of a single cell or a single battery
-
- 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
- H01M50/262—Mountings; Secondary casings or frames; Racks, modules or packs; Suspension devices; Shock absorbers; Transport or carrying devices; Holders with fastening means, e.g. locks
-
- 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)
- Chemical & Material Sciences (AREA)
- Chemical Kinetics & Catalysis (AREA)
- Electrochemistry (AREA)
- General Chemical & Material Sciences (AREA)
- Aviation & Aerospace Engineering (AREA)
- Remote Sensing (AREA)
- Mechanical Engineering (AREA)
- Microelectronics & Electronic Packaging (AREA)
- Combustion & Propulsion (AREA)
- Battery Mounting, Suspending (AREA)
Abstract
A kind of unmanned plane, the unmanned plane include：Frame main body and battery, the frame main body includes battery accommodating chamber, the elastic body in the battery accommodating chamber and the limiting section being set on the elastic body for housing the battery, and the battery is equipped with the fitting for lock coordinated with the limiting section；Wherein, when the battery is assemblied in the battery accommodating chamber, the limiting section is with fitting for lock cooperation locking to limit the movement of the battery.In the unmanned plane of the utility model, elastic body and limiting section are equipped in the battery accommodating chamber of frame main body, and the fitting for lock coordinated with limiting section is equipped on battery, when battery assembles frame main body, user only needs, by the way that battery to be inserted into battery accommodating chamber, to lock by the fitting for lock and limiting section cooperation at this time, it can be ensured that battery lock is in battery accommodating chamber, mode of operation is simple and direct, to improve the usage experience of user.
Description
Technical field
The utility model is related to air vehicle technique field more particularly to a kind of unmanned planes improving battery fixed form.
Background technology
With the development of unmanned air vehicle technique, among unmanned plane becomes increasingly widespread the production and living applied to people, such as
The numerous areas such as electric inspection process, ground mapping, traffic control security protection, advertisement celebration.The flight of unmanned plane at present substantially passes through electricity
Pond provides energy, however the energy that battery can provide is limited, in battery capacity deficiency, needs to replace electricity for unmanned plane
Pond, so that the sustainable continuation of the journey of unmanned plane.In existing unmanned plane, when replacing battery, need to be arranged on battery with hand-held pressing
Elastic element or press with finger the elastic element being arranged on the fuselage of unmanned plane so as to be unlocked with battery slave, behaviour
Make relatively complicated, influence user experience, in addition, elastic element is arranged on battery either fuselage influences the outer of battery or fuselage
It sees.
Utility model content
In view of this, the utility model proposes a kind of unmanned planes improving battery fixed form to be asked with solving above-mentioned technology
Topic.
In order to achieve the above objectives, technical solution used by the utility model is：
Embodiment according to the present utility model provides a kind of unmanned plane, including：Frame main body and battery, the machine
Frame body includes for housing the battery accommodating chamber of the battery, the elastic body in the battery accommodating chamber and setting
Limiting section on the elastic body, the battery are equipped with the fitting for lock coordinated with the limiting section；
Wherein, when the battery is assemblied in the battery accommodating chamber, the cooperation of the limiting section and fitting for lock lock with
Limit the movement of the battery.
Further, the limiting section is through-hole or groove, and the fitting for lock is protrusion.
Further, the limiting section is protrusion, and the fitting for lock is through-hole or groove.
Further, the protrusion include for the battery enter the battery accommodating chamber in the first guide surface and
By the second guide surface of battery accommodating chamber described in the battery removal.
Further, the limiting section include be adapted to first guide surface first guiding mating surface and with institute
State the second guiding mating surface of the second guide surface adaptation.
Further, the frame main body further includes horn and the mounting portion for being set to the horn free end, described
Mounting portion is used to be installed as the power plant that the unmanned plane provides flying power.
Further, the frame main body is integrally formed setting.
Further, the battery further includes being set to the battery main body for applying the grip part of external force.
Further, the frame main body further includes the lid for closing the battery accommodating chamber；Wherein, when the electricity
After pond is assemblied in the battery accommodating chamber, there is activity spacing between the battery and the lid.
