CN106715268A - Holder fixing support and UAV including the same - Google Patents
Holder fixing support and UAV including the same Download PDFInfo
- Publication number
- CN106715268A CN106715268A CN201680002495.9A CN201680002495A CN106715268A CN 106715268 A CN106715268 A CN 106715268A CN 201680002495 A CN201680002495 A CN 201680002495A CN 106715268 A CN106715268 A CN 106715268A
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- China
- Prior art keywords
- head
- fuselage
- fixed mount
- main part
- unmanned plane
- Prior art date
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- Granted
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- 238000009434 installation Methods 0.000 description 7
- 238000000034 method Methods 0.000 description 5
- 230000008901 benefit Effects 0.000 description 4
- 230000005489 elastic deformation Effects 0.000 description 4
- 238000010586 diagram Methods 0.000 description 3
- 230000006978 adaptation Effects 0.000 description 2
- 230000000694 effects Effects 0.000 description 2
- 230000009471 action Effects 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 239000000686 essence Substances 0.000 description 1
- 239000000463 material Substances 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000008569 process Effects 0.000 description 1
- 230000000452 restraining effect Effects 0.000 description 1
- 238000006467 substitution reaction Methods 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U20/00—Constructional aspects of UAVs
- B64U20/80—Arrangement of on-board electronics, e.g. avionics systems or wiring
- B64U20/87—Mounting of imaging devices, e.g. mounting of gimbals
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- Engineering & Computer Science (AREA)
- Microelectronics & Electronic Packaging (AREA)
- Mechanical Engineering (AREA)
- Remote Sensing (AREA)
- Aviation & Aerospace Engineering (AREA)
- Studio Devices (AREA)
- Accessories Of Cameras (AREA)
Abstract
The invention provides a holder fixing support and a UAV including the same. The holder fixing support (6) comprises a main body part (61), a snap part (62) for fixing to a UAV body (71) of a UAV (7) and a positioning part (63) for limiting the motion of a holder (72). The positioning part (63) comprises a positioning space (634) for holding at least a part of the holder (72). The holder fixing support (76) is connected with the holder (72) of the UAV (7) and is fixed to the UAV body (71) of the UAV (7), thereby limiting the relative movement of the holder (72) to the UAV body (71) of the UAV (7). The holder fixing support (6) has a small size, can be detachably connected with the UAV body (71) of the UAV (7), and is convenient in operation.
Description
Technical field
The application is related to unmanned plane field, especially a kind of head fixed mount and the unmanned plane with the head fixed mount.
Background technology
In the prior art, head is typically all to be mounted on unmanned plane.Head and installation in transport or carrying process
There are device for shooting head and the fuselage of unmanned plane to be also easy to produce relative motion, cause head and the device for shooting on head cannot get
Protection.
Existing head fixed rack structure is broadly divided into two parts, and a part is fixed with device for shooting camera lens, another part and
The propeller frame of unmanned aerial vehicle body is fixed.Because propeller frame typically has a certain distance with unmanned aerial vehicle body, so
The volume of head fixed mount of the prior art just becomes very greatly and unsightly, to be also susceptible to come off in transportation etc. existing
As, and need to fix respectively the part fixed with device for shooting camera lens and the propeller frame with unmanned aerial vehicle body when mounted
Fixed part, inconvenient operation.
The content of the invention
The application provides a kind of head fixed mount and the unmanned plane with the head fixed mount.
According to the first aspect of the embodiment of the present application, there is provided a kind of head fixed mount, the fuselage for being installed on unmanned plane
On, be fixed for carry device for shooting head, the head fixed mount include main part, be arranged on main part to
Access Division and be used to limit the location division of the head motion that the fuselage of unmanned plane is fixed, wherein the location division includes using
In the located space for accommodating at least partly head.
According to the second aspect of the embodiment of the present application, there is provided a kind of unmanned plane, including fuselage, the cloud for carrying device for shooting
Platform, the unmanned plane also includes being installed on the fuselage of unmanned plane, is used to fix the head fixed mount of the device for shooting；The head
Fixed mount includes main part, the Access Division fixed with the fuselage of unmanned plane being arranged on the main part and is used to limit described
The location division of head motion, wherein the location division includes the located space for head described in accommodating portion.
