CN218806546U - Unmanned aerial vehicle counter-braking equipment integrating search and counter-braking - Google Patents
Unmanned aerial vehicle counter-braking equipment integrating search and counter-braking Download PDFInfo
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- CN218806546U CN218806546U CN202223041398.2U CN202223041398U CN218806546U CN 218806546 U CN218806546 U CN 218806546U CN 202223041398 U CN202223041398 U CN 202223041398U CN 218806546 U CN218806546 U CN 218806546U
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Abstract
The utility model relates to an unmanned air vehicle technique field, concretely relates to search and unmanned aerial vehicle of anti-system integration equipment of making a reaction, its technical scheme is: including unmanned aerial vehicle body, search against the mechanism and the stabilizer blade of symmetry fixed mounting on unmanned aerial vehicle body bottom both sides, still include rotary mechanism, the fixed mounting of fixed mounting on unmanned aerial vehicle body bottom center and be used for adjusting the adjustment mechanism of angle in the vertical direction of search against the mechanism on the rotary mechanism bottom, the beneficial effects of the utility model are that: can realize adjusting the ascending angle of search anti-mechanism in horizontal direction and vertical side of the last search anti-mechanism of unmanned aerial vehicle, the flexibility is high, and the regulative mode is simple, need not to adjust unmanned aerial vehicle's flight gesture and can adjust the last search anti-mechanism angle of unmanned aerial vehicle, very big has made things convenient for the staff to use the last search anti-mechanism of unmanned aerial vehicle to search for and strike the anti-mechanism of unmanned aerial vehicle of breaking into.
Description
Technical Field
The utility model relates to an unmanned air vehicle technique field, concretely relates to search and unmanned aerial vehicle of anti-system integration equipment of making a reaction.
Background
Along with the rapid development of unmanned aerial vehicle trade, unmanned aerial vehicle has brought very big facility in fields such as short video shooting, commodity circulation transportation, agriculture by extensive application, for the life of ordinary people, but unmanned aerial vehicle floods, uses unmanned aerial vehicle probably to cause the problem in some no-fly areas, consequently need use the unmanned aerial vehicle that has search and counter-measure function to search for the unmanned aerial vehicle of breaking into and strike the counter-measure.
Unmanned aerial vehicle that has search and counter-measure function at present generally comprises unmanned aerial vehicle and search counter-measure mechanism, with unmanned aerial vehicle and the integrated design of search counter-measure mechanism, but current search counter-measure mechanism generally is fixed mounting on unmanned aerial vehicle's bottom, can't adjust the angle of search counter-measure mechanism, when searching for and counter-measure the unmanned aerial vehicle of rushing into, subaerial staff needs to adjust unmanned aerial vehicle's flight gesture many times, thereby realize that the angle of adjustment search counter-measure mechanism searches for and strikes the counter-measure to the unmanned aerial vehicle of rushing into, unmanned aerial vehicle's flight gesture adjustment is comparatively troublesome, the staff of being inconvenient in uses the unmanned aerial vehicle that has search and counter-measure function to search for and strike the counter-measure the unmanned aerial vehicle of rushing into.
Therefore, the invention is necessary to provide unmanned aerial vehicle counter-braking equipment integrating search and counter-braking.
SUMMERY OF THE UTILITY MODEL
Therefore, the utility model provides an unmanned aerial vehicle of integration is turned over to search and counter-system equipment, can realize adjusting the angle of unmanned ascending search counter-system mechanism on vertical direction and horizontal direction through rotary mechanism and adjustment mechanism, the flexibility is high, the adjustment is simple, the staff of being convenient for searches for and strikes the counter-system to the unmanned aerial vehicle of rushing into, generally fix on unmanned aerial vehicle with solving current search counter-system mechanism, when searching for and strike the counter-system to the unmanned aerial vehicle of rushing into, the staff need continuous adjustment unmanned aerial vehicle's flight gesture is with the angle of adjustment search counter-system mechanism, unmanned aerial vehicle flight gesture adjustment is troublesome, the staff of being not convenient for uses the unmanned aerial vehicle that has search and counter-system function to search for and strike the problem of counter-system to the unmanned aerial vehicle of rushing into.