Further, the unmanned plane further includes the upper shell and lower housing for being assemblied in the frame main body；Wherein, described
The function of the unmanned plane is respectively constituted between upper shell and the frame main body, between the lower housing and the frame main body
The accommodation space of module.
The technical solution that the embodiments of the present invention provide can include the following benefits：The utility model nobody
In machine, elastic body and limiting section are equipped in the battery accommodating chamber of frame main body, and be equipped on battery and match with limiting section
The fitting for lock of conjunction, when battery assembles frame main body, user only needs, by the way that battery to be inserted into battery accommodating chamber, at this time to lead to
It crosses the fitting for lock to lock with limiting section cooperation, it can be ensured that for battery lock in battery accommodating chamber, mode of operation is simple and direct, to carry
The usage experience of high user.
It should be understood that above general description and following detailed description is only exemplary and explanatory, not
The utility model can be limited.
Description of the drawings
Fig. 1 is a kind of overall structure diagram of unmanned plane shown in one exemplary embodiment of the utility model；
Fig. 2 is a kind of schematic cross-section of unmanned plane shown in one exemplary embodiment of the utility model；
Fig. 3 is the enlarged schematic partial view in Fig. 2；
Fig. 4 is a kind of structural schematic diagram of frame main body shown in one exemplary embodiment of the utility model；
Fig. 5 is a kind of enlarged schematic partial view of frame main body shown in one exemplary embodiment of the utility model；
Fig. 6 is a kind of structural schematic diagram of battery shown in one exemplary embodiment of the utility model；
Fig. 7 is a kind of side schematic view of battery shown in one exemplary embodiment of the utility model；
Fig. 8 is the structural representation that battery is assembled in a kind of frame main body shown in one exemplary embodiment of the utility model
Figure；
Fig. 9 is the structural representation that the battery shown in one exemplary embodiment of the utility model is removed from frame main body
Figure.
Specific implementation mode
The utility model is described in detail below with reference to specific implementation mode shown in the drawings.But these embodiment party
Formula is not intended to limit the utility model, structure that those skilled in the art are made according to these embodiments, method or
Transformation functionally is all contained in the scope of protection of the utility model.
It is the purpose only merely for description specific embodiment in the term that the utility model uses, is not intended to be limiting this reality
With novel.In the "an" of the utility model and singulative used in the attached claims, " described " and "the"
It is intended to include most forms, unless context clearly shows that other meanings.It is also understood that term used herein " and/
Or " refer to and include one or more associated list items purposes any or all may combine.
Below in conjunction with the accompanying drawings, it elaborates to some embodiments of the utility model, in the absence of conflict, under
Feature in the embodiment and embodiment stated can be combined with each other.
As shown in Figures 1 to 4, the unmanned plane 100 of the utility model embodiment including frame main body 10 and is assemblied in machine
The battery 20 of frame body 10, the frame main body 10 include the battery accommodating chamber 11 for set battery 20.In the present embodiment, the machine
Frame body 10 further includes the elastic body 12 being located in battery accommodating chamber 11 and the limiting section being set on elastic body 12
13, which is equipped with the fitting for lock 22 coordinated with limiting section 13, so that battery 20 can be locked in battery accommodating chamber 11.
Wherein, as shown in Fig. 2 combinations Fig. 8, battery 20 can be assembled in battery accommodating chamber 11 under the effect of external force,
When battery 20 is assemblied in battery accommodating chamber 11, limiting section 13 is locked with the cooperation of fitting for lock 22 to limit the movement of battery 20,
That is the battery 20 realization is assemblied in frame main body 10, while battery 20 and the Implement of Function Module that is arranged in frame main body 10
Electrical connection；As shown in Fig. 5 combinations Fig. 9, when battery 20 releases the locking of limiting section 13 and fitting for lock 22 under the effect of external force
Battery 20 is removed battery accommodating chamber 11, to stop being that unmanned plane 100 is powered.
