CN114194406B - Unmanned aerial vehicle carries on platform - Google Patents
Unmanned aerial vehicle carries on platform Download PDFInfo
- Publication number
- CN114194406B CN114194406B CN202111543651.1A CN202111543651A CN114194406B CN 114194406 B CN114194406 B CN 114194406B CN 202111543651 A CN202111543651 A CN 202111543651A CN 114194406 B CN114194406 B CN 114194406B
- Authority
- CN
- China
- Prior art keywords
- aerial vehicle
- unmanned aerial
- platform
- mechanical claw
- sliding sleeve
- 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.)
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Links
- 210000000078 claw Anatomy 0.000 claims abstract description 44
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 claims description 6
- 238000003466 welding Methods 0.000 claims description 5
- 229910052742 iron Inorganic materials 0.000 claims description 3
- 239000000463 material Substances 0.000 claims description 3
- 230000000452 restraining effect Effects 0.000 description 5
- 238000009434 installation Methods 0.000 description 2
- 238000005259 measurement Methods 0.000 description 2
- 238000000926 separation method Methods 0.000 description 2
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 description 1
- 241000607479 Yersinia pestis Species 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 229910052802 copper Inorganic materials 0.000 description 1
- 239000010949 copper Substances 0.000 description 1
- 201000010099 disease Diseases 0.000 description 1
- 208000037265 diseases, disorders, signs and symptoms Diseases 0.000 description 1
- 230000009977 dual effect Effects 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 230000005484 gravity Effects 0.000 description 1
- 239000007769 metal material Substances 0.000 description 1
- 230000000007 visual effect Effects 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D47/00—Equipment not otherwise provided for
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C25/00—Alighting gear
- B64C25/32—Alighting gear characterised by elements which contact the ground or similar surface
- B64C25/58—Arrangements or adaptations of shock-absorbers or springs
- B64C25/62—Spring shock-absorbers; Springs
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Load-Engaging Elements For Cranes (AREA)
- Forklifts And Lifting Vehicles (AREA)
Abstract
The invention discloses an unmanned aerial vehicle carrying platform. The platform not only can enable LiDAR to be quickly carried on the unmanned aerial vehicle, but also can enable the unmanned aerial vehicle to land in a pothole smoothly. The platform is an automatic carrying device, a cylinder at the center above the platform is operated by controlling a remote controller switch, a built-in rod of the cylinder penetrates through the platform to the lower part of the platform to be fixedly connected with the double rods, the built-in rod of the cylinder moves up and down to drive the double rods to move up and down, and a sliding sleeve on the double rods, a connecting rod and a single mechanical claw part form a crank sliding block mechanism. When the built-in rod of the cylinder moves upwards, the double rods move upwards, and the total mechanical claw is clamped through the crank sliding block mechanism; otherwise, the double rods move downwards, and the mechanical claws are loosened. The LiDAR can be fixed and separated through the operation of the cylinder, and the efficiency of carrying the LiDAR on the unmanned aerial vehicle can be improved. And when the unmanned aerial vehicle lands, if the nearby ground is not flat, the unmanned aerial vehicle lands steadily by means of the springs of the platform supporting frame.
Description
Technical Field
The invention relates to an unmanned aerial vehicle carrying platform capable of carrying laser radar measurement (LiDAR) equipment on an unmanned aerial vehicle, and belongs to the technical field of agricultural machinery.
Background
The laser radar measurement (LiDAR) technology is widely applied to the technical field of agriculture, and not only can acquire crop growth information, but also can accurately acquire a ground plant canopy structure; by utilizing the data obtained by LiDAR, the pest and disease information, estimated yield and the like of crops can be analyzed.
The patent application number 202022678142.7 discloses an unmanned aerial vehicle laser radar installation device, which mainly comprises a device connecting plate for connecting a laser radar device and a mounting fixing plate for connecting an unmanned aerial vehicle, wherein the device connecting plate is connected with the mounting fixing plate through a buckle; this patent has mainly designed the quick connection that is used for carrying between the equipment connecting plate that carries fixed plate and be used for connecting laser radar on unmanned aerial vehicle to can not make laser radar carry on unmanned aerial vehicle fast.
But this patent provides an unmanned aerial vehicle carries on platform, and this carries on platform and can carry on LiDAR voluntarily. The device is provided with a remote controller, a cylinder is operated through a control switch, a rod arranged in the cylinder moves up and down to drive a double rod to move up and down, and a sliding sleeve on the double rod, a connecting rod and a single mechanical claw part form a crank sliding block mechanism. When the built-in rod of the cylinder moves upwards, the double rods move upwards, and the total mechanical claw is clamped through the crank sliding block mechanism; otherwise, the double rods move downwards, and the mechanical claws are loosened. The LiDAR can be automatically fixed and separated through the operation of the cylinder, so that the installation efficiency can be finally improved more quickly, and the workload of operators is reduced.
Disclosure of Invention
The invention relates to an unmanned aerial vehicle carrying platform which can carry LiDAR on an unmanned aerial vehicle and enable the unmanned aerial vehicle to land on uneven ground at the same time. When the built-in rod of the cylinder moves upwards, the double rods move upwards, and the total mechanical claw is clamped through the crank sliding block mechanism; otherwise, the double rods move downwards, and the mechanical claws are loosened. By means of an external remote controller switch, the pneumatic cylinder can be operated to fix and separate LiDAR, the efficiency of loading LiDAR can be improved, and the LiDAR can be used for working more quickly.
The U-shaped hook of the unmanned aerial vehicle is connected to the platform has the following advantages: the platform can be easily connected to the support frame of the unmanned aerial vehicle. The U-shaped hook is connected with the spring, the U-shaped hook is fixed on the platform groove, the U-shaped hook is enabled to have elastic force, the spring can be freely stretched according to the width of the unmanned aerial vehicle support, and the U-shaped hook is enabled to hook the unmanned aerial vehicle support so as to firmly fix the unmanned aerial vehicle and the platform. Each groove is provided with two U-shaped hooks, so that firmness can be enhanced.
The function of the mechanical claw is: when the LiDAR is clamped, the LiDAR can be clamped rapidly, and the stability of the LiDAR is kept; when the LiDAR is loosened, the LiDAR can be quickly loosened, and the disassembly efficiency of the device can be improved. A layer of rubber material is attached in the mechanical claw, so that LiDAR damage can be prevented.
Normally, the unmanned aerial vehicle can stop on a flat ground when descending, and the shockproof support frame of the unmanned aerial vehicle carrying platform has the following functions: when the unmanned aerial vehicle lands, if the nearby ground is not flat, the unmanned aerial vehicle lands stably by stopping on the pits through the springs of the platform supporting frames.
In order to achieve the above purpose, the technical scheme of the invention is as follows:
an unmanned aerial vehicle carries on platform device, its characterized in that: the device comprises a U-shaped hook 1, a pneumatic cylinder 2, a double rod 3, a small baffle 4, a sliding sleeve 5, a supporting frame 6, a spring 7, a small circular plate 8, a mechanical claw 9, a connecting rod 10, a mechanical claw constraint support 19, a table top 15 and a platform groove 16.
The length of the open end of the U-shaped hook 1 is unequal, the tail end of the short end is provided with a small baffle socket 11, the top point of the long end is a spring connection point 12, and a part of the U-shaped hook 1 is pressed below the platform.
The sliding sleeve 5 is sleeved on the double rods.
Two equiaxed symmetrically distributed pins 51 are arranged on two sides of the sliding sleeve 5.
The small baffle 4 is made of metal materials with heavier specific gravity, such as iron and copper, and when the small baffle 4 is inserted on the U-shaped hook 1, the small baffle 4 is stable and is not easy to be overturned.
The two ends of the connecting rod 10 are respectively provided with a hole, one end of the hole penetrates through a pin 51 at one side of the sliding sleeve 5 to form a hinge joint with the sliding sleeve, and the other end of the connecting rod 10 is matched with a pin 192 at the outer side of the mechanical claw restraining support 19 below the table top 15; the hole at one end of the other connecting rod 10 passes through the pin 51 at the other side of the sliding sleeve 5 to form a hinge joint with the sliding sleeve 5, and the hole at the other end of the connecting rod 10 is matched with the pin 92 at the side of the mechanical claw 9. The two connecting rods 10, one sliding sleeve 5, the mechanical claw 9 and the mechanical claw restraining support 19 form a crank slide block mechanism.
Four grooves 16 are formed in the edges of four corners of the table top 15, and two semicircular rings are designed in each groove 16 to be connected with the springs. One end of the spring hooks the semicircle ring, and the other end of the spring hooks the U-shaped hook 1. The U-shaped hook 1 is buckled on the support of the unmanned aerial vehicle, and the small baffle 4 on the U-shaped hook 1 is attached to the unmanned aerial vehicle support, so that the U-shaped hook 1 hooks the unmanned aerial vehicle support more stably, and the platform is stably and fixedly connected to the unmanned aerial vehicle.
The pneumatic cylinder 2 is in the center of the table top 15, the rod of the pneumatic cylinder 2 is fixed with the double rods 3 through welding, and the pneumatic cylinder 2 is cylindrical and is provided with an external remote controller. The pneumatic cylinder 2 is controlled by a remote controller to operate so as to drive the crank block mechanism to clamp or loosen the mechanical claw 9.
The support frame 6, the spring 7 and the small circular plate 8 are combined, one end of the spring is welded on the bottom surface of the support frame 6, and the other end of the spring is welded at the center of the small circular plate 8, so that the support frame with the shockproof function is formed.
The invention has the beneficial effects that: according to the unmanned aerial vehicle carrying platform, liDAR can be quickly installed and detached on an unmanned aerial vehicle, and on the premise that the LiDAR is firmly fixed on the unmanned aerial vehicle, the time for installing and separating the LiDAR is saved, and the labor efficiency is improved; in addition, the shockproof support frame can enable the platform to be randomly parked on the ground, and can also facilitate the carrying and moving of the automobile. The unmanned aerial vehicle carrying platform provided by the invention provides a guarantee for rapidly acquiring agricultural information and timely making corresponding decisions according to the information.
Drawings
Fig. 1 is a structural isometric view of the device of the present invention.
Fig. 2 is a structural lower view of the device of the present invention.
Fig. 3 is a three-dimensional view of the structure of the device of the present invention.
Fig. 4 is an isometric view of a clevis of the device of the present invention.
Fig. 5 is a three-dimensional view of a platform of the apparatus of the present invention.
Fig. 6 is a top view of a dual rod of the device of the present invention.
Fig. 7 is a three-dimensional view of a sliding sleeve of the device of the present invention.
Fig. 8 is a three-dimensional view of a platform support for the apparatus of the present invention.
Figure 9 is a cross-sectional view of a land groove of the device of the present invention.
Fig. 10 is a left side view of a land recess of the inventive apparatus.
FIG. 11 is a three-dimensional view of the gripper components of the device of the present invention.
In the figure: a 1-U-shaped hook; 11-small baffle socket; 12-spring connection points; 2-a pneumatic cylinder; 21-the pneumatic cylinder is provided with a rod; 3-double bars; 4-small baffles; 5-sliding sleeve; 51-sliding sleeve side pins; 6-supporting frames; 7-a spring; 8-small circular plate; 9-mechanical claws; 91-a gripper extension plate; 92-gripper side pins; 10-connecting rods; 15-a table top; 16-land grooves; 19-a mechanical claw restraining support; 191-mechanical jaw restraining support perforations; 192-mechanical jaw restrains the support side pin.
Detailed Description
The structure, principles and operation of the present invention are further described with reference to the accompanying drawings.
Fig. 1 is a structural isometric view of the device of the present invention, wherein many of the structures of the device can be seen: the device comprises a U-shaped hook 1, a pneumatic cylinder 2, a double rod 3, a small baffle 4, a sliding sleeve 5, a supporting frame 6, a spring 7, a small circular plate 8, a mechanical claw 9, a connecting rod 10, a table top 15, a platform groove 16 and a mechanical claw constraint support 19.
The open ends of the U-shaped hooks 1 are unequal in length, small baffle plate sockets 11 are arranged at the tail ends of the short ends, the tops of the long ends are spring connection points 12, and a part of the U-shaped hooks 1 are pressed below the platform.
Wherein the sliding sleeve 5 is sleeved on the double rod 3.
Wherein two equiaxed symmetrically distributed pins are arranged on two sides of the sliding sleeve 5.
Wherein, the material of little baffle 4 is the iron that the quality is heavy slightly, and little baffle 4 is stable be difficult for jolting out when little baffle 4 inserts on U-shaped hook 1.
Wherein, two ends of the connecting rod 10 are respectively provided with a hole, one end of the hole passes through a pin at one side of the sliding sleeve 5 to form a hinge joint with the sliding sleeve, and the other end of the connecting rod 10 is matched with a pin 192 at the outer side of the mechanical claw constraint support 19 below the table top 15; the hole at one end of the other connecting rod 10 passes through the pin at the other side of the sliding sleeve 5 to form a hinge joint with the sliding sleeve 5, and the hole at the other end of the connecting rod 10 is matched with the pin 92 at the side of the mechanical claw 9. The two connecting rods 10, one sliding sleeve 5, the mechanical claw 9 and the mechanical claw restraining support 19 form a crank slide block mechanism.
Four grooves 16 are formed in the edges of four corners of the table top 15, two semicircular rings are designed in each groove, the two semicircular rings are formed in an M shape side by side, one end of each spring hooks the semicircular ring, and the other end of each spring hooks the U-shaped hook 1. The U-shaped hook 1 is buckled on the support of the unmanned aerial vehicle, and the small baffle 4 on the U-shaped hook 1 is attached to the support of the unmanned aerial vehicle, so that the U-shaped hook is hooked on the support of the unmanned aerial vehicle more stably, and the platform is stably and fixedly connected to the unmanned aerial vehicle.
The pneumatic cylinder 2 is arranged in the center of the table top 15, the rod of the pneumatic cylinder 2 is fixed with the double rods 3 through welding, and the pneumatic cylinder 2 is cylindrical and is provided with an external remote controller. The pneumatic cylinder 2 is controlled to operate by a remote controller so as to drive the crank block mechanism to clamp or loosen the mechanical claw 9.
Wherein, support frame 6, spring 7 and little plectane 8 three combination, spring one end welding is in support frame 6 bottom surface, and the spring other end welding is in little plectane 8 center, constitutes the support frame that has shockproof function.
Fig. 2 and 3 are a lower view and a three-dimensional view of the device of the present invention, further reflecting the structure of the present invention, and it is known that the grooves of the platform are at four corners of the platform, and there are four grooves, each of which can be used to place two U-shaped hooks.
Fig. 4 is an isometric view of a clevis of the device of the present invention. The placement position of the small baffle can be known to be the small baffle socket 11 through an isometric view; the spring connecting point 12 at the tail part of the long end of the U-shaped hook 1 is provided with a small groove, and one end of the spring hooks the spring connecting point to achieve the connecting effect. The U-shaped hook 1 is connected in the groove of the platform by a spring, so that a device for fixing the unmanned aerial vehicle is formed.
Fig. 5 is a three-dimensional view of the platform of the apparatus of the present invention, with an intuitive understanding of the location of pins 192 and holes 191 on the platform gripper restraint support 19 of the present invention.
Fig. 6 shows a double-rod structure of the device of the invention, the four ends of the double rod 3 are sleeved with the sliding sleeve 5, so that the sliding sleeve 5 can freely slide left and right on the rod, single claws of 4 mechanical claws 9 are placed into the claw restraint device through holes 191, and then the mechanical claws 9 are connected with the double rod 3 through connecting pins 192, 92 and 51 by connecting rods 10 to form a device capable of clamping and loosening.
Fig. 7 is a three-dimensional view of a sliding sleeve of the device of the invention, two pins are arranged on two sides of the sliding sleeve 5, and the pins on two sides are equiaxed symmetrical.
Fig. 8 is a three-dimensional view of a platform support frame of the device of the invention, one end of a spring 7 is welded on the bottom surface of the support frame 6, and the other end of the spring 7 is welded on the center of a small circular plate 8, so that the support frame with the shockproof function is formed.
Fig. 9 and 10 are cross-sectional views and left side views of a platform groove of the device of the present invention, and it can be seen from the figures that two semicircular rings are provided in the groove 16, one end of the spring hooks the semicircular rings, and the other end of the spring is connected with the U-shaped hook 1, so that the U-shaped hook 1 is fixed in the platform groove 16.
Fig. 11 is a three-dimensional view of the gripper of the device of the present invention, with a visual understanding of the location of the extension plate 91 and pin 92 on the gripper.
The platform of the invention comprises the following steps:
a) And taking the unmanned aerial vehicle and the unmanned aerial vehicle carrying platform out for carrying out loading.
B) Firstly, placing a carrying platform on the ground, then placing an unmanned aerial vehicle on the carrying platform, righting the unmanned aerial vehicle, taking out the small baffle plate 4 in the U-shaped hook 1, manually or adopting an auxiliary tool to pull the U-shaped hook 1 outwards, placing an unmanned aerial vehicle support frame in the range of the U-shaped hook 1, loosening the U-shaped hook 1, clamping the unmanned aerial vehicle support frame, clamping 8U-shaped hooks 1, and finally inserting the small baffle plate 4 into the socket 11 at the short end of the U-shaped hook 1, thereby fixing the unmanned aerial vehicle on the carrying platform.
C) And then the remote controller is used for controlling the operation of the pneumatic cylinder 2, the built-in rod is driven to move upwards, the mechanical claw 9 is fast clamped under the action of the crank slider mechanism, before LiDAR is clamped, the LiDAR is placed at the lengthening plate of the mechanical claw 9, and after the LiDAR is clamped, the pneumatic cylinder is stopped by the remote controller, so that the mechanical claw is in a constantly clamped state. And then fix LiDAR on the platform, the platform links to each other with unmanned aerial vehicle, so unmanned aerial vehicle can stably carry the LiDAR and work.
D) After the unmanned aerial vehicle works, the unmanned aerial vehicle can descend at any time, the shockproof support frame which is arranged on the platform can land on uneven ground, after the unmanned aerial vehicle is stopped, the small baffle plate 4 is firstly taken out, then 8U-shaped hooks 1 are pulled outwards to separate the unmanned aerial vehicle, the unmanned aerial vehicle is put aside, then the remote controller is used for controlling the pneumatic cylinder 2 to operate, the built-in rod of the unmanned aerial vehicle moves downwards, the mechanical claw is loosened again through the crank sliding block mechanism, and then the laser radar is taken out. And then realize carrying platform and unmanned aerial vehicle separation, carrying platform and laser radar separation.
E) And finally, sequentially placing the unmanned aerial vehicle, the carrying platform and the LiDAR to a storage place, and finally realizing quick carrying, working and dismounting of the unmanned aerial vehicle.
Claims (2)
1. An unmanned aerial vehicle carries on platform, its characterized in that: the device comprises a U-shaped hook (1), a pneumatic cylinder (2), a double rod (3), a small baffle plate (4), a sliding sleeve (5), a supporting frame (6), a spring (7), a small circular plate (8), a mechanical claw (9), a connecting rod (10), a table top (15), a platform groove (16) and a mechanical claw constraint support (19);
The length of the opening end of the U-shaped hook (1) is unequal, the tail end of the short end is provided with a small baffle socket (11), the top point of the long end is a spring connection point (12), and the part of the long end, which is close to the spring connection point (12), is pressed below the table top (15); the U-shaped hook (1) is buckled on the unmanned aerial vehicle support, and is tightly attached to the unmanned aerial vehicle support through the small baffle plate (4), so that the U-shaped hook (1) is hooked on the unmanned aerial vehicle support more stably, and the platform is stably and fixedly connected to the unmanned aerial vehicle; the number of the U-shaped hooks (1) is 8, every two hooks are in a group, and the U-shaped hooks are respectively arranged on grooves (16) at the edges of four corners of the table top (15);
Four grooves (16) are formed in the four corners of the table top (15), two semicircular rings are arranged in the grooves (16) at the right center of one side close to the center of the table, and the two semicircular rings are connected and arranged side by side to form an M shape; the other end of the spring connected with the U-shaped hook (1) hooks the semicircular ring so that the U-shaped hook (1) is fixed in the groove (16);
The small baffle (4) is made of iron, and when the small baffle (4) is inserted into the U-shaped hook (1), the small baffle (4) is stable and is not easy to be overturned;
The pneumatic cylinder (2) is arranged in the center of the table top (15), and the rod of the pneumatic cylinder (2) is fixed with the double rods (3) through welding; clamping or loosening the mechanical claw (9) through a remote control pneumatic cylinder (2); a sliding sleeve (5) is sleeved on the double rod (3), and two equiaxed symmetrically distributed pins are arranged on two sides of the sliding sleeve (5);
The two ends of the connecting rod (10) are respectively provided with a hole, one end of the hole penetrates through a pin at one side of the sliding sleeve (5) to form a hinge joint with the sliding sleeve, and the other end of the connecting rod (10) is sleeved on the pin at the outer side of the mechanical claw constraint support (19) below the table top (15) to form clearance fit; the hole at one end of the other connecting rod (10) passes through the pin at the other side of the sliding sleeve (5) to form a hinge joint with the sliding sleeve (5), and the hole at the other end of the connecting rod (10) is sleeved on the pin at the side of the mechanical claw (9) to form clearance fit; the last two connecting rods (10), a sliding sleeve (5), a mechanical claw (9) and a mechanical claw constraint support (19) form a crank slide block mechanism;
The support frame (6), the spring (7) and the small circular plate (8) are combined, one end of the spring is welded on the bottom surface of the support frame (6), and the other end of the spring is welded at the center of the small circular plate (8).
2. The unmanned aerial vehicle mounting platform of claim 1, wherein: an extension plate (91) is arranged at the tail part of the mechanical claw (9) so as to increase the contact area between the mechanical claw (9) and the carrying equipment; a layer of rubber material is attached to the inner side of the mechanical claw (9) to prevent damage to the carrying equipment.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202111543651.1A CN114194406B (en) | 2021-12-16 | 2021-12-16 | Unmanned aerial vehicle carries on platform |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202111543651.1A CN114194406B (en) | 2021-12-16 | 2021-12-16 | Unmanned aerial vehicle carries on platform |
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| Publication Number | Publication Date |
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| CN114194406A CN114194406A (en) | 2022-03-18 |
| CN114194406B true CN114194406B (en) | 2024-05-14 |
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| CN202111543651.1A Active CN114194406B (en) | 2021-12-16 | 2021-12-16 | Unmanned aerial vehicle carries on platform |
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| CN (1) | CN114194406B (en) |
Citations (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN207346114U (en) * | 2017-05-18 | 2018-05-11 | 深圳市道通智能航空技术有限公司 | A kind of head assembly, bogey and unmanned plane |
| CN208271423U (en) * | 2017-12-26 | 2018-12-21 | 石家庄慷派世纪数码科技有限公司 | A kind of unmanned plane instructional device |
| CN208278342U (en) * | 2018-06-14 | 2018-12-25 | 四川翼空智控科技有限公司 | A kind of multi-rotor unmanned aerial vehicle holder damping device |
| CN110450968A (en) * | 2019-09-06 | 2019-11-15 | 中嘉(广东)工程检测有限公司 | Quick clamping bracket and its unmanned plane for engineering mapping |
| CN211844928U (en) * | 2020-03-02 | 2020-11-03 | 扬州翊翔航空科技有限公司 | Adjustable unmanned aerial vehicle carries support |
| CN111874245A (en) * | 2020-07-28 | 2020-11-03 | 深圳职业技术学院 | Unmanned aerial vehicle mounting device and unmanned aerial vehicle |
| CN213473544U (en) * | 2020-11-18 | 2021-06-18 | 吉鸥信息技术（杭州）有限公司 | Unmanned aerial vehicle laser radar installation device |
| CN113202899A (en) * | 2021-05-26 | 2021-08-03 | 万航星空科技发展有限公司 | Airborne laser radar damping device |
| CN113247284A (en) * | 2021-06-16 | 2021-08-13 | 广西瀚维智测科技有限公司 | Unmanned aerial vehicle carries on support platform that ground removed laser scanner used |
-
2021
- 2021-12-16 CN CN202111543651.1A patent/CN114194406B/en active Active
Patent Citations (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN207346114U (en) * | 2017-05-18 | 2018-05-11 | 深圳市道通智能航空技术有限公司 | A kind of head assembly, bogey and unmanned plane |
| CN208271423U (en) * | 2017-12-26 | 2018-12-21 | 石家庄慷派世纪数码科技有限公司 | A kind of unmanned plane instructional device |
| CN208278342U (en) * | 2018-06-14 | 2018-12-25 | 四川翼空智控科技有限公司 | A kind of multi-rotor unmanned aerial vehicle holder damping device |
| CN110450968A (en) * | 2019-09-06 | 2019-11-15 | 中嘉(广东)工程检测有限公司 | Quick clamping bracket and its unmanned plane for engineering mapping |
| CN211844928U (en) * | 2020-03-02 | 2020-11-03 | 扬州翊翔航空科技有限公司 | Adjustable unmanned aerial vehicle carries support |
| CN111874245A (en) * | 2020-07-28 | 2020-11-03 | 深圳职业技术学院 | Unmanned aerial vehicle mounting device and unmanned aerial vehicle |
| CN213473544U (en) * | 2020-11-18 | 2021-06-18 | 吉鸥信息技术（杭州）有限公司 | Unmanned aerial vehicle laser radar installation device |
| CN113202899A (en) * | 2021-05-26 | 2021-08-03 | 万航星空科技发展有限公司 | Airborne laser radar damping device |
| CN113247284A (en) * | 2021-06-16 | 2021-08-13 | 广西瀚维智测科技有限公司 | Unmanned aerial vehicle carries on support platform that ground removed laser scanner used |
Also Published As
| Publication number | Publication date |
|---|---|
| CN114194406A (en) | 2022-03-18 |
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