CN106428596A - Overall structure of unmanned aerial vehicle for patrolling distribution network and unmanned aerial vehicle thereof - Google Patents
Overall structure of unmanned aerial vehicle for patrolling distribution network and unmanned aerial vehicle thereof Download PDFInfo
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- CN106428596A CN106428596A CN201610972395.0A CN201610972395A CN106428596A CN 106428596 A CN106428596 A CN 106428596A CN 201610972395 A CN201610972395 A CN 201610972395A CN 106428596 A CN106428596 A CN 106428596A
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- unmanned plane
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- overall structure
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- 238000009434 installation Methods 0.000 claims description 24
- 238000013016 damping Methods 0.000 claims description 12
- 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 description 10
- 230000001360 synchronised effect Effects 0.000 claims description 5
- 239000003292 glue Substances 0.000 claims 1
- 230000000694 effects Effects 0.000 abstract description 7
- 238000000034 method Methods 0.000 abstract description 4
- 238000007689 inspection Methods 0.000 description 3
- 238000012544 monitoring process Methods 0.000 description 3
- 230000000007 visual effect Effects 0.000 description 3
- 238000005516 engineering process Methods 0.000 description 2
- 241000282472 Canis lupus familiaris Species 0.000 description 1
- 244000025254 Cannabis sativa Species 0.000 description 1
- 240000007594 Oryza sativa Species 0.000 description 1
- 235000007164 Oryza sativa Nutrition 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
- 238000010586 diagram Methods 0.000 description 1
- 230000005611 electricity Effects 0.000 description 1
- 230000007613 environmental effect Effects 0.000 description 1
- 238000007726 management method Methods 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 238000013507 mapping Methods 0.000 description 1
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Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT 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 invention provides an overall structure of an unmanned aerial vehicle for patrolling a distribution network and the unmanned aerial vehicle thereof. The overall structure of the unmanned aerial vehicle comprises an electric platform and an undercarriage arranged under the unmanned aerial vehicle, wherein the electric platform comprises a motor, a mounting base and a mounting platform; the electric platform is fixedly connected with the bottom of the unmanned aerial vehicle through the mounting base; one end of the motor is fixedly connected with the mounting base; the other end of the motor is connected with the mounting platform and is used for driving the mounting platform to horizontally rotate; and the undercarriage is fixedly connected with the mounting platform and is synchronously rotated following the mounting platform. According to the invention, the structure is simple, the use is convenient, and the undercarriage is capable of synchronously rotating following a camera of the unmanned aerial vehicle, so that the problem that the camera shooting field is influenced by the undercarriage in the rotation process of the platform of the prior art is solved, and the shooting effect is promoted.
Description
Technical field
The present invention relates to unmanned air vehicle technique field, especially relate to a kind of Distribution itineration check unmanned plane overall structure and its nobody
Machine.
Background technology
At present, China's unmanned plane market has been developed nearly more than 30 years, gradually expands to consumption from initial military domain
Field.At present domestic consumption unmanned plane market is burning hot, and general public is gradually risen to the degree of recognition of unmanned plane and demand degree, mistake
Go over 2 years, unmanned plane enterprise, financing number of times, number of aircraft and product purpose have and significantly increase, or even occur in that finger
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 civilian unmanned plane production marketing market scale of the year two thousand twenty China is up to 26,500,000,000 yuan of (Data Sources：Space occasion
Net).
Except military purpose, the commercial market of unmanned plane is boundless, including police, city management, agricultural,
The wide spectrums such as matter, meteorology, electric power, rescue and relief work, video capture.
For example in electric inspection process field, be equipped with high-definition digital video camera and photographing unit and GPS positioning system nobody
Machine, can carry out positioning autonomous cruise along electrical network, transmit filmed image in real time, and monitoring personnel synchronously can be watched and behaviour on computers
Control.And traditional artificial power-line patrolling mode is adopted, condition is arduous, inefficiency, and the electric power inspection work occasional of a line meets with
The danger of " being driven away by Canis familiaris L. " " being stung by Serpentiss ".
Unmanned plane achieves electronization, informationization, intellectuality and patrols and examines, improve power circuit polling work efficiency, should
Suddenly speedily carry out rescue work level 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 is surveyed and is promptly investigated, and is not at all affected by pavement behavior, has both removed climbing shaft tower from
Hardship, the visual dead angle of human eye can be surveyed again, helpful for restoring electricity rapidly.
And for example in agricultural insurance field, filled using high-definition digital camera, spectroanalysis instrument, thermal infrared sensor etc. is integrated with
The unmanned plane that puts is flown on farmland, accurately calculates the cultivated area in plot of insuring, and institute's gathered data can be used to assess crops
Risk situation, insurance premium rate, and can be disaster affected farmland setting loss, additionally, the inspection of unmanned plane also achieves the monitoring to crops.
Rationale for the recommendation：Natural disaster takes place frequently, and in the face of the situation that No kernels or seeds are gathered, as in a year of scarcity, agricultural insurance is sometimes a help rice of peasants
Grass, but because Claims Resolution is difficult, a stomachful of misery that allowed people many again.On the one hand unmanned plane was both can ensure that in the application in agricultural insurance field
The accuracy of setting loss and the high efficiency of Claims Resolution, can monitor the normal growth of crops again, help peasant household to carry out and targetedly arrange
Apply, 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
The aspects such as remote sensing mapping.
And current unmanned plane can be frequently necessary to rotary head motor, but existing unmanned plane rises in the task of execution
Frame fall because the support of undercarriage can block sight line when horizontal stage electric machine rotates, the angle for causing horizontal stage electric machine to rotate
Less, when the angle for needing to adjust unmanned plane, it is necessary to control unmanned plane direction of rotation, but so, hold in unmanned plane
Row shoot etc. task when, will strong influence shooting effect, reduce shooting quality.
Content of the invention
It is an object of the invention to provide a kind of Distribution itineration check unmanned plane overall structure and its unmanned plane, to solve existing skill
Blocking or interfere the not good technical problem of caused shooting effect due to support present in art.
For solving above-mentioned technical problem, a kind of Distribution itineration check unmanned plane overall structure that the present invention is provided, including unmanned plane
Electric platform and undercarriage that lower section is arranged, electric platform includes motor, installation pedestal and mounting platform；
Electric platform is fixedly connected with unmanned motor spindle by installation pedestal, and one end of motor is fixedly connected on installation pedestal
On, the other end of motor is connected with mounting platform, and drive installation plateau levels are rotated；
The undercarriage is rotatably arranged in the bottom of unmanned plane, and is fixedly connected with the mounting platform, and with peace
Assembling platform synchronous axial system.
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 below unmanned plane by mounting bracket.
Further, the mounting bracket includes annular fixed disk, annular rotary table and connector, in vertical direction, institute
State annular fixed disk and hold annular rotary table；In the horizontal direction, the annular fixed disk and annular rotary table are concentric and can phase
Connection is rotated to coordinating；The annular rotary table is fixedly connected with the mounting platform by connector.
Further, between the annular rotary table and the annular fixed disk, bearing is provided with, 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 seat being provided with the mounting platform for fixed camera, installing plate is put down with described installation
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, and four rubber springs are arranged
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, is provided with wire rope spring on intermediate plate；
During installation, the bottom of rubber spring is fixedly connected with mounting platform, and installing plate is then fixedly installed on wire rope spring
On.
Further, camera is fixed in the mounting seat by cantilever；Installing hole is provided with mounting seat, the cantilever
Union joint be removably inserted into the installation in the hole；The lock of both lockings is provided between union joint and the mounting seat
Determine mechanism.
Further, the locking mechanism is that semi-circular clamp, the two ends of semi-circular clamp are hinged and connected to the mounting seat
On, the middle part of semi-circular clamp is provided with dop；The chuck for matching with the dop, union joint is provided with the union joint
After being inserted into the installation in the hole, the semi-circular clamp is screwed off, the dop is connected in chuck to prevent the union joint
Depart from from the hole is installed.
Further, between the dop and the chuck, retaining mechanism is provided with, the retaining mechanism is hoodle jackscrew,
Hoodle jackscrew is arranged in the dop or chuck, and the chuck or dop are provided with card with hoodle jackscrew corresponding position
Hole.
Further, the hoodle jackscrew includes jackscrew main body, spring and hoodle；Spring is formed with the jackscrew main body
Groove, the hoodle is connected in the spring groove by the spring.
Further, the cantilever includes head linking arm and camera support, described head linking arm one end and the company
Joint connects, and the other end is connected with the camera support.
Further, between the camera support and the head linking arm, oscillating motor is provided with.
Further, between the camera support and the camera, pitching motor is provided with.
The present invention also provides a kind of with above-mentioned integrally-built unmanned plane.
Using technique scheme, the present invention has the advantages that：
A kind of Distribution itineration check unmanned plane overall structure that the present invention is provided, simple structure, easy to use, undercarriage can be with
The camera synchronous axial system of unmanned plane, so as to avoid in prior art, during cloud platform rotation, undercarriage impact camera shoots the visual field
Problem, so as to improve shooting effect.
Meanwhile, the carries such as camera are arranged on shock-damping structure, additionally it is possible to during unmanned plane during flying, play damping
Effect, improve shoot quality.
Description of the drawings
In order to be illustrated more clearly that the specific embodiment of the invention or technical scheme of the prior art below will be to concrete
Needed for embodiment or description of the prior art, accompanying drawing to be used is briefly described, it should be apparent that, in describing below
Accompanying drawing is some embodiments of the present invention, for those of ordinary skill in the art, before creative work is not paid
Put, other accompanying drawings can also be obtained according to these accompanying drawings.
Fig. 1 is the structural representation 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 axonometric chart in unmanned plane overall structure provided in an embodiment of the present invention；
Fig. 5 is the decomposing schematic representation of camera mounting structure in unmanned plane overall structure provided in an embodiment of the present invention；
Fig. 6 is the structural representation of hoodle jackscrew in the embodiment of the present invention；
Fig. 7 is the structural representation of damping module in the embodiment of the present invention.
Reference：
3- mounting seat；9- camera；
10- unmanned plane；11- annular fixed disk；
12- cantilever；13- camera support；
14- oscillating motor；15- pitching motor；
21- mounting platform；22- motor；
23- annular rotary table；24- undercarriage；
25- connecting rod；26- connector；
27- installation pedestal；28- connector；
31- damping module；32- semi-circular clamp；
33- hoodle jackscrew；34- installing hole；
121- union joint；122- chuck；
311- rubber spring；312- intermediate plate；
313- wire rope spring；
331- jackscrew main body；332- spring；
333- hoodle；334- spring groove.
Specific embodiment
Below in conjunction with accompanying drawing, technical scheme is clearly and completely described, it is clear that described enforcement
Example is a part of embodiment of the present invention, rather than whole embodiments.Based on the embodiment in the present invention, ordinary skill
The every other embodiment obtained under the premise of creative work is not made by personnel, belongs to the scope of protection of the invention.
In describing the invention, it should be noted that term " " center ", " on ", D score, "left", "right", " vertical ",
The orientation of instruction such as " level ", " interior ", " outward " or position relationship be based on orientation shown in the drawings or position relationship, merely to
Be easy to describe the present invention and simplify description, rather than indicate or the hint device of indication or element must with specific orientation,
With specific azimuth configuration and operation, therefore it is not considered as limiting the invention.Additionally, term " first ", " second ",
" the 3rd " is only used for describing purpose, and it is not intended that indicating or hint relative importance.
In describing the invention, it should be noted that unless otherwise clearly defined and limited, term " installation ", " phase
Even ", " connection " should be interpreted broadly, for example, it may be being fixedly connected, or being detachably connected, or be integrally connected；Can
To be to be mechanically connected, or electrically connect；Can be joined directly together, it is also possible to be indirectly connected to by intermediary, Ke Yishi
The connection of two element internals.For the ordinary skill in the art, above-mentioned term can be understood at this with concrete condition
Concrete meaning in invention.
With reference to specific embodiment, explanation is further explained to the present invention.
As shown in figures 1 to 6, a kind of Distribution itineration check unmanned plane overall structure that the present embodiment is provided, including 10 lower section of unmanned plane
The electric platform of setting and undercarriage 24, electric platform includes motor 22, installation pedestal 27 and mounting platform 21；
Electric platform is fixedly connected with 10 bottom of unmanned plane by installation pedestal 27, and one end of motor 22 is fixedly connected on peace
On dress pedestal 27, the other end of motor 22 is connected with mounting platform 21 by connecting rod 25, and 21 level of drive installation platform turns
Dynamic；
Undercarriage 24 is fixedly connected with mounting platform 21, and with 21 synchronous axial system of mounting platform.
The lower section of unmanned plane 10 is rotatably arranged with there is mounting bracket；Mounting bracket is fixedly connected with mounting platform 21.Rise and fall
Frame 24 is rotationally lifted on below unmanned plane by mounting bracket.
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 unmanned motor spindle, and in vertical direction, annular fixed disk 11 is holding annular rotary table 23；In the horizontal direction, ring
Shape fixed disk 11 and annular rotary table 23 concentric and can relative engagement rotate connection；Annular rotary table 23 is by connector 26 and installation
Platform 21 is fixedly connected.Undercarriage 24 is arranged on annular rotary table 23.
Bearing is provided 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 actual applications, annular fixed disk 11
May be located at the outer ring of annular rotary table 23.
The mounting seat 3 being provided with mounting platform 21 for fixed camera 9, is arranged between mounting seat 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 of rubber spring 311 and intermediate plate
312 butted line overlaps, also, the axis of rubber spring 311 is obliquely installed horizontal by 45 degree, arranges on intermediate plate 312
There is wire rope spring 313.
During installation, the bottom of rubber spring 311 is fixedly connected with mounting platform 21, and mounting seat 3 is then fixedly installed on steel wire
On rope spring 313.
Camera 9 is fixed in mounting seat 3 by cantilever 12；Installing hole 34, the union joint of cantilever 12 is provided with mounting seat 3
121 are removably inserted in installing hole 34；The locking mechanism of both lockings is provided between union joint 121 and mounting seat 3.
Locking mechanism is semi-circular clamp 32, and the two ends of semi-circular clamp 32 are hinged and connected in mounting seat 3, semi-circular clamp
32 middle part is provided with dop；The chuck 122 for matching with dop is provided with union joint 121, and union joint 121 is inserted into installation
After in hole 34, semi-circular clamp 32 is screwed off, dop is connected in chuck to prevent union joint 121 from departing from from installing hole 34.
Retaining mechanism is provided between dop and chuck, and retaining mechanism is that hoodle jackscrew 33, hoodle jackscrew 33 is arranged on card
On head or chuck, chuck or dop are provided with hole clipping with 33 corresponding position of hoodle jackscrew.
Hoodle jackscrew 33 includes jackscrew main body 331, spring 332 and hoodle 333；Spring groove is formed with jackscrew main body 331
334, hoodle 333 is by 332 elastic connection of spring in spring groove 334.
Cantilever 12 includes head linking arm and camera support 13, and head linking arm one end is connected with union joint 121, the other end
It is connected with camera support 13.
Oscillating motor 14 is provided between camera support 13 and head linking arm.
Pitching motor 15 is provided between camera support 13 and camera 9.
The present invention also provides a kind of with above-mentioned integrally-built unmanned plane；The other structures of unmanned plane are prior art,
Will not be described here.
A kind of 10 overall structure of Distribution itineration check unmanned plane that the present invention is provided, simple structure, easy to use, 24 energy of undercarriage
Enough with 9 synchronous axial system of camera of unmanned plane 10, so as to avoid in prior art, during cloud platform rotation, undercarriage 24 affects phase
Machine 9 shoots the problem in the visual field, so as to improve shooting effect.
Meanwhile, 9 grade carry of camera is arranged on shock-damping structure, additionally it is possible to play during unmanned plane 10 flies and subtract
The effect of shake, improves the quality for shooting.
Finally it should be noted that：Various embodiments above only in order to technical scheme to be described, rather than a limitation；To the greatest extent
Pipe has been described in detail to the present invention with reference to foregoing embodiments, it will be understood by those within the art that：Its according to
So the technical scheme described in foregoing embodiments can be modified, or which part or all technical characteristic are entered
Row equivalent；And these modifications or replacement, do not make the essence of appropriate technical solution depart from various embodiments of the present invention technology
The scope of scheme.
Claims (10)
1. a kind of Distribution itineration check unmanned plane overall structure, it is characterised in that including the electric platform that arranges below unmanned plane and rise
Fall frame, and electric platform includes motor, installation pedestal and mounting platform；
Electric platform is fixedly connected with unmanned motor spindle by installation pedestal, and one end of motor is fixedly connected in installation pedestal,
The other end of motor is connected with mounting platform, and drive installation plateau levels are rotated；
The undercarriage is rotatably arranged in the bottom of unmanned plane, and is fixedly connected with the mounting platform, and flat with installing
Platform synchronous axial system.
2. Distribution itineration check unmanned plane overall structure according to claim 1, it is characterised in that can turn under the unmanned plane
Mounting bracket is provided with dynamicly；The mounting bracket is fixedly connected with the mounting platform；The undercarriage passes through mounting bracket
Rotationally it is lifted on below unmanned plane.
3. Distribution itineration check unmanned plane overall structure according to claim 2, it is characterised in that the mounting bracket includes ring
Shape fixed disk, annular rotary table and connector, in vertical direction, the annular fixed disk is holding annular rotary table；In level side
Upwards, the annular fixed disk and annular rotary table concentric and can relative engagement rotate connection；The annular rotary table is by connection
Part is fixedly connected with the mounting platform.
4. Distribution itineration check unmanned plane overall structure according to claim 3, it is characterised in that the annular rotary table with described
Pushing tow bearing is provided between annular fixed disk.
5. Distribution itineration check unmanned plane overall structure according to claim 1, it is characterised in that arrange on the mounting platform
The mounting seat having for fixed camera, is provided with damping module between installing plate and the mounting platform.
