CN112678195A - Unmanned aerial vehicle - Google Patents
Unmanned aerial vehicle Download PDFInfo
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- CN112678195A CN112678195A CN202011638990.3A CN202011638990A CN112678195A CN 112678195 A CN112678195 A CN 112678195A CN 202011638990 A CN202011638990 A CN 202011638990A CN 112678195 A CN112678195 A CN 112678195A
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Abstract
The invention provides an unmanned aerial vehicle, and relates to the field of unmanned aerial vehicle shooting. This unmanned aerial vehicle, including unmanned aerial vehicle organism, mounting panel, screw, balance compensation mechanism, camera mechanism and buffer bracket, the outer wall fixed connection of mounting panel and unmanned aerial vehicle organism, the mounting panel is four, the screw is connected with the top outer wall of mounting panel, the bottom inner wall fixed connection of balance compensation mechanism and mounting panel, the bottom outer wall fixed connection of buffer bracket and unmanned aerial vehicle organism, camera mechanism sets up the below at the unmanned aerial vehicle organism, camera mechanism is including solid fixed ring, connecting plate and camera, gu fixed ring's one end is connected with the electric reversing bar in the unmanned aerial vehicle organism. This unmanned aerial vehicle has avoided unmanned aerial vehicle to cause great influence to the picture of making a video recording when taking place great shake, has improved the shooting effect, can make unmanned aerial vehicle be difficult to take place great rocking and upset, prevents that unmanned aerial vehicle from turning on one's side, has improved its security.
Description
Technical Field
The invention relates to the technical field of unmanned aerial vehicle shooting, in particular to an unmanned aerial vehicle.
Background
Unmanned aircraft are simply "drones" and, in contrast to manned aircraft, drones are often better suited to tasks that are too "fool, dirty, or dangerous". Unmanned aerial vehicles can be classified into military and civil applications according to the application field. For military use, unmanned aerial vehicles divide into reconnaissance aircraft and target drone. In the civil aspect, the unmanned aerial vehicle + the industry application is really just needed by the unmanned aerial vehicle; at present, the unmanned aerial vehicle is applied to the fields of aerial photography, agriculture, plant protection, miniature self-timer, express transportation, disaster relief, wild animal observation, infectious disease monitoring, surveying and mapping, news reporting, power inspection, disaster relief, film and television shooting, romantic manufacturing and the like, the application of the unmanned aerial vehicle is greatly expanded, and developed countries actively expand industrial application and develop unmanned aerial vehicle technology.
When utilizing unmanned aerial vehicle to shoot, can receive the influence of strong wind, not only can produce and rock the influence camera, make the picture shake of shooting, influence the shooting effect, too big rocking also can make unmanned aerial vehicle unbalance simultaneously, the camera can cause the damage to inside part in jolting repeatedly, influence the life of camera, if can not in time balance, unmanned aerial vehicle can overturn and crash, has the potential safety hazard.
Disclosure of Invention
Technical problem to be solved
Aiming at the defects of the prior art, the invention provides an unmanned aerial vehicle, which solves the problems that when the unmanned aerial vehicle is used for shooting, the unmanned aerial vehicle is possibly influenced by strong wind, the camera is influenced by shaking, a shot picture shakes to influence a shooting effect, meanwhile, the unmanned aerial vehicle is unbalanced by overlarge shaking, the camera can damage internal parts in repeated bumping to influence the service life of the camera, and if the camera cannot be balanced in time, the unmanned aerial vehicle can be overturned and crashed, so that potential safety hazards exist.
(II) technical scheme
In order to achieve the purpose, the invention is realized by the following technical scheme: the utility model provides an unmanned aerial vehicle, includes unmanned aerial vehicle organism, mounting panel, screw, balance compensation mechanism, camera mechanism and cushion frame, the outer wall fixed connection of mounting panel and unmanned aerial vehicle organism, the mounting panel is four, the screw is connected with the top outer wall of mounting panel, the bottom inner wall fixed connection of balance compensation mechanism and mounting panel, the bottom outer wall fixed connection of cushion frame and unmanned aerial vehicle organism, the mechanism setting of making a video recording is in the below of unmanned aerial vehicle organism.
Preferably, the camera shooting mechanism comprises a fixing ring, a connecting plate and a camera, wherein one end of the fixing ring is connected with an electric reversing rod in the unmanned aerial vehicle body, the connecting plate is movably connected with the fixing ring, and the camera is fixedly connected with the inside of the connecting plate.