In order to achieve the above object, the present invention provides the following technical solutions: a search and reaction integrated unmanned aerial vehicle reaction device comprises an unmanned aerial vehicle body, a search reaction mechanism, support legs symmetrically and fixedly arranged on two sides of the bottom end of the unmanned aerial vehicle body, a rotating mechanism fixedly arranged on the center of the bottom end of the unmanned aerial vehicle body, and an adjusting mechanism fixedly arranged on the bottom end of the rotating mechanism and used for adjusting the angle of the search reaction mechanism in the vertical direction;
the searching and countering mechanism is fixedly arranged at the bottom end of the adjusting mechanism.
Preferably, search anti-mechanism includes casing and signal transceiver, fixed mounting has infrared transceiver, laser emitter, camera and radar in the bottom of casing, the camera sets up on casing bottom center, infrared transceiver and laser emitter set up on bottom one side of casing, the radar sets up on one side that infrared transceiver was kept away from to the casing, casing upper portion fixed mounting has battery and stabilizer blade, signal transceiver sets up in one side that the casing is close to the radar, the battery sets up in one side that the casing is close to infrared transceiver, the well lower part fixed mounting of casing has the controller, one side bottom fixed mounting that the casing is close to signal transceiver has the interface that charges.
Preferably, the top end fixed mounting of casing is on adjustment mechanism's bottom, battery and the interface and the controller electric connection that charge, controller and camera, radar, infrared transceiver, laser emitter, adjustment mechanism and rotary mechanism electric connection, infrared transceiver and laser emitter electric connection.
Preferably, the adjusting mechanism comprises a square plate, a second concave plate is fixedly mounted at the bottom end of one side of the square plate, a connecting plate is rotatably mounted on the second concave plate through a rotating shaft, a driving assembly is arranged in the square plate, a push-pull plate is rotatably connected to the bottom end of the driving assembly, and a first concave plate is rotatably mounted at the bottom end of the push-pull plate through a rotating shaft.
Preferably, the top center of the square plate is fixedly mounted at the bottom end of the rotating mechanism, the bottom end of the connecting plate is fixedly mounted at one side of the top end of the shell, and the bottom end of the first concave plate is fixedly mounted at one side, far away from the connecting plate, of the top of the shell.
Preferably, the driving assembly comprises a screw rod, the screw rod is rotatably installed in one side of the middle of the square plate, the screw rod is connected with a concave sliding plate through threads arranged on the surface, sliding rods are symmetrically arranged on two sides of the concave sliding plate in a sliding mode, the sliding rods are two groups of sliding rods and fixedly installed in the square plate, and one end, far away from the second concave plate, of the screw rod is fixedly connected with a first stepping motor.
Preferably, the housing of the first stepping motor is fixedly mounted on one side, away from the second concave plate, of the square plate, the output shaft of the first stepping motor is fixedly connected with one end, away from the second concave plate, of the lead screw, the first stepping motor is electrically connected with the controller, and the bottom end of the concave sliding plate is rotatably connected with the top end of the push-pull plate through the rotating shaft.
Preferably, rotary mechanism includes a ring section of thick bamboo, circular slab and second step motor, circular slab fixed mounting is on the bottom center of unmanned aerial vehicle body, the casing fixed mounting of second step motor is on circular slab top center, and second step motor and controller electric connection, the output shaft of second step motor rotates and installs on the center of circular slab, the bottom fixed mounting of second step motor output shaft is on square slab top center, the middle part of circular slab is provided with the annular groove, a ring section of thick bamboo fixed mounting is on the top of square slab, the top of a ring section of thick bamboo slides and sets up in the annular groove.
The utility model has the advantages that: the angle of the search anti-braking mechanism on the unmanned aerial vehicle can be adjusted in the horizontal direction and the vertical direction through the rotating mechanism and the adjusting mechanism, the flexibility is high, the adjusting mode is simple, the angle of the search anti-braking mechanism on the unmanned aerial vehicle can be adjusted without adjusting the flight attitude of the unmanned aerial vehicle, and the unmanned aerial vehicle which is rushed into is greatly searched and beaten by the search anti-braking mechanism on the unmanned aerial vehicle by workers.
Drawings
Fig. 1 is a front view of a reverse braking device of an unmanned aerial vehicle provided by the present invention;
FIG. 2 is a structural diagram of an adjusting mechanism provided by the present invention;
fig. 3 is a structural view of a rotating mechanism provided by the present invention;
FIG. 4 is a structural diagram of a search reaction mechanism provided by the present invention;
in the figure: the unmanned aerial vehicle comprises a unmanned aerial vehicle body, a shell, a camera, a signal transceiver, a charging interface, a radar, an infrared transceiver, a laser transmitter, a controller, a first concave plate, a push-pull plate, a concave sliding plate, a connecting plate, a second concave plate, a lead screw, a sliding rod, a first step motor, a square plate, a circular cylinder, a circular plate, a second step motor, a 22 circular groove, a 23 storage battery and a 24 support foot, wherein the unmanned aerial vehicle body comprises the following components 1, 2 shell, 3 camera, 4 signal transceiver, 5 charging interface, 6 radar, 7 infrared transceiver, 8 laser transmitter, 9 controller, 10 first concave plate, 11 push-pull plate, 12 concave sliding plate, 13 connecting plate, 14 second concave plate, 15 lead screw, 16 sliding rod, 17 first step motor, 18 square plate, 19 circular cylinder, 20 circular plate, 21 second step motor, 22 circular groove, 23 storage battery and 24 support foot.
Detailed Description
The preferred embodiments of the present invention will be described hereinafter with reference to the accompanying drawings, and it should be understood that the preferred embodiments described herein are merely for purposes of illustration and explanation, and are not intended to limit the present invention.
Referring to the accompanying drawings 1-4, the utility model provides a pair of search and anti-system integrated unmanned aerial vehicle system of turning over, including unmanned aerial vehicle body 1, search anti-system mechanism and symmetry fixed mounting stabilizer blade 24 on 1 bottom both sides of unmanned aerial vehicle body, still include fixed mounting at the central rotary mechanism of 1 bottom of unmanned aerial vehicle body, fixed mounting is used for adjusting the adjustment mechanism who searches for the angle in the vertical direction of anti-system mechanism on the rotary mechanism bottom, and search anti-system mechanism fixed mounting is on adjustment mechanism's bottom.
The search anti-braking mechanism comprises a shell 2 and a signal transceiver 4, an infrared transceiver 7, a laser transmitter 8, a camera 3 and a radar 6 are fixedly installed in the bottom end of the shell 2, the camera 3 is arranged on the center of the bottom end of the shell 2, the infrared transceiver 7 and the laser transmitter 8 are arranged on one side of the bottom end of the shell 2, the radar 6 is arranged on one side of the shell 2 away from the infrared transceiver 7, a storage battery 23 and a support leg 24 are fixedly installed on the upper portion of the shell 2, the signal transceiver 4 is arranged in one side of the shell 2 close to the radar 6, the storage battery 23 is arranged in one side of the shell 2 close to the infrared transceiver 7, a controller 9 is fixedly installed on the middle lower portion of the shell 2, a charging interface 5 is fixedly installed in the bottom end of the shell 2 close to the signal transceiver 4, the top end of the shell 2 is fixedly installed on the bottom end of the adjusting mechanism, and the storage battery 23 is electrically connected with the charging interface 5 and the controller 9, the controller 9 is electrically connected with the camera 3, the radar 6, the infrared transceiver 7, the laser transmitter 8, the adjusting mechanism and the rotating mechanism, the storage battery 23 supplies power to the controller 9, the camera 3, the signal transceiver 4, the radar 6, the infrared transceiver 7, the laser transmitter 8, the adjusting mechanism and the rotating mechanism are supplied with power through the controller 9, the infrared transceiver 7 is electrically connected with the laser transmitter 8, in the process of searching for the countermeasures, the camera 3 can shoot a picture below to search for a target and send the shot picture to the controller 9, the controller 9 sends the shot picture to ground workers through the signal transceiver 4, when the target unmanned aerial vehicle is searched, the radar 6 can detect the distance between the target unmanned aerial vehicle and the unmanned aerial vehicle body 1 and send distance information to the controller 9, the controller 9 sends the distance information to ground workers through the signal transceiver 4, the infrared transceiver 7 can identify a moving target, and the laser transmitter 8 is controlled to transmit laser to strike a target unmanned aerial vehicle, so that striking and countering of the intruding unmanned aerial vehicle are achieved.
The adjusting mechanism comprises a square plate 18, a second concave plate 14 is fixedly arranged at the bottom end of one side of the square plate 18, a connecting plate 13 is rotatably arranged on the second concave plate 14 through a rotating shaft, a driving assembly is arranged in the square plate 18, a push-pull plate 11 is rotatably connected at the bottom end of the driving assembly, the driving assembly can drive the top end of the push-pull plate 11 to move in the horizontal direction, a first concave plate 10 is rotatably arranged at the bottom end of the push-pull plate 11 through the rotating shaft, the top center of the square plate 18 is fixedly arranged at the bottom end of a rotating mechanism, the bottom end of the connecting plate 13 is fixedly arranged at one side of the top end of the shell 2, the shell 2 can rotate around the top end of the connecting plate 13 in the vertical direction, the bottom end of the first concave plate 10 is fixedly installed on one side, far away from the connecting plate 13, of the top of the shell 2, the driving assembly comprises a lead screw 15, the lead screw 15 is rotatably installed in one side of the middle of the square plate 18, a concave sliding plate 12 is connected to a thread arranged on the surface of the lead screw 15, the lead screw 15 is rotatably connected with the concave sliding plate 12 through a thread, the concave sliding plate 12 can drive the top end of the push-pull plate 11 to move in the horizontal direction, sliding rods 16 are symmetrically arranged on two sides of the concave sliding plate 12 in a sliding mode, and the two groups of sliding rods 16 are fixedly installed in the square plate 18, the concave sliding plate 12 is limited by two groups of sliding rods 16, one end of the screw rod 15 far away from the second concave plate 14 is fixedly connected with a first stepping motor 17, a shell of the first stepping motor 17 is fixedly arranged on one side of the square plate 18 far away from the second concave plate 14, an output shaft of the first stepping motor 17 is fixedly connected with one end of the screw rod 15 far away from the second concave plate 14, the first stepping motor 17 is electrically connected with the controller 9, the controller 9 controls the on/off of the first stepping motor 17 and the rotation direction of the output shaft of the first stepping motor 17, and the bottom end of the concave sliding plate 12 is rotatably connected with the top end of the push-pull plate 11 through a rotating shaft.
Rotary mechanism includes annular cylinder 19, circular slab 20 and second step motor 21, circular slab 20 fixed mounting is on the bottom center of unmanned aerial vehicle body 1, the casing fixed mounting of second step motor 21 is on the center of circular slab 20 top, and second step motor 21 and controller 9 electric connection, open and close and the opening and close of second step motor 21 output shaft through controller 9 control second step motor 21, the output shaft of second step motor 21 rotates and installs on the center of circular slab 20, the bottom fixed mounting of second step motor 21 output shaft is on the center of square slab 18 top, second step motor 21 work can drive square slab 18 and rotate in the horizontal direction, thereby make casing 2 rotate in the horizontal direction, the middle part of circular slab 20 is provided with annular groove 22, annular cylinder 19 fixed mounting is on the top of square slab 18, the top of annular cylinder 19 slides and sets up in annular groove 22, the annular cylinder 19 that sets up can make square slab 18 and casing 2 the stability of rotating in the horizontal direction better.
The utility model discloses a use as follows: when the unmanned aerial vehicle is used, a worker on the ground remotely controls the unmanned aerial vehicle body 1 to fly, in the flying process, the storage battery 23 supplies power to the controller 9, the controller 9 supplies power to the camera 3, the signal transceiver 4, the radar 6, the infrared transceiver 7, the laser transmitter 8, the first stepping motor 17 and the second stepping motor 21, when the angle of the shell 2 in the vertical direction needs to be adjusted, the worker on the ground sends an instruction to the signal transceiver 4, the signal transceiver 4 sends the instruction information to the controller 9, the controller 9 starts the first stepping motor 17, the first stepping motor 17 works to drive the lead screw 15 to rotate, the lead screw 15 rotates to be in threaded connection with the concave sliding plate 12, namely, the concave sliding plate 12 moves in the horizontal direction, the concave sliding plate 12 moves to drive the top end of the push-pull plate 11 to move in the horizontal direction, thereby make casing 2 rotate in the vertical direction around the top of connecting plate 13, thereby realize adjusting casing 2 angle in the vertical direction, when needs adjustment casing 2 angle in the horizontal direction, ground staff sends the instruction to signal transceiver 4, signal transceiver 4 sends instruction information to controller 9, controller 9 starts second step motor 21, second step motor 21 works and makes the output shaft of second step motor 21 rotate, the output shaft of second step motor 21 rotates and drives square plate 18 and casing 2 and rotate, thereby realize that casing 2 rotates in the horizontal direction, can realize adjusting the angle of search anti-braking mechanism on unmanned aerial vehicle in horizontal direction and vertical direction, the flexibility is high, the control mode is simple, make search anti-braking mechanism on unmanned aerial vehicle can strike anti-braking with more accurate search target, in the process of search anti-braking, the picture that camera 3 can shoot the below is searched the target, and send the picture of shooing for controller 9, the picture that controller 9 will shoot through signal transceiver 4 is sent for ground staff, when searching target unmanned aerial vehicle, distance between 6 detectable target unmanned aerial vehicle of radar and the unmanned aerial vehicle body 1, and send distance information for controller 9, controller 9 sends distance information for ground staff through signal transceiver 4, infrared transceiver 7 can discern the moving target, and control laser emitter 8 strikes target unmanned aerial vehicle to the transmission laser, thereby realize striking the counter-system to the unmanned aerial vehicle of rushing into.
The above description is only a preferred embodiment of the present invention, and any person skilled in the art may modify the present invention or modify it into an equivalent technical solution by using the technical solutions described above. Therefore, any simple modifications or equivalent replacements made according to the technical solution of the present invention belong to the scope of the claimed invention as far as possible.
Claims (8)
1. The utility model provides a search and unmanned aerial vehicle of anti-system integration equipment of turning over, includes unmanned aerial vehicle body (1), search anti-system mechanism and symmetry fixed mounting stabilizer blade (24) on unmanned aerial vehicle body (1) bottom both sides, its characterized in that: the unmanned aerial vehicle further comprises a rotating mechanism fixedly mounted on the center of the bottom end of the unmanned aerial vehicle body (1), and an adjusting mechanism fixedly mounted on the bottom end of the rotating mechanism and used for adjusting the angle of the search and reverse mechanism in the vertical direction;
the searching and countering mechanism is fixedly arranged at the bottom end of the adjusting mechanism.
2. The unmanned aerial vehicle reaction device integrating search and reaction according to claim 1, wherein: search anti-mechanism includes casing (2) and signal transceiver (4), the bottom internal fixation of casing (2) installs infrared transceiver (7), laser emitter (8), camera (3) and radar (6), camera (3) set up on casing (2) bottom center, infrared transceiver (7) and laser emitter (8) set up on bottom one side of casing (2), radar (6) set up on one side of infrared transceiver (7) is kept away from in casing (2), casing (2) upper portion fixed mounting has battery (23) and stabilizer blade (24), signal transceiver (4) set up in one side that casing (2) are close to radar (6), battery (23) set up in one side that casing (2) are close to infrared transceiver (7), the well lower part fixed mounting of casing (2) has controller (9), casing (2) are close to one side bottom internal fixation of signal transceiver (4) and have interface (5) that charge.
