CN220891685U - Low-altitude airspace aircraft monitoring device - Google Patents
Low-altitude airspace aircraft monitoring device Download PDFInfo
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- CN220891685U CN220891685U CN202322536469.4U CN202322536469U CN220891685U CN 220891685 U CN220891685 U CN 220891685U CN 202322536469 U CN202322536469 U CN 202322536469U CN 220891685 U CN220891685 U CN 220891685U
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- 238000012806 monitoring device Methods 0.000 title claims abstract description 39
- 238000001514 detection method Methods 0.000 claims abstract description 17
- 238000012544 monitoring process Methods 0.000 abstract description 53
- 230000003287 optical effect Effects 0.000 description 4
- 238000007781 pre-processing Methods 0.000 description 4
- 238000011161 development Methods 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- 238000013459 approach Methods 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000006243 chemical reaction Methods 0.000 description 1
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Abstract
The utility model discloses a low-altitude airspace aircraft monitoring device which comprises a base and a supporting column, wherein the supporting column is arranged at the center of the top end of the base, a supporting disc is arranged at the top end of the supporting column, a rotating box is arranged at the top end of the supporting disc, a supporting arm is movably arranged on the outer wall of the rotating box, a limiting arm is movably arranged on the outer wall of one side of the rotating box, which is far away from the supporting arm, a C-shaped arm is arranged between the supporting arm and the limiting arm, a connecting arm is arranged on the outer wall of the C-shaped arm, a monitoring controller is arranged in the connecting arm, a detection radar is arranged on the surface of the monitoring controller, and a monitor is arranged on the surface of the monitoring controller on one side of the detection radar. The utility model not only realizes convenient rotary control monitoring, but also expands the detection monitoring range of the monitoring device.
Description
Technical Field
The utility model relates to the technical field of monitoring devices, in particular to a low-altitude airspace aircraft monitoring device.
Background
The civil aviation flight height is generally more than 6000 m, the low-altitude airspace is a flight area below 1000 m, and on the national low-altitude airspace management reform seminar in 2009, related aspects propose to divide the airspace below 3000 m into 3 categories: the conference of the control airspace, the monitoring airspace and the report airspace, which determines that the airspace is truly higher than one kilometer, is to be orderly released by classification management, and along with the development of society, the opening potential of the low-altitude airspace is to drive the market economic scale of more than three trillion yuan and the rapid development golden period of the whole industry chain, but the existence of the opening is to cause the confusion of the low-altitude airspace flight, and the low-altitude airspace aircraft represented by an unmanned aircraft is not flown according to a specified route or runs into a forbidden area, so that the consequence is not considered, and the low-altitude airspace aircraft is required to be monitored.
The invention discloses a method and a device for reconnaissance and monitoring of an ultra-low altitude aircraft, as disclosed in an authorized bulletin number CN115373419B, wherein the method comprises the following steps: acquiring position information of the optical equipment and not less than 2 batches of azimuth information, pitching information and distance information of the ultra-low altitude aircraft at preset time by using preset optical acquisition equipment, initially measuring to acquire distance data of the ultra-low altitude aircraft, transmitting the position information of the optical equipment, the azimuth information of the ultra-low altitude aircraft, the pitching information and the distance data to a data acquisition terminal, acquiring the position information of the optical equipment, the azimuth information of the ultra-low altitude aircraft, the pitching information and the distance data by using the data acquisition terminal, performing coordinate conversion preprocessing and track display preprocessing to acquire acquisition terminal preprocessing information, and transmitting the acquisition terminal preprocessing information to a data fusion terminal by using an ith data acquisition terminal through preset communication equipment to fuse tracks of the ultra-low altitude aircraft;
Although the invention solves the technical problems of poor reconnaissance continuity, low precision and low monitoring stability, the invention does not solve the problems that the conventional monitoring device is unfavorable for convenient rotary control monitoring during use, is unfavorable for convenient multi-angle movement control adjustment of the monitoring device, influences the detection monitoring range of the monitoring device, influences the adjustment range of the monitoring device and greatly influences the rotation adjustment flexibility of the monitoring device.
Disclosure of utility model
The utility model aims to provide a low-altitude airspace aircraft monitoring device, which solves the problems that in the background technology, the monitoring device is inconvenient to carry out convenient rotary control monitoring, the detection monitoring range of the monitoring device is influenced, the convenient multi-angle movement control adjustment of the monitoring device is inconvenient, the adjustment range of the monitoring device is influenced, and the rotation adjustment flexibility of the monitoring device is influenced.
In order to achieve the above purpose, the present utility model provides the following technical solutions: the utility model provides a low altitude airspace aircraft monitoring device, includes base and support column, the top central point department of base installs the support column, the supporting disk is installed on the top of support column, the rotating case is installed on the top of supporting disk, movable mounting has the support arm on the outer wall of rotating case, movable mounting has the spacing arm on the outer wall of one side that the support arm was kept away from to the rotating case, and installs C type arm between support arm and the spacing arm, install the linking arm on the outer wall of C type arm, the internally mounted of linking arm has monitor controller, monitor controller's surface mounting has the detection radar, monitor controller surface mounting in one side of the detection radar has the monitor, monitor controller surface mounting in monitor below has equidistant three sound detector of group, support column internally mounted of base top has driving motor, driving motor's output installs the drive shaft, the internally mounted of supporting disk has the rotary disk, the top and the rotary disk are connected.
Preferably, the internally mounted of rotatory case has step motor, the axis of rotation is installed to step motor's output, and the axis of rotation extends to the outside of rotatory case, install the connection pad on the support arm outer wall of rotatory case one side, step motor's one end is kept away from to the axis of rotation one is connected with the connection pad, and the axis of rotation extends to the inside of support arm.
Preferably, a servo motor is installed on the outer wall of the support arm on one side of the rotating shaft, a movable shaft is installed at the output end of the servo motor, the movable shaft is connected with the C-shaped arm through the support arm, a connecting shaft is movably installed on the outer wall of the limit arm on one side of the C-shaped arm, and the connecting shaft extends to the inside of the C-shaped arm.
Preferably, a linkage shaft is movably mounted on the outer wall of the limiting arm at one side of the connecting shaft, extends to the inside of the limiting arm, and is connected with the rotating box.
Preferably, the travelling car is installed to the bottom of base, the equidistant multiunit lock bolt of surface mounting of base, and lock bolt extends to the inside of travelling car.
Preferably, a control panel is installed on the outer wall of the rotary box, and the output end of the control panel is electrically connected with the input ends of the servo motor, the driving motor and the stepping motor.
Compared with the prior art, the utility model has the beneficial effects that: the monitoring device not only realizes convenient rotary control monitoring, expands the monitoring range of the monitoring device, but also realizes convenient multi-angle movement control adjustment of the monitoring device, increases the adjusting range of the monitoring device and improves the flexibility of rotation adjustment of the monitoring device;
(1) The driving motor drives the driving shaft to rotate, the driving shaft drives the rotating disc to rotate, the rotating disc drives the supporting disc to integrally rotate, the supporting disc drives the rotating box to rotate, the rotating box drives the supporting arm to rotate, the supporting arm drives the C-shaped arm to rotate, the C-shaped arm drives the connecting arm to rotate, the connecting arm drives the monitoring controller to rotate, the monitoring controller drives the detection radar, the monitor and the sound detector to synchronously rotate, when the flying object approaches to the no-fly area, the monitor and the sound detector feed back to the monitoring controller, and the monitoring controller sends an alarm signal to the monitoring controller to withdraw the flying object, so that the monitoring device can conveniently and rotatably control and monitor, and the detection and monitoring range of the monitoring device is enlarged;
(2) The rotating shaft is driven by the stepping motor, the connecting disc is driven by the rotating shaft to rotate, the supporting arm is driven by the connecting disc to rotate, the C-shaped arm is driven by the supporting arm to rotate, the connecting arm is driven by the C-shaped arm to rotate, the monitoring controller is driven by the connecting arm to rotate, the monitoring controller drives the detection radar, the monitor and the sound detector to rotate, the position adjustment monitoring is carried out, the movable shaft is driven by the servo motor to rotate, the C-shaped arm is driven by the movable shaft to rotate and adjust, the limiting arm carries out limiting supporting rotation on the C-shaped arm through the connecting shaft, the connecting arm drives the monitoring controller to rotate and adjust the height, the monitoring controller drives the detection radar, the monitor and the sound detector to carry out height adjustment, the multi-angle movement control adjustment convenient to the monitoring device is realized, the adjustment range of the monitoring device is increased, and the rotation adjustment flexibility of the monitoring device is improved.