Preferably, solid fixed ring includes planking, spherical board, activity ball, universal head and fixed establishment, the mounting groove has been seted up to one side inner wall of planking, the inner wall fixed connection of spherical board and mounting groove, universal head and spherical board swing joint, the activity ball sets up between universal head and spherical board, the inner wall of activity ball is provided with the elastic support pole, the inside packing gas that is provided with of activity ball, evenly distributed's recess is seted up to universal head's outer wall, activity ball and recess looks adaptation, universal head's one end outer wall and connecting plate fixed connection, fixed establishment sets up the inner wall at solid fixed ring. .
Preferably, the cavity is left to the inner wall of universal head, universal head is including activity head, backup pad, balancing pole, gravity ring, limiting plate, probe and sensor, the sensor sets up the inner wall at the activity head, the backup pad is connected with the bottom inner wall of activity head, the balancing pole rotates with the backup pad to be connected, the limiting plate sets up the both sides at the balancing pole, the gravity ring cup joints with the balancing pole mutually, the probe is connected with the both ends outer wall of balancing pole.
Preferably, the fixing mechanism comprises a fixing plate, an air bag, a fixing head, a piston and a connecting spring, a sliding cylinder is arranged on the inner wall of the fixing plate, the piston is movably connected with the sliding cylinder, a sliding block is arranged at one end of the connecting spring, the other end of the connecting spring is fixedly connected with the piston, and the fixing head is rotatably connected with the outer wall of one side of the piston.
Preferably, the fixed head comprises a pressing rod, a rotating plate, an elastic sheet and a rubber head, the pressing rod is fixedly connected with the rotating plate, the elastic plate is movably connected with the rotating plate through a spring, the elastic sheet is arranged on the inner wall of the elastic plate, and the rubber head is fixedly connected with one end of the elastic sheet.
Preferably, the balance compensation mechanism comprises a shell plate, a magnetic plate, an elastic layer, a sliding rod, an electromagnet and a starting plate, the starting plate is rotatably connected with the magnetic plate, the elastic layer is arranged on the outer walls of the two sides of the shell plate, the sliding rod is slidably connected with the shell plate, the outer wall of one end of the sliding rod is fixedly connected with the elastic layer, and the electromagnet is fixedly connected with the inner wall of the bottom end of the shell plate. When the unmanned aerial vehicle is used, the buffer frame plays a role in buffer protection for the unmanned aerial vehicle, can reduce vibration during take-off and falling, and simultaneously plays a role in protecting the camera, the propeller is started to enable the unmanned aerial vehicle to take off, so that the camera on the unmanned aerial vehicle can shoot in the air, due to the arrangement of the fixing ring, the universal head can rotate along the movable ball, the elastic supporting rod and the filling gas are arranged inside the movable ball, slight deformation can be generated under the action of the gravity of the camera, the elastic ball is embedded in the groove on the surface of the universal head, a certain fixing effect is realized on the universal head, when slight shaking occurs, the elastic ball has a buffer effect, the influence of vibration on the camera is reduced, when the unmanned aerial vehicle shakes due to strong wind, the camera has larger weight, the camera cannot deflect immediately under the action of inertia, and the universal head can rotate along the movable ball, make the camera can keep original position to cause great influence to the picture of making a video recording when having avoided unmanned aerial vehicle to take place great shake, improved the shooting effect. The gasbag moves the movable block pressure, the movable block drives the piston on the connecting spring and removes, thereby hug closely the fixed head at the outer wall of connecting plate, the fixed effect to the connecting plate has been improved, prevent that the camera can produce continuous rocking because of shake or wind-force, when unmanned aerial vehicle receives strong wind and takes place to rock, the piston that one side can be pressed to the connecting plate rotates inwards, pressure also can change along with taking place in the gasbag, make the piston of opposite side stretch out, thereby when the camera can keep original position, also can strengthen fixed effect, the depression bar can drive the rotor plate and rotate, make the elastic plate closely paste on the fixed head, thereby strengthened the fixed effect to the connecting plate, when the elastic plate takes place deformation simultaneously, can make the flexure strip take place the compression, make the rubber head pop out, further make the rotor plate be difficult for taking place to rotate. When unmanned aerial vehicle took place great shake, the movable head took place to deflect, and the balancing pole is balanced because the effect of gravity and limiting plate, and the sensor can receive the deflection signal of probe, can make the electro-magnet circular telegram of unbalance side, and the electro-magnet produces suction to the magnetic plate to make unmanned aerial vehicle can be balanced fast, can drive simultaneously and start the board and rotate, pop out the slide bar, drive the elastic layer and open the resistance of strengthening.
(III) advantageous effects
(1) According to the unmanned aerial vehicle, due to the arrangement of the fixing ring, the universal head can rotate along the movable ball, the elastic supporting rod and the filling gas are arranged inside the movable ball, the elastic supporting rod can deform slightly under the action of the gravity of the camera, the elastic ball is embedded in the groove on the surface of the universal head, a certain fixing effect is achieved on the universal head, when the unmanned aerial vehicle shakes slightly, the elastic ball has a buffering effect, the influence of vibration on the camera is reduced, when the unmanned aerial vehicle shakes under strong wind, the camera cannot deflect immediately under the action of inertia due to the fact that the camera has larger weight, the universal head can rotate along the movable ball, the original position of the camera can be kept, the problem that when the unmanned aerial vehicle shakes greatly, the camera is greatly influenced is avoided, and the shooting effect is improved.
(2) According to the unmanned aerial vehicle, the movable block is pressed by the air bag, the movable block drives the piston on the connecting spring to move, so that the fixed head is tightly attached to the outer wall of the connecting plate, the fixing effect on the connecting plate is improved, the camera is prevented from continuously shaking due to shaking or wind power, when the unmanned aerial vehicle shakes due to strong wind, the piston on one side can be pressed by the connecting plate to rotate inwards, the pressure in the air bag can be changed along with the change of the pressure in the air bag, the piston on the other side extends out, and the fixing effect can be enhanced while the original position of the camera can be kept.
(3) According to the unmanned aerial vehicle, the compression rod can drive the rotating plate to rotate, so that the elastic plate is tightly attached to the fixing head, the fixing effect on the connecting plate is enhanced, meanwhile, when the elastic plate deforms, the elastic sheet is compressed, the rubber head is popped out, and the rotating plate is further not prone to rotating.
(4) When the unmanned aerial vehicle shakes greatly, the movable head deflects, the balance rod keeps balance due to the action of gravity and the limiting plate, the sensor receives a deflection signal of the probe, the electromagnet on the unbalanced side is electrified, the electromagnet generates suction to the magnetic plate, so that the unmanned aerial vehicle can quickly balance, the starting plate is driven to rotate at the same time, the sliding rod is popped out to drive the elastic layer to open, the resistance is enhanced, and the unmanned aerial vehicle is prevented from turning sideways, so that the problem that when the unmanned aerial vehicle is used for shooting is effectively solved, the influence of strong wind can be caused, the camera is influenced by shaking, the shot picture shakes, the shooting effect is influenced, the unmanned aerial vehicle is unbalanced by overlarge shaking, the camera can damage internal parts in repeated bumping, the service life of the camera is influenced, if the camera cannot be balanced in time, the unmanned aerial vehicle can overturn and crash, the potential safety hazard exists.
Drawings
Fig. 1 is a front view of a structure of an unmanned aerial vehicle according to the present invention;
FIG. 2 is a cross-sectional view of a retaining ring according to the present invention;
FIG. 3 is a cross-sectional view of a universal head according to the present invention;
FIG. 4 is a structural cross-sectional view of a securing mechanism of the present invention;
FIG. 5 is an enlarged view of the structure of the present invention at A;
fig. 6 is a structural sectional view of a balance compensation mechanism of the present invention.
The system comprises an unmanned aerial vehicle body 1, an unmanned aerial vehicle body 2, a mounting plate 2, a propeller 3, a balance compensation mechanism 4, a buffer frame 5, a fixing ring 6, a connecting plate 7, a camera 8, an outer plate 9, a spherical plate 10, a movable ball 11, a universal head 12, a fixing mechanism 13, a movable head 14, a support plate 15, a balance rod 16, a gravity ring 17, a limiting plate 18, a probe 19, a sensor 20, a fixing plate 21, an air bag 22, a fixing head 23, a piston 24, a connecting spring 25, a pressure rod 26, a rotating plate 27, an elastic plate 28, an elastic sheet 29, a rubber head 30, a shell plate 31, a magnetic plate 32, a magnetic plate 30, a magnetic head 24, a magnetic, 33-elastic layer, 34-sliding rod, 35-electromagnet and 36-starting plate.
Detailed Description
The technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the accompanying drawings of the present invention, and it is obvious that the described embodiments are only a part of the embodiments of the present invention, and not all of the embodiments. All other embodiments, which can be derived by a person skilled in the art from the embodiments given herein without making any creative effort, shall fall within the protection scope of the present invention.
Examples
As shown in fig. 1-6, an embodiment of the invention provides an unmanned aerial vehicle, which includes an unmanned aerial vehicle body 1, a mounting plate 2, four propeller screws 3, a balance compensation mechanism 4, a camera mechanism and a buffer frame 5, wherein the mounting plate 2 is fixedly connected with the outer wall of the unmanned aerial vehicle body 1, the four mounting plates 2 are provided, the propeller screws 3 are connected with the outer wall of the top end of the mounting plate 2, the balance compensation mechanism 4 is fixedly connected with the inner wall of the bottom end of the mounting plate 2, the buffer frame 5 is fixedly connected with the outer wall of the bottom end of the unmanned aerial vehicle body 1, and the camera mechanism is arranged.
According to the unmanned aerial vehicle, the camera shooting mechanism comprises a fixing ring 6, a connecting plate 7 and a camera 8, one end of the fixing ring 6 is connected with an electric reversing rod in the unmanned aerial vehicle body 1, the connecting plate 7 is movably connected with the fixing ring 6, and the camera 8 is fixedly connected with the inside of the connecting plate 7.
In the invention, the fixing ring 6 comprises an outer plate 9, a spherical plate 10, a movable ball 11, a universal head 12 and a fixing mechanism 13, wherein an installation groove is formed in the inner wall of one side of the outer plate 9, the spherical plate 10 is fixedly connected with the inner wall of the installation groove, the universal head 12 is movably connected with the spherical plate 10, the movable ball 11 is arranged between the universal head 12 and the spherical plate 10, an elastic supporting rod is arranged on the inner wall of the movable ball 11, filling gas is filled in the movable ball 11, uniformly distributed grooves are formed in the outer wall of the universal head 12, the movable ball 11 is matched with the grooves, the outer wall of one end of the universal head 12 is fixedly connected with the connecting plate 7, and the fixing mechanism 13 is arranged on the inner. .
According to the invention, a cavity is reserved on the inner wall of the universal head 12, the universal head 12 comprises a movable head 14, a supporting plate 15, a balance bar 16, a gravity ring 17, a limiting plate 18, a probe 19 and a sensor 20, the sensor 20 is arranged on the inner wall of the movable head 14, the supporting plate 15 is connected with the inner wall of the bottom end of the movable head 14, the balance bar 16 is rotatably connected with the supporting plate 15, the limiting plate 18 is arranged on two sides of the balance bar 16, the gravity ring 17 is sleeved with the balance bar 16, and the probe 19 is connected with the outer walls of two ends of the balance bar 16.
In the invention, the fixing mechanism 13 comprises a fixing plate 21, an air bag 22, a fixing head 23, a piston 24 and a connecting spring 25, wherein a sliding cylinder is arranged on the inner wall of the fixing plate 21, the piston 24 is movably connected with the sliding cylinder, a sliding block is arranged at one end of the connecting spring 25, the other end of the connecting spring 25 is fixedly connected with the piston 24, and the fixing head 23 is rotatably connected with the outer wall of one side of the piston 24.
In the invention, the fixed head 23 comprises a compression bar 26, a rotating plate 27, an elastic plate 28, an elastic sheet 29 and a rubber head 30, wherein the compression bar 26 is fixedly connected with the rotating plate 27, the elastic plate 28 is movably connected with the rotating plate 27 through a spring, the elastic sheet 29 is arranged on the inner wall of the elastic plate 28, and the rubber head 30 is fixedly connected with one end of the elastic sheet 29.
In the invention, the balance compensation mechanism 4 comprises a shell plate 31, a magnetic plate 32, an elastic layer 33, a sliding rod 34, an electromagnet 35 and a starting plate 36, wherein the starting plate 36 is rotatably connected with the magnetic plate 32, the elastic layer 33 is arranged on the outer walls of two sides of the shell plate 31, the sliding rod 34 is slidably connected with the shell plate 31, the outer wall of one end of the sliding rod 34 is fixedly connected with the elastic layer 33, and the electromagnet 35 is fixedly connected with the inner wall of the bottom end of the shell plate 31.
The working principle is as follows: when the unmanned aerial vehicle is used, when the unmanned aerial vehicle shoots at high altitude, strong wind can be possibly applied, the camera 8 can be affected by shaking, the shot picture can be shaken, the shooting effect can be affected, meanwhile, the unmanned aerial vehicle can be unbalanced due to overlarge shaking, the camera 8 can damage internal parts in repeated jolting, the service life of the camera 8 can be affected, if the camera cannot be balanced in time, the unmanned aerial vehicle can be overturned and crashed, potential safety hazards exist, the buffer frame 5 plays a role in buffering and protecting the unmanned aerial vehicle, the vibration can be reduced during taking off and falling, meanwhile, the camera 8 can be protected, the propeller 3 is started, the unmanned aerial vehicle can take off, the camera 8 on the unmanned aerial vehicle can carry out aerial shooting, due to the arrangement of the fixing ring 6, the universal head 12 can rotate along the movable ball 11, the elastic supporting rod and the filling gas are arranged inside the movable ball 11, under the effect of camera 8 gravity, can produce slight deformation, make the elastic ball gomphosis in the recess on universal head 12 surface, have certain fixed effect to universal head 12, when taking place slight shake, the elastic ball has buffering effect, the influence of vibrations to camera 8 has been reduced, receive strong wind at unmanned aerial vehicle and take place to rock the time, because camera 8 has great weight, camera 8 can not take place to deflect at once under inertial effect, universal head 12 can take place to rotate along activity ball 11, make camera 8 can keep original position, thereby caused great influence to the picture of making a video recording when having avoided unmanned aerial vehicle to take place great shake, the shooting effect is improved. The air bag 22 presses the movable block, the movable block drives the piston 24 connected with the spring 25 to move, thereby the fixed head 23 is tightly attached to the outer wall of the connecting plate 7, the fixing effect to the connecting plate 7 is improved, the camera 8 is prevented from continuously shaking due to shaking or wind power, when the unmanned aerial vehicle shakes by strong wind, the connecting plate 7 can press the piston 24 on one side to rotate inwards, the pressure in the air bag 22 can be changed along with the pressure, so that the piston 24 on the other side extends out, so that the camera 8 can keep the original position and enhance the fixing effect, the pressure lever 26 can drive the rotating plate 27 to rotate, the elastic plate 28 is tightly attached to the fixed head 23, thereby enhancing the fixing effect of the connecting plate 7, and when the elastic plate 28 is deformed, the elastic piece 29 is compressed to eject the rubber head 30, so that the rotating plate 27 is further prevented from rotating easily. When unmanned aerial vehicle took place great shake, the movable head 14 took place to deflect, balancing pole 16 is balanced owing to gravity and limiting plate 18's effect, sensor 20 can receive probe 19 deflection signal, can make the electro-magnet 35 of unbalance side circular telegram, electro-magnet 35 produces suction to magnetic plate 32, thereby make unmanned aerial vehicle can be balanced fast, can drive simultaneously and start up 36 rotations of board, pop out slide bar 34, it opens to drive elastic layer 33, can strengthen the resistance when elastic layer 33 opens, cooperation electro-magnet 35's suction, can make unmanned aerial vehicle be difficult to take place great rocking and upset, guard action has been played camera 8, prevent that unmanned aerial vehicle from turning on one's side, the security has been improved.
It is noted that, herein, relational terms such as first and second, and the like may be used solely to distinguish one entity or action from another entity or action without necessarily requiring or implying any actual such relationship or order between such entities or actions. Also, the terms "comprises," "comprising," or any other variation thereof, are intended to cover a non-exclusive inclusion, such that a process, method, article, or apparatus that comprises a list of elements does not include only those elements but may include other elements not expressly listed or inherent to such process, method, article, or apparatus. Without further limitation, an element defined by the phrase "comprising an … …" does not exclude the presence of other identical elements in a process, method, article, or apparatus that comprises the element.
Claims (7)
1. The utility model provides an unmanned aerial vehicle, includes unmanned aerial vehicle organism (1), mounting panel (2), screw (3), balance compensation mechanism (4), camera mechanism and cushion frame (5), its characterized in that: mounting panel (2) and the outer wall fixed connection of unmanned aerial vehicle organism (1), mounting panel (2) are four, screw (3) are connected with the top outer wall of mounting panel (2), the bottom inner wall fixed connection of balance compensation mechanism (4) and mounting panel (2), the bottom outer wall fixed connection of cushion frame (5) and unmanned aerial vehicle organism (1), the mechanism of making a video recording sets up the below at unmanned aerial vehicle organism (1).
