CN214041742U - Remote deployment geological disaster monitoring device with anti-swing structure - Google Patents
Remote deployment geological disaster monitoring device with anti-swing structure Download PDFInfo
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- CN214041742U CN214041742U CN202022473152.7U CN202022473152U CN214041742U CN 214041742 U CN214041742 U CN 214041742U CN 202022473152 U CN202022473152 U CN 202022473152U CN 214041742 U CN214041742 U CN 214041742U
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Abstract
The utility model relates to the technical field of geological disaster monitoring, in particular to a remote deployment geological disaster monitoring device with an anti-swing structure, which comprises a monitoring box body, a GNSS receiver and a power supply system, wherein the GNSS receiver and the power supply system are arranged in the monitoring box body and are electrically connected, the monitoring box body is provided with a GNSS satellite antenna and a solar power supply structure and can be connected with a flying platform of an unmanned aerial vehicle through the anti-swing structure capable of eliminating horizontal swing, thereby being safely and efficiently airdropped at a designated place, realizing the deployment and monitoring of the GNSS monitoring equipment under the extremely complex scene that conventional monitoring equipment and personnel can not enter the field installation and deployment and the safe monitoring deployment of the GNSS monitoring equipment under the emergency monitoring dangerous scene, and ensuring that the monitoring device can not be frequently leveled due to the shaking of the unmanned aerial vehicle in the sailing process through the designed anti-swing structure, the risk of unmanned aerial vehicle crash has been avoided.
Description
Technical Field
The utility model relates to a geological disaster monitoring technology field specifically relates to a long-range geological disaster monitoring devices that deploys with anti swing structure.
Background
The property loss caused by geological disasters in China exceeds billions of yuan every year, and the real-time observation of a disaster body, the acquisition of deformation information of the disaster body and the early warning information sending in advance are important ways for guaranteeing the life safety of personnel and reducing the property loss. In the existing monitoring technical means, earth surface (crack gauges and GNSS) and underground (deep inclinometer, soil moisture content and soil pressure gauge) monitoring equipment are adopted, and personnel are required to enter a disaster deformation area for field construction; and the real-time monitoring can not be realized by adopting the aerospace monitoring technologies such as low-altitude photogrammetry, airborne radar, satellite remote sensing and the like.
The air-drop monitoring device has a good application prospect as a novel monitoring method which can be safely deployed without personnel entering the field, but the air-drop monitoring device has a problem: because at the navigation in-process, unmanned aerial vehicle opportunity rocks, so monitoring devices can frequently make level, therefore has the risk of unmanned aerial vehicle crash.
Therefore, there is a need for an anti-swing device for an aerial delivery monitoring device.
SUMMERY OF THE UTILITY MODEL
In order to realize above purpose, the utility model provides a long-range geological disasters monitoring devices that deploys with anti swing structure solves under the extremely complicated scene monitoring facilities can not deploy the monitoring and the dangerous scene of emergent monitoring problem that monitoring facilities can not deploy the monitoring safely, and specific technical scheme is as follows:
the utility model discloses a geological disasters monitoring devices of long-range deployment is by the monitoring box to and set up in the monitoring box, electric connection's GNSS receiver and power supply system constitute, power supply system includes solar control ware and lithium cell. The solar controller is used for realizing voltage stabilization and voltage conversion functions, converting 18V solar energy into 12V direct current and storing the direct current in a lithium battery, and realizing functions of overcharge protection, overdischarge protection, load overcurrent and short circuit protection and the like; the GNSS receiver is used for receiving satellite observation data and transmitting the observation data back to the monitoring cloud platform by using the built-in integrated 4G communication module.
Be provided with anti swing structure on the monitoring box, anti swing structure can guarantee that unmanned aerial vehicle carries on monitoring devices flight in-process horizontal direction can not take place to rock to ensure that unmanned aerial vehicle can not frequently make level because of rocking, and cause it to take place to crash.
The anti-swing structure comprises a flight platform connected with the unmanned aerial vehicle, a tripod head dispenser is arranged at the center of the bottom of the flight platform, and tripod head controllers are symmetrically arranged at the bottom of the flight platform by taking the tripod head dispenser as a central line.
The monitoring box body and the top of the side face opposite to the holder controller are respectively provided with an anti-swing joint, the middle of the edge of the top face of the monitoring box body close to the anti-swing joint is respectively provided with a hanging ring, and the hanging ring is provided with a rubber ring for protecting a hanging wire from being broken.
The holder dispenser is connected with the two lifting rings on the monitoring box body through the two lifting wires respectively.