Drawings
FIG. 1 is a schematic three-dimensional perspective view of the present utility model;
FIG. 2 is a schematic view of a three-dimensional structure of a driving motor according to the present utility model;
FIG. 3 is a schematic view of a three-dimensional structure of a stepper motor according to the present utility model;
FIG. 4 is a schematic elevational view of the present utility model;
fig. 5 is a schematic diagram showing a sectional front view of the driving motor of the present utility model.
In the figure: 1. a base; 2. a support column; 3. a support plate; 4. a rotating box; 5. a support arm; 6. a servo motor; 7. a C-arm; 8. a connecting shaft; 9. a connecting arm; 10. a driving motor; 11. a drive shaft; 12. a rotating disc; 13. a stepping motor; 14. a rotating shaft; 15. a connecting disc; 16. detecting a radar; 17. a monitor; 18. a sound detector; 19. a locking bolt; 20. a monitor controller; 21. a movable shaft; 22. a linkage shaft; 23. a walking vehicle; 24. a control panel; 25. and a limiting arm.
Detailed Description
The technical solutions in the embodiments of the present utility model will be clearly and completely described below with reference to the accompanying drawings in the embodiments of the present utility model. All other embodiments, which can be made by those skilled in the art based on the embodiments of the utility model without making any inventive effort, are intended to be within the scope of the utility model.
Referring to fig. 1-5, an embodiment of the present utility model is provided: the low-altitude airspace aircraft monitoring device comprises a base 1 and a support column 2, wherein the support column 2 is arranged at the center position of the top end of the base 1, a support disc 3 is arranged at the top end of the support column 2, a rotary box 4 is arranged at the top end of the support disc 3, a support arm 5 is movably arranged on the outer wall of the rotary box 4, a limit arm 25 is movably arranged on the outer wall of one side of the rotary box 4, which is far away from the support arm 5, a C-shaped arm 7 is arranged between the support arm 5 and the limit arm 25, a connecting arm 9 is arranged on the outer wall of the C-shaped arm 7, a monitoring controller 20 is arranged in the connecting arm 9, a detection radar 16 is arranged on the surface of the monitoring controller 20, three groups of sound detectors 18 are arranged on the surface of one side of the detection radar 16 at equal intervals, a driving motor 10 is arranged in the support column 2 above the base 1, the driving motor 10 plays a role in power output, a driving shaft 11 is arranged at the output end of the driving motor 10, a rotating disc 12 is arranged in the support disc 3, and the top end of the driving shaft 11 is connected with the rotating disc 12;
When the aircraft is used, the external power supply is firstly used for opening the driving motor 10 through the operation control panel 24, under the support of the base 1, the driving motor 10 drives the driving shaft 11 to rotate, the driving shaft 11 drives the rotating disk 12 to rotate, the rotating disk 12 drives the supporting disk 3 to integrally rotate, the supporting disk 3 drives the rotating box 4 to rotate, the rotating box 4 drives the supporting arm 5 to rotate, the supporting arm 5 drives the C-shaped arm 7 to drive the connecting arm 9 to rotate, the connecting arm 9 drives the monitoring controller 20 to rotate, the monitoring controller 20 drives the detecting radar 16, the monitor 17 and the sound detector 18 to synchronously rotate, the monitoring controller 20 is a similar device of the wide-area radar microwave detector DTAM D, the detecting radar 16 is a similar civil device of 346 radar, the monitor 17 is a high-definition camera of the ocean-vision ECU-3XXX, the sound detector 18 is an NA-39A sound detection system, the detecting radar 16, the monitor 17 and the sound detector 18 receive signals from Beidou satellites, the signals are connected with terminal equipment, the detecting radar 16 detects low-altitude flight targets, the obtained by the detecting radar 16 detect the low-altitude targets, the detected targets are fed back to the detecting targets by the detecting controller 20, and the detecting targets are fed back to the detecting device by the detecting controller 17, and the detecting targets are fed back to the detecting device by the detecting device when the detecting device is in a flight region 20, and the flying region is conveniently controlled by the flying region 20, the flying region is controlled by the flying device, and the flying region is convenient to realize;
The inside of the rotary box 4 is provided with a stepping motor 13, the stepping motor 13 plays a role in power output, the output end of the stepping motor 13 is provided with a rotating shaft 14, the rotating shaft 14 extends to the outside of the rotary box 4, the outer wall of a supporting arm 5 at one side of the rotary box 4 is provided with a connecting disc 15, one end of the rotating shaft 14, which is far away from the stepping motor 13, is connected with the connecting disc 15, the rotating shaft 14 extends to the inside of the supporting arm 5, the outer wall of the supporting arm 5 at one side of the rotating shaft 14 is provided with a servo motor 6, and the servo motor 6 plays a role in power output;
