CN106428596B - A kind of Distribution itineration check unmanned plane overall structure and its unmanned plane - Google Patents
A kind of Distribution itineration check unmanned plane overall structure and its unmanned plane Download PDFInfo
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- CN106428596B CN106428596B CN201610972395.0A CN201610972395A CN106428596B CN 106428596 B CN106428596 B CN 106428596B CN 201610972395 A CN201610972395 A CN 201610972395A CN 106428596 B CN106428596 B CN 106428596B
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- unmanned plane
- mounting
- platform
- overall structure
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- 238000009434 installation Methods 0.000 claims abstract description 21
- 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 12
- 238000013016 damping Methods 0.000 claims description 12
- 239000003292 glue Substances 0.000 claims 1
- 230000000694 effects Effects 0.000 abstract description 7
- 230000000007 visual effect Effects 0.000 abstract description 4
- 238000010586 diagram Methods 0.000 description 5
- 238000007689 inspection Methods 0.000 description 4
- 238000012544 monitoring process Methods 0.000 description 3
- 238000005516 engineering process Methods 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- 244000025254 Cannabis sativa Species 0.000 description 1
- 240000007594 Oryza sativa Species 0.000 description 1
- 235000007164 Oryza sativa Nutrition 0.000 description 1
- 241000270295 Serpentes Species 0.000 description 1
- 229910000831 Steel Inorganic materials 0.000 description 1
- 230000000903 blocking effect Effects 0.000 description 1
- 230000009194 climbing Effects 0.000 description 1
- 238000000354 decomposition reaction Methods 0.000 description 1
- 230000005611 electricity Effects 0.000 description 1
- 230000007613 environmental effect Effects 0.000 description 1
- 238000011835 investigation Methods 0.000 description 1
- 238000007726 management method Methods 0.000 description 1
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- 230000000630 rising effect Effects 0.000 description 1
- 239000010959 steel Substances 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D47/00—Equipment not otherwise provided for
- B64D47/08—Arrangements of cameras
-
- 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
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- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Accessories Of Cameras (AREA)
Abstract
The present invention provides a kind of Distribution itineration check unmanned plane overall structure and its unmanned plane, unmanned plane overall structure includes the electric platform and undercarriage being arranged below unmanned plane, and electric platform includes motor, installation pedestal and mounting platform；Electric platform is fixedly connected by installation pedestal with uav bottom, and one end of motor is fixedly connected in installation pedestal, and the other end of motor is connect with mounting platform, and mounting platform is driven to horizontally rotate；The undercarriage is fixedly connected with the mounting platform, and is rotated synchronously with mounting platform.The configuration of the present invention is simple, easy to use, undercarriage can be rotated synchronously with the camera of unmanned plane, so as to avoid in the prior art, when cloud platform rotation, and the problem of undercarriage influences the camera shooting visual field, to improve shooting effect.
Description
Technical field
The present invention relates to air vehicle technique field, more particularly, to a kind of Distribution itineration check unmanned plane overall structure and its nobody
Machine.
Background technology
Currently, nearly more than 30 years have been developed in China unmanned plane market, consumption is gradually expanded to from initial military domain
Field.Domestic consumption unmanned plane market is burning hot at present, and general public gradually rises to the degree of recognition and demand degree of unmanned plane, mistake
It goes over 2 years, unmanned plane enterprise, financing number, number of aircraft and product purpose, which have, significantly to be increased, or even occurs referring to
Number type increases, and there has also been further perfect in terms of supervisory system.The civilian unmanned plane industry of the coming five years will persistently keep very fast
Developing state, the year two thousand twenty China civilian unmanned plane product selling market scale is up to 26,500,000,000 yuan of (data sources：Space occasion
Net).
In addition to military purpose, the commercial market of unmanned plane is boundless, including police, city management, agricultural,
The wide range of areas such as matter, meteorology, electric power, rescue and relief work, video capture.
Such as in electric inspection process field, it is equipped with high-definition digital video camera and nobody of camera and GPS positioning system
Machine can carry out positioning autonomous cruise along power grid, transmit filmed image in real time, and monitoring personnel can synchronize and watch and grasp on computers
Control.And traditional artificial power-line patrolling mode is used, condition is arduous, inefficiency, and the electric power inspection work occasional of a line is met with
The danger of " being driven away by dog " " being stung by snake ".