The anti-swing structure comprises a pair of support frames, and each support frame consists of an unmanned aerial vehicle undercarriage and a limiting rod through a three-way pipe arranged on the unmanned aerial vehicle undercarriage; the upper end and the cloud platform controller of unmanned aerial vehicle undercarriage are connected, the joint and the anti swing joint of gag lever post. The monitoring box body can be guaranteed not to shake in the horizontal direction in the process of sailing through the matching of the limiting rod and the anti-swing joint.
Furthermore, the monitoring box body is a hollow cube and is used for protecting the equipment main body from being damaged by impact and preventing rainwater from entering. The top of the monitoring box body is of an openable cover opening structure, the GNSS receiver, the solar controller and the lithium battery can be placed in the monitoring box body after the monitoring box body is opened, and finally the cover opening cover can be fastened on the monitoring box body through bolts.
The GNSS satellite antenna is arranged at the top of the monitoring box body and comprises an antenna supporting rod made of a stainless steel hollow circular tube, one end of the antenna supporting rod is vertically connected with the center of the top surface of the monitoring box body, and an SMA-KF male head is arranged at the other end of the antenna supporting rod; the SMA-KF male head is connected with the GNSS receiver through an antenna connecting line arranged in the antenna supporting rod. The GNSS satellite antenna adopts the helical antenna to receive satellite signals, so that the overall weight of the monitoring device is reduced to the maximum degree, and meanwhile, the helical antenna can ensure that a receiver can normally receive satellite observation data under a certain inclination angle.
Two solar supports are arranged on the top surface of the monitoring box body in a mirror image mode by taking the GNSS satellite antenna as a symmetrical position; the upper ends of the two solar brackets can be folded and connected to the butt joint circular ring on the antenna supporting rod; and the upper surfaces of the two solar supports are connected with solar films through fixing bolts. The utility model discloses a solar rack can keep balance as far as possible, and can satisfy the redundant demand of electricity generation, can be so that whether orientation of worry solar film when monitoring devices puts in faces south (for example when solar film is north and south orientation, have one side must face south, can satisfy the illumination power generation requirement, even solar film is the east and west orientation, no matter in the morning or afternoon, always have one side can just to illumination direction, generate electricity), with the maximize when satisfying long-term continuous observation absorb solar energy.
Four corners of the bottom surface of the monitoring box body are respectively provided with contact pins made of stainless steel materials, and the bottoms of the contact pins are sharpened and are used for being inserted into the ground for fixing.
Furthermore, the direction parallel to the plane where the two solar supports are located is taken as the observation direction, the clockwise direction is taken as the rotation direction, the included angle range between the right solar support and the horizontal plane is 45-60 degrees, and the large angle adjusting range can adapt to the use requirements of different latitude areas.
Furthermore, be provided with waterproof terminal box on the solar rack, the pole body of antenna bracing piece, the below position that is located the butt joint ring is provided with the wire mouth that the opening is down, the opening of wire mouth is down, can effectively prevent the rainwater and flow backward, and the opening part uses rubber seal and the electric wire that passes is fixed together in addition, can further avoid the foreign matter to get into. And the solar connecting wire on the solar film is connected with a solar controller in the monitoring box body through a waterproof junction box and a wire connecting nozzle.
Furthermore, the top surface of monitoring box is provided with 4G gain antenna, 4G gain antenna bottom is the magnetism paster, adsorbs on the monitoring box surface that has the iron material, and is connected with the GNSS receiver, and 4G gain antenna is mainly for reinforcing 4G communication network for the built-in communication module of GNSS receiver is better carries out data transmission.
Furthermore, the bottom surface of the inner cavity of the monitoring box body, corner points of the GNSS receiver, the solar controller and the lithium battery are all provided with buffer materials, namely expandable polystyrene materials EPS, so that the monitoring box body can be protected from being damaged due to impact when falling to the ground.
Further, the utility model discloses be provided with the platform of taking off, the main effect of the platform of taking off is: because the unmanned aerial vehicle frame height is limited, and in order to raise GNSS satellite antenna as far as possible to obtain the observation data that data quality is good, the height of GNSS satellite antenna is generally higher than unmanned aerial vehicle frame height, consequently uses flight platform can solve when placing in the level land, and monitoring devices can not directly settle the problem under flight platform.
Compare with current geological disasters monitoring devices, the beneficial effects of the utility model are that:
the utility model discloses can be under the extremely complicated scene that conventional monitoring facilities and personnel can't get into the field installation and deploy, realize that GNSS monitoring facilities deploys the monitoring to and the safe monitoring of deploying of GNSS monitoring facilities under the dangerous scene of emergent monitoring, and the anti swing structure through the design has guaranteed monitoring devices at the navigation in-process, can not frequently make level because of rocking of unmanned aerial vehicle, has avoided the risk of unmanned aerial vehicle crash.