According to the third aspect of the embodiment of the present application, there is provided a kind of unmanned plane, including fuselage, the cloud for carrying device for shooting
Platform, the unmanned plane also includes the head fixed mount being arranged between the fuselage and head, device for shooting, the head fixed mount
So that the head and device for shooting are fixed relative to the fuselage；The head fixed mount includes and the fuselage fixation of unmanned plane
Access Division and being used to limits the location division of the head motion.
The technical scheme that embodiments herein is provided can include the following benefits：The head fixed mount has body
Product it is small, can be detachably connected with the fuselage of unmanned plane and easy to operate advantage.
Brief description of the drawings
Fig. 1 is a kind of the first axonometric drawing of the head fixed mount shown in the embodiment of the present application.
Fig. 2 is a kind of the second axonometric drawing of the head fixed mount shown in the embodiment of the present application.
Fig. 3 is a kind of front view of the head fixed mount shown in the embodiment of the present application.
Fig. 4 is a kind of schematic diagram of the fuselage with the installation of head fixed mount of the unmanned plane shown in the embodiment of the present application.
Fig. 5 is the axonometric drawing of the fuselage, head and the connection of head fixed mount of a kind of unmanned plane shown in the embodiment of the present application.
Fig. 6 is the front view of the fuselage, head and the connection of head fixed mount of a kind of unmanned plane shown in the embodiment of the present application.
Fig. 7 is a kind of schematic diagram of the unmanned plane equipped with head fixed mount shown in the embodiment of the present application.
Specific embodiment
Here exemplary embodiment will be illustrated in detail, its example is illustrated in the accompanying drawings.Following description 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 implementation method do not represent all implementation methods consistent with the application.Conversely, they be only with it is such as appended
The example of the consistent apparatus and method of some aspects described in detail in claims, the application.
Below in conjunction with the accompanying drawings, some embodiments of the present invention are elaborated.It is following in the case where not conflicting
Feature in embodiment and embodiment can be mutually combined.
Refer to Fig. 1 to Fig. 5, a kind of unmanned plane 7 shown in the application implementation method, including fuselage 71, for carry clap
Take the photograph the head 72 of device 73 and be installed on the fuselage 71 of unmanned plane 7, be used to fix the head fixed mount 6 of the head 72.
The head fixed mount 6 includes main part 61, is arranged at consolidating to the fuselage 71 with unmanned plane 7 on main part 61
Fixed Access Division 62, and it is used to limit the location division 63 of the motion of the head 72.The Access Division 62 and the fuselage of unmanned plane 7
71 clampings are connected, and the main part 61 of the head fixed mount 6 is connected with the fuselage 71 of the unmanned plane 7 and fixed.It is i.e. described
The connection spacing with the head 72 of unmanned plane 7 of head fixed mount 6 is simultaneously fixed with the fuselage 71 of unmanned plane 7, so as to limit head 72
With respect to the relative motion of fuselage 71 of unmanned plane 7.
Referring in particular to shown in Fig. 1, the location division 63 includes the located space for accommodating at least part of head 72
634.The located space 634 can accommodate the part-structure of the head 72.The part-structure be install device for shooting 73 or
The structure of the limitation movement of device for shooting 73.Shown in reference picture 6, in one embodiment, the part-structure refers to the armshaft of head 72
721.The inner side of location division 63 described in the present embodiment forms the located space 634, and the boundary of the located space 634 can be with
The outer surface contact connection of the structure of part head 72 is used to constrain head 72, so as to limit the front and rear dynamic of head 72, left and right
Mobile and rotation.
In the present embodiment, head fixed mount 6 is fixed by Access Division 62 with the fuselage 71 of unmanned plane 7, fixes head
The main part 61 of frame 6 is fixed relative to fuselage 7.The location division 63 and its located space 634 constrain the motion of head.The card
Socket part 62 is connected and fixed with fuselage 7, facilitates the attended operation of head fixed mount 6 and fuselage 71, and head fixed mount 6 clamping
Portion 62 and the simple structure of location division 63 occupancy installation volume are small, and installation site is between the fuselage 71 of unmanned plane 7 and head 72,
Installing space is taken full advantage of, the overall appearance of unmanned plane is not influenceed.
As shown in fig. 7, in the present embodiment, supporting part 622 and the fuselage of unmanned plane that the both sides of the main part 61 are set
Connect and fix.With reference to shown in Fig. 1 and Fig. 2, the Access Division 62 includes the supporting part 622 positioned at the both sides of the main part 61, institute
Stating supporting part 622 can also be located at the top of the main part 61 or rear portion etc., and be arranged on the outside of the upper end of the supporting part 622
Lug boss 621.The lug boss 621 is connected with the fuselage clamping of unmanned plane, and the supporting part 622 connects institute as support member
Main part 61 is stated, so that the main part 61 is relatively fixed relative to the fuselage of unmanned plane.The setting of the Access Division 62 simplifies
The fuselage attended operation of head fixed mount 6 and unmanned plane, it is only necessary to a step snap action.
Further, above-mentioned lug boss 621 is set to arc-shaped convex, the fuselage 71 of the unmanned plane be provided with it is described
The draw-in groove 711 that the lug boss 621 of Access Division 62 coordinates, as shown in Figure 4.The slot structure of the draw-in groove 711 and the lug boss 621
Arc-shaped convex snapping, complete being fixedly connected for the head fixed mount 6 and fuselage 7.The shape of certain lug boss 621
Shape may be alternatively provided as other shapes, such as trapezoidal.
As shown in figure 1, open up insulating space 623 in the side of the Access Division 62 being separated by with a part for the main part 61
From making the supporting part 622 of the Access Division 62 has more preferable elastic deformation function.By the head fixed mount 6 and the machine
The supporting part 622 produces elastic deformation to adapt to the installing space of the fuselage 7 when body 7 is connected.The insulating space 623 is located at
Between guide part 65 on the Access Division 62 and main part 61, on this, will describe in detail later.
As shown in Figures 2 and 3, the location division 63 also includes the intermediate plate 631 to coordinate with the head 72.The folder
Piece 631 is connected with the gap of the head 72.As shown in fig. 6, in the present embodiment, the head 72 includes that a grafting is empty
Between 723, the intermediate plate 631 inserts the grafting space 723 and is used to constrain the movable of head.The shape of grafting space 723
Between the component of head 72 described in Cheng Yu.Head 72 described in the present embodiment includes armshaft 721 and head shield line plate 722, described
Grafting space 723 is located between the armshaft 721 and head shield line plate 722.I.e. described intermediate plate 631 is plugged on the armshaft
In gap between 721 and head shield line plate 722, it is used to limit the movable of head.
Further, as shown in figures 1 and 3, the location division 63 also includes two side 633, and the intermediate plate 631 is arranged at
The inner side of the side wall 633 is simultaneously extended in the located space 634.In the present embodiment, with reference to shown in Fig. 6, the head 72
Including armshaft 721, the two side 633 is semicircle side wall, and the two side 633 is fitted simultaneously with the armshaft 721 of the head 72
The armshaft 721 is clamped to be used to constrain moving left and right (i.e. Fig. 6 directions is movable) for head.In one embodiment, described two
Side wall 633 clamps the implementation of the armshaft 721, includes but is not limited to make the encircling space between the inwall of two side 633
Volume is slightly less than the volume that the armshaft 721 is surrounded part, to increase restraining force.
With reference to shown in Fig. 5, the location division 63 also include be arranged at the bottom of the main part 61, to the head 72
The fluting 632 of adaptation, the wherein fluting 632 are connected with the located space 634.Fluting 632 is arranged at described in the present embodiment
The bottom of the main part 61, to be adapted to the camera lens conduit bushing 724, as shown in Figure 2.The fluting 632 is located at described two
Between side wall 633, i.e., positioned at the bottom of the main part 61.The head 72 includes camera lens conduit bushing 724, the fluting 632
The structure setting of the correspondence head 72, as shown in Figure 6 and Figure 7, the fluting 632 is stuck in the both sides of camera lens conduit bushing 724,
The bottom of the head 72 is limited, the head 72 limits rotation of the head 72 along rotary shaft.
Further, the head fixed mount 6 is used to be installed on the fuselage 71 of unmanned plane 7, is shot with being fixed for carrying
The head 72 of device 73.As shown in Figure 1, Figure 2 and Figure 4, the head fixed mount 6 also includes being arranged on the main part 61 being used to
The guide part 65 coordinated with the fuselage 71 of unmanned plane 7, the guide part 65 can make the head fixed mount 6 relative to the machine
Body 71 is slided along preset direction, until the Access Division 62 fastens with the fuselage 71.The guide part 65 is installed and is oriented to
Effect, wherein the guide part 65 can be guide rail or spigot surface.With reference to shown in Fig. 5, the guide part 65 includes guide ramp
651, the fuselage 71 of the unmanned plane 7 is provided with the chute 712 coordinated with the guide ramp 651.
The guide part 65 is arranged on the both sides of the main part 61 in the present embodiment.The guide part 65 is set to ladder
Shape or triangle, are raised on the lateral wall of the main part 61.In trapezoidal or triangle sides, guide ramp 651 and institute are set
State the relative slip of chute 712 and clamping.Two guide parts 65 can further be fixed described after being adapted to the chute 712
The connection of head fixed mount 6 and the fuselage 7.Certainly may also set up a guide part 65 in the suitable position of main part 61,
Make the convenient installation of head fixed mount 6.
As shown in figures 1 and 3, the main part 61 of the head fixed mount 6 includes top 67 and bottom 66, wherein described lead
The top 67 of the main part 61 is arranged on to portion 65 and Access Division 62, the location division 63 is arranged under the main part 61
Portion 66.The guide part 65 is arranged at the both sides on the top 67 of the main part 61, and the guide part 65 with the Access Division 62
Insulating space 623 is provided between the Access Division 62.
The both sides of top 67 of the head fixed mount 6 are respectively provided with Access Division 62 described in guide part 65 and described in, institute
State guide part 65 to be connected with the chute 712 of the fuselage 71, the Access Division 62 is connected with the draw-in groove 711 of the fuselage 71, such as
Shown in Fig. 4.Insulating space 623 is provided between the guide part 65 and the Access Division 62, the insulating space 623 makes the clamping
The elastic deformation of supporting part 622 in portion 62, when head fixed mount 6 is connected with fuselage 71, the supporting part 622 is to head fixed mount
6 inner elastic deformation, when the lug boss 621 of Access Division 62 is adapted to the draw-in groove 711 of fuselage 71, the supporting part 622 is extensive
Complex deformation.The installation and clamping that are provided with beneficial to the head fixed mount 6 of the insulating space 623.
As shown in figure 1, the main part 61 of the head fixed mount 6 also includes middle part 64 and is arranged on the main part 61
64 liang of the middle part Handheld Division in outside 641.The setting of the Handheld Division 641 facilitates the hand-held head fixed mount 6, the Handheld Division 641
With anti-skidding effect.
As shown in Fig. 1, Fig. 4 to Fig. 7, when using, the head fixed mount 6 is placed in the head 72 with the fuselage 71
Between, the guide part 65 of the head fixed mount 6 is aligned with the chute 712 set on fuselage 71, is pushed.The guide part 65
Slided along the chute 712, until the snapping of draw-in groove 711 set on the lug boss 621 of the Access Division 62 and the fuselage 71.
Now the location division 63 of the head fixed mount 6 is connected with the head 72 and limits the motion of the head 72.That is location division
63 intermediate plate 631 coordinates the movable of the limitation head 72 with the grafting space 723 of the head 72；The location division 63
Two side 633 surround the part armshaft 721 of institute head 72 and limit moving left and right for the head 72；The location division 63 is opened
Groove 632 is adapted to the rotation for limiting the head 72 with the camera lens conduit bushing 724 of the head 72.The head fixed mount 6 and nothing
State diagram during man-machine 7 71 installation of fuselage is as shown in Figure 7.
As shown in Fig. 1, Fig. 4 to Fig. 7, the application also provides a kind of unmanned plane 7.The unmanned plane 7 includes fuselage 71, is used for
The head 72 for carrying device for shooting 73, the head fixed mount 6 being arranged between the fuselage 71 and head 72, device for shooting 73.Should
Head fixed mount 6 causes that the head 72 and device for shooting 73 are fixed relative to the fuselage 71.The head fixed mount 6 include with
Access Division 62 and be used to limit the location division 63 of the motion of the device for shooting 73 that the fuselage 71 of unmanned plane 7 is fixed.The application's
The head locating rack 6 has same or similar structure with the head fixed mount 6 of above-described embodiment of the application, herein
Repeat no more.
The head fixed mount 6 is arranged between the head 72 of unmanned plane 7 and fuselage 71, makes the head 72 and device for shooting
73 fix relative to the fuselage 71, realize and the device for shooting 73 and the head 72 are set near the fixation of the fuselage 71
Put.
As shown in Figure 1 and Figure 4, the Handpiece Location 74 of the fuselage 71 is provided with the holding part for receiving the head 72
741, the holding part 741 is provided with roof 7411 and two opposing sidewalls 7412 being connected with the roof 7411, the cloud
Platform 72 is detachably connected with the roof 7411, and the Access Division 62 is two, respectively with the phase of described two opposing sidewalls 7412
Clamping.Described two opposing sidewalls 7412 are provided with draw-in groove 711 with the clamping of the Access Division 62.
Described two opposing sidewalls 7412 also include chute 712, and the head fixed mount 6 includes guide part 65, described to lead
It is connected with the adaptation of the chute 712 to portion 65.
The head fixed mount 6 is connected with the head 72 of unmanned plane 7 and is fixed with the fuselage of unmanned plane 7, so as to limit
The fuselage relative motion of the relative unmanned plane 7 of head 72, and the overall appearance of unmanned plane is not influenceed.Further, the head is consolidated
Determining frame 6 has the advantages that small volume, installing space are small, can be detachably connected with the fuselage of unmanned plane and easy to operate.
The preferred embodiment of the application is the foregoing is only, is not used to limit the application, all essences in the application
Within god and principle, any modification, equivalent substitution and improvements done etc. should be included within the scope of the application protection.
This patent document disclosure includes material protected by copyright.The copyright is all for copyright holder.Copyright
Owner does not oppose that anyone replicates the patent document in the presence of the proce's-verbal of Patent＆Trademark Office and archives or is somebody's turn to do
Patent is disclosed.
Claims (20)
1. a kind of head fixed mount, the fuselage for being installed on unmanned plane, to be fixed for carrying the head of device for shooting, it is special
Levy and be, the head fixed mount includes main part, the clamping fixed to the fuselage with unmanned plane being arranged on main part
Portion and being used to limits the location division of the head motion, wherein the location division is included for accommodating at least part of head
Located space.
2. head fixed mount according to claim 1, it is characterised in that the Access Division includes being located at the main part two
The supporting part of side, and it is arranged at the lug boss on the outside of the supporting part upper end.
3. head fixed mount according to claim 1, it is characterised in that the location division also includes being used to and the head
The intermediate plate of cooperation.
4. head fixed mount according to claim 3, it is characterised in that the location division includes two side, the intermediate plate
It is arranged at the inner side of the side wall and extends in the located space.
5. head fixed mount according to claim 1, it is characterised in that the location division also includes being arranged at the main body
Portion bottom, the fluting to be adapted to the head, the wherein fluting are connected with the located space.
6. head fixed mount according to claim 1, it is characterised in that also including be arranged on the main part be used to
The guide part that the fuselage of unmanned plane coordinates, the guide part can make the head fixed mount relative to the fuselage along default side
To slip, until the Access Division fastens with the fuselage.
7. head fixed mount according to claim 6, it is characterised in that the main part includes upper and lower part, wherein
The guide part and Access Division are arranged on the top of the main part, and the location division is arranged on the bottom of the main part.
8. head fixed mount according to claim 7, it is characterised in that the guide part is arranged at institute with the Access Division
State and be provided with insulating space between the both sides on main part top, and the guide part and the Access Division.
9. head fixed mount according to claim 7, it is characterised in that also including being arranged on outside the main part middle part two
The Handheld Division of side.
10. a kind of unmanned plane, including fuselage, the head for carrying device for shooting, it is characterised in that the unmanned plane also includes peace
On fuselage loaded on unmanned plane, it is used to fix the head fixed mount of the device for shooting；The head fixed mount includes main part, sets
In the Access Division of the fuselage fixation with unmanned plane on the main part and the location division for being used to limit the head motion, wherein
The location division includes the located space for device for shooting described in accommodating portion.
11. unmanned planes according to claim 10, it is characterised in that the Access Division includes being located at the main part both sides
Supporting part, and be arranged at the lug boss on the outside of the supporting part upper end；The fuselage is provided with the projection with the Access Division
The draw-in groove that portion coordinates.
12. unmanned planes according to claim 10, it is characterised in that the head includes a grafting space；The positioning
Portion also includes the intermediate plate with the grafting interference fit.
13. unmanned planes according to claim 12, it is characterised in that the head includes armshaft and head shield line plate, institute
Grafting is stated to be spatially located between the armshaft and head shield line plate.
14. unmanned planes according to claim 10, it is characterised in that the head includes camera lens conduit bushing, the positioning
Portion also includes being arranged at the main part bottom, the fluting to be adapted to the camera lens conduit bushing, wherein the fluting with it is described
Located space is connected.
15. unmanned planes according to claim 10, it is characterised in that the head fixed mount also includes being arranged at main part
The guide part that the upper fuselage to unmanned plane coordinates, the guide part can make the head fixed mount relative to the fuselage
Slided along preset direction, until the Access Division fastens with the fuselage.
16. unmanned planes according to claim 10, it is characterised in that the main part includes upper and lower part, wherein institute
State guide part and the Access Division is arranged on the top of the main part, the location division is arranged on the bottom of the main part.
17. unmanned planes according to claim 16, it is characterised in that the guide part is arranged at described with the Access Division
Insulating space is provided between the both sides on main part top, and the guide part and the Access Division.
18. unmanned planes according to claim 16, it is characterised in that the head fixed mount also includes being arranged on the master
The Handheld Division in the outside of body portion middle part two.
A kind of 19. unmanned planes, including fuselage, the head for carrying device for shooting, it is characterised in that the unmanned plane also includes setting
The head fixed mount being placed between the fuselage and head, device for shooting, the head fixed mount causes the head and device for shooting
Fixed relative to the fuselage；The head fixed mount includes the Access Division fixed with the fuselage of unmanned plane and is used to limit institute
State the location division of head motion.
20. unmanned planes according to claim 19, it is characterised in that the Handpiece Location of the fuselage is provided with for receiving
State the holding part of head, the holding part is provided with roof and two opposing sidewalls being connected with the roof, the head with
The roof is detachably connected, and the Access Division is two, respectively with described two opposing sidewalls phase clampings.
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| PCT/CN2016/099528 WO2018053697A1 (en) | 2016-09-21 | 2016-09-21 | Head fixing mount and unmanned aerial vehicle having same |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN106715268A true CN106715268A (en) | 2017-05-24 |
| CN106715268B CN106715268B (en) | 2019-04-23 |
Family
ID=58903817
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201680002495.9A Expired - Fee Related CN106715268B (en) | 2016-09-21 | 2016-09-21 | Holder fixed frame and unmanned plane with the holder fixed frame |
Country Status (2)
| Country | Link |
|---|---|
| CN (1) | CN106715268B (en) |
| WO (1) | WO2018053697A1 (en) |
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| CN107878774A (en) * | 2017-11-30 | 2018-04-06 | 广州市华科尔科技股份有限公司 | A kind of unmanned machine head |
| CN110869282A (en) * | 2018-06-26 | 2020-03-06 | 深圳市大疆创新科技有限公司 | Unmanned aerial vehicle and fuselage, cloud platform camera thereof |
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| CN204254205U (en) * | 2014-09-26 | 2015-04-08 | 深圳市大疆创新科技有限公司 | Fixed mechanism and use the The Cloud Terrace of this fixed mechanism |
| WO2016112124A2 (en) * | 2015-01-08 | 2016-07-14 | Vantage Robotics, Llc | Unmanned aerial vehicle with propeller protection and high impact survivability |
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- 2016-09-21 WO PCT/CN2016/099528 patent/WO2018053697A1/en active Application Filing
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| US20150014503A1 (en) * | 2013-07-15 | 2015-01-15 | Richard Earl Owen | Strut mount |
| CN203461140U (en) * | 2013-09-10 | 2014-03-05 | 北京臻迪科技有限公司 | Unmanned aerial vehicle |
| CN203832759U (en) * | 2014-04-04 | 2014-09-17 | 田瑜 | Plastic camera bracket applied to holder |
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| CN107856851A (en) * | 2017-11-30 | 2018-03-30 | 广州市华科尔科技股份有限公司 | A kind of compact collapsible unmanned plane |
| CN107878774A (en) * | 2017-11-30 | 2018-04-06 | 广州市华科尔科技股份有限公司 | A kind of unmanned machine head |
| CN110869282A (en) * | 2018-06-26 | 2020-03-06 | 深圳市大疆创新科技有限公司 | Unmanned aerial vehicle and fuselage, cloud platform camera thereof |
Also Published As
| Publication number | Publication date |
|---|---|
| CN106715268B (en) | 2019-04-23 |
| WO2018053697A1 (en) | 2018-03-29 |
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Effective date of registration: 20170516 Address after: 518057 Guangdong city of Shenzhen province Nanshan District Guangdong streets south four Road No. 18 building in the West SKYWORTH semiconductor design 12 Applicant after: SZ DJI OSMO TECHNOLOGY Co.,Ltd. Address before: 518057 Guangdong province Shenzhen city Nanshan District high tech Zone South Hing a No. 9 Hongkong, Shenzhen building 6 floor Applicant before: SZ DJI TECHNOLOGY Co.,Ltd. |
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