Unmanned plane realizes electronization, information-based, intelligence inspection, improves the working efficiency of power circuit polling, answers
The suddenly level of speedily carrying out rescue work and power supply reliability.And Freshets roar down from the mountains, earthquake disaster etc. in emergency circumstances, unmanned plane can be to the potential of circuit
The problems such as danger, such as column foot are subside carries out exploration and urgent investigation, is not influenced by pavement behavior at all, has both removed climbing shaft tower from
Hardship, and the visual dead angle of human eye can be surveyed, it is helpful for restoring electricity rapidly.
For another example in agricultural insurance field, using being integrated with the dresses such as high-definition digital camera, spectroanalysis instrument, thermal infrared sensor
The unmanned plane set flies on farmland, and the accurate cultivated area for calculating plot of insuring, institute's gathered data can be used to assess crops
Risk situation, insurance premium rate, and can be disaster affected farmland setting loss, in addition, the inspection of unmanned plane also achieves the monitoring to crops.
Rationale for the recommendation：Natural calamity takes place frequently, and in face of the situation that No kernels or seeds are gathered, as in a year of scarcity, agricultural insurance is sometimes the help rice of peasants
Grass, but because Claims Resolution is difficult, and a stomachful of misery that made people more.On the one hand unmanned plane both can ensure that in the application in agricultural insurance field
The accuracy of setting loss and the high efficiency of Claims Resolution, and the normal growth of crops can be monitored, it helps peasant household to carry out and targetedly arranges
It applies, to reduce risks and lose.
In addition, unmanned plane be also widely used for environmental monitoring, movie and television play shooting, streetscape shooting, express delivery, Post disaster relief and
Remote sensing mapping etc..
And current unmanned plane can be frequently necessary to rotary head motor in the task of execution, but existing unmanned plane rises
Frame is fallen when horizontal stage electric machine rotates because the holder of undercarriage can block sight, leads to the angle of horizontal stage electric machine rotation
It is smaller, when needing to adjust the angle of unmanned plane, it is necessary to control unmanned plane direction of rotation, but in this way, be held in unmanned plane
Row shooting etc. tasks when, will strong influence shooting effect, reduce shooting quality.
Invention content
The purpose of the present invention is to provide a kind of Distribution itineration check unmanned plane overall structure and its unmanned planes, to solve existing skill
The bad technical problem of shooting effect present in art caused by the blocking or interfere of holder.
In order to solve the above technical problems, a kind of Distribution itineration check unmanned plane overall structure provided by the invention, including unmanned plane
The electric platform and undercarriage of lower section setting, electric platform includes motor, installation pedestal and mounting platform；
Electric platform is fixedly connected by installation pedestal with uav bottom, and one end of motor is fixedly connected on installation pedestal
On, the other end of motor is connect with mounting platform, and mounting platform is driven to horizontally rotate；
The undercarriage is rotatably arranged in the bottom of unmanned plane, and is fixedly connected with the mounting platform, and with peace
Assembling platform rotates synchronously.
Further, below the unmanned plane rotatably arranged with there is mounting bracket；The mounting bracket and the installation
Platform is fixedly connected；The undercarriage is rotationally lifted on by mounting bracket below unmanned plane.
Further, the mounting bracket includes annular fixed disk, annular rotary table and connector, in vertical direction, institute
It states annular fixed disk and holds annular rotary table；In the horizontal direction, the annular fixed disk and annular rotary table are concentric and can be opposite
Cooperation rotation connection；The annular rotary table is fixedly connected by connector with the mounting platform.
Further, it is provided with bearing between the annular rotary table and the annular fixed disk, it is therefore preferable to pushing tow bearing.
Further, the annular fixed disk is located at the inner ring of the annular rotary table.
Further, the annular fixed disk is located at the outer ring of the annular rotary table.
Further, the mounting base for fixed camera is provided on the mounting platform, mounting base and the installation are flat
Damping module is provided between platform.
Further, the damping module is wire rope spring.