Drawings
Fig. 1 is a schematic structural diagram of a first embodiment of the present invention;
fig. 2 is a cross-sectional view of a first embodiment of the present invention;
fig. 3 is a schematic connection diagram according to a first embodiment of the present invention;
fig. 4 is a schematic view of the first embodiment of the present invention;
fig. 5 is a schematic structural diagram of a second embodiment of the present invention;
fig. 6 is a sectional view of a second embodiment of the present invention;
fig. 7 is a schematic connection diagram of a second embodiment of the present invention;
fig. 8 is a schematic view of the second embodiment of the present invention;
FIG. 9 is a schematic view of the connection of the monitoring box of the present invention to the drone;
fig. 10 is a diagram of practical application of the present invention.
In the figure: the system comprises a 1-GNSS receiver, a 2-power supply system, a 21-solar controller, a 22-lithium battery, a 3-monitoring box body, a 31-GNSS satellite antenna, a 311-SMA-KF male head, a 312-antenna supporting rod, a 313-antenna connecting line, a 314-butt-joint circular ring, a 315-wire connector, a 316-solar connecting line, a 32-solar bracket, a 321-solar thin film, a 322-waterproof junction box, a 323-fixing bolt, a 324-inserting pin, a 325-hanging ring, a 326-anti-swing joint, a 327-4G gain antenna, 328-buffer materials, a 329-anti-swing clamping ring, a 4-anti-swing structure, a 41-flight platform, a 411-cloud platform dispenser, a 412-cloud platform controller, a 413-hanging line, a 414-hinge, 42-support frame, 421-unmanned aerial vehicle landing gear, 422-three-way pipe, 423-limiting rod, 424-anti-swing support and 5-takeoff platform.
Detailed Description
To further illustrate the manner in which the present invention is made and the effects obtained, the technical solutions of the present invention will be clearly and completely described below with reference to the accompanying drawings.
Example one
The first embodiment is to illustrate the structure and the materials for preparing the parts of the present invention, and the specific contents are as follows:
as shown in fig. 1-3, the utility model relates to a geological disaster monitoring device of long-range deployment is by monitoring box 3 to and set up in monitoring box 3, electric connection's GNSS receiver 1 and power supply system 2 constitute, power supply system 2 includes solar control ware 21 and lithium cell 22. The solar controller 21 is used for realizing voltage stabilization and voltage conversion functions, converting 18V solar energy into 12V direct current and storing the direct current in the lithium battery 22, and realizing functions of overcharge protection, overdischarge protection, load overcurrent and short circuit protection and the like; the GNSS receiver 1 is used for receiving satellite observation data and transmitting the observation data back to the monitoring cloud platform by using a built-in integrated 4G communication module.
Be provided with anti swing structure 4 on the monitoring box 3, anti swing structure 4 can guarantee that unmanned aerial vehicle carries on monitoring devices flight in-process horizontal direction and can not take place to rock to ensure that unmanned aerial vehicle can not frequently make level because of rocking, and cause it to take place to crash.
The anti-swing structure 4 comprises a flying platform 41 connected with the unmanned aerial vehicle, a tripod head dispenser 411 is arranged at the center of the bottom of the flying platform 41, and tripod head controllers 412 are symmetrically arranged at the bottom of the flying platform 41 by taking the tripod head dispenser 411 as a central line.
The top of the side face, opposite to the position of the holder controller 412, of the monitoring box body 3 is provided with an anti-swing joint 326, the middle of the edge of the top face of the monitoring box body 3, close to the anti-swing joint 326, is provided with a hanging ring 325, and the hanging ring 325 is provided with a rubber ring for protecting the hanging wire 413 from being broken.
The holder dispenser 411 is connected to the two hanging rings 325 on the monitoring box 3 through two hanging wires 413.
The anti-swing structure 4 comprises a pair of support frames 42, and the support frames 42 are composed of an unmanned aerial vehicle landing gear 421 through a three-way pipe 422 and a limiting rod 423 arranged thereon; the upper end and the cloud platform controller 412 of unmanned aerial vehicle undercarriage 421 are connected, the joint and the anti swing joint 326 joint of gag lever post 423. Through the cooperation of gag lever post 423 with anti swing joint 326, can guarantee that monitoring box 3 can not take place to rock at the horizontal direction in the process of navigating.