3. A search and counter-control integrated drone counter-control device according to claim 2, characterized in that: the top fixed mounting of casing (2) is on adjustment mechanism's bottom, battery (23) and charge interface (5) and controller (9) electric connection, controller (9) and camera (3), radar (6), infrared transceiver (7), laser emitter (8), adjustment mechanism and rotary mechanism electric connection, infrared transceiver (7) and laser emitter (8) electric connection.
4. A search and reaction integrated drone reaction device according to claim 3, characterized in that: the adjusting mechanism comprises a square plate (18), a second concave plate (14) is fixedly mounted at the bottom end of one side of the square plate (18), a connecting plate (13) is rotatably mounted on the second concave plate (14) through a rotating shaft, a driving assembly is arranged in the square plate (18), a push-pull plate (11) is rotatably connected to the bottom end of the driving assembly, and a first concave plate (10) is rotatably mounted at the bottom end of the push-pull plate (11) through the rotating shaft.
5. A search and counter-control integrated unmanned aerial vehicle counter-control device according to claim 4, characterized in that: the top center of square plate (18) is fixed on the bottom end of rotary mechanism, the bottom end of connecting plate (13) is fixed on one side of the top end of casing (2), and the bottom end of first concave plate (10) is fixed on one side of casing (2) top far away from connecting plate (13).
6. A search and reaction integrated unmanned aerial vehicle reaction device according to claim 4, wherein: the drive assembly comprises a screw rod (15), the screw rod (15) is rotatably installed in one side of the middle of a square plate (18), the screw rod (15) is connected with a concave sliding plate (12) in a threaded mode, the two sides of the concave sliding plate (12) are symmetrically provided with sliding rods (16) in a sliding mode, the sliding rods (16) are fixedly installed in the square plate (18) in an equal mode, and the screw rod (15) is far away from a first step motor (17) fixedly connected with one end of a second concave plate (14).
7. A search and reaction integrated unmanned aerial vehicle reaction device according to claim 5, wherein: rotary mechanism includes an annular cylinder (19), circular plate (20) and second step motor (21), circular plate (20) fixed mounting is on the bottom center of unmanned aerial vehicle body (1), the casing fixed mounting of second step motor (21) is on circular plate (20) top center, and second step motor (21) and controller (9) electric connection, the output shaft of second step motor (21) rotates and installs on the center of circular plate (20), the bottom fixed mounting of second step motor (21) output shaft is on square plate (18) top center, the middle part of circular plate (20) is provided with annular groove (22), annular cylinder (19) fixed mounting is on the top of square plate (18), the top of annular cylinder (19) slides and sets up in annular groove (22).
8. The unmanned aerial vehicle reaction device integrating search and reaction according to claim 6, wherein: the shell of the first stepping motor (17) is fixedly installed on one side, away from the second concave plate (14), of the square plate (18), an output shaft of the first stepping motor (17) is fixedly connected with one end, away from the second concave plate (14), of the screw rod (15), the first stepping motor (17) is electrically connected with the controller (9), and the bottom end of the concave sliding plate (12) is rotatably connected with the top end of the push-pull plate (11) through a rotating shaft.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202223041398.2U CN218806546U (en) | 2022-11-16 | 2022-11-16 | Unmanned aerial vehicle counter-braking equipment integrating search and counter-braking |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202223041398.2U CN218806546U (en) | 2022-11-16 | 2022-11-16 | Unmanned aerial vehicle counter-braking equipment integrating search and counter-braking |
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| Publication Number | Publication Date |
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| CN218806546U true CN218806546U (en) | 2023-04-07 |
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| Application Number | Title | Priority Date | Filing Date |
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| CN202223041398.2U Active CN218806546U (en) | 2022-11-16 | 2022-11-16 | Unmanned aerial vehicle counter-braking equipment integrating search and counter-braking |
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| CN (1) | CN218806546U (en) |
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2022
- 2022-11-16 CN CN202223041398.2U patent/CN218806546U/en active Active
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