CN206087260U - Unmanned aerial vehicle's frame subassembly and have unmanned aerial vehicle of this frame subassembly - Google Patents
Unmanned aerial vehicle's frame subassembly and have unmanned aerial vehicle of this frame subassembly Download PDFInfo
- Publication number
- CN206087260U CN206087260U CN201621081501.8U CN201621081501U CN206087260U CN 206087260 U CN206087260 U CN 206087260U CN 201621081501 U CN201621081501 U CN 201621081501U CN 206087260 U CN206087260 U CN 206087260U
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- China
- Prior art keywords
- circuit board
- housing assembly
- battery
- electric
- upper lid
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Abstract
The utility model provides an unmanned aerial vehicle's frame subassembly and have unmanned aerial vehicle of this frame subassembly, unmanned aerial vehicle include the fuselage, with horn and setting that the fuselage is connected are in screw on the horn, the fuselage includes the frame subassembly and sets up upper cover (2) and lower cover (3) on the frame subassembly, the frame subassembly includes casing (1) and circuit board components, be equipped with electrical cavity (10) in the casing, electrical cavity has upper shed (12) and under shed, circuit board components includes first circuit board (4) and second Circuit Board (5), the first circuit board certainly the upper shed install in among the electrical cavity, second Circuit Board certainly the under shed install in among the electrical cavity and with first circuit board looks interval. Through independently installing first circuit board and second Circuit Board in the electrical cavity, be convenient for circuit board components's assembly and disassembly and heat dissipation.
Description
Technical field
This utility model is related to unmanned plane field, more particularly to the housing assembly and the nothing with the housing assembly of unmanned plane
It is man-machine.
Background technology
At present unmanned plane would generally arrange two pieces of circuit boards to arrange that electricity mediation flies control function element and figure passes function element；
From top to bottom it is sequentially arranged in casing for two pieces of circuit boards of save space, locating dowel is provided with casing two pieces of circuit boards are entered
Row pre-determined bit, the locating dowel positioned at upper layer circuit board can be also cross lower circuit plate, and make lower circuit plate effectively uses face
Product is reduced.Cover plate after circuit board pre-determined bit by being arranged in casing realizes encapsulation.When it is time for repair, for example when lower floor's electricity
Road plate breaks down when needing repairing, and needs simultaneously to be dismantled upper layer circuit board, causes inconvenient maintenance simultaneously in unloading process
In be likely to upper layer circuit board cause damage.
In addition, circuit board superposition is arranged, also there is the defects such as weak heat-dissipating.
The content of the invention
This utility model provides a kind of housing assembly and the unmanned plane with the housing assembly of unmanned plane.
According to the first aspect of this utility model embodiment, there is provided a kind of housing assembly of unmanned plane, including casing and electricity
Road board component, is provided with electric chamber in the casing, the electric chamber has upper shed and under shed, and the circuit board assemblies include
First circuit board and second circuit board, the first circuit board is installed from the upper shed and is positioned in the electric chamber, institute
State second circuit board to install from the under shed and be positioned in the electric chamber and with the first circuit board separately.
Further, the first circuit board and the second circuit board are removable installed in the electric intracavity.
Further, the first circuit board is provided with the first location hole, and the second circuit board is provided with the second location hole, leads to
Cross and be assembled in first location hole and the screw of the second location hole, the first circuit board, second circuit board is solid respectively
Due to electric intracavity.
Further, the electric intracavity is provided with some locating dowels, sets on the first circuit board and/or second circuit board
There are some location holes corresponding with the locating dowel.
Further, the first circuit board is provided with electron speed regulator control unit and flight control units, and described
Two circuit boards are provided with image transmitting administrative unit.
Further, the electric chamber upper shed over-assemble has the upper lid above first circuit board, the electric chamber
Under shed over-assemble have lower cover below second circuit board.
Further, the lower cover is metal cap body.
Further, the casing is provided with assembling socket on the side wall in electric chamber, and the lower lid is provided with and is plugged in institute
State the clamping part of socket.
Further, the upper lid includes housing the battery container portion of battery；Battery is located at described first after installing
The top of circuit board simultaneously isolates with first circuit board.
Further, the upper lid is provided with least one limited block, and the limited block is connected on first circuit board.
Further, the limited block is downwardly extending from the upper interior surface, and is spaced apart.
Further, one is formed between the limited block and the upper interior surface and first circuit board upper surface and installs empty
Between, the installing space is used to house the electric elements being installed on the first circuit board.
According to the second aspect of this utility model embodiment, there is provided a kind of unmanned plane, including fuselage and fuselage connection
Horn and the propeller that is arranged on the horn, the fuselage is provided with housing assembly as above.
Further, the upper shed over-assemble in the electric chamber has the upper lid above first circuit board, described
Electrically the under shed over-assemble in chamber has the lower cover below second circuit board.
Further, the lower cover is metal cap body.
Further, the casing is provided with assembling socket on the side wall in the electric chamber, and the lower lid is provided with grafting
In the clamping part of the socket.
Further, the unmanned plane also includes battery, and the upper lid includes housing the battery container of the battery
Portion；The upper lid includes base plate, and the base plate is the bottom in the battery container portion, and the mounting batteries are simultaneously electrically connected to described
In upper lid and it is carried on the base plate.
Further, the battery and the first circuit board are respectively arranged at the both sides up and down of the base plate.
Further, the distance between the first circuit board and described battery are less than the second circuit board and the electricity
The distance between pond.
Further, the upper surface of the battery is a part for the fuselage.
Further, the upper lid, the lower cover and the casing are a part for the fuselage.
Further, the upper lid is provided with least one limited block, and the limited block is connected on first circuit board.
Further, the limited block is downwardly extending from the upper interior surface, and is spaced apart.
Further, one is formed between the limited block and the upper interior surface and first circuit board upper surface and installs empty
Between, the installing space is used to house the electric elements being installed on the first circuit board.
The housing assembly of the unmanned plane of this utility model embodiment and the unmanned plane with the housing assembly, there is provided a kind of
Two pieces of stacked circuit boards can be carried out independently installed housing assembly, two pieces of circuit boards will without order in installation process
Ask, and only need to dismantle corresponding circuit board in maintenance, easy accessibility, while the independently installed guarantee circuit of two pieces of circuit boards
Effective usable floor area of plate is unaffected.
It should be appreciated that the general description of the above and detailed description hereinafter are only exemplary and explanatory, not
This utility model can be limited.
Description of the drawings
Fig. 1 is the three-dimensional exploded view of housing assembly in the embodiment of this utility model one；
Fig. 2 is the casing structure figure of housing assembly in the embodiment of this utility model one；
Fig. 3 is the sectional view of housing assembly in the embodiment of this utility model one；
Fig. 4 is the sectional view of upper lid in the embodiment of this utility model one；
Fig. 5 is the structural representation of lower cover in the embodiment of this utility model one.
Main element symbol description
Casing 1
Electric chamber 10
Socket 110
Locating dowel 101,111
Upper shed 12
Head 13
Assembly mouth 130
Afterbody 14
Assembling block 141
Assembly hole 142,143
Screw hole 144
Installing plate 15
Mounting post 151,152
Horn 16
Motor 17
Upper lid 2
Battery container portion 20
Base plate 201
Limited block 202
First installation portion 21
Column block 211
Second installation portion 22
Assembly hole 221
Lower cover 3
Raised 31
Screw hole 32
Clamping part 33
Resettlement section 34
First circuit board 4
First location hole 40
Opening 41
Second circuit board 5
Second location hole 50
Ultrasonic element 51
Specific embodiment
Here exemplary embodiment will be illustrated in detail, its example is illustrated in the accompanying drawings.Explained below is related to
During accompanying drawing, unless otherwise indicated, the same numbers in different accompanying drawings represent same or analogous key element.Following exemplary embodiment
Described in embodiment do not represent all embodiments consistent with this utility model.Conversely, they be only with it is such as appended
Some the consistent device of aspect, examples of system, apparatus and method being described in detail in claims, of the present utility model.
The term used in this utility model is, only merely for the purpose of description specific embodiment, and to be not intended to be limiting this reality
With new." one kind ", " described " and " being somebody's turn to do " of singulative used in this utility model and appended claims
It is intended to include most forms, unless context clearly shows that other implications.It is also understood that term used herein " and/
Or " refer to and comprising one or more associated any or all possible combinations for listing project.
It will be appreciated that though various information may be described using term first, second, third, etc. in this utility model,
But these information should not necessarily be limited by these terms.These terms are only used for that same type of information is distinguished from each other out.For example, not
In the case of departing from this utility model scope, the first information can also be referred to as the second information, and similarly, the second information can also
It is referred to as the first information.In the case where not conflicting, the feature in following embodiment and embodiment can be mutually combined.
With the fast development of unmanned air vehicle technique, for unmanned plane operational stability and figure transfer performance requirement increasingly
It is high.In order to meet the performance requirement of product, unmanned plane generally needs to arrange two pieces of circuit boards, and traditional structure is by two pieces of circuits
Plate is assembled up and down in order, and this structure setting is not only required to assemble sequence, while installed in the circuit on upper strata
The locating dowel or fixed structure of plate can be also cross the circuit board positioned at lower floor, and effective usable floor area of lower circuit plate is therefore
Can reduce.Instantly when layer circuit board breaks down and needs repairing, need to dismantle upper layer circuit board and cap simultaneously, increased and tear open
Operation is unloaded while being likely to result in the damage of layer circuit board in unloading process.
This utility model embodiment provides the solution that a kind of two pieces of circuit boards are stacked, and is not increasing equipment volume
On the basis of, by the way that two pieces of circuit boards are reversely independently mounted in casing, it is ensured that effective usable floor area of every piece of circuit board, circuit
The order that is assembled without of plate is limited and need to only dismantle corresponding circuit board in maintenance.
Fig. 1 is the three-dimensional exploded view of housing assembly in one embodiment.
In embodiment shown in Fig. 1, a kind of unmanned plane, it includes the horn 16 of fuselage and fuselage connection and arranges
Propeller (not shown) on the horn.The fuselage is provided with housing assembly.The housing assembly includes casing 1 and electricity
Road board component.Electric chamber 10 is provided with the casing 1.The electric chamber 10 has upper shed 12 and under shed (non-label).Institute
Circuit board assemblies are stated including first circuit board 4 and second circuit board 5, the first circuit board 4 is installed in from the upper shed 12
In the electric chamber 10, the second circuit board 5 is installed in the electric chamber 10 and electric with described first from the under shed
Road plate 4 is separately.
Further, the first circuit board 4 is installed and is positioned in the electric chamber 10, and the second circuit board 5 is filled
And if being positioned in the electric chamber 10.
In the present embodiment, the plate of the first circuit 4 and/or the second circuit board 4 are removable installed in the electricity
In air cavity 10.
The over-assemble of the upper shed 12 in the electric chamber 10 has the upper lid 2 positioned at the top of first circuit board 4.It is described electric
The under shed over-assemble in chamber 10 has the lower cover 3 positioned at the lower section of second circuit board 5.I.e. when the first circuit board 4 is opened on described
Mouth 12 is installed in the electric chamber 10, and the upper lid 2 is arranged on the top of the first circuit board 4；When the second circuit board 5
It is installed in behind the electric chamber 10 from the under shed, the lower cover 3 is located at the lower section of second circuit board 5.
In the present embodiment, the casing 1 is a part for fuselage, and the upper lid 2 and lower cover 3 constitute the fuselage
Exterior contour.I.e. described casing 1 forms fuselage main body after assembling with the upper lid 2 and the lower cover 3.