Specifically, the monitoring box body 3 is a hollow cube, and the specific size can be 180mm × 180mm × 100mm, so that the monitoring box body is used for protecting the equipment main body from being damaged by impact and preventing rainwater from entering. The top of the monitoring box body 3 is of an openable cover opening structure, the GNSS receiver 1, the solar controller 21 and the lithium battery 22 can be placed in the monitoring box body after the monitoring box body is opened, and finally the cover opening cover can be fastened on the monitoring box body 3 through bolts.
The GNSS satellite antenna 31 comprises an antenna support rod 312 made of a stainless steel hollow circular tube, one end of the antenna support rod 312 is vertically connected with the center of the top surface of the monitoring box body 3, and the other end of the antenna support rod 312 is provided with an SMA-KF male head 311; the SMA-KF male head 311 is connected with the GNSS receiver 1 through an antenna connecting line 313 arranged inside the antenna supporting rod 312. The GNSS satellite antenna 31 receives satellite signals by adopting a helical antenna, so that the overall weight of the monitoring device is reduced to the maximum, and meanwhile, the helical antenna can ensure that a receiver normally receives satellite observation data under a certain inclination angle.
Two solar supports 32 are arranged on the top surface of the monitoring box body 3 in a mirror image mode by taking the GNSS satellite antenna 31 as a symmetrical position; the upper ends of the two solar brackets 32 can be folded and connected to a butt-joint ring 314 on the antenna support rod 312; and the upper surfaces of the two solar brackets 32 are connected with solar films 321 through fixing bolts 323. The utility model discloses a solar rack 32 can keep balance as far as possible, and can satisfy the redundant demand of electricity generation, whether can be so that when monitoring devices put in orientation of solar film 321 need not be considered south or not (for example, when solar film 321 is north-south orientation, have one side must south, can satisfy the illumination power generation requirement, even solar film 321 is the east-west orientation, no matter in the morning or afternoon, always one side can just to illumination direction, generate electricity), with the maximize when satisfying long-term continuous observation absorb solar energy.
Four corners of the bottom surface of the monitoring box body 3 are respectively provided with a contact pin 324 made of stainless steel material, and the bottom of the contact pin 324 is sharpened for being inserted into the ground for fixing.
Specifically, the direction parallel to the plane where the two solar supports 32 are located is used as the observation direction, the clockwise direction is used as the rotation direction, the included angle range between the right solar support 32 and the horizontal plane is 45 degrees, and the large angle adjusting range can adapt to the use requirements of different latitude areas.
Specifically, be provided with waterproof terminal box 322 on the solar rack 32, the pole body of antenna bracing piece 312, the below position that is located butt joint ring 314 is provided with the wire mouth 315 that the opening is down, the opening of wire mouth 315 is down, can effectively prevent the rainwater and flow backward, and the opening part uses rubber seal and the electric wire that passes together fixed, can further avoid the foreign matter to get into in addition. The solar connecting wire 316 on the solar film 321 is connected with the solar controller 21 in the monitoring box 3 through the waterproof junction box 322 and the wire connecting nozzle 315.
Specifically, the top surface of monitoring box 3 is provided with 4G gain antenna 327, 4G gain antenna 327 bottom is the magnetic patch, adsorbs on the monitoring box 3 surface that has the iron material, and is connected with GNSS receiver 1, and 4G gain antenna 327 is mainly for reinforcing 4G communication network for better data transmission of the built-in communication module of GNSS receiver 1.
Specifically, the bottom surface of the inner cavity of the monitoring box body 3, the corner points of the GNSS receiver 1, the solar controller 21 and the lithium battery 22 are all provided with the buffer material 328, namely, the expandable polystyrene material EPS, so that the monitoring box body 3 can be protected from being damaged due to impact when falling to the ground.
Specifically, the utility model discloses be provided with take-off platform 5, the main effect of take-off platform 5 is: because the height of the unmanned aerial vehicle frame is limited, and in order to raise the GNSS satellite antenna 31 as much as possible to obtain observation data with good data quality, the height of the GNSS satellite antenna 31 is generally higher than the height of the unmanned aerial vehicle frame, so that the problem that the monitoring device cannot be directly placed under the flying platform 41 when the flying platform 5 is placed on flat ground can be solved.
Example two
In the second embodiment, compared with the first embodiment, an anti-swing structure 4 with another structure is provided, and the rest parts except the structure are the same as those in the first embodiment, and the specific contents are as follows:
as shown in fig. 8 to 7, the anti-swing structure 4 includes a flying platform 41 connected to the unmanned aerial vehicle, a tripod head dispenser 411 is disposed at a central position of the bottom of the flying platform 41, and hinges 414 are symmetrically disposed at the bottom of the flying platform 41 by taking the tripod head dispenser 411 as a central line. The anti-swing structure 4 can ensure that the unmanned aerial vehicle cannot swