CN111017242B - Unmanned aerial vehicle satellite full-automatic reconnaissance equipment - Google Patents
Unmanned aerial vehicle satellite full-automatic reconnaissance equipment Download PDFInfo
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- CN111017242B CN111017242B CN201911394453.6A CN201911394453A CN111017242B CN 111017242 B CN111017242 B CN 111017242B CN 201911394453 A CN201911394453 A CN 201911394453A CN 111017242 B CN111017242 B CN 111017242B
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- 230000001360 synchronised effect Effects 0.000 claims description 3
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- 238000010586 diagram Methods 0.000 description 6
- 238000013461 design Methods 0.000 description 3
- 230000007547 defect Effects 0.000 description 2
- 238000013459 approach Methods 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000006835 compression Effects 0.000 description 1
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- 238000002474 experimental method Methods 0.000 description 1
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- 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
- B64D47/08—Arrangements of cameras
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- G—PHYSICS
- G01—MEASURING; TESTING
- G01C—MEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY
- G01C11/00—Photogrammetry or videogrammetry, e.g. stereogrammetry; Photographic surveying
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U2101/00—UAVs specially adapted for particular uses or applications
- B64U2101/30—UAVs specially adapted for particular uses or applications for imaging, photography or videography
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- Accessories Of Cameras (AREA)
Abstract
The invention discloses full-automatic reconnaissance equipment for an unmanned aerial vehicle satellite, which comprises a fixed plate, wherein the fixed plate is fixed on a body of the unmanned aerial vehicle, a fixed clamping groove and a fixed clamping plate are arranged on the fixed plate, one end of the clamping groove is sealed by an end plate, an induction hole is formed in the end plate, and a button switch of an induction component is arranged in the induction hole; the fixed clamping groove is clamped and assembled with the holder clamping plate, the holder clamping plate is arranged on the holder shell, the holder clamping groove is arranged on the holder shell, and the holder clamping groove is clamped and assembled with the fixed clamping plate; the holder shell belongs to a holder assembly; the end of the fixed clamping plate far away from the end plate is provided with a guide groove, a locking hole and a guide inclined surface, the locking hole is assembled with one end of a locking rod in a clamping manner, the other end of the locking rod penetrates through the holder partition plate and then is assembled with a limiting electromagnet, and the locking rod and the limiting electromagnet both belong to limiting components. According to the invention, the fixing plate is fixed on the unmanned aerial vehicle, and then the holder assembly and the fixing plate are designed to be detachable structures, so that the holder assembly is convenient to detach.
Description
Technical Field
The invention relates to the technical field of unmanned aerial vehicles, in particular to a satellite full-automatic reconnaissance device for an unmanned aerial vehicle.
Background
Along with the continuous research and development of the unmanned aerial vehicle in China, the unmanned aerial vehicle is an unmanned aerial vehicle which is operated by utilizing a radio remote control device and a self-contained program control device, a camera device is a device for shooting when the unmanned aerial vehicle carries out reconnaissance, part of the existing unmanned aerial vehicle has the condition that the camera device is not installed, when the unmanned aerial vehicle is additionally installed in the later stage, the cloud deck is installed on the unmanned aerial vehicle in a mode of punching and fixing screws, and then the camera device (camera) is fixed on the cloud deck. This approach, while simple, is cumbersome when disassembly is required.
In view of the above defects in the prior art, the invention provides a camera device for a full-automatic reconnaissance unmanned aerial vehicle, which aims to solve the technical problem that a holder is inconvenient to detach after being additionally mounted in the later period.
Disclosure of Invention
In view of the above defects in the prior art, the technical problem to be solved by the present invention is to provide a full-automatic surveying apparatus for unmanned aerial vehicle satellites.
In order to achieve the purpose, the invention provides full-automatic satellite reconnaissance equipment for an unmanned aerial vehicle, which comprises a fixed plate, wherein the fixed plate is fixed on a body of the unmanned aerial vehicle, a fixed clamping groove and a fixed clamping plate are arranged on the fixed plate, one end of the clamping groove is sealed by an end plate, an induction hole is formed in the end plate, and a button switch of an induction component is arranged in the induction hole;
the fixed clamping groove is clamped and assembled with the holder clamping plate, the holder clamping plate is arranged on the holder shell, the holder clamping groove is arranged on the holder shell, and the holder clamping groove is clamped and assembled with the fixed clamping plate; the holder shell belongs to a holder assembly; the fixed clamping plate is provided with a guide groove, a locking hole and a guide inclined plane at one end far away from the end plate, the locking hole is assembled with one end of a locking rod in a clamping manner, the other end of the locking rod penetrates through the holder partition plate and then is assembled with a limiting electromagnet, and the locking rod and the limiting electromagnet both belong to limiting components.
Preferably, the second brake disc is tightly attached to the first brake disc, the first brake disc is fixedly assembled with one end of the telescopic shaft, the other end of the telescopic shaft penetrates through the holder vertical plate and then is assembled with the electromagnet, a brake spring is arranged between the first brake disc and the holder vertical plate, and the brake spring is used for generating thrust to the first brake disc, so that the first brake disc and the second brake disc are tightly attached to each other.
Preferably, the holder assembly further comprises a matching shell, a matching inner cavity is formed in the matching shell, and a matching partition plate is fixed in the matching inner cavity; a second motor is arranged in the matching inner cavity, and an output shaft of the second motor is fixedly connected with the third shaft body; the third shaft body penetrates through the matching partition plate, the matching shell, the rotating block and the holder shell and then is installed in the holder inner cavity, one end of the third shaft body installed in the holder inner cavity is fixedly assembled with the second brake disc, the rotating block is fixed on the first supporting plate, and the third shaft body and the rotating block are fixedly assembled; the bottom of the first supporting plate is provided with a notch, an adjusting block is arranged in the notch, a camera is arranged on the adjusting block, the first shaft body penetrates through one side of the first supporting plate, the notch and the adjusting block and then is rotatably assembled with the other side of the first supporting plate, and the first shaft body and the adjusting block are assembled and fixed;
one end of the first shaft body extends out of the first supporting plate and is fixedly assembled with the first belt pulley, the first belt pulley is connected with the first auxiliary belt pulley through a synchronous belt and forms a belt transmission mechanism, the first auxiliary belt pulley is fixed on the first auxiliary shaft body, a helical gear a is further fixed on the first auxiliary shaft body, and one end of the first auxiliary shaft body is assembled with the first motor;
the bevel gear a is in meshing transmission with the auxiliary bevel gear a, the auxiliary bevel gear a is fixedly assembled with one end of the second shaft body, and the other end of the second shaft body is fixedly connected with an input shaft of the angle sensor;
the third shaft body is fixedly provided with a bevel gear b, the bevel gear b is in meshing transmission with the auxiliary bevel gear b, the auxiliary bevel gear b is fixedly assembled with one end of the fourth shaft body, and the other end of the fourth shaft body penetrates through the holder partition plate and then is fixedly connected with an input shaft of the angle sensor; the cradle head vertical plate and the cradle head partition plate are both fixed inside the inner cavity of the cradle head.
Preferably, the limiting assembly further comprises a convex ring arranged on the lock rod, a lock rod spring is arranged between the convex ring and the holder partition plate, and the lock rod spring is used for pushing the lock rod to move towards the locking hole all the time; the guide inclined plane is arranged from the open end of the guide groove to the locking hole in a downward inclined mode.
Preferably, a first conductive block and a second conductive block are respectively fixed on the top surface of the inner side of the fixed clamping groove close to the end plate, the first conductive block and the second conductive block are respectively in conductive connection with the conducting wire and the data wire, and a first conductive groove and a second conductive groove which are in conductive clamping connection with the first conductive block and the second conductive block are respectively arranged at the corresponding positions of the holder clamping plate and the first conductive block and the second conductive block.