In the present embodiment, using the resilient property of the elastic body 12 in frame main body 10, can meet limiting section 13 with
Fitting for lock 22 is locked and is unlocked under the resilient engagement of elastic body 12, such that the fixed form of battery 20 and dismounting
Mode is more convenient, in this way, may not need on the fuselage or battery 20 of unmanned plane 100 be arranged elastic element with
The locking and unlock for realizing battery 20 and fuselage, improve the aesthetic measure of fuselage and battery 20.In addition, user can directly lead to
It crosses and battery 20 is pushed into battery accommodating chamber 11 to realize that the locking of battery 20, user can be directly by pull battery 20 to realize
The unlock of battery 20, optimizes mode of operation.And the unmanned plane 100 is in accidental falling or when being hit, due to elasticity
The vibration elastic of main body 12 can be such that fitting for lock 22 is released with limiting section 13, to make battery 20 and the work(in frame main body 10
Energy module disconnects electrical connection, and then plays the role of power-off protection unmanned plane 100.Optionally, which is elasticity
Arm.
Elastic body 12 and limiting section 13 are set to frame main body 10 and constitute in the either side cavity wall of battery accommodating chamber 11, lock
Accessory 22 is set to the position on battery 20 and then coordinates with the position where limiting section 13, meets battery 20 and is assemblied in battery receiving
Limiting section 13 is locked with the cooperation of fitting for lock 22 in chamber 11.In the present embodiment, the elastic body 12 and limiting section 13 are set to
Frame main body 10 is constituted on the upper side wall of battery accommodating chamber 11, and correspondingly, fitting for lock 22 is set to the upper surface of battery 20.When
So, the setting of elastic body 12 and limiting section 13 is not limited to only constitute the upper side wall of battery accommodating chamber 11 in frame main body 10
On, elastic body 12 and limiting section 13 can be multiple, can be set to frame main body 10 according to design requirement and constitute battery appearance
It receives in the either side cavity wall of chamber 11.
As shown in Fig. 6 and Fig. 7 combinations Fig. 4 and Fig. 5, battery 20 includes battery main body 21 and is set on battery main body 21
Electrical connection section (not shown), frame main body 10 be equipped with electrical connection section cooperation be electrically connected electrically mated portion (not shown).
Wherein, when the completion of battery 20 is assemblied in battery accommodating chamber 11, electrical connection section electric connection corresponding with electrically mated portion is to be embodied as
The function module power supply being arranged in frame main body 10.In the present embodiment, the direction of battery accommodating chamber 11 is assemblied in battery 20
On, one end that battery 20 enters battery accommodating chamber 11 at first is top, and the other end opposite with the top of battery 20 is battery 20
Tail end.The electrical connection section is set on the top end face of battery main body 21.Certainly, in other embodiments, the electrical connection section
It can be set on all sides of battery main body 21 or any other position.
Further, which further includes the grip part 23 for receiving the external force being applied in, so as to be convenient for using
Family forces in the battery 20, so that battery 20 can be exited from battery accommodating chamber 11.In the present embodiment, the grip part 23 setting
In the tail end of battery main body 21, wherein when the completion of battery 20 is assemblied in battery accommodating chamber 11, which is located at battery appearance
It receives at the installation opening of chamber 11.In an alternative embodiment, which is two, is divided into the upper and lower of 21 tail end of battery main body
Two sides or left and right sides can so hold in order to user.
In one embodiment, which can be through-hole or groove, and fitting for lock 22 is protrusion.Wherein, work as battery
20 when being assemblied in battery accommodating chamber 11, which inserts in receiving through-hole or in groove, so as to limit the movement of battery 20,
The function module that i.e. battery 20 realization is assemblied in frame main body 10, while realizing battery 20 and being arranged in frame main body 10
Electrical connection.When battery 20 under the effect of external force, elastic body 12 deform upon so that protrusion out of through-hole or groove
After removal, then the locking of battery 20 and frame main body 10 is released, so as to remove battery 20 from battery accommodating chamber 11.
As shown in Figures 5 to 7, further, which includes that first entered in battery accommodating chamber 11 for battery 20 is drawn
Guide face 221 and the second guide surface 222 that battery 20 is removed to battery accommodating chamber 11.First guide surface 221 and second guides
Face 222 is oppositely arranged, wherein first guide surface 221 and the second guide surface 222 can be plane or arcwall face.When this
When one guide surface 221 and the second guide surface 222 are plane, in protrusion towards on the direction of limiting section 13, the first guide surface 221 with
Spacing between second guide surface 222 is gradually reduced along the direction of limiting section 13.
Correspondingly, which includes the first guiding mating surface 131 being adapted to the first guide surface 221, Yi Jiyu
Second guiding mating surface 132 of the second guide surface 222 adaptation, can so meet battery 20 being fixed on frame main body 10
On, and be easy to unlock with frame main body 10 under certain outer force effect, thus in 100 accidental falling of unmanned plane or by
To when hitting, battery 20 is easy to unlock and disconnect with frame main body 10 to connect with the electrical of the function module in frame main body 10
It connects, so as to protect the unmanned plane 100, and by making the safety out of service that can ensure user of unmanned plane 100.
Specifically, as shown in Figures 1 to 9, when battery 20 is assemblied in the battery accommodating chamber 11 of frame main body 10, battery 20
On protrusion be held in elastic body 12 so that 12 deformation of elastic body avoid, until protrusion correspond to through-hole (in the example with
Illustrate for through-hole) when, the first guide surface 221 of the protrusion is adapted to the first guiding mating surface 131 of limiting section 13, so that should
Protrusion is defined in through-hole, that is, is realized battery 20 and be locked in battery accommodating chamber 11, at this time the electrical connection section and machine of battery 20
Electrically mated portion on frame body 10 is electrically connected.When battery 20 is disassembled from frame main body 10, user is by forcing in
The grip part 23 of battery 20 extracts battery 20 out of battery accommodating chamber 11, the second guide surface 222 opposite second of the protrusion
Mating surface 132 is guided to slide, the deformation under the resist force of protrusion of elastic body 12, so that protrusion is removed out of through-hole, it is electric at this time
Pond 20 and the function module that is arranged in frame main body 10, which disconnect, to be electrically connected, can so make user easily by battery 20 from
It is removed in frame main body 10.
In another embodiment, limiting section can also be protrusion, and fitting for lock is through-hole or groove, i.e. fit structure is set
It changes.In this embodiment, the protrusion and the fit system of through-hole or groove are same as the previously described embodiments, just no longer superfluous herein
It states.
Further, as shown in Figure 1 and Figure 4, frame main body 10 further includes horn 14 and is set to 14 free end of horn
Mounting portion 15, the mounting portion 15 be used for be installed as unmanned plane 100 provide flying power power plant 30.The horn 14 is more
It is a, it is divided on all sides of unmanned plane 100.Wherein, which is integrally formed setting, the i.e. fuselage of unmanned plane 100
It partial frame main body 10, horn 14, mounting portion 15 and constitutes multiple wall surfaces of battery accommodating chamber 11 and is integrally formed system
At.
In another embodiment, which further includes the lid (not shown) for closing battery accommodating chamber；Wherein,
When battery is assemblied in battery accommodating chamber, there is activity spacing between battery and lid.In the embodiment, battery is integrally assemblied in
In battery accommodating chamber, lid can be used for protecting the battery, after which is assemblied in battery accommodating chamber, between battery and lid
With spacing, which is more than size of the fitting for lock on battery and frame main body assembly direction, and grip part can be set to electricity
On the tail end face of tank main body, it so can equally meet in unmanned plane accidental falling or hit against when, battery are easy
It unlocks with frame main body and disconnects the electrical connection with the function module in frame main body, so as to protect this nobody
Machine, and by making the unmanned plane safety out of service that can ensure user.
As depicted in figs. 1 and 2, unmanned plane 100 further includes the upper shell 101 and lower housing 102 for being assemblied in frame main body 10；
Wherein, unmanned plane 100 is respectively constituted between the upper shell 101 and frame main body 10, between lower housing 102 and frame main body 10
The accommodation space of function module.In addition, (can not also be marked equipped with the department of assembly for installation function module in the frame main body 10
Show), such as：It is equipped with the department of assembly of assembly visual sensor or filming apparatus etc. in the front end face of frame main body.
In the unmanned plane of the utility model, elastic body and limiting section are equipped in the battery accommodating chamber of frame main body,
And the fitting for lock coordinated with limiting section is equipped on battery, when battery assembles frame main body, user only needs by inserting battery
Enter in battery accommodating chamber, is locked at this time by the fitting for lock and limiting section cooperation, it can be ensured that battery lock is held in battery
Receive intracavitary, mode of operation is simple and direct, to improve the usage experience of user.In this way, it may not need the machine in unmanned plane
Elastic element is set on body or battery to realize the locking and unlock of battery and fuselage, improves the beautiful journey of fuselage and battery
Degree.In addition, user can be directly by being pushed into battery accommodating chamber to realize that the locking of battery, user can directly pass through by battery
Pull battery optimizes mode of operation to realize the unlock of battery.Further, special by the structure to fitting for lock and limiting section
The restriction of sign, can make battery convenient for being locked in frame main body, can be in order to being dismantled in slave frame body under certain external force
Go out, mode of operation is easy, but also can be after unmanned plane is hit so that battery is disconnected with frame main body and frame main body
On function module electrical connection, to realize power-off protection unmanned plane.
Those skilled in the art will readily occur to this practicality after considering specification and putting into practice utility model disclosed herein
Novel other embodiments.This application is intended to cover any variations, uses, or adaptations of the utility model, these
Variations, uses, or adaptations follow the general principle of the utility model and include undocumented skill of the utility model
Common knowledge in art field or conventional techniques.The description and examples are only to be considered as illustrative, the utility model
True scope and spirit are pointed out by claims hereof.
It should be understood that the utility model is not limited to the accurate knot for being described above and being shown in the accompanying drawings
Structure, and various modifications and changes may be made without departing from the scope thereof.The scope of the utility model is only wanted by appended right
It asks to limit.
Claims (10)
1. a kind of unmanned plane, which is characterized in that including：Frame main body and battery, the frame main body include for accommodating described
The battery accommodating chamber of battery, the elastic body in the battery accommodating chamber and the limit being set on the elastic body
Position portion, the battery are equipped with the fitting for lock coordinated with the limiting section；
Wherein, when the battery is assemblied in the battery accommodating chamber, the limiting section is with fitting for lock cooperation locking to limit
The movement of the battery.
2. unmanned plane according to claim 1, which is characterized in that the limiting section is through-hole or groove, and the lock is matched
Part is protrusion.
3. unmanned plane according to claim 1, which is characterized in that the limiting section is protrusion, and the fitting for lock is through-hole
Or groove.
4. unmanned plane according to claim 2, which is characterized in that the protrusion includes entering the battery for the battery
The first guide surface in accommodating chamber and by the second guide surface of battery accommodating chamber described in the battery removal.
5. unmanned plane according to claim 4, which is characterized in that the limiting section includes being adapted to first guide surface
First guiding mating surface and be adapted to second guide surface second guide mating surface.
6. unmanned plane according to claim 1, which is characterized in that the frame main body further includes horn and is set to institute
The mounting portion of horn free end is stated, the mounting portion is used to be installed as the power plant that the unmanned plane provides flying power.
7. unmanned plane according to any one of claim 1 to 6, which is characterized in that the frame main body integrated molding is set
It sets.
8. unmanned plane according to claim 1, which is characterized in that the battery further include be set to the battery main body with
For applying the grip part of external force.
9. unmanned plane according to claim 1, which is characterized in that the frame main body further includes for closing the battery
The lid of accommodating chamber；Wherein, after the battery is assemblied in the battery accommodating chamber, have between the battery and the lid
There is activity spacing.
10. unmanned plane according to claim 1, which is characterized in that the unmanned plane further includes being assemblied in the rack master
The upper shell and lower housing of body；Wherein, between the upper shell and the frame main body, the lower housing and the frame main body
Between respectively constitute the unmanned plane function module accommodation space.