Further, the damping module includes rubber spring, intermediate plate and wire rope spring, four rubber spring settings
On four corners of intermediate plate, on horizontal projection plane, the axis of rubber spring is overlapped with the butted line of intermediate plate, and
And the axis of rubber spring is obliquely installed horizontal by degree, and wire rope spring is provided on intermediate plate；
When installation, the bottom of rubber spring is fixedly connected with mounting platform, and mounting base is then fixed at wire rope spring
On.
Further, camera is fixed on by cantilever in the mounting base；Mounting hole, the cantilever are provided in mounting base
Connector be removably inserted into the mounting hole；Lock of the setting for the two locking between connector and the mounting base
Determine mechanism.
Further, the locking mechanism is semi-circular snap-gauge, and the both ends of semi-circular snap-gauge are hinged and connected to the mounting base
On, it is provided with clamp in the middle part of semi-circular snap-gauge；It is provided on the connector and the matched chuck of the clamp, connector
After being inserted into the mounting hole, the semi-circular snap-gauge is screwed off, the clamp is connected in chuck to prevent the connector
It is detached from out of mounting hole.
Further, retaining mechanism is provided between the clamp and the chuck, the retaining mechanism is hoodle jackscrew,
Hoodle jackscrew is arranged on the clamp either chuck the chuck or clamp and hoodle jackscrew corresponding position is provided with card
Hole.
Further, the hoodle jackscrew includes jackscrew main body, spring and hoodle；It is formed with spring in the jackscrew main body
Slot, the hoodle are connected to by the spring in the spring groove.
Further, the cantilever includes holder linking arm and camera support, holder linking arm one end and the company
Connector connects, and the other end is connect with the camera support.
Further, it is provided with oscillating motor between the camera support and the holder linking arm.
Further, it is provided with pitching motor between the camera support and the camera.
The present invention also provides one kind having above-mentioned integrally-built unmanned plane.
Using above-mentioned technical proposal, the present invention has the advantages that：
A kind of Distribution itineration check unmanned plane overall structure provided by the invention, simple in structure, easy to use, undercarriage can be with
The camera for unmanned plane rotates synchronously, and so as to avoid in the prior art, when cloud platform rotation, undercarriage influences camera and shoots the visual field
The problem of, to improve shooting effect.
Meanwhile the carries such as camera being arranged on shock-damping structure, additionally it is possible to play damping during unmanned plane during flying
Effect, improve the quality of shooting.
Description of the drawings
It below will be to specific in order to illustrate more clearly of the specific embodiment of the invention or technical solution in the prior art
Embodiment or attached drawing needed to be used in the description of the prior art are briefly described, it should be apparent that, in being described below
Attached drawing is some embodiments of the present invention, for those of ordinary skill in the art, before not making the creative labor
It puts, other drawings may also be obtained based on these drawings.
Fig. 1 is the structural schematic diagram of unmanned plane overall structure electric platform provided in an embodiment of the present invention；
Fig. 2 is electric platform and frame installing structure signal of rising and falling in unmanned plane overall structure provided in an embodiment of the present invention
Figure；
Fig. 3 is the mounting support structure schematic diagram in unmanned plane overall structure provided in an embodiment of the present invention；
Fig. 4 is camera mounting structure stereogram in unmanned plane overall structure provided in an embodiment of the present invention；
Fig. 5 is the decomposition diagram of camera mounting structure in unmanned plane overall structure provided in an embodiment of the present invention；
Fig. 6 is the structural schematic diagram of hoodle jackscrew in the embodiment of the present invention；
Fig. 7 is the structural schematic diagram of damping module in the embodiment of the present invention.
Reference numeral：
3- mounting bases；9- cameras；
10- unmanned planes；11- annular fixed disks；
12- cantilevers；13- camera supports；
14- oscillating motors；15- pitching motors；
21- mounting platforms；22- motors；
23- annular rotary tables；24- undercarriages；
25- connecting rods；26- connectors；
27- installation pedestals；28- connectors；
31- damping modules；32- semi-circular snap-gauges；
33- hoodle jackscrews；34- mounting holes；
121- connectors；122- chuck；
311- rubber springs；312- intermediate plates；
313- wire rope springs；
331- jackscrew main bodys；332- springs；
333- hoodles；334- spring grooves.
Specific implementation mode
Technical scheme of the present invention is clearly and completely described below in conjunction with attached drawing, it is clear that described implementation
Example is a part of the embodiment of the present invention, instead of all the embodiments.Based on the embodiments of the present invention, ordinary skill
The every other embodiment that personnel are obtained without making creative work, shall fall within the protection scope of the present invention.
In the description of the present invention, it should be noted that term "center", "upper", "lower", "left", "right", "vertical",
The orientation or positional relationship of the instructions such as "horizontal", "inner", "outside" be based on the orientation or positional relationship shown in the drawings, merely to
Convenient for the description present invention and simplify description, do not indicate or imply the indicated device or element must have a particular orientation,
With specific azimuth configuration and operation, therefore it is not considered as limiting the invention.In addition, term " first ", " second ",
" third " is used for description purposes only, and is not understood to indicate or imply relative importance.
In the description of the present invention, it should be noted that unless otherwise clearly defined and limited, term " installation ", " phase
Even ", " connection " shall be understood in a broad sense, for example, it may be being fixedly connected, may be a detachable connection, or be integrally connected；It can
Can also be electrical connection to be mechanical connection；It can be directly connected, can also indirectly connected through an intermediary, Ke Yishi
Connection inside two elements.For the ordinary skill in the art, above-mentioned term can be understood at this with concrete condition
Concrete meaning in invention.
Explanation is further explained to the present invention with reference to specific embodiment.
As shown in figures 1 to 6, a kind of Distribution itineration check unmanned plane overall structure provided in this embodiment, including 10 lower section of unmanned plane
The electric platform and undercarriage 24 of setting, electric platform include motor 22, installation pedestal 27 and mounting platform 21；
Electric platform is fixedly connected by installation pedestal 27 with 10 bottom of unmanned plane, and one end of motor 22 is fixedly connected on peace
It fills on pedestal 27, the other end of motor 22 is connect by connecting rod 25 with mounting platform 21, and drives mounting platform 21 is horizontal to turn
It is dynamic；
Undercarriage 24 is fixedly connected with mounting platform 21, and is rotated synchronously with mounting platform 21.
The lower section of unmanned plane 10 is rotatably arranged with there is mounting bracket；Mounting bracket is fixedly connected with mounting platform 21.It rises and falls
Frame 24 is rotationally lifted on by mounting bracket below unmanned plane.
Mounting bracket includes annular fixed disk 11, annular rotary table 23 and connector 26, and annular fixed disk 11 passes through connector
28 are fixed on uav bottom, and in vertical direction, annular fixed disk 11 holds annular rotary table 23；In the horizontal direction, annular
Fixed disk 11 and annular rotary table 23 are concentric and can relative engagement rotation connection；Annular rotary table 23 is flat with installation by connector 26
Platform 21 is fixedly connected.Undercarriage 24 is arranged on annular rotary table 23.
It is provided with bearing between annular rotary table 23 and annular fixed disk 11, it is therefore preferable to pushing tow bearing.
Wherein, annular fixed disk 11 is located at the inner ring of annular rotary table 23.Certainly in practical applications, annular fixed disk 11
The outer ring of annular rotary table 23 can be located at.
It is provided with the mounting base 3 for fixed camera 9 on mounting platform 21, is arranged between mounting base 3 and mounting platform 21
There is damping module 31.
As shown in fig. 7, damping module 31 includes rubber spring 311, intermediate plate 312 and wire rope spring 313, four rubber
Spring 311 is arranged on four corners of intermediate plate 312, on horizontal projection plane, the axis and intermediate plate of rubber spring 311
312 butted line overlaps, also, the axis of rubber spring 311 is obliquely installed horizontal by 45 degree, is arranged on intermediate plate 312
There is wire rope spring 313.
When installation, the bottom of rubber spring 311 is fixedly connected with mounting platform 21, and mounting base 3 is then fixed at steel wire
It restricts on spring 313.
Camera 9 is fixed on by cantilever 12 in mounting base 3；Mounting hole 34, the connector of cantilever 12 are provided in mounting base 3
121 are removably inserted into mounting hole 34；Locking mechanism of the setting for the two locking between connector 121 and mounting base 3.
Locking mechanism is semi-circular snap-gauge 32, and the both ends of semi-circular snap-gauge 32 are hinged and connected in mounting base 3, semi-circular snap-gauge
32 middle part is provided with clamp；It is provided on connector 121 and is inserted into installation with the matched chuck 122 of clamp, connector 121
After in hole 34, semi-circular snap-gauge 32 is screwed off, clamp is connected in chuck to prevent connector 121 to be detached from out of mounting hole 34.
Retaining mechanism is provided between clamp and chuck, retaining mechanism is hoodle jackscrew 33, and hoodle jackscrew 33 is arranged in card
Either chuck or clamp are provided with card hole to head with 33 corresponding position of hoodle jackscrew in chuck.
Hoodle jackscrew 33 includes jackscrew main body 331, spring 332 and hoodle 333；It is formed with spring groove in jackscrew main body 331
334, hoodle 333 is by 332 elastic connection of spring in spring groove 334.
Cantilever 12 includes holder linking arm and camera support 13, and holder linking arm one end is connect with connector 121, the other end
It is connect with camera support 13.
Oscillating motor 14 is provided between camera support 13 and holder linking arm.
Pitching motor 15 is provided between camera support 13 and camera 9.
The present invention also provides one kind having above-mentioned integrally-built unmanned plane；The other structures of unmanned plane are the prior art,
Details are not described herein.
A kind of 10 overall structure of Distribution itineration check unmanned plane provided by the invention, simple in structure, easy to use, 24 energy of undercarriage
Enough to be rotated synchronously with the camera 9 of unmanned plane 10, so as to avoid in the prior art, when cloud platform rotation, undercarriage 24 influences phase
Machine 9 shoots the problem of visual field, to improve shooting effect.
Meanwhile the equal carries of camera 9 being arranged on shock-damping structure, additionally it is possible to play and subtract during unmanned plane 10 flies
The effect of shake improves the quality of shooting.
Finally it should be noted that：The above embodiments are only used to illustrate the technical solution of the present invention., rather than its limitations；To the greatest extent
Present invention has been described in detail with reference to the aforementioned embodiments for pipe, it will be understood by those of ordinary skill in the art that：Its according to
So can with technical scheme described in the above embodiments is modified, either to which part or all technical features into
Row equivalent replacement；And these modifications or replacements, various embodiments of the present invention technology that it does not separate the essence of the corresponding technical solution
The range of scheme.
Claims (7)
1. a kind of Distribution itineration check unmanned plane overall structure, which is characterized in that including the electric platform being arranged below unmanned plane and rise
Frame is fallen, electric platform includes motor, installation pedestal and mounting platform；
Electric platform is fixedly connected by installation pedestal with uav bottom, and one end of motor is fixedly connected in installation pedestal,
The other end of motor is connect with mounting platform, and mounting platform is driven to horizontally rotate；
The undercarriage is rotatably arranged in the bottom of unmanned plane, and is fixedly connected with the mounting platform, and flat with installation
Platform rotates synchronously；
Rotatably arranged with there is mounting bracket below the unmanned plane；The mounting bracket is fixedly connected with the mounting platform；
The undercarriage is rotationally lifted on by mounting bracket below unmanned plane；
The mounting bracket includes annular fixed disk, annular rotary table and connector, in vertical direction, the annular fixed disk support
Firmly annular rotary table；In the horizontal direction, the annular fixed disk and annular rotary table it is concentric and can relative engagement rotation connection；Institute
Annular rotary table is stated to be fixedly connected with the mounting platform by connector；
Pushing tow bearing is provided between the annular rotary table and the annular fixed disk.
2. Distribution itineration check unmanned plane overall structure according to claim 1, which is characterized in that be arranged on the mounting platform
It is useful for the mounting base of fixed camera, damping module is provided between mounting base and the mounting platform.
3. Distribution itineration check unmanned plane overall structure according to claim 2, which is characterized in that the damping module includes rubber
Glue spring, intermediate plate and wire rope spring, four rubber springs are arranged on four corners of intermediate plate, in horizontal projection plane
On, the axis of rubber spring is overlapped with the butted line of intermediate plate, also, the axis of rubber spring is tilted horizontal by degree and set
It sets, wire rope spring is provided on intermediate plate；
When installation, the bottom of rubber spring is fixedly connected with mounting platform, and mounting base is then fixed on wire rope spring.
4. Distribution itineration check unmanned plane overall structure according to claim 2, which is characterized in that camera is fixed on by cantilever
In the mounting base；Mounting hole is provided in mounting base, the connector of the cantilever is removably inserted into the mounting hole；
Locking mechanism of the setting for the two locking between connector and the mounting base.
5. Distribution itineration check unmanned plane overall structure according to claim 4, which is characterized in that the locking mechanism is semi-ring
The both ends of shape snap-gauge, semi-circular snap-gauge are hinged and connected in the mounting base, and clamp is provided in the middle part of semi-circular snap-gauge；The company
It is provided on connector and screws off the semi-circular after connector is inserted into the mounting hole with the clamp matched chuck
Snap-gauge, the clamp are connected in chuck to prevent the connector to be detached from out of mounting hole.
6. Distribution itineration check unmanned plane overall structure according to claim 5, which is characterized in that the clamp and the chuck
Between be provided with retaining mechanism, the retaining mechanism is hoodle jackscrew, and hoodle jackscrew is arranged on the clamp or chuck, institute
It states chuck or clamp and hoodle jackscrew corresponding position is provided with card hole.
7. one kind having the integrally-built unmanned plane of claim 1-6 any one of them Distribution itineration check unmanned planes.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610972395.0A CN106428596B (en) | 2016-10-28 | 2016-10-28 | A kind of Distribution itineration check unmanned plane overall structure and its unmanned plane |
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610972395.0A CN106428596B (en) | 2016-10-28 | 2016-10-28 | A kind of Distribution itineration check unmanned plane overall structure and its unmanned plane |
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| CN106428596A CN106428596A (en) | 2017-02-22 |
| CN106428596B true CN106428596B (en) | 2018-09-11 |
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Families Citing this family (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108058819A (en) * | 2017-12-13 | 2018-05-22 | 萍乡市旭华电瓷电器制造有限公司 | A kind of isolator detecting unmanned plane |
| WO2019173990A1 (en) * | 2018-03-14 | 2019-09-19 | 深圳市大疆创新科技有限公司 | Mounting mechanism, landing gear, rack and unmanned aerial vehicle |
| WO2019173988A1 (en) * | 2018-03-14 | 2019-09-19 | 深圳市大疆创新科技有限公司 | Rotating mechanism, landing gear and frame of unmanned aerial vehicle, and unmanned aerial vehicle |
| WO2020042159A1 (en) * | 2018-08-31 | 2020-03-05 | 深圳市大疆创新科技有限公司 | Rotation control method and apparatus for gimbal, control device, and mobile platform |
| CN109178330B (en) * | 2018-09-27 | 2023-12-22 | 哈尔滨理工大学 | Unmanned aerial vehicle carries on camera fixed bolster |
| CN109193453A (en) * | 2018-09-29 | 2019-01-11 | 国网浙江省电力有限公司 | Multi-functional unmanned plane suitable for electric inspection process |
| CN110001948B (en) * | 2019-04-30 | 2021-02-12 | 南京涵铭置智能科技有限公司 | Double-blade shooting unmanned aerial vehicle and using method thereof |
| CN112789218A (en) * | 2020-06-17 | 2021-05-11 | 深圳市大疆创新科技有限公司 | Cloud platform, camera carrier and movable platform |
| CN113844664A (en) * | 2021-09-17 | 2021-12-28 | 贵州电网有限责任公司 | Three optical pod vibration isolation device of gaN |
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| Publication number | Priority date | Publication date | Assignee | Title |
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| US9457901B2 (en) * | 2014-04-22 | 2016-10-04 | Fatdoor, Inc. | Quadcopter with a printable payload extension system and method |
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| CN204433078U (en) * | 2015-01-30 | 2015-07-01 | 深圳市大疆创新科技有限公司 | The Cloud Terrace and use the aircraft of this The Cloud Terrace |
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| CN205293106U (en) * | 2016-01-08 | 2016-06-08 | 浙江天马行空创新科技有限公司 | Novel unmanned aerial vehicle nacelle mounting structure |
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