The output end of the servo motor 6 is provided with a movable shaft 21, the movable shaft 21 is connected with the C-shaped arm 7 through a supporting arm 5, a connecting shaft 8 is movably arranged on the outer wall of a limiting arm 25 on one side of the C-shaped arm 7, the connecting shaft 8 extends into the C-shaped arm 7, a linkage shaft 22 is movably arranged on the outer wall of the limiting arm 25 on one side of the connecting shaft 8, the linkage shaft 22 extends into the limiting arm 25, the linkage shaft 22 is connected with a rotating box 4, a travelling carriage 23 is arranged at the bottom end of the base 1, a plurality of groups of equally-spaced locking bolts 19 are arranged on the surface of the base 1, the locking bolts 19 extend into the travelling carriage 23, a control panel 24 is arranged on the outer wall of the rotating box 4, and the output end of the control panel 24 is electrically connected with the servo motor 6, the driving motor 10 and the input end of the stepping motor 13;
When the walking device is used, the stepping motor 13 is opened through the operation control panel 24, the rotating shaft 14 is driven by the stepping motor 13, the connecting disc 15 is driven by the rotating shaft 14 to rotate, the supporting arm 5 is driven by the connecting disc 15 to rotate, the C-shaped arm 7 is driven by the supporting arm 5 to rotate under the limiting support of the limiting arm 25, the supporting arm 5 is limited and supported by the linkage shaft 22, the connecting arm 9 is driven by the C-shaped arm 7 to rotate, the monitoring controller 20 is driven by the connecting arm 9 to rotate, the monitoring controller 20 is driven by the monitoring controller 20 to rotate, the position adjustment monitoring is carried out, meanwhile, the servo motor 6 is driven by the operation control panel 24 to rotate under the support of the supporting arm 5, the C-shaped arm 7 is driven by the servo motor 6 to rotate and adjust through the movable shaft 21, the C-shaped arm 7 is driven by the connecting shaft 8 to rotate and the C-shaped arm 7, the connecting arm 9 is driven by the connecting arm 9 to rotate and adjust the height, the monitoring controller 20 is driven by the monitoring controller 20 to rotate, the monitoring controller 20 to rotate the monitoring radar 16, the monitoring controller 17 and the sound detector 18 are driven by the monitoring controller 20 to rotate the height adjustment, the monitoring device is driven by the monitoring controller to rotate the monitoring controller, the monitoring device is driven by the monitoring controller to move in a multi-angle adjustment device, and the walking device can move conveniently.
Working principle: when in use, the driving motor 10 is firstly turned on by operating the control panel 24, under the support of the base 1, the driving motor 10 drives the driving shaft 11 to rotate, the driving shaft 11 drives the rotating disk 12 to rotate, the rotating disk 12 drives the supporting disk 3 to integrally rotate, the supporting disk 3 drives the rotating box 4 to rotate, the rotating box 4 drives the supporting arm 5 to rotate, the supporting arm 5 drives the C-shaped arm 7 to rotate, the C-shaped arm 7 drives the connecting arm 9 to rotate, the connecting arm 9 drives the monitoring controller 20 to rotate, the monitoring controller 20 drives the detecting radar 16, the monitor 17 and the sound detector 18 to synchronously rotate, the monitoring controller 20 sends out alarm signals to the detecting radar, so that a flying target is evacuated, then the stepping motor 13 is turned on by operating the control panel 24, the rotating shaft 14 is driven by the stepping motor 13, the connecting disk 15 is driven by the rotating shaft 14 to rotate, the support arm 5 is driven to rotate by the connecting disc 15, the C-shaped arm 7 is driven to rotate by the support arm 5 under the limit support of the limit arm 25, the limit arm 25 carries out limit support on the support arm 5 through the linkage shaft 22, the connecting arm 9 is driven to rotate by the C-shaped arm 7, the monitoring controller 20 is driven to rotate by the connecting arm 9, the monitoring controller 20 drives the detection radar 16, the monitor 17 and the sound detector 18 to rotate so as to carry out position adjustment monitoring, the servo motor 6 is opened by the operation control panel 24, the movable shaft 21 is driven to rotate by the servo motor 6 under the support of the support arm 5, the C-shaped arm 7 is driven to rotate and adjust by the movable shaft 21, the C-shaped arm 7 is limited and supported by the limit arm 25 through the connecting shaft 8, the C-shaped arm 7 drives the connecting arm 9 to rotate and adjust the height, the monitoring controller 20 is driven by the connecting arm 9 to rotate and adjust the height, the monitoring controller 20 drives the detecting radar 16, the monitor 17 and the sound detector 18 to adjust the height so as to carry out height adjustment monitoring, and meanwhile, the traveling vehicle 23 can be pushed to drive the monitoring device to carry out traveling monitoring so as to complete the use work of the monitoring device.
Claims (6)
1. The utility model provides a low altitude airspace aircraft monitoring device, includes base (1) and support column (2), its characterized in that: support column (2) are installed in top central point department of base (1), supporting disk (3) are installed on the top of support column (2), rotatory case (4) are installed on the top of supporting disk (3), movable mounting has support arm (5) on the outer wall of rotatory case (4), movable mounting has spacing arm (25) on the outer wall of one side that rotatory case (4) kept away from support arm (5), and installs C type arm (7) between support arm (5) and spacing arm (25), install linking arm (9) on the outer wall of C type arm (7), internally mounted of linking arm (9) has monitor controller (20), monitor controller (20) surface mounting has detection radar (16), monitor controller (20) surface mounting of detection radar (16) one side has monitor (17), monitor controller (20) surface mounting of monitor (17) below has equidistant three sound detector (18) of group, support column (2) internally mounted motor (10) above base (1) have, drive disk (10) have drive shaft (11) internally mounted, drive disk (11) are installed, the top end of the driving shaft (11) is connected with the rotating disc (12).
2. A low altitude airspace aircraft monitoring device in accordance with claim 1, wherein: the internally mounted of rotatory case (4) has step motor (13), axis of rotation (14) are installed to step motor (13) output, and axis of rotation (14) extend to the outside of rotatory case (4), install connection pad (15) on support arm (5) outer wall of rotatory case (4) one side, the one end that step motor (13) was kept away from to axis of rotation (14) is connected with connection pad (15), and axis of rotation (14) extend to the inside of support arm (5).
3. A low altitude airspace aircraft monitoring device in accordance with claim 2, wherein: install servo motor (6) on support arm (5) outer wall on axis of rotation (14) one side, movable shaft (21) are installed to the output of servo motor (6), and movable shaft (21) are connected with C type arm (7) through support arm (5), movable mounting has connecting axle (8) on spacing arm (25) outer wall on C type arm (7) one side, and connecting axle (8) extend to the inside of C type arm (7).
4. A low altitude airspace aircraft monitoring device according to claim 3, in which: the outer wall of a limiting arm (25) at one side of the connecting shaft (8) is movably provided with a linkage shaft (22), the linkage shaft (22) extends to the inside of the limiting arm (25), and the linkage shaft (22) is connected with the rotating box (4).
5. A low altitude airspace aircraft monitoring device in accordance with claim 1, wherein: the walking vehicle (23) is installed at the bottom of base (1), equidistant multiunit locking bolt (19) are installed to the surface mounting of base (1), and locking bolt (19) extend to the inside of walking vehicle (23).
6. A low altitude airspace aircraft monitoring device in accordance with claim 1, wherein: the outer wall of the rotary box (4) is provided with a control panel (24), and the output end of the control panel (24) is electrically connected with the input ends of the servo motor (6), the driving motor (10) and the stepping motor (13).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202322536469.4U CN220891685U (en) | 2023-09-19 | 2023-09-19 | Low-altitude airspace aircraft monitoring device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202322536469.4U CN220891685U (en) | 2023-09-19 | 2023-09-19 | Low-altitude airspace aircraft monitoring device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN220891685U true CN220891685U (en) | 2024-05-03 |
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ID=90836729
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202322536469.4U Active CN220891685U (en) | 2023-09-19 | 2023-09-19 | Low-altitude airspace aircraft monitoring device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN220891685U (en) |
-
2023
- 2023-09-19 CN CN202322536469.4U patent/CN220891685U/en active Active
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