Priority Applications (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820028597.4U CN207773491U (en) | 2018-01-05 | 2018-01-05 | Unmanned plane |
| PCT/CN2018/107944 WO2019134406A1 (en) | 2018-01-05 | 2018-09-27 | Unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820028597.4U CN207773491U (en) | 2018-01-05 | 2018-01-05 | Unmanned plane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN207773491U true CN207773491U (en) | 2018-08-28 |
Family
ID=63223800
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201820028597.4U Active CN207773491U (en) | 2018-01-05 | 2018-01-05 | Unmanned plane |
Country Status (2)
| Country | Link |
|---|---|
| CN (1) | CN207773491U (en) |
| WO (1) | WO2019134406A1 (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109455291A (en) * | 2018-12-25 | 2019-03-12 | 拓攻（南京）机器人有限公司 | A kind of rack and unmanned plane for unmanned plane |
| CN111824442A (en) * | 2020-08-18 | 2020-10-27 | 广东北研航空遥感科技有限公司 | Multifunctional unmanned aerial vehicle |
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| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113895635B (en) * | 2021-11-03 | 2023-10-24 | 四川省天域航通科技有限公司 | Make things convenient for large-scale unmanned aerial vehicle of battery case dismouting change |
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| CN204230318U (en) * | 2014-08-29 | 2015-03-25 | 深圳市大疆创新科技有限公司 | Electric device, battery module and battery compartment |
| CN204230319U (en) * | 2014-08-29 | 2015-03-25 | 深圳市大疆创新科技有限公司 | Electric device, battery module and battery compartment |
| CN204144349U (en) * | 2014-08-29 | 2015-02-04 | 深圳市大疆创新科技有限公司 | Electric device, battery module and battery unit |
| JP6242030B2 (en) * | 2014-11-10 | 2017-12-06 | エスゼット ディージェイアイ テクノロジー カンパニー リミテッドＳｚ Ｄｊｉ Ｔｅｃｈｎｏｌｏｇｙ Ｃｏ．，Ｌｔｄ | Battery, thermal management device thereof, and UAV having this battery |
| CN204179174U (en) * | 2014-11-10 | 2015-02-25 | 深圳市大疆创新科技有限公司 | Battery and heat management device thereof and there is the UAV of this battery |
| CN204596856U (en) * | 2015-04-17 | 2015-08-26 | 深圳一电科技有限公司 | Power brick and unmanned plane |
| WO2017091948A1 (en) * | 2015-11-30 | 2017-06-08 | 深圳市大疆创新科技有限公司 | Battery-accommodating device and unmanned aircraft and electronic device |
| CN106927060A (en) * | 2017-04-14 | 2017-07-07 | 深圳市世纪南方科技有限公司 | A kind of fixed seat of intelligent battery on unmanned plane with vibration-damping function |
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2018
- 2018-01-05 CN CN201820028597.4U patent/CN207773491U/en active Active
- 2018-09-27 WO PCT/CN2018/107944 patent/WO2019134406A1/en active Application Filing
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| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109455291A (en) * | 2018-12-25 | 2019-03-12 | 拓攻（南京）机器人有限公司 | A kind of rack and unmanned plane for unmanned plane |
| CN111824442A (en) * | 2020-08-18 | 2020-10-27 | 广东北研航空遥感科技有限公司 | Multifunctional unmanned aerial vehicle |
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| Publication number | Publication date |
|---|---|
| WO2019134406A1 (en) | 2019-07-11 |
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| TR01 | Transfer of patent right |
Effective date of registration: 20190709 Address after: 518005 Baiwang Creative Factory, 1051 Songbai Road, Xili Street, Nanshan District, Shenzhen City, Guangdong Province, 7 101, 102-1 and 201/9 buildings Patentee after: Shenzhen City, Jiang Baiwang science and Technology Co Ltd Address before: 518057 Shenzhen Nanshan High-tech Zone, Shenzhen, Guangdong Province, 6/F, Shenzhen Industry, Education and Research Building, Hong Kong University of Science and Technology, No. 9 Yuexingdao, South District, Nanshan District, Shenzhen City, Guangdong Province Patentee before: Shenzhen Dji Technology Co., Ltd. |