2. A drone according to claim 1, characterised in that: the camera shooting mechanism comprises a fixing ring (6), a connecting plate (7) and a camera (8), one end of the fixing ring (6) is connected with an electric reversing rod in the unmanned aerial vehicle body (1), the connecting plate (7) is movably connected with the fixing ring (6), and the camera (8) is fixedly connected with the inside of the connecting plate (7).
3. A drone according to claim 2, characterised in that: solid fixed ring (6) include planking (9), spherical board (10), activity ball (11), universal head (12) and fixed establishment (13), the mounting groove has been seted up to one side inner wall of planking (9), the inner wall fixed connection of spherical board (10) and mounting groove, universal head (12) and spherical board (10) swing joint, activity ball (11) set up between universal head (12) and spherical board (10), the inner wall of activity ball (11) is provided with the elastic support pole, the inside packing gas that is provided with of activity ball (11), evenly distributed's recess has been seted up to the outer wall of universal head (12), activity ball (11) and recess looks adaptation, the one end outer wall and connecting plate (7) fixed connection of universal head (12), fixed establishment (13) set up the inner wall at solid fixed ring (6).
4. A drone according to claim 3, characterised in that: the cavity is left to the inner wall of universal head (12), universal head (12) is including activity head (14), backup pad (15), balancing pole (16), gravity ring (17), limiting plate (18), probe (19) and sensor (20), sensor (20) set up the inner wall at activity head (14), backup pad (15) are connected with the bottom inner wall of activity head (14), balancing pole (16) are rotated with backup pad (15) and are connected, limiting plate (18) set up the both sides at balancing pole (16), gravity ring (17) cup joint with balancing pole (16) mutually, probe (19) are connected with the both ends outer wall of balancing pole (16).
5. A drone according to claim 3, characterised in that: fixed establishment (13) are including fixed plate (21), gasbag (22), fixed head (23), piston (24) and coupling spring (25), the inner wall of fixed plate (21) is provided with the slide cartridge, piston (24) and slide cartridge swing joint, the one end of coupling spring (25) is provided with the slider, the other end and piston (24) fixed connection of coupling spring (25), fixed head (23) are connected with one side outer wall rotation of piston (24).
6. A drone according to claim 5, characterised in that: fixed head (23) include depression bar (26), rotor plate (27), elastic plate (28), flexure strip (29) and rubber head (30), depression bar (26) and rotor plate (27) fixed connection, elastic plate (28) pass through spring swing joint with rotor plate (27), flexure strip (29) set up at elastic plate (28) inner wall, the one end fixed connection of rubber head (30) and flexure strip (29).
7. A drone according to claim 1, characterised in that: the balance compensation mechanism (4) comprises a shell plate (31), a magnetic plate (32), an elastic layer (33), a sliding rod (34), an electromagnet (35) and a starting plate (36), wherein the starting plate (36) is rotatably connected with the magnetic plate (32), the elastic layer (33) is arranged on the outer walls of two sides of the shell plate (31), the sliding rod (34) is slidably connected with the shell plate (31), the outer wall of one end of the sliding rod (34) is fixedly connected with the elastic layer (33), and the electromagnet (35) is fixedly connected with the inner wall of the bottom end of the shell plate (31).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202011638990.3A CN112678195A (en) | 2020-12-31 | 2020-12-31 | Unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202011638990.3A CN112678195A (en) | 2020-12-31 | 2020-12-31 | Unmanned aerial vehicle |
Publications (1)
| Publication Number | Publication Date |
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| CN112678195A true CN112678195A (en) | 2021-04-20 |
Family
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
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| CN202011638990.3A Withdrawn CN112678195A (en) | 2020-12-31 | 2020-12-31 | Unmanned aerial vehicle |
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| CN (1) | CN112678195A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
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| CN113320707A (en) * | 2021-07-07 | 2021-08-31 | 四川省天域航通科技有限公司 | A camera linkage for unmanned aerial vehicle takes photo by plane |
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| CN104379959A (en) * | 2014-03-31 | 2015-02-25 | 深圳市大疆创新科技有限公司 | Damping device and aircraft employing same |
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Application publication date: 20210420 |