CN106081141A - Many rotor wing unmanned aerial vehicles - Google Patents
Many rotor wing unmanned aerial vehicles Download PDFInfo
- Publication number
- CN106081141A CN106081141A CN201610405413.7A CN201610405413A CN106081141A CN 106081141 A CN106081141 A CN 106081141A CN 201610405413 A CN201610405413 A CN 201610405413A CN 106081141 A CN106081141 A CN 106081141A
- Authority
- CN
- China
- Prior art keywords
- cloud terrace
- chamber
- unmanned aerial
- rotor wing
- wing unmanned
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Pending
Links
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
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U10/00—Type of UAV
- B64U10/10—Rotorcrafts
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U2101/00—UAVs specially adapted for particular uses or applications
- B64U2101/30—UAVs specially adapted for particular uses or applications for imaging, photography or videography
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Remote Sensing (AREA)
- Accessories Of Cameras (AREA)
Abstract
The invention provides many rotor wing unmanned aerial vehicles, rotor wing unmanned aerial vehicle, including: fuselage and tripod head frame, The Cloud Terrace lifting controller and The Cloud Terrace crane；The bottom of fuselage is offered The Cloud Terrace and is accommodated chamber；It is corresponding to the profile of video camera to be placed that The Cloud Terrace accommodates chamber, and the bottom that tripod head frame accommodates chamber by The Cloud Terrace crane with The Cloud Terrace is flexibly connected；The outfan of The Cloud Terrace lifting controller is connected with the raise-lower hydraulic motor of The Cloud Terrace crane, when The Cloud Terrace lifting controller receives recovery video camera information, drive hydraulic motor to drive The Cloud Terrace crane to regain, make the video camera to be placed being carried in tripod head frame be recovered to The Cloud Terrace and accommodate in chamber.Thus the apparatus for making a video recording solving existing many rotor wing unmanned aerial vehicles disposes the problem that reliability is low.Thus, improve the apparatus for making a video recording reliability when unmanned plane during flying, ensure that reliability when apparatus for making a video recording uses, extend equipment service life, reduce use and maintenance cost.
Description
Technical field
The present invention relates to unmanned air vehicle technique field, particularly relate to many rotor wing unmanned aerial vehicles.
Background technology
Many rotor wing unmanned aerial vehicles, as the one of unmanned plane, are widely used in military and civil area, at civil area
Application process in, being mainly used in takes photo by plane etc. freely shoot during.And there is the functions such as navigation, automatic lifting/lowering support.Existing
Many rotor wing unmanned aerial vehicles during taking photo by plane, the installation forms using picture pick-up devices underlying more.This form during taking photo by plane, when
When unmanned plane collides, easily cause the damage of picture pick-up device.For the problems referred to above, use of those skilled in the art reinforces video camera more
The mode of bracing frame realizes, but which, when impulsive force is bigger, if bracing frame blastic deformation, also will be to apparatus for making a video recording
Cannot be carried out protection.It follows that the placement safety of the apparatus for making a video recording of many rotor wing unmanned aerial vehicles of the prior art is low, use the longevity
Order short and maintenance cost is high.
Summary of the invention
For above-mentioned defect of the prior art, it is an object of the invention to provide many rotor wing unmanned aerial vehicles.Thus solve existing
The apparatus for making a video recording having many rotor wing unmanned aerial vehicles disposes the problem that reliability is low.
In order to achieve the above object, the present invention provides following technical scheme:
Many rotor wing unmanned aerial vehicles, including: fuselage and tripod head frame, described tripod head frame is arranged at the lower section of described fuselage；Wherein, bag
Include: The Cloud Terrace lifting controller and The Cloud Terrace crane；The bottom of described fuselage is offered The Cloud Terrace and is accommodated chamber；Described The Cloud Terrace accommodates chamber and treats
The profile placing video camera is corresponding, and described tripod head frame accommodates the bottom activity in chamber even by described The Cloud Terrace crane and described The Cloud Terrace
Connect；The outfan of described The Cloud Terrace lifting controller is connected with the raise-lower hydraulic motor of described The Cloud Terrace crane, when described The Cloud Terrace liter
When drop controller receives recovery video camera information, drive described hydraulic motor to drive described The Cloud Terrace crane to regain, make carrying
Video camera to be placed in described tripod head frame is recovered to The Cloud Terrace and accommodates in chamber；Transfer when described The Cloud Terrace lifting controller receives
During video camera information, drive described hydraulic motor to drive described The Cloud Terrace crane to stretch out, make to be carried on treating in described tripod head frame
Place video camera to stretch out from described The Cloud Terrace receiving chamber.
In a preferred embodiment, also include: distance measuring sensor and velocity sensor；Distance measuring sensor and speed
The outfan of sensor is connected with described The Cloud Terrace lifting controller, and described distance measuring sensor obtains obstacle distance information；Described
Velocity sensor obtains current velocity amplitude；If described obstacle distance information is setting value, then judge that described velocity amplitude is
No for setting value, the most then send to described The Cloud Terrace lifting controller and reclaim video camera information.
In a preferred embodiment, also include: direction information test cell, the output of direction information test cell
End is connected with the input of The Cloud Terrace lifting controller, and described direction information test cell is to turning to activation bit to be acquired；If
Activation bit is turned to, then according to reclaiming setpoint distance value generation recovery video camera information described in collecting；Lift to described The Cloud Terrace
Controller sends this recovery video camera information.
In a preferred embodiment, also include: air velocity transducer；The outfan of described air velocity transducer is with described
The input of The Cloud Terrace lifting controller connects, and described air velocity transducer gathers current air speed value；According to described current air speed value with
Wind speed setting reclaims setpoint distance value synopsis, obtains current recovery setpoint distance value.
In a preferred embodiment, upper surface or the bottom surface of described fuselage offers air velocity transducer installing hole；
Described air velocity transducer is fixedly installed in described air velocity transducer installing hole.
In a preferred embodiment, the bore edges of described air velocity transducer installing hole is arc, along described wind speed
Sensor mounting hole laterally or longitudinally offer wind-guiding groove, the bottom of described wind-guiding groove offer arc hold wind chamber；Described lead
The bottom of wind groove is to the lopsidedness of described air velocity transducer installing hole.
In a preferred embodiment, the width of described wind-guiding groove is 3～5mm.
In a preferred embodiment, also include: The Cloud Terrace seals lid；Described The Cloud Terrace seals edge shape and the institute of lid
Stating The Cloud Terrace and accommodate the opening in chamber accordingly, side is connected by return spring is fixing with the edge of opening in described The Cloud Terrace receiving chamber, when
Video camera to be placed in described tripod head frame is regained when described The Cloud Terrace accommodates in chamber, time described The Cloud Terrace seal cap sealing be fastened on
Described The Cloud Terrace accommodates the opening part in chamber.
In a preferred embodiment, described film The Cloud Terrace seals the marginal center of lid and offers sealing strip groove, internal
Sealing strip is set.
In a preferred embodiment, the intracavity bottom in described The Cloud Terrace receiving chamber arranges drying layer.
The present invention the many rotor wing unmanned aerial vehicles having the beneficial effect that in the present invention by apparatus for making a video recording is recovered to unmanned plane
In cavity, thus improve unmanned plane and carry the arrangement reliability of apparatus for making a video recording.Further, lid is sealed to video camera by The Cloud Terrace
And The Cloud Terrace fixes further, thus, improve the apparatus for making a video recording reliability when unmanned plane during flying, ensure that apparatus for making a video recording
Reliability during use, extends equipment service life, reduces use and maintenance cost.
Accompanying drawing explanation
In order to be illustrated more clearly that the embodiment of the present invention or technical scheme of the prior art, below will be to embodiment or existing
In having technology to describe, the required accompanying drawing used is briefly described, it should be apparent that, the accompanying drawing in describing below is only this
Some embodiments of invention, for those of ordinary skill in the art, on the premise of not paying creative work, it is also possible to
Other accompanying drawing is obtained according to these accompanying drawings.
Fig. 1 is in one embodiment of the present invention, internal structure schematic diagram when many rotor wing unmanned aerial vehicles The Cloud Terrace stretches out；
Fig. 2 is in one embodiment of the present invention, the internal structure schematic diagram during The Cloud Terrace retraction of many rotor wing unmanned aerial vehicles；
Fig. 3 is in one embodiment of the present invention, the system connection diagram of many rotor wing unmanned aerial vehicles；
Fig. 4 is in one embodiment of the present invention, and the cross-section structure at the air velocity transducer on many rotor wing unmanned aerial vehicles surface shows
It is intended to；
Fig. 5 is in one embodiment of the present invention, the top surface structure signal of the air velocity transducer on many rotor wing unmanned aerial vehicles surface
Figure；
Fig. 6 is in one embodiment of the present invention, in Fig. 4 A-A to structural scheme of mechanism；
Fig. 7 is in another embodiment of the present invention, the internal structure schematic diagram during The Cloud Terrace retraction of many rotor wing unmanned aerial vehicles；
Fig. 8 is in another embodiment of the present invention, internal structure schematic diagram when many rotor wing unmanned aerial vehicles The Cloud Terrace stretches out.
Detailed description of the invention
Below in conjunction with the accompanying drawing of the present invention, technical scheme is clearly and completely described, it is clear that institute
The embodiment described is only a part of embodiment of the present invention rather than whole embodiments.Based on the embodiment in the present invention,
The every other embodiment that those of ordinary skill in the art are obtained under not making creative work premise, broadly falls into this
The scope of bright protection.
The invention discloses a kind of many rotor wing unmanned aerial vehicles, such as Fig. 1, shown in 2 and 3, including: fuselage 10 and tripod head frame 20, cloud
Stand 20 is arranged at the lower section of fuselage 10.And also include: The Cloud Terrace lifting controller 40 and The Cloud Terrace crane 30.The bottom of fuselage 10
Offering The Cloud Terrace and accommodate chamber 11, it is corresponding to the profile of video camera 12 to be placed that The Cloud Terrace accommodates chamber 11, and tripod head frame 20 is lifted by The Cloud Terrace
The bottom that frame 30 accommodates chamber 11 with The Cloud Terrace is flexibly connected；The outfan of The Cloud Terrace lifting controller 40 and the lifting of The Cloud Terrace crane 30
Hydraulic motor connects, and when The Cloud Terrace lifting controller 40 receives recovery video camera 12 information, drives hydraulic motor to drive The Cloud Terrace
Crane 30 is regained, and makes the video camera to be placed being carried in tripod head frame 20 be recovered to The Cloud Terrace and accommodates in chamber 11, as shown in Figure 2.
When The Cloud Terrace lifting controller 40 receives and transfers video camera information, drive hydraulic motor to drive The Cloud Terrace crane 30 to stretch out, make
The video camera to be placed 12 being carried in tripod head frame 20 stretches out, as shown in Figure 1 from The Cloud Terrace receiving chamber 11.
As it is shown on figure 3, for making unmanned plane when collision can be caused with barrier, can regain in time, in the one of the present invention
In embodiment, also include: distance measuring sensor 41 and velocity sensor 42.Distance measuring sensor 41 obtains obstacle distance information；
Velocity sensor 42 obtains current velocity amplitude；If obstacle distance information is setting value, then judge that whether velocity amplitude is for setting
Definite value, the most then send to The Cloud Terrace lifting controller 40 and reclaim video camera information.
As it is shown on figure 3, for making unmanned plane when turning to, reduce the vibrations of video camera 12, make The Cloud Terrace crane suitably regain
Its outer outstanding length, in one embodiment of the invention, also includes: direction information test cell 43, direction information test is single
Unit's outfan of 43 is connected with the input of The Cloud Terrace lifting controller 40.Direction information test cell 43 enters turning to activation bit
Row gathers；Activation bit is turned to, then according to reclaiming setpoint distance value generation recovery video camera 12 information if collecting；To The Cloud Terrace liter
Drop controller 40 sends this recovery video camera 12 information.Above-mentioned recovery setpoint distance value is preferably 5～10mm.For making above-mentioned shooting
Machine is in removal process, it is contemplated that the impact that wind speed impacts and produces, and in one embodiment of the invention, also includes: wind
Speed sensor 44；Air velocity transducer 44 gathers current air speed value；Setpoint distance value is reclaimed with wind speed setting according to current air speed value
Synopsis, obtains current recovery setpoint distance value.
For make above-mentioned air velocity transducer sensing time the most accurate, in one embodiment of the invention, such as Fig. 4 institute
Showing, upper surface or bottom surface at fuselage 10 offer air velocity transducer 44 installing hole 50.Air velocity transducer 44 is fixedly installed in wind
In speed sensor 44 installing hole 50.
For ease of the most accurate, as shown in Figure 5,6 to wind speed sensing, it is preferred that the hole of air velocity transducer 44 installing hole 50
Edge is arc, laterally or longitudinally offers wind-guiding groove 45 along air velocity transducer 44 installing hole, and arc is offered in the bottom of groove 45
Describe wind chamber 46.The bottom of wind-guiding groove 45 is to the lopsidedness of air velocity transducer 44 installing hole.The width of described wind-guiding groove
It is 3～5mm.
For ease of to The Cloud Terrace accommodate chamber 11 seal, the present invention one preferred embodiment in, also include: cloud
Platform seals lid 13.The Cloud Terrace seals edge shape and the The Cloud Terrace of lid 13, and to accommodate the opening in chamber 11 corresponding, side pass through return spring and
The Cloud Terrace accommodates the fixing connection of edge of opening in chamber 11, as it is shown in fig. 7, when the video camera to be placed 12 in tripod head frame 20 is regained in cloud
When platform accommodates in chamber 11, The Cloud Terrace seal cap sealing is fastened on The Cloud Terrace and accommodates the opening part in chamber 11.When tripod head frame 20 carries video camera
12 when the opening part in The Cloud Terrace receiving chamber 11 stretches out, as shown in Figure 8.For strengthening sealing effectiveness, a kind of embodiment party of the present invention
In formula, film The Cloud Terrace seals the marginal center of lid and offers sealing strip groove, and inside arranges sealing strip.The Cloud Terrace accommodates at the bottom of the inner chamber in chamber 11
Portion arranges drying layer.
The above, the only detailed description of the invention of the present invention, but protection scope of the present invention is not limited thereto, and any
Those familiar with the art, in the technical scope that the invention discloses, can readily occur in change or replace, should contain
Cover within protection scope of the present invention.Therefore, protection scope of the present invention should described be as the criterion with scope of the claims.
Claims (10)
1. rotor wing unmanned aerial vehicle more than, including: fuselage and tripod head frame, described tripod head frame is arranged at the lower section of described fuselage；Its feature exists
In, including: The Cloud Terrace lifting controller and The Cloud Terrace crane；The bottom of described fuselage is offered The Cloud Terrace and is accommodated chamber；Described The Cloud Terrace accommodates
Chamber is corresponding to the profile of video camera to be placed, and described tripod head frame accommodates the bottom in chamber by described The Cloud Terrace crane and described The Cloud Terrace
It is flexibly connected；The outfan of described The Cloud Terrace lifting controller is connected with the raise-lower hydraulic motor of described The Cloud Terrace crane, when described
When The Cloud Terrace lifting controller receives recovery video camera information, described hydraulic motor is driven to drive described The Cloud Terrace crane to regain,
Make the video camera to be placed being carried in described tripod head frame be recovered to The Cloud Terrace to accommodate in chamber；When described The Cloud Terrace lifting controller receives
To when transferring video camera information, drive described hydraulic motor to drive described The Cloud Terrace crane to stretch out, make to be carried on described tripod head frame
On video camera to be placed accommodate chamber from described The Cloud Terrace and stretch out.
Many rotor wing unmanned aerial vehicles the most according to claim 1, it is characterised in that also include: distance measuring sensor and velocity pick-up
Device；The outfan of distance measuring sensor and velocity sensor is connected with described The Cloud Terrace lifting controller, and described distance measuring sensor obtains
Obstacle distance information；Described velocity sensor obtains current velocity amplitude；If described obstacle distance information is setting value,
Then judge whether described velocity amplitude is setting value, the most then send to described The Cloud Terrace lifting controller and reclaim video camera information.
Many rotor wing unmanned aerial vehicles the most according to claim 1 and 2, it is characterised in that also include: direction information test cell,
The outfan of direction information test cell is connected with the input of The Cloud Terrace lifting controller, and described direction information test cell is to turning
It is acquired to activation bit；If turning to activation bit described in collecting, then according to reclaiming the generation recovery shooting of setpoint distance value
Machine information；This recovery video camera information is sent to described The Cloud Terrace lifting controller.
Many rotor wing unmanned aerial vehicles the most according to claim 3, it is characterised in that also include: air velocity transducer；Described wind speed passes
The outfan of sensor is connected with the input of described The Cloud Terrace lifting controller, and described air velocity transducer gathers current air speed value；Root
Reclaim setpoint distance value synopsis according to described current air speed value with wind speed setting, obtain current recovery setpoint distance value.
Many rotor wing unmanned aerial vehicles the most according to claim 4, it is characterised in that upper surface or the bottom surface of described fuselage are offered
Air velocity transducer installing hole；Described air velocity transducer is fixedly installed in described air velocity transducer installing hole.
Many rotor wing unmanned aerial vehicles the most according to claim 5, it is characterised in that the bore edges of described air velocity transducer installing hole
For arc, laterally or longitudinally offering wind-guiding groove along described air velocity transducer installing hole, the bottom of described wind-guiding groove is offered
Arc holds wind chamber；The bottom of described wind guide tank is to the lopsidedness of described air velocity transducer installing hole.
Many rotor wing unmanned aerial vehicles the most according to claim 1, it is characterised in that the width of described wind-guiding groove is 3～5mm.
Many rotor wing unmanned aerial vehicles the most according to claim 1, it is characterised in that also include: The Cloud Terrace seals lid；Described The Cloud Terrace is close
The opening that the edge shape of capping accommodates chamber to described The Cloud Terrace is corresponding, and side accommodates opening of chamber by return spring with described The Cloud Terrace
Mouthful edge is fixing to be connected, when the video camera to be placed in described tripod head frame is regained and is accommodated in chamber in described The Cloud Terrace, time described cloud
Platform seal cap sealing is fastened on described The Cloud Terrace and accommodates the opening part in chamber.
Many rotor wing unmanned aerial vehicles the most according to claim 8, it is characterised in that described film The Cloud Terrace seals the marginal center of lid and opens
If sealing strip groove, inside arranges sealing strip.
Many rotor wing unmanned aerial vehicles the most according to claim 9, it is characterised in that described The Cloud Terrace accommodates the intracavity bottom in chamber and sets
Put drying layer.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610405413.7A CN106081141A (en) | 2016-06-08 | 2016-06-08 | Many rotor wing unmanned aerial vehicles |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610405413.7A CN106081141A (en) | 2016-06-08 | 2016-06-08 | Many rotor wing unmanned aerial vehicles |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN106081141A true CN106081141A (en) | 2016-11-09 |
Family
ID=57228413
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201610405413.7A Pending CN106081141A (en) | 2016-06-08 | 2016-06-08 | Many rotor wing unmanned aerial vehicles |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN106081141A (en) |
Cited By (15)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106596551A (en) * | 2016-12-19 | 2017-04-26 | 重庆信首科技有限公司 | Disease and insect pest monitoring device based on unmanned aerial vehicle |
| CN106828959A (en) * | 2017-03-08 | 2017-06-13 | 深圳市雷凌广通技术研发有限公司 | A kind of intelligent unmanned plane of taking photo by plane based on Internet of Things |
| CN107499527A (en) * | 2017-07-19 | 2017-12-22 | 深圳市雷凌广通技术研发有限公司 | A kind of intelligent unmanned plane with information monitoring function for being used for agricultural |
| CN108482658A (en) * | 2018-03-09 | 2018-09-04 | 芜湖翼讯飞行智能装备有限公司 | A kind of camera shooting unmanned plane |
| CN108609181A (en) * | 2018-05-09 | 2018-10-02 | 重庆睿宇测绘有限责任公司 | Outdoor scene three-dimensional surveys and draws take photo by plane unmanned plane and its control method |
| CN108698706A (en) * | 2017-08-11 | 2018-10-23 | 深圳市大疆创新科技有限公司 | Rack components and unmanned plane |
| CN108778931A (en) * | 2017-10-10 | 2018-11-09 | 深圳市大疆灵眸科技有限公司 | A kind of method for controlling rotation of photographic device, control device and aircraft |
| CN109159905A (en) * | 2018-10-31 | 2019-01-08 | 上海歌尔泰克机器人有限公司 | A kind of holder and the unmanned plane with the holder |
| CN109974585A (en) * | 2019-04-18 | 2019-07-05 | 甘肃博程技术咨询服务有限公司 | A kind of elevator shaft structure recognition and data measurement unit |
| CN110612493A (en) * | 2018-09-19 | 2019-12-24 | 深圳市大疆创新科技有限公司 | Unmanned aerial vehicle, control method and control device thereof, and computer-readable storage medium |
| CN111361750A (en) * | 2020-03-04 | 2020-07-03 | 吉林工程技术师范学院 | A folding device for unmanned aerial vehicle robot |
| CN113022853A (en) * | 2021-03-27 | 2021-06-25 | 孙鹏 | Mobile 5G communication signal test platform and use method thereof |
| CN113179392A (en) * | 2021-04-25 | 2021-07-27 | 广东电网有限责任公司中山供电局 | Inspection robot |
| CN113627392A (en) * | 2021-09-02 | 2021-11-09 | 南京工业职业技术大学 | Rape waterlogging hyperspectral image detection method based on Spark platform and image acquisition device thereof |
| CN113955133A (en) * | 2021-10-28 | 2022-01-21 | 浙江省水利河口研究院(浙江省海洋规划设计研究院) | Unmanned aerial vehicle panoramic camera protection method and structure |
Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20120025021A1 (en) * | 2010-07-16 | 2012-02-02 | James Jorgensen | Payload door and elevator system |
| CN103744430A (en) * | 2013-02-07 | 2014-04-23 | 山东英特力光通信开发有限公司 | Flight control method of small unmanned helicopter |
| CN203889080U (en) * | 2014-06-05 | 2014-10-22 | 中孚航空科技（天津）有限公司 | Vertical lifting holder device of unmanned aerial vehicle |
| CN204846371U (en) * | 2015-05-22 | 2015-12-09 | 刘道满 | Can keep away unmanned aerial vehicle system of barrier |
| CN204979265U (en) * | 2015-05-22 | 2016-01-20 | 上海九鹰电子科技有限公司 | Elevating system and aircraft of taking photo by plane |
| CN205168935U (en) * | 2015-11-11 | 2016-04-20 | 杭州深空实业股份有限公司 | Many rotor unmanned aerial vehicle do not have all -round program recording system of shake |
-
2016
- 2016-06-08 CN CN201610405413.7A patent/CN106081141A/en active Pending
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20120025021A1 (en) * | 2010-07-16 | 2012-02-02 | James Jorgensen | Payload door and elevator system |
| CN103744430A (en) * | 2013-02-07 | 2014-04-23 | 山东英特力光通信开发有限公司 | Flight control method of small unmanned helicopter |
| CN203889080U (en) * | 2014-06-05 | 2014-10-22 | 中孚航空科技（天津）有限公司 | Vertical lifting holder device of unmanned aerial vehicle |
| CN204846371U (en) * | 2015-05-22 | 2015-12-09 | 刘道满 | Can keep away unmanned aerial vehicle system of barrier |
| CN204979265U (en) * | 2015-05-22 | 2016-01-20 | 上海九鹰电子科技有限公司 | Elevating system and aircraft of taking photo by plane |
| CN205168935U (en) * | 2015-11-11 | 2016-04-20 | 杭州深空实业股份有限公司 | Many rotor unmanned aerial vehicle do not have all -round program recording system of shake |
Cited By (22)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106596551A (en) * | 2016-12-19 | 2017-04-26 | 重庆信首科技有限公司 | Disease and insect pest monitoring device based on unmanned aerial vehicle |
| CN106828959A (en) * | 2017-03-08 | 2017-06-13 | 深圳市雷凌广通技术研发有限公司 | A kind of intelligent unmanned plane of taking photo by plane based on Internet of Things |
| CN107499527A (en) * | 2017-07-19 | 2017-12-22 | 深圳市雷凌广通技术研发有限公司 | A kind of intelligent unmanned plane with information monitoring function for being used for agricultural |
| CN107499527B (en) * | 2017-07-19 | 2021-01-08 | 武汉思众空间信息科技有限公司 | A intelligent unmanned aerial vehicle that is used for having of agricultural information monitoring function |
| WO2019028871A1 (en) * | 2017-08-11 | 2019-02-14 | 深圳市大疆创新科技有限公司 | Frame assembly and unmanned aerial vehicle |
| CN108698706A (en) * | 2017-08-11 | 2018-10-23 | 深圳市大疆创新科技有限公司 | Rack components and unmanned plane |
| CN108698706B (en) * | 2017-08-11 | 2021-10-22 | 深圳市大疆创新科技有限公司 | Frame subassembly and unmanned aerial vehicle |
| WO2019071444A1 (en) * | 2017-10-10 | 2019-04-18 | 深圳市大疆灵眸科技有限公司 | Turning control method for photographic device, control apparatus and aircraft |
| CN108778931A (en) * | 2017-10-10 | 2018-11-09 | 深圳市大疆灵眸科技有限公司 | A kind of method for controlling rotation of photographic device, control device and aircraft |
| CN108778931B (en) * | 2017-10-10 | 2021-10-29 | 深圳市大疆灵眸科技有限公司 | Rotation control method and control equipment of camera device and aircraft |
| CN108482658B (en) * | 2018-03-09 | 2020-05-08 | 芜湖翼讯飞行智能装备有限公司 | Unmanned aerial vehicle makes a video recording |
| CN108482658A (en) * | 2018-03-09 | 2018-09-04 | 芜湖翼讯飞行智能装备有限公司 | A kind of camera shooting unmanned plane |
| CN108609181A (en) * | 2018-05-09 | 2018-10-02 | 重庆睿宇测绘有限责任公司 | Outdoor scene three-dimensional surveys and draws take photo by plane unmanned plane and its control method |
| CN110612493A (en) * | 2018-09-19 | 2019-12-24 | 深圳市大疆创新科技有限公司 | Unmanned aerial vehicle, control method and control device thereof, and computer-readable storage medium |
| CN109159905A (en) * | 2018-10-31 | 2019-01-08 | 上海歌尔泰克机器人有限公司 | A kind of holder and the unmanned plane with the holder |
| CN109974585A (en) * | 2019-04-18 | 2019-07-05 | 甘肃博程技术咨询服务有限公司 | A kind of elevator shaft structure recognition and data measurement unit |
| CN111361750A (en) * | 2020-03-04 | 2020-07-03 | 吉林工程技术师范学院 | A folding device for unmanned aerial vehicle robot |
| CN113022853A (en) * | 2021-03-27 | 2021-06-25 | 孙鹏 | Mobile 5G communication signal test platform and use method thereof |
| CN113179392A (en) * | 2021-04-25 | 2021-07-27 | 广东电网有限责任公司中山供电局 | Inspection robot |
| CN113627392A (en) * | 2021-09-02 | 2021-11-09 | 南京工业职业技术大学 | Rape waterlogging hyperspectral image detection method based on Spark platform and image acquisition device thereof |
| CN113955133A (en) * | 2021-10-28 | 2022-01-21 | 浙江省水利河口研究院(浙江省海洋规划设计研究院) | Unmanned aerial vehicle panoramic camera protection method and structure |
| CN113955133B (en) * | 2021-10-28 | 2023-10-03 | 浙江省水利河口研究院(浙江省海洋规划设计研究院) | Unmanned aerial vehicle panoramic camera protection method and structure |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN106081141A (en) | Many rotor wing unmanned aerial vehicles | |
| US10086956B2 (en) | Light adjustment control for cameras of an aerial vehicle | |
| CN107651205A (en) | Unmanned plane positions power taking cell system | |
| CN112947202B (en) | Intelligent cleaning system for water surface floating garbage and control method | |
| CN103413846A (en) | Solar power generating system | |
| CN106555381A (en) | Bore extension and retraction system in a kind of automatization road | |
| CN107795827A (en) | Tunnel IMAQ regulation platform | |
| CN106602460A (en) | Outdoor cable support system | |
| CN106314305A (en) | Vehicle road condition monitoring device | |
| CN204940157U (en) | A kind of automation road cone extension and retraction system | |
| CN209814315U (en) | Charging take-off and landing platform suitable for mooring unmanned aerial vehicle | |
| CN110733607B (en) | Group type unmanned boat laying and recycling system | |
| CN210460636U (en) | Shaft attitude detection equipment and shaft excavating equipment | |
| CN110525676B (en) | Vehicle-mounted fixed wing unmanned aerial vehicle receiving and transmitting integrated platform and control method thereof | |
| KR101271615B1 (en) | Examination apparatus for lower portion of vessel | |
| CN106412525A (en) | Warning light | |
| CN106241657B (en) | A kind of manufacturing method for starting rapid lifting machine | |
| CN205711742U (en) | A kind of bridge machinery mechanism | |
| CN110539856A (en) | Water surface garbage cleaning ship | |
| CN104922941B (en) | Floating-ball-type automatic-adjusting electric degasifier | |
| CN213546982U (en) | Full-automatic net sealing/removing telescopic crossing structure | |
| CN113619754A (en) | Dock and unmanned ship system | |
| CN211139689U (en) | Urban viaduct detection unmanned aerial vehicle | |
| CN208984072U (en) | Comprehensive bridge monitoring device | |
| CN111879291A (en) | Automatic geological disaster characteristic monitoring device |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| RJ01 | Rejection of invention patent application after publication | ||
| RJ01 | Rejection of invention patent application after publication |
Application publication date: 20161109 |