Preferably, the sensing assembly comprises a button switch, one end of the button switch, which is provided with a trigger button, is installed in the sensing hole, a sensing partition plate is further fixed in the sensing hole, one end of a trigger rod penetrates through the sensing partition plate and then is right opposite to the trigger button, the other end of the trigger rod is installed in a fixed clamping groove, a driving ring is arranged at the end of the trigger rod, the trigger rod is positioned at two sides of the sensing partition plate and is respectively assembled and fixed with a limiting ring and a spring piece, the limiting ring is used for limiting the movement distance of the trigger rod to the fixed clamping groove, and the spring piece has elasticity;
the first conductive block and the second conductive block are respectively in conductive connection with different relay power-out ends, the power-in ends of the two relays are respectively in conductive connection with the unmanned aerial vehicle battery and the unmanned aerial vehicle CPU signal end, and the relays are in a disconnected state in an initial state; the button switch power-in end is connected with the unmanned aerial vehicle CPU signal end in a communication mode, and the power-out end is connected with the two relay signal ends in a communication mode.
Preferably, the first motor and the second motor are both stepping motors.
The invention has the beneficial effects that: according to the invention, the fixing plate is fixed on the unmanned aerial vehicle, the holder assembly and the fixing plate are designed into a detachable structure, and the camera is fixed on the holder assembly, so that the holder assembly is convenient to detach, and in the installation process, the holder assembly is locked on the fixing plate through the limiting lock assembly, so that the holder assembly is very stable, and the problems that the holder is difficult to detach and not stable enough after the existing unmanned aerial vehicle is refitted with the holder are solved.
Drawings
FIG. 1 is a schematic structural diagram of the present invention.
Fig. 2 is a schematic structural diagram of the present invention.
Fig. 3 is a schematic structural diagram of the present invention.
Fig. 4 is a schematic diagram of a fixing plate structure according to the present invention.
Fig. 5 is a schematic view of the limit lock assembly of the present invention.
Fig. 6 is a schematic view of the internal structure of the pan/tilt head assembly of the present invention.
Fig. 7 is a schematic view of the internal structure of the pan/tilt head assembly of the present invention.
Fig. 8 is a schematic view of the internal structure of the pan/tilt head assembly of the present invention.
Fig. 9 is a schematic view of the internal structure of the pan/tilt head assembly of the present invention.
Fig. 10 is a schematic structural diagram of a camera and a first support plate according to the present invention.
Fig. 11 is a schematic structural diagram of the sensing assembly of the present invention.
Detailed Description
The invention is further illustrated by the following examples in conjunction with the accompanying drawings:
referring to fig. 1 to 11, the full-automatic satellite reconnaissance equipment for the unmanned aerial vehicle comprises a fixing plate 110, wherein the fixing plate 110 is fixed on a body of the unmanned aerial vehicle, a fixing clamping groove 111 and a fixing clamping plate 120 are arranged on the fixing plate 110, one end of the clamping groove 111 is sealed by an end plate 130, an induction hole 131 is arranged on the end plate 130, and a button switch 310 of an induction component is installed in the induction hole 131;
the fixed clamping groove 111 is clamped and assembled with the holder clamping plate 212, the holder clamping plate 212 is arranged on the holder shell 210, the holder shell 210 is provided with the holder clamping groove 211, and the holder clamping groove 211 is clamped and assembled with the fixed clamping plate 120;
the holder shell 210 belongs to a holder assembly, the holder assembly further comprises a matching shell 220, a matching inner cavity 221 is formed inside the matching shell 220, and a matching partition plate 222 is fixed in the matching inner cavity 221;
a second motor 460 is installed in the matching inner cavity 221, an output shaft of the second motor 460 is fixedly connected with a third shaft body 530, and the second motor 460 can drive the third shaft body to rotate circumferentially;
the third shaft body 530 penetrates through the matching partition plate 222, the matching shell 220, the rotating block 242 and the holder shell 210 and then is loaded into the holder inner cavity 214, one end of the third shaft body loaded into the holder inner cavity 214 is fixedly assembled with the second brake disc 722, the rotating block 242 is fixed on the first supporting plate 240, and the third shaft body 530 is fixedly assembled with the rotating block 242;
the second brake disc 722 is tightly attached to the first brake disc 721 so as to limit the rotation of the third shaft 530, the first brake disc 721 is fixedly assembled with one end of the telescopic shaft 550, the other end of the telescopic shaft 550 passes through the cradle head vertical plate 213 and then is assembled with the electromagnet 470, the electromagnet 470 can drive the telescopic shaft 550 to move in the axial direction after being electrified, a brake spring 710 is arranged between the first brake disc 721 and the cradle head vertical plate 213, and the brake spring 710 is used for generating thrust to the first brake disc 721 so as to tightly attach the first brake disc 721 to the second brake disc 722;
the bottom of the first supporting plate 240 is provided with a notch 241, an adjusting block 420 is installed in the notch 241, a camera 410 is installed on the adjusting block 420, a first shaft body 511 penetrates through one side of the first supporting plate 240, the notch 241 and the adjusting block 420 and then is rotatably assembled with the other side of the first supporting plate 240, and the first shaft body 511 is fixedly assembled with the adjusting block 420;
one end of the first shaft body 511 extends out of the first support plate 240 and is assembled and fixed with the first pulley 611, the first pulley 611 is connected with the first pulley 612 through a timing belt 610 to form a belt transmission mechanism, the first pulley 612 is fixed on the first shaft body 512, a helical gear a621 is further fixed on the first shaft body 512, one end of the first shaft body 512 is assembled with the first motor 480, and the first motor 480 can drive the first shaft body 512 to rotate circumferentially, so that the first shaft body 511 is driven to rotate through the timing belt 610, and the camera 410 is driven to rotate around the first shaft body 511;
the bevel gear a621 is in meshing transmission with the secondary bevel gear a622, the secondary bevel gear a622 is fixedly assembled with one end of the second shaft body 520, the other end of the second shaft body 520 is fixedly connected with an input shaft of the angle sensor 452, when the first secondary shaft body 512 rotates, the second shaft body 520 is driven to rotate circumferentially, so that the input shaft of the angle sensor 452 is driven to rotate, the angle sensor 452 can obtain a signal capable of detecting the rotation angle of the second shaft body, and the rotation angle of the first shaft body can be converted through the signal, so that the rotation angle of the camera is further enabled;
a bevel gear b631 is fixed on the third shaft body 530, the bevel gear b631 is in meshing transmission with a secondary bevel gear b632, the secondary bevel gear b632 is fixedly assembled with one end of the fourth shaft body 540, and the other end of the fourth shaft body 540 passes through the tripod head partition plate 230 and then is fixedly connected with an input shaft of the angle sensor 451;
when the third shaft 530 rotates, the fourth shaft 540 is driven to rotate, so that the angle sensor 451 can detect the rotation angle of the fourth shaft 540, and the rotation angle of the third shaft can be converted through the rotation angle; the cradle head vertical plate
213. The holder partition plates 230 are all fixed inside the holder inner cavity 214;
the end, far away from the end plate 130, of the fixed snap-fit plate 120 is provided with a guide groove 121, a locking hole 122 and a guide inclined surface 123, the locking hole 122 is assembled with one end of a lock rod 431 in a clamping manner, the other end of the lock rod 431 penetrates through the holder partition plate 230 and then is assembled with a limiting electromagnet 430, the lock rod 431 and the limiting electromagnet 430 both belong to limiting components, the limiting components further comprise a convex ring 4311 arranged on the lock rod 431, a lock rod spring 440 is arranged between the convex ring 4311 and the holder partition plate 230, and the lock rod spring 440 is used for pushing the lock rod 431 to move towards the locking hole 122 all the time;
when the limiting electromagnet 430 is electrified, the locking rod 431 can be driven to move in the axial direction, and the guide inclined surface 123 is inclined downwards from the open end of the guide groove 121 to the locking hole 122. Due to the design, when the fixed clamping plate 120 is assembled with the holder clamping groove 211, the lock rod 431 gradually enters the holder inner cavity 214 through the compression of the guide inclined plane 123 until the lock rod 431 is opposite to the locking hole 122, and the lock rod is assembled into the locking hole 122 under the action of the lock rod spring, so that the holder shell 210 is prevented from being separated from the fixed clamping groove 111. When the cradle head housing needs to be detached, only the locking electromagnet 430 needs to be electrified, so that the locking rod 431 overcomes the elastic force of the locking rod spring 440 to move towards the direction away from the locking hole 122, and the cradle head housing 210 can be taken out of the fixed clamping groove 111 until the locking rod spring is separated from the locking hole 122. The design can prevent the cloud platform component from falling off in the use process, so that unnecessary loss is caused.
The fixed engaging groove 111 is fixed with a first conductive block 361 and a second conductive block 362 on the inner top surface of the end plate 130, the first conductive block 361 and the second conductive block 362 are electrically connected with the conducting wire 141 and the data line 142, and the holder engaging plate 212 is provided with a first conductive groove 2121 and a second conductive groove 2122 corresponding to the first conductive block 361 and the second conductive block 362 for electrically engaging with the first conductive block 361 and the second conductive block 362. During the use, first motor, second motor, first angle sensor, electro-magnet, locking lever electro-magnet access power through first conducting block 361, first conducting groove 2121 respectively, first angle sensor, angle sensor respectively through second conducting block 362, second conducting groove 2122 with signal transmission to unmanned aerial vehicle's CPU on to be convenient for unmanned aerial vehicle knows camera turned angle degree
And a location.
Referring to fig. 11, preferably, in order to avoid the situation that when the pan/tilt head assembly is not installed, the first conductive block 361 and the second conductive block 362 are still powered on to cause electric leakage and short circuit, the present invention further designs an inductive assembly, wherein the inductive assembly includes a button switch 310, one end of the button switch 310, which is provided with a trigger button 311, is installed in an inductive hole 131, an inductive partition 340 is further fixed in the inductive hole 131, one end of a trigger rod 320, which passes through the inductive partition 340, is directly opposite to the trigger button 311, the other end of the trigger rod is installed in a fixed engaging groove 111, and is provided with a driving ring 321, the trigger rod 320 is located at two sides of the inductive partition 340 and is respectively assembled and fixed with a limiting ring 350 and a spring leaf 330, the limiting ring 350 is used for limiting the distance that the trigger rod 320 moves into the fixed engaging groove 111, the spring leaf 330 is used for generating elastic deformation when the trigger rod moves towards the trigger button 311, when the pressure of the trigger bar 320 is released, the spring strip 330 can drive the trigger bar 320 to reset, i.e. restore the state of fig. 11;
the first conductive block 361 and the second conductive block 362 are respectively in conductive connection with different relay power-out ends, the power-in ends of the two relays are respectively in conductive connection with an unmanned aerial vehicle battery and an unmanned aerial vehicle CPU signal end, and the relays are in a disconnected state in an initial state;
the power inlet end of the button switch is in communication connection with the signal end of the CPU of the unmanned aerial vehicle, and the power outlet end of the button switch is in communication connection with the signal ends of the two relays; after the holder engaging plate 212 is installed in the fixing engaging groove 111, the holder engaging plate 212 needs to be pushed toward the end plate 130 until the holder engaging plate 212 drives the trigger rod 320 to move toward the trigger button 311 through the driving ring 321, and the trigger rod 320 presses the trigger button 311 to close the button switch 310, and at this time, the relay is closed, so as to supply power to the first conductive block 361 and the second conductive block 362, after the holder assembly is taken out, the trigger rod resets, the trigger button loses pressure to open the button switch, so that the button switch is opened, at this time, the two relays are opened, thereby preventing electric leakage and short circuit.
The first motor and the second motor are both stepping motors. When the camera is used, the electromagnet is directly controlled to separate the first brake disc 721 from the second brake disc 722, then the first motor is driven to be powered on, the first supporting plate is driven to rotate, and the camera 410 is driven to rotate to view;
after the second motor is powered on, the camera is driven by the synchronous belt to rotate around the first shaft body 511, so that the rotation angle of the camera 410 is adjusted in the other direction.
The invention is not described in detail, but is well known to those skilled in the art.
The foregoing detailed description of the preferred embodiments of the invention has been presented. It should be understood that numerous modifications and variations could be devised by those skilled in the art in light of the present teachings without departing from the inventive concepts. Therefore, the technical solutions available to those skilled in the art through logic analysis, reasoning and limited experiments based on the prior art according to the concept of the present invention should be within the scope of protection defined by the claims.
Claims (3)
1. The utility model provides a full-automatic reconnaissance equipment of unmanned aerial vehicle satellite, includes, the fixed plate is fixed on the unmanned aerial vehicle fuselage, characterized by: a fixed clamping groove and a fixed clamping plate are arranged on the fixed plate, one end of the clamping groove is sealed by an end plate, an induction hole is formed in the end plate, and a button switch of an induction component is arranged in the induction hole;
the fixed clamping groove is clamped and assembled with the holder clamping plate, the holder clamping plate is arranged on the holder shell, the holder clamping groove is arranged on the holder shell, and the holder clamping groove is clamped and assembled with the fixed clamping plate; the holder shell belongs to a holder assembly; the end, far away from the end plate, of the fixed clamping plate is provided with a guide groove, a locking hole and a guide inclined plane, the locking hole is clamped and assembled with one end of a locking rod, the other end of the locking rod penetrates through the holder partition plate and then is assembled with a limiting electromagnet, and the locking rod and the limiting electromagnet both belong to limiting components;
the holder assembly also comprises a matching shell, a matching inner cavity is arranged in the matching shell, and a matching partition plate is fixed in the matching inner cavity; a second motor is arranged in the matching inner cavity, and an output shaft of the second motor is fixedly connected with the third shaft body;
the third shaft body penetrates through the matching partition plate, the matching shell, the rotating block and the holder shell and then is installed in the holder inner cavity, one end of the third shaft body installed in the holder inner cavity is fixedly assembled with the second brake disc, the rotating block is fixed on the first supporting plate, and the third shaft body and the rotating block are fixedly assembled;
the bottom of the first supporting plate is provided with a notch, an adjusting block is arranged in the notch, a camera is arranged on the adjusting block, the first shaft body penetrates through one side of the first supporting plate, the notch and the adjusting block and then is rotatably assembled with the other side of the first supporting plate, and the first shaft body and the adjusting block are assembled and fixed;
one end of the first shaft body extends out of the first supporting plate and is fixedly assembled with the first belt pulley, the first belt pulley is connected with the first auxiliary belt pulley through a synchronous belt and forms a belt transmission mechanism, the first auxiliary belt pulley is fixed on the first auxiliary shaft body, a helical gear a is further fixed on the first auxiliary shaft body, and one end of the first auxiliary shaft body is assembled with the first motor;
the bevel gear a is in meshing transmission with the auxiliary bevel gear a, the auxiliary bevel gear a is fixedly assembled with one end of the second shaft body, and the other end of the second shaft body is fixedly connected with an input shaft of the angle sensor;
the third shaft body is fixedly provided with a bevel gear b, the bevel gear b is in meshing transmission with the auxiliary bevel gear b, the auxiliary bevel gear b is fixedly assembled with one end of the fourth shaft body, and the other end of the fourth shaft body penetrates through the holder partition plate and then is fixedly connected with an input shaft of the angle sensor; the cradle head vertical plate and the cradle head partition plate are fixed in the inner cavity of the cradle head;
a first conductive block and a second conductive block are respectively fixed on the top surface of the inner side of the fixed clamping groove close to the end plate, the first conductive block and the second conductive block are respectively in conductive connection with a lead and a data line, and a first conductive groove and a second conductive groove which are in conductive clamping connection with the first conductive block and the second conductive block are respectively arranged at the positions of the holder clamping plate corresponding to the first conductive block and the second conductive block;
the induction assembly comprises a button switch, one end of the button switch, which is provided with a trigger button, is installed in the induction hole, an induction partition plate is fixed in the induction hole, one end of a trigger rod passes through the induction partition plate and then is right opposite to the trigger button, the other end of the trigger rod is installed in a fixed clamping groove, a driving ring is arranged at the end of the trigger rod, the trigger rod is positioned at two sides of the induction partition plate and is respectively assembled and fixed with a limiting ring and a spring piece, the limiting ring is used for limiting the moving distance of the trigger rod to the fixed clamping groove, and the spring piece has elasticity;
the first conductive block and the second conductive block are respectively in conductive connection with different relay power-out ends, the power-in ends of the two relays are respectively in conductive connection with the unmanned aerial vehicle battery and the unmanned aerial vehicle CPU signal end, and the relays are in a disconnected state in an initial state; the power inlet end of the button switch is in communication connection with the signal end of the CPU of the unmanned aerial vehicle, and the power outlet end of the button switch is in communication connection with the signal ends of the two relays;
the second brake disc is tightly attached to the first brake disc, the first brake disc is fixedly assembled with one end of the telescopic shaft, the other end of the telescopic shaft penetrates through the holder vertical plate and then is assembled with the electromagnet, a brake spring is arranged between the first brake disc and the holder vertical plate, and the brake spring is used for generating thrust to the first brake disc, so that the first brake disc and the second brake disc are tightly attached to each other.
2. The full-automatic reconnaissance apparatus of unmanned aerial vehicle satellite of claim 1, characterized by: the limiting assembly also comprises a convex ring arranged on the lock rod, a lock rod spring is arranged between the convex ring and the holder partition plate, and the lock rod spring is used for pushing the lock rod to move towards the locking hole all the time; the guide inclined plane is arranged from the open end of the guide groove to the locking hole in a downward inclined mode.
3. The full-automatic reconnaissance apparatus of unmanned aerial vehicle satellite of claim 1, characterized by: the first motor and the second motor are both stepping motors.
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910128073 | 2019-02-21 | ||
| CN2019101280731 | 2019-02-21 |
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| Publication Number | Publication Date |
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| CN111017242A CN111017242A (en) | 2020-04-17 |
| CN111017242B true CN111017242B (en) | 2021-08-20 |
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| Application Number | Title | Priority Date | Filing Date |
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| CN201911394453.6A Active CN111017242B (en) | 2019-02-21 | 2019-12-30 | Unmanned aerial vehicle satellite full-automatic reconnaissance equipment |
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| US20180022455A1 (en) * | 2016-07-20 | 2018-01-25 | Dustin McCaslin | Dropping mechanism with universal mounting points |
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| CN205861051U (en) * | 2016-07-21 | 2017-01-04 | 许昌学院 | A kind of aviation three-dimensional geographic information harvester |
| CN107572001A (en) * | 2017-09-29 | 2018-01-12 | 成都鑫晨航空科技有限公司 | A kind of Quick Release unmanned plane task platform interface and unmanned plane |
| CN207450284U (en) * | 2017-10-16 | 2018-06-05 | 歌尔科技有限公司 | Holder fixing device and the unmanned plane including the device |
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Also Published As
| Publication number | Publication date |
|---|---|
| CN111017242A (en) | 2020-04-17 |
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