CN110382362A - A kind of positioning device of unmanned plane - Google Patents
A kind of positioning device of unmanned plane Download PDFInfo
- Publication number
- CN110382362A CN110382362A CN201780088030.4A CN201780088030A CN110382362A CN 110382362 A CN110382362 A CN 110382362A CN 201780088030 A CN201780088030 A CN 201780088030A CN 110382362 A CN110382362 A CN 110382362A
- Authority
- CN
- China
- Prior art keywords
- driving
- positioning
- unmanned plane
- positioning device
- driving section
- 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
- 230000007246 mechanism Effects 0.000 claims description 92
- 230000005540 biological transmission Effects 0.000 claims description 35
- 238000010586 diagram Methods 0.000 description 7
- 238000000034 method Methods 0.000 description 4
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000007429 general method Methods 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
- B64F1/00—Ground or aircraft-carrier-deck installations
- B64F1/36—Other airport installations
-
- 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
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Automatic Assembly (AREA)
Abstract
A kind of positioning device of unmanned plane (10), comprising: support plate (20), for carrying the unmanned plane；First positioning component (30), in a first direction from the opposite sides clamp or release of the unmanned plane unmanned plane；Second positioning component (40), for other opposite sides clamp or release unmanned plane in the second direction perpendicular to the first direction from the unmanned plane.The positioning device (10) makes when unmanned plane needs to take off, first positioning component (30) and the second positioning component (40) unclamp unmanned plane, in unmanned plane landing, first positioning component (30) clamps unmanned plane in the circumferential direction of unmanned plane with the second positioning component (40) to position to unmanned plane, relative to manually positioning, precision is high, error is small, reduces cost of labor, improves the convenience used.
Description
This application involves air vehicle technique fields, more particularly to a kind of positioning device of unmanned plane.
UAV is referred to as " unmanned plane ", it is the not manned aircraft using radio remote controller and the presetting apparatus provided for oneself manipulation, in the actual operation process, since unmanned plane flies control program and camera contraposition limitation, in unmanned plane landing, it will appear level point and takeoff point not the same position the case where, such case can have a huge impact the follow-up work of unmanned plane.
In the prior art, when unmanned plane takes off with landing, the general method by manually calibrating, so that level point and takeoff point be in same position, but the method precision of manual calibration is low, error is big.
[summary of the invention]
The application mainly provides a kind of positioning device of unmanned plane, it is intended to which precision is low when solving the problems, such as to be positioned manually unmanned plane, error is big.
In order to solve the above technical problems, the technical solution that the application uses is: providing a kind of positioning device of unmanned plane, which includes: support plate, for carrying the unmanned plane；First positioning component, for unmanned plane described in the opposite sides clamp or release in a first direction from the unmanned plane；Second positioning component, for unmanned plane described in the other opposite sides clamp or release on the second direction perpendicular to the first direction from the unmanned plane.
The beneficial effect of the application is: being in contrast to the prior art, positioning device provided by the present application includes support plate, first positioning component and the second positioning component, support plate is for carrying unmanned plane, first positioning component is used in a first direction from the opposite sides clamp or release unmanned plane of unmanned plane, second positioning component, for in a second direction perpendicular to the first direction from the other opposite sides clamp or release unmanned plane of unmanned plane, so that when unmanned plane needs to take off, first positioning component and the second positioning component unclamp unmanned plane, in unmanned plane landing, first positioning component clamps unmanned plane in the circumferential direction of unmanned plane with the second positioning component to position to unmanned plane, manually positioning in compared with the existing technology, precision is high, error is small, reduce cost of labor, improve the convenience used.
In order to more clearly explain the technical solutions in the embodiments of the present application, the accompanying drawings required for describing the embodiments of the present invention are briefly described below, apparently, the drawings in the following description are only some examples of the present application, for those of ordinary skill in the art, without creative efforts, it is also possible to obtain other drawings based on these drawings, in which:
Fig. 1 is the structural schematic diagram of the positioning device embodiment positioning of unmanned plane provided by the present application；
Fig. 2 is the structural schematic diagram of the first positioning component in Fig. 1；
Fig. 3 is the enlarged diagram of part A in Fig. 2；
Fig. 4 is the enlarged diagram of part B in Fig. 2；
Fig. 5 is the structural schematic diagram of the second positioning component in Fig. 1；
Fig. 6 is the enlarged diagram of C portion in Fig. 5.
Below in conjunction with the attached drawing in the embodiment of the present application, the technical scheme in the embodiment of the application is clearly and completely described, it is clear that described embodiment is only a part of the embodiment of the application, instead of all the embodiments.Based on the embodiment in the application, every other embodiment obtained by those of ordinary skill in the art without making creative efforts, shall fall in the protection scope of this application.
Refering to fig. 1, the structural schematic diagram of 10 embodiment of the positioning device positioning of unmanned plane provided by the present application, the positioning device 10 of the present embodiment include support plate 20, the first positioning component 30 and the second positioning component 40.
Support plate 20 is for carrying unmanned plane 50.
Wherein, support plate 20 sets that there are two flutings 21, and optionally, each fluting 21 includes two son flutings 211, and two son flutings 211 are oppositely arranged.
First positioning component 30 in a first direction from the opposite sides clamp or release unmanned plane 50 of unmanned plane 50 namely the first positioning component 30 as shown in Figure 1 unmanned plane 50 left and right sides clamp or release unmanned plane 50.
Refering to Fig. 2, first positioning component 30 includes the first driving mechanism 31 and two the first positioning mechanisms 32, first driving mechanism 31 at least drives at least one of two first positioning mechanisms 32 close to each other or separate in a first direction relative to another, and then from the opposite sides clamp or release unmanned plane 50 of unmanned plane 50.
Optionally, the first driving mechanism 31 drives two the first positioning mechanisms 32 close to each other or separate in a first direction simultaneously.
Wherein, the first driving mechanism 31 includes first motor 311 and the first transmission mechanism 312, and first motor 311 is driven the first positioning mechanism 32 by the first transmission mechanism 312.
Jointly refering to Fig. 2, Fig. 3 and Fig. 4, first motor 311 is connect in the side of support plate 20 with support plate 20, first transmission mechanism 312 includes the first driving wheel 312a and the first driving member 312b, the output shaft of first driving wheel 312a connection first motor 311, first driving member 312b is connect with the first driving wheel 312a, and including the first driving section 3121 and the second driving section 3122, the first driving section 3121 and the second driving section 3122 being capable of the movements reversely with each other under the driving of the first driving wheel 312a.
Optionally, first driving mechanism 31 further comprises the first driven wheel 313, first driving member 312b is the first transmission belt being wound around on the first driving wheel 312a and the first driven wheel 313, and the first driving section 3121 and the second driving section 3122 correspond to the part relative to each other and heterodromous between the first driving wheel 312a and the first driven wheel 313 of the first transmission belt.
In other embodiments, the first driving member 312b may be the first transmission chain.
Further, first transmission mechanism 312 further includes two the first connector 312c, two the first connector 312c are separately connected the first driving section 3121 and the second driving section 3122, close to each other or separate at the first driving section 3121 and the second 3122 movement reversely with each other of driving section.
Optionally, two the first connector 312c are respectively arranged on support plate 20 in corresponding two flutings 21, and can be moved in corresponding fluting 21 when close to each other or separate, in the present embodiment, every one first connector 312c is set in two son flutings 211 of corresponding fluting 211.
It should be understood that the length direction of fluting 21 is identical as above-mentioned first direction.
Optionally, two the first connector 312c are each passed through corresponding fluting 21 to extend to the side far from first motor 311 close to the side of first motor 311 from support plate 20.
Further, first transmission mechanism 312 further includes two the first guide part 312d, two the first guide part 312d are connect with support plate 20, to support corresponding two the first connector 312c respectively, and two the first connector 312c can be moved on two the first guide part 312d.
Wherein, two the first guide part 312d are oppositely arranged, and extending direction is identical as above-mentioned first direction.
Jointly refering to Fig. 5 and Fig. 6, two the first positioning mechanisms 32 are separately connected two the first connector 312c, to be connected to the first driving section 3121 and the second driving section 3122 by two the first connector 312c, so that the first driving section 3121 and the second driving section 3122 are under driving of the first motor 311 by the first driving wheel 312a when movement reversely with each other, two the first connector 312c are away from each other or close, so that two the first positioning mechanisms 32 are away from each other or close, to realize the first above-mentioned driving mechanism 31 while drive two the first positioning mechanisms 32 close to each other or separate in a first direction, and then it realizes in a first direction from the opposite sides clamp or release unmanned plane 50 of unmanned plane 50.
Optionally, first positioning mechanism 32 includes locating piece 321 and connecting plate 322, two connecting plates 322 of two the first positioning mechanisms 32 are connect with two the first connector 312c respectively, and two locating pieces 321 of two the first positioning mechanisms 32 are connect with two connecting plates 322 respectively.
Optionally, locating piece 321 is arranged in cover, and covers at connecting plate 322.
Optionally, the side in support plate 20 far from first motor 311 is connect two the first positioning mechanisms 32 with two the first connector 312c respectively, so that two the first positioning mechanisms 32 are set to the opposite sides of support plate 20 with first motor 311 namely two the first positioning mechanisms 32 are connect with the part for passing through fluting 21 two the first connector 312c respectively.
Further regard to Fig. 1, second positioning component 40 is in a second direction perpendicular to the first direction from the other clamp or release unmanned plane of two sides up and down 50 of opposite two sides clamp or release unmanned plane 50 namely the second positioning component 40 as shown in Figure 1 in unmanned plane 50 of unmanned plane 50.
Further regard to Fig. 6, second positioning component 40 includes the second driving mechanism 41 and two the second positioning mechanisms 42, second driving mechanism 41 at least drives at least one of two second positioning mechanisms 42 close to each other or separate in a second direction relative to another, and then from the opposite sides clamp or release unmanned plane 50 of unmanned plane 50.
Optionally, the second driving mechanism 41 drives two the second positioning mechanisms 42 close to each other or separate in a second direction simultaneously.
Wherein, the second driving mechanism 41 includes the second motor 411 and the second transmission mechanism 412, and the second motor 411 is driven the second positioning mechanism 42 by the second transmission mechanism 412.
Specifically, second transmission mechanism 412 includes the second driving wheel 412a and the second driving member 412b, the output shaft of second the second motor of driving wheel 412a connection 411, second driving member 412b is connect with the second driving wheel 412a, and including third driving section 4121 and the 4th driving section 4122, third driving section 4121 and the 4th driving section 4122 being capable of the movements reversely with each other under the driving of the second driving wheel 412a.
Optionally, second driving wheel 412a includes the first sub- driving wheel 4123, second sub- driving wheel 4124 and the sub- driving wheel 4125 of third, first sub- driving wheel 411 connects the output shaft of the second motor 411, second transmission mechanism 412 further comprises third driving member 412c, the sub- driving wheel 4123 of third driving member 412c connection first and the second sub- driving wheel 4124, the sub- driving wheel 4125 of third is connect with the second sub- driving wheel 4124, so that the second motor 411 can drive the sub- driving wheel 4125 of third to rotate, second driving member 412b is connect with the sub- driving wheel 4125 of third, so that third driving section 4121 and the 4th driving section 4122 being capable of the movements reversely with each other under the driving of the sub- driving wheel 4125 of third.
Optionally, third driving member 412c is the third transmission belt for being set around the first sub- driving wheel 4123 and the second sub- driving wheel 4124, and in other embodiments, third driving member 412c may be third transmission chain.
Optionally, second driving mechanism 41 further comprises the second driven wheel 413, second driving member 412b is the second transmission belt being wound around on the second driving wheel 412a and the second driven wheel 413, and third driving section 4121 and the 4th driving section 4122 correspond to the part relative to each other and heterodromous between the second driving wheel 412a and the second driven wheel 413 of the second transmission belt.
Optionally, second driving member 412b is the second transmission belt for being set around third sub- driving wheel 4123 and the second driven wheel 413, and third driving section 4121 and the 4th driving section 4122 correspond to the part relative to each other and heterodromous between the sub- driving wheel 4123 of third and the second driven wheel 413 of the second transmission belt.
In other embodiments, the second driving member 412b may be the second transmission chain.
Further, second transmission mechanism 412 further includes two the second connector 412d, two the second connector 412d are separately connected third driving section 4121 and the 4th driving section 4122, close to each other or separate at third driving section 4121 and the 4th 4122 movement reversely with each other of driving section.
Further, the second transmission mechanism 412 further includes that two second guide parts 412e, two the second guide part 412e support corresponding two the second connector 412d respectively, and two the second connector 412d can be moved on two the second guide part 412e.
Wherein, the extending direction of two the second guide part 412e is identical as above-mentioned second direction.
Two the second positioning mechanisms 42 are separately connected two the second connector 412d, to be connected to third driving section 4121 and the 4th driving section 4122 by two the second connector 412d, so that third driving section 4121 and the 4th driving section 4122 are under driving of second motor 411 by the second driving wheel 412a when movement reversely with each other, two the second connector 412d are away from each other or close, so that two the second positioning mechanisms 42 are away from each other or close, to realize the second above-mentioned driving mechanism 41 while drive two the second positioning mechanisms 42 close to each other or separate in a second direction, and then it realizes in a second direction from the other opposite sides clamp or release unmanned plane 50 of unmanned plane 50.
Optionally, the second positioning component 40 and two the first positioning mechanisms 32 are set to the same side of support plate 20.
Optionally, the second positioning component 40 is installed on the first positioning mechanism 32, and when the first driving mechanism 31 drives the second positioning mechanism 32, is moved together with the first positioning mechanism 32.
Optionally, the second positioning component 40 is installed on the connecting plate 322 of the first positioning mechanism 32, specifically, the second motor 411 in the second driving mechanism 41 is connect with the second driven wheel 413 with connecting plate 322.
Wherein, the second positioning component 40 is covered in the locating piece 321 that cover is arranged.
Optionally, as shown in figure 5, the quantity of the second positioning component 40 is two, two the second positioning components 40 are respectively arranged on corresponding first positioning mechanism 32.
It is different from the prior art, positioning device provided by the present application includes support plate, first positioning component and the second positioning component, support plate is for carrying unmanned plane, first positioning component is used in a first direction from the opposite sides clamp or release unmanned plane of unmanned plane, second positioning component, for in a second direction perpendicular to the first direction from the other opposite sides clamp or release unmanned plane of unmanned plane, so that when unmanned plane needs to take off, first positioning component and the second positioning component unclamp unmanned plane, in unmanned plane landing, first positioning component clamps unmanned plane in the circumferential direction of unmanned plane with the second positioning component to position to unmanned plane, manually positioning in compared with the existing technology, precision is high, error is small, reduce cost of labor, improve the convenience used.
Above is only an example of the present application; it is not intended to limit the scope of the patents of the application; it is all to utilize equivalent structure or equivalent flow shift made by present specification and accompanying drawing content; be applied directly or indirectly in other relevant technical fields, similarly includes in the scope of patent protection of the application.
Claims (20)
- A kind of positioning device of unmanned plane, which is characterized in that the positioning device includes:Support plate, for carrying the unmanned plane；First positioning component, for unmanned plane described in the opposite sides clamp or release in a first direction from the unmanned plane；Second positioning component, for unmanned plane described in the other opposite sides clamp or release on the second direction perpendicular to the first direction from the unmanned plane.
- Positioning device according to claim 1, it is characterized in that, first positioning component includes the first driving mechanism and two the first positioning mechanisms, wherein first driving mechanism at least drives at least one of described two first positioning mechanisms close to each other or separate in said first direction relative to another, and then unmanned plane described in the opposite sides clamp or release from the unmanned plane.
- Positioning device according to claim 2, which is characterized in that first driving mechanism drives described two first positioning mechanisms close to each other or separate in said first direction simultaneously.
- Positioning device according to claim 2, which is characterized in that first driving mechanism includes first motor and the first transmission mechanism, and the first motor is driven first positioning mechanism by first transmission mechanism.
- Positioning device according to claim 4, it is characterized in that, first transmission mechanism includes the first driving wheel and the first driving member, first driving wheel connects the output shaft of the first motor, first driving member is connect with first driving wheel, and including the first driving section and the second driving section, first driving section and the second driving section being capable of the movements reversely with each other under the driving of first driving wheel, described two first positioning mechanisms are respectively connected to first driving section and the second driving section, and then it is close to each other or separate in the case where first driving section and the second driving section drive.
- Positioning device according to claim 5, it is characterized in that, first transmission mechanism further comprises two the first connectors, and described two first connectors are separately connected one in first driving section and described two first positioning mechanisms and another in second driving section and described two first positioning mechanisms.
- Positioning device according to claim 6, which is characterized in that the first motor and described two first positioning mechanisms are set to the opposite sides of the support plate.
- Positioning device according to claim 7, which is characterized in that there are two fluting, described two first connectors are separately positioned in the corresponding fluting, and can be moved in the fluting for setting on the support plate.
- Positioning device according to claim 6, it is characterized in that, first transmission mechanism further comprises two the first guide parts, and described two first connectors are respectively supported on corresponding first guide part and can move relative to first guide part.
- Positioning device according to claim 5, it is characterized in that, first driving mechanism further comprises the first driven wheel, first driving member is the first transmission belt being wound around on first driving wheel and first driven wheel, and first driving section and second driving section correspond to the part relative to each other and heterodromous between first driving wheel and first driven wheel of first transmission belt.
- Positioning device according to claim 1, it is characterized in that, second positioning component includes the second driving mechanism and two the second positioning mechanisms, wherein second driving mechanism at least drives at least one of described second positioning mechanism close to each other or separate in this second direction relative to another, and then unmanned plane described in the opposite sides clamp or release from the unmanned plane.
- Positioning device according to claim 11, which is characterized in that second driving mechanism drives described two second positioning mechanisms close to each other or separate in this second direction simultaneously.
- Positioning device according to claim 11, which is characterized in that second driving mechanism includes the second motor and the second transmission mechanism, and second motor is driven second positioning mechanism by second transmission mechanism.
- Positioning device according to claim 13, it is characterized in that, second transmission mechanism includes the second driving wheel and the second driving member, second driving wheel connects the output shaft of second motor, second driving member is connect with second driving wheel, and including third driving section and the 4th driving section, the third driving section and the 4th driving section being capable of the movements reversely with each other under the driving of second driving wheel, described two second positioning mechanisms are respectively connected to the third driving section and the 4th driving section, and then it is close to each other or separate in the case where the third driving section and the 4th driving section drive.
- Positioning device according to claim 14, it is characterized in that, second transmission mechanism further comprises two the second connectors, and described two second connectors are separately connected one in the third driving section and described two second positioning mechanisms and another in the 4th driving section and described two second positioning mechanisms.
- Positioning device according to claim 15, it is characterized in that, second transmission mechanism further comprises two the second guide parts, and described two second connectors are respectively supported on corresponding second guide part and can move relative to second guide part.
- Positioning device according to claim 14, it is characterized in that, second driving mechanism further comprises the second driven wheel, second driving member is the second transmission belt being wound around on second driving wheel and second driven wheel, and the third driving section and the 4th driving section correspond to the part relative to each other and heterodromous between second driving wheel and second driven wheel of second transmission belt.
- Positioning device according to claim 7, which is characterized in that second positioning component is set to the same side of the support plate with described two first positioning mechanisms.
- Positioning device according to claim 18, which is characterized in that second positioning component is installed on first positioning mechanism, and when first driving mechanism drives first positioning mechanism, is moved together with first positioning mechanism.
- Positioning device according to claim 19, which is characterized in that the quantity of second positioning component is two, and described two second positioning components are respectively arranged on corresponding first positioning mechanism.
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| PCT/CN2017/119435 WO2019127225A1 (en) | 2017-12-28 | 2017-12-28 | Positioning device for unmanned aerial vehicle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN110382362A true CN110382362A (en) | 2019-10-25 |
Family
ID=67062825
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201780088030.4A Pending CN110382362A (en) | 2017-12-28 | 2017-12-28 | A kind of positioning device of unmanned plane |
Country Status (2)
| Country | Link |
|---|---|
| CN (1) | CN110382362A (en) |
| WO (1) | WO2019127225A1 (en) |
Citations (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104668703A (en) * | 2013-11-30 | 2015-06-03 | 陕西子竹电子有限公司 | Movement mechanism of spot welding machine PCB (printed circuit board) |
| CN106144576A (en) * | 2016-08-12 | 2016-11-23 | 橙果信息技术有限公司 | A kind of Traverse Displacement Unit |
| CN205790709U (en) * | 2016-05-18 | 2016-12-07 | 深圳市菁创未来科技有限公司 | Unmanned plane interface automatic butt system |
| CN106542109A (en) * | 2016-11-04 | 2017-03-29 | 上海云犀智能系统有限公司 | A kind of unmanned plane recharging platform |
| CN107176047A (en) * | 2017-05-27 | 2017-09-19 | 先测电子科技（上海）有限公司 | A kind of unmanned plane shuts down storehouse |
| CN107697314A (en) * | 2017-05-19 | 2018-02-16 | 成都天麒科技有限公司 | A kind of unmanned plane lifting gear |
| CN207028881U (en) * | 2017-05-27 | 2018-02-23 | 星逻智能科技(苏州)有限公司 | A kind of unmanned plane shuts down storehouse |
| CN207466993U (en) * | 2017-10-30 | 2018-06-08 | 深圳市大疆创新科技有限公司 | Clamping device and the base station with clamping device and UAV system |
| CN207466991U (en) * | 2017-10-30 | 2018-06-08 | 深圳市大疆创新科技有限公司 | Unmanned machine positioning device and airplane parking area |
| CN207826577U (en) * | 2017-12-28 | 2018-09-07 | 深圳市大疆创新科技有限公司 | A kind of positioning device of unmanned plane |
Family Cites Families (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN206520762U (en) * | 2017-02-28 | 2017-09-26 | 郑州大学 | A kind of novel intelligent vehicle-mounted unmanned aerial vehicle launcher |
| CN107010241A (en) * | 2017-05-27 | 2017-08-04 | 辛亚行 | A kind of vehicle-mounted unmanned aerial vehicle landing platform |
-
2017
- 2017-12-28 WO PCT/CN2017/119435 patent/WO2019127225A1/en active Application Filing
- 2017-12-28 CN CN201780088030.4A patent/CN110382362A/en active Pending
Patent Citations (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104668703A (en) * | 2013-11-30 | 2015-06-03 | 陕西子竹电子有限公司 | Movement mechanism of spot welding machine PCB (printed circuit board) |
| CN205790709U (en) * | 2016-05-18 | 2016-12-07 | 深圳市菁创未来科技有限公司 | Unmanned plane interface automatic butt system |
| CN106144576A (en) * | 2016-08-12 | 2016-11-23 | 橙果信息技术有限公司 | A kind of Traverse Displacement Unit |
| CN106542109A (en) * | 2016-11-04 | 2017-03-29 | 上海云犀智能系统有限公司 | A kind of unmanned plane recharging platform |
| CN107697314A (en) * | 2017-05-19 | 2018-02-16 | 成都天麒科技有限公司 | A kind of unmanned plane lifting gear |
| CN107176047A (en) * | 2017-05-27 | 2017-09-19 | 先测电子科技（上海）有限公司 | A kind of unmanned plane shuts down storehouse |
| CN207028881U (en) * | 2017-05-27 | 2018-02-23 | 星逻智能科技(苏州)有限公司 | A kind of unmanned plane shuts down storehouse |
| CN207466993U (en) * | 2017-10-30 | 2018-06-08 | 深圳市大疆创新科技有限公司 | Clamping device and the base station with clamping device and UAV system |
| CN207466991U (en) * | 2017-10-30 | 2018-06-08 | 深圳市大疆创新科技有限公司 | Unmanned machine positioning device and airplane parking area |
| CN207826577U (en) * | 2017-12-28 | 2018-09-07 | 深圳市大疆创新科技有限公司 | A kind of positioning device of unmanned plane |
Also Published As
| Publication number | Publication date |
|---|---|
| WO2019127225A1 (en) | 2019-07-04 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| US9512864B2 (en) | Method and system for conforming assembly systems to contours of curved surfaces | |
| CN103777637B (en) | Areflexia plate Laser Self navigation AGV dolly and air navigation aid thereof | |
| US10618579B2 (en) | Autonomous crawling assembly system | |
| US20170355481A1 (en) | Labeling device | |
| US10053165B2 (en) | Automated maintenance of surface skins using transporter system | |
| CN105599915A (en) | Steering engine driven flexible cable transmission two-shaft cradle head structure | |
| US11434024B2 (en) | Automated engagement of and disengagement from a fitting | |
| CN207826577U (en) | A kind of positioning device of unmanned plane | |
| CN110382362A (en) | A kind of positioning device of unmanned plane | |
| US20160067868A1 (en) | Modular end effector | |
| CN107285006B (en) | Mask plate manipulator pre-alignment mechanism, mask plate mounting method and application | |
| US10870180B2 (en) | Automated engagement and handling of a structure | |
| CN213287502U (en) | Automatic assembling and dispensing system and equipment | |
| CN102248746B (en) | Position holding device | |
| BR112017012687B1 (en) | AUTOMOBILE BODY ASSEMBLY DEVICE | |
| KR101545622B1 (en) | Cable pulling system | |
| KR100453625B1 (en) | Apparatus for fuselage automated splicing | |
| CN210943918U (en) | Power driving mechanism and clamp assembly | |
| US20150026962A1 (en) | Device for attaching chip on film onto panel and method for using the same | |
| KR102114807B1 (en) | Education rc kit | |
| CN209938925U (en) | A horn for unmanned aerial vehicle | |
| CA2896848C (en) | Vacuum dip coating apparatus | |
| CN209583218U (en) | A kind of adhesive tape laying apparatus | |
| DE102017216134A1 (en) | A method of identifying a robot, portable robotic handheld device, and robotic workstation | |
| CN106064528B (en) | Can online motorized adjustment anodized aluminium lateral position deviation correcting device and its working method |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20191025 |
|
| WD01 | Invention patent application deemed withdrawn after publication |