6. Distribution itineration check unmanned plane overall structure according to claim 5, it is characterised 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 set horizontal by degree inclination
Put, on intermediate plate, be provided with wire rope spring；
During installation, the bottom of rubber spring is fixedly connected with mounting platform, and installing plate is then fixedly installed on wire rope spring.
7. Distribution itineration check unmanned plane overall structure according to claim 5, it is characterised in that camera is fixed on by cantilever
In the mounting seat；Installing hole is provided with mounting seat, and the union joint of the cantilever is removably inserted into the installation in the hole；
The locking mechanism of both lockings is provided between union joint and the mounting seat.
8. Distribution itineration check unmanned plane overall structure according to claim 7, it is characterised in that the locking mechanism be
Shape clamp, the two ends of semi-circular clamp are hinged and connected in the mounting seat, and the middle part of semi-circular clamp is provided with dop；The company
The chuck for matching with the dop is provided with joint, after union joint is inserted into the installation in the hole, screws off the semi-circular
Clamp, the dop is connected in chuck to prevent the union joint from departing from from the hole is installed.
9. Distribution itineration check unmanned plane overall structure according to claim 8, it is characterised in that the dop and the chuck
Between be provided with retaining mechanism, the retaining mechanism is that hoodle jackscrew, hoodle jackscrew is arranged in the dop or chuck, institute
State chuck or dop and hoodle jackscrew corresponding position is provided with hole clipping.
10. the integrally-built unmanned plane of a kind of Distribution itineration check unmanned plane with described in any one of claim 1-9.
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 |
Applications Claiming Priority (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 |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN106428596A true CN106428596A (en) | 2017-02-22 |
| CN106428596B CN106428596B (en) | 2018-09-11 |
Family
ID=58180696
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|---|---|---|---|
| CN201610972395.0A Expired - Fee Related 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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Cited By (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 |
| CN109178330A (en) * | 2018-09-27 | 2019-01-11 | 哈尔滨理工大学 | A kind of UAV flight's camera fixing support |
| 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 |
| CN110001948A (en) * | 2019-04-30 | 2019-07-12 | 南京涵铭置智能科技有限公司 | A kind of double blades shooting unmanned plane and its application method |
| 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 |
| CN110621581A (en) * | 2018-03-14 | 2019-12-27 | 深圳市大疆创新科技有限公司 | Installation mechanism, undercarriage, frame 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 |
| 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 |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| 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 |
| US20150298799A1 (en) * | 2014-04-22 | 2015-10-22 | Blaise Bertrand | Quadcopter with a printable payload extension system and method |
| CN105292475A (en) * | 2015-11-12 | 2016-02-03 | 甘肃上航电力运维有限公司 | Infrared aerial photographic system for large power station and infrared aerial photographic method |
| 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 |
| CN206012947U (en) * | 2016-08-31 | 2017-03-15 | 北京深远世宁科技有限公司 | A kind of unmanned plane undercarriage, unmanned plane |
-
2016
- 2016-10-28 CN CN201610972395.0A patent/CN106428596B/en not_active Expired - Fee Related
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20150298799A1 (en) * | 2014-04-22 | 2015-10-22 | Blaise Bertrand | Quadcopter with a printable payload extension system and method |
| 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 |
| CN105292475A (en) * | 2015-11-12 | 2016-02-03 | 甘肃上航电力运维有限公司 | Infrared aerial photographic system for large power station and infrared aerial photographic method |
| 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 |
| CN206012947U (en) * | 2016-08-31 | 2017-03-15 | 北京深远世宁科技有限公司 | A kind of unmanned plane undercarriage, unmanned plane |
Cited By (13)
| 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 |
| 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 |
| CN110461709A (en) * | 2018-03-14 | 2019-11-15 | 深圳市大疆创新科技有限公司 | The undercarriage and rack, unmanned plane of a kind of rotating mechanism, unmanned plane |
| CN110621581A (en) * | 2018-03-14 | 2019-12-27 | 深圳市大疆创新科技有限公司 | Installation mechanism, undercarriage, frame 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 |
| CN109178330A (en) * | 2018-09-27 | 2019-01-11 | 哈尔滨理工大学 | A kind of UAV flight's camera fixing support |
| 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 |
| CN110001948A (en) * | 2019-04-30 | 2019-07-12 | 南京涵铭置智能科技有限公司 | A kind of double blades shooting unmanned plane and its application method |
| 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 |
| WO2021253287A1 (en) * | 2020-06-17 | 2021-12-23 | 深圳市大疆创新科技有限公司 | Pan-tilt, 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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