Specifically, with reference to shown in Fig. 1 and Fig. 2, if the casing 1 is the cavity body structure that dry side wall is collectively forming, from described
Electrically the either side wall of chamber 10 extends to form installing plate 15 to side wall corresponding thereto, and to coordinate the first circuit board 4 is installed
And/or second circuit board 5.The installing plate 15 is provided with along the mounting post 151 of the direction of the upper shed 12 extension and along institute
State the mounting post 152 of under shed direction extension.
Further, the first circuit board 4 is provided with the first location hole 40, and the second circuit board 5 is provided with the second positioning
Hole 50, by being assembled in first location hole 40 and the screw of the second location hole 50, by the first circuit board 4, second
Circuit board 5 is individually fixed in electric chamber 10.
Wherein, some locating dowels 101 corresponding with first location hole 40 are additionally provided with the electric chamber 10.It is described fixed
Position post 101 can protrude out to be formed from the side wall in the electric chamber 10, also can protrude out to be formed from the installing plate 15.
Wherein, the first circuit board 4 is assembled in downwards in electric chamber 10 from upper shed.Locating dowel 101 wears after assembling
The fixation to the first circuit board 4 is realized in the first location hole 40.In another embodiment, the locating dowel 101 is to set
Female column structure, by being assembled in the first location hole 40 and locating dowel 101 in screw by the first circuit board 4
It is assembled in electric chamber 10.
It is additionally provided with the electric chamber 10 some with the corresponding locating dowel 111 of the second location hole 50.The second circuit board 5
It is assembled in upwards in the electric chamber 10 under shed.Locating dowel 111 is arranged in the second location hole 50 and realizes to institute after assembling
State the fixation of second circuit board 5.The installing plate 15 limits the highest mounting surface of second circuit board 5.
In another embodiment, the locating dowel 111 is to set female column structure.By being assembled in the second positioning
Screw in hole 50 and locating dowel 111 is assembled in the second circuit board 5 in the electric chamber 10.In addition, the casing 1 exists
The lower wall in the electric chamber 10 is provided with assembling socket 110, and the lower cover 3 is provided with the buckle for being plugged in the socket 110
Portion 33.
Fig. 3 is the sectional view of housing assembly in one embodiment of the invention.
As shown in figure 3, the casing 1 is horizontally extending to form head 13 and afterbody 14.The afterbody is provided with assembling
Block 141, assembles block 141 and is provided with the assembly hole 142 of fixed first circuit board 4 and the assembly hole 143 of fixed second circuit board 5.
The first circuit board 4 is fixed in the electric chamber 10 by the screw being assembled in assembly hole 142.The second circuit board
5 are fixed in the electric chamber 10 by the screw being assembled in assembly hole 143.
Fig. 4 is the sectional view of upper lid in one embodiment of the invention.
As shown in Fig. 1 and Fig. 4, the upper lid 2 is adapted with the structure of casing 1 and is assembled in casing 1, and it includes and casing
The first installation portion 21 that 1 head 13 is mutually assembled and the second installation portion 22 mutually assembled with the afterbody 14 of casing 1.First installation portion
The battery container portion 20 for housing battery is provided between 21 and second installation portion 22.Further, the case head
13 are provided with some assembly mouths 130, and first installation portion 21 is provided with the column block 211 in the insertion assembly mouth 130.Institute
State the second installation portion 22 and be provided with screw assembling holes 221, when the upper lid 2 is assembled with the casing 1, be assembled in the assembling
Screw in hole 221 is screwed in fixes the upper lid 2 and the casing 1 in the corresponding screw hole 144 of assembling block 141 of casing 1.
The battery container portion 20 is located at the top of the electric chamber 10 and with base plate 201, and the base plate is the battery
The bottom of resettlement section.The battery (not shown) is installed and is electrically connected in the upper lid 2 and is carried on the base plate 201.
The battery is respectively arranged at the both sides up and down of the base plate 201 with the first circuit board 4.The battery is located at institute after installing
State the top of first circuit board 4 and isolate with the first circuit board 4, and the upper surface of the battery is of the fuselage
Point.
The distance between the first circuit board 4 and the battery are less than between the second circuit board 5 and the battery
Distance.
The base plate 201 is downwardly extending some limited blocks 202 towards the inner surface in the electric chamber 10.It is described spacing
Block 202 is spaced apart and is connected on the first circuit board 4 after circuit board is assembled.The limited block 202 and the base plate
An installing space is formed between 201 inner surfacies and the upper surface of the first circuit board 4, the installing space is installed in for collecting
Electric elements on the first circuit board 4.When the base plate 201 undertakes pressure (during dismounting cell), the limited block 202
Can with dispersive pressure with avoid to the first circuit board 4 cause damage.
Fig. 5 is the structural representation of lower cover in one embodiment of the invention.
As shown in Figures 1 and 5, the lower cover 3 is string configuration, and the lower cover is provided with some with the phase of casing 1 along edge
The projection 31 of buckle.Some screw holes 32 are additionally provided with the lower lid lower cover is assembled in casing 1 by screw.It is described
Second circuit board 5 is provided with ultrasonic element 51, and the lower cover 3 is provided with the resettlement section 34 for housing the ultrasonic element 51
It is interior.
The first circuit board 4 is provided with electron speed regulator control unit and flight control units, as shown in figure 1, described
First circuit board 4 is provided with opening 41 and flies control component to weld.It is single that the second circuit board 5 is provided with image transmitting management
Unit, therefore the first circuit board 4 that generates heat of the second circuit board 5 becomes apparent from, and group is carried out to it by the lower cover 3 of monolayer
Dress is fixed, and is conducive to the Quick diffusing of heat.In the present embodiment, the first circuit board 4 and the second circuit board 5 are separated by
It is arranged in the electric chamber 10 of casing 1, is conducive to the overall radiating of battery component while to enhance first circuit board electric with second
The effectiveness of road plate；The second circuit board 5 is arranged far from the position of battery to be also beneficial to battery component entirety
Radiating.To strengthen the effectiveness of second circuit board 5, the lower cover 3 is metal cap body.
As shown in figure 1, the casing 1 is provided with linking arm 16, the linking arm 16 being provided with to be connected with propeller
Motor 17.
Preferred embodiment of the present utility model is the foregoing is only, it is all at this not to limit this utility model
Within the spirit and principle of utility model, any modification, equivalent substitution and improvements done etc. should be included in this utility model
Within the scope of protection.
Claims (24)
1. a kind of housing assembly of unmanned plane, including casing and circuit board assemblies, it is characterised in that be provided with the casing electrically
Chamber, the electric chamber has upper shed and under shed, and the circuit board assemblies include first circuit board and second circuit board, described
First circuit board is installed and is positioned in the electric chamber from the upper shed, and the second circuit board is installed from the under shed
And be positioned in the electric chamber and with the first circuit board separately.
2. the housing assembly of unmanned plane as claimed in claim 1, it is characterised in that the first circuit board and described second electric
Road plate is removable installed in the electric intracavity.
3. the housing assembly of unmanned plane as claimed in claim 2, it is characterised in that the first circuit board is provided with the first positioning
Hole, the second circuit board is provided with the second location hole, by being assembled in first location hole screw with the second location hole,
The first circuit board, second circuit board are individually fixed in into electric intracavity.
4. the housing assembly of unmanned plane as claimed in claim 2, it is characterised in that the electric intracavity is provided with some positioning
Post, the first circuit board and/or second circuit board are provided with some location holes corresponding with the locating dowel.
5. the housing assembly of unmanned plane as claimed in claim 1, it is characterised in that the first circuit board is provided with electronics tune
Fast device control unit and flight control units, the second circuit board is provided with image transmitting administrative unit.
6. the housing assembly of unmanned plane as claimed in claim 1, it is characterised in that group in the upper shed in the electric chamber
Equipped with the upper lid above first circuit board, under the under shed over-assemble in the electric chamber has below second circuit board
Lid.
7. the housing assembly of unmanned plane as claimed in claim 6, it is characterised in that the lower cover is metal cap body.
8. the housing assembly of unmanned plane as claimed in claim 7, it is characterised in that side wall of the casing in the electric chamber
Assembling socket is provided with, the lower lid is provided with the clamping part for being plugged in the socket.
9. the housing assembly of unmanned plane as claimed in claim 6, it is characterised in that the upper lid includes housing battery
Battery container portion；Battery is located at the top of the first circuit board and isolates with first circuit board after installing.
10. the housing assembly of unmanned plane as claimed in claim 6, it is characterised in that the upper lid is provided with least one limit
Position block, the limited block is connected on first circuit board.
The housing assembly of 11. unmanned planes as claimed in claim 10, it is characterised in that the limited block is from table in the upper lid
The extension that faces down is formed, and is spaced apart.
The housing assembly of 12. unmanned planes as claimed in claim 11, it is characterised in that the limited block and table in the upper lid
An installing space is formed between face and first circuit board upper surface, the installing space is installed in first circuit for collecting
Electric elements on plate.
A kind of 13. unmanned planes, including fuselage and the fuselage horn for connecting and the propeller being arranged on the horn, its
It is characterised by, the fuselage is provided with the housing assembly described in any one of claim 1 to 5.
The housing assembly of 14. unmanned planes as claimed in claim 13, it is characterised in that in the upper shed in the electric chamber
The upper lid being assembled with above first circuit board, the under shed over-assemble in the electric chamber has below second circuit board
Lower cover.
15. unmanned planes as claimed in claim 14, it is characterised in that the lower cover is metal cap body.
16. unmanned planes as claimed in claim 14, it is characterised in that the casing is provided with group on the side wall in the electric chamber
Mouth is plugged, the lower lid is provided with the clamping part for being plugged in the socket.
17. unmanned planes as claimed in claim 14, it is characterised in that also including battery, the upper lid is included to asylum
State the battery container portion of battery；The upper lid includes base plate, and the base plate is the bottom in the battery container portion, the battery dress
And if being electrically connected in the upper lid and being carried on the base plate.
18. unmanned planes as claimed in claim 17, it is characterised in that the battery is respectively arranged at the first circuit board
The both sides up and down of the base plate.
19. unmanned planes as claimed in claim 17, it is characterised in that the distance between the first circuit board and described battery
Less than the distance between the second circuit board and described battery.
20. unmanned planes as claimed in claim 17, it is characterised in that the upper surface of the battery is of the fuselage
Point.
21. unmanned planes as claimed in claim 14, it is characterised in that the upper lid, the lower cover and the casing are institute
State a part for fuselage.
22. unmanned planes as claimed in claim 14, it is characterised in that the upper lid is provided with least one limited block, described
Limited block is connected on first circuit board.
23. unmanned planes as claimed in claim 22, it is characterised in that the limited block is extended downwardly from the upper interior surface
Formed, and be spaced apart.
24. unmanned planes as claimed in claim 22, it is characterised in that the limited block is electric with the upper interior surface and first
An installing space is formed between the plate upper surface of road, the installing space is used to house the electrical equipment being installed on the first circuit board
Element.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201621081501.8U CN206087260U (en) | 2016-09-26 | 2016-09-26 | Unmanned aerial vehicle's frame subassembly and have unmanned aerial vehicle of this frame subassembly |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201621081501.8U CN206087260U (en) | 2016-09-26 | 2016-09-26 | Unmanned aerial vehicle's frame subassembly and have unmanned aerial vehicle of this frame subassembly |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206087260U true CN206087260U (en) | 2017-04-12 |
Family
ID=58480587
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201621081501.8U Expired - Fee Related CN206087260U (en) | 2016-09-26 | 2016-09-26 | Unmanned aerial vehicle's frame subassembly and have unmanned aerial vehicle of this frame subassembly |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN206087260U (en) |
Cited By (7)
| Publication number | Priority date | Publication date | Assignee | Title |
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| CN107074341A (en) * | 2016-09-26 | 2017-08-18 | 深圳市大疆创新科技有限公司 | The housing assembly of unmanned plane and the unmanned plane with the housing assembly |
| CN107187586A (en) * | 2017-04-28 | 2017-09-22 | 重庆零度智控智能科技有限公司 | Unmanned vehicle body and unmanned vehicle |
| CN107487432A (en) * | 2017-09-22 | 2017-12-19 | 贵州信鸽科技有限公司 | Unmanned vehicle and flight instruments |
| WO2018209771A1 (en) * | 2017-05-19 | 2018-11-22 | 深圳市大疆创新科技有限公司 | Unmanned aerial vehicle and heat dissipation structure |
| WO2020000206A1 (en) * | 2018-06-26 | 2020-01-02 | 深圳市大疆创新科技有限公司 | Unmanned aerial vehicle |
| CN110678389A (en) * | 2018-09-26 | 2020-01-10 | 深圳市大疆创新科技有限公司 | Unmanned aerial vehicle |
| WO2020119248A1 (en) * | 2018-12-13 | 2020-06-18 | 广州极飞科技有限公司 | Frame for aircraft and aircraft |
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| CN108928457B (en) * | 2016-09-26 | 2020-12-29 | 深圳市大疆创新科技有限公司 | Unmanned aerial vehicle's frame subassembly and have unmanned aerial vehicle of this frame subassembly |
| WO2018053837A1 (en) * | 2016-09-26 | 2018-03-29 | 深圳市大疆创新科技有限公司 | Frame assembly for unmanned aerial vehicle, and unmanned aerial vehicle provided with frame assembly |
| CN107074341A (en) * | 2016-09-26 | 2017-08-18 | 深圳市大疆创新科技有限公司 | The housing assembly of unmanned plane and the unmanned plane with the housing assembly |
| CN108928457A (en) * | 2016-09-26 | 2018-12-04 | 深圳市大疆创新科技有限公司 | The rack components of unmanned plane and unmanned plane with the rack components |
| CN109131822A (en) * | 2016-09-26 | 2019-01-04 | 深圳市大疆创新科技有限公司 | Unmanned plane |
| US11040763B2 (en) | 2016-09-26 | 2021-06-22 | SZ DJI Technology Co., Ltd. | Frame assembly for unmanned aerial vehicle (UAV), and UAV having the same |
| CN107187586A (en) * | 2017-04-28 | 2017-09-22 | 重庆零度智控智能科技有限公司 | Unmanned vehicle body and unmanned vehicle |
| CN107187586B (en) * | 2017-04-28 | 2023-09-15 | 北京远度互联科技有限公司 | Unmanned vehicles organism and unmanned vehicles |
| WO2018209771A1 (en) * | 2017-05-19 | 2018-11-22 | 深圳市大疆创新科技有限公司 | Unmanned aerial vehicle and heat dissipation structure |
| US11192622B2 (en) | 2017-05-19 | 2021-12-07 | SZ DJI Technology Co., Ltd. | Unmanned aerial vehicle and heat dissipation structure |
| CN107487432A (en) * | 2017-09-22 | 2017-12-19 | 贵州信鸽科技有限公司 | Unmanned vehicle and flight instruments |
| CN110770120A (en) * | 2018-06-26 | 2020-02-07 | 深圳市大疆创新科技有限公司 | Unmanned plane |
| WO2020000206A1 (en) * | 2018-06-26 | 2020-01-02 | 深圳市大疆创新科技有限公司 | Unmanned aerial vehicle |
| WO2020061838A1 (en) * | 2018-09-26 | 2020-04-02 | 深圳市大疆创新科技有限公司 | Unmanned aerial vehicle |
| CN110678389A (en) * | 2018-09-26 | 2020-01-10 | 深圳市大疆创新科技有限公司 | Unmanned aerial vehicle |
| WO2020119248A1 (en) * | 2018-12-13 | 2020-06-18 | 广州极飞科技有限公司 | Frame for aircraft and aircraft |
| AU2019399622B2 (en) * | 2018-12-13 | 2022-06-02 | Guangzhou Xaircraft Technology Co., Ltd. | Frame for aircraft and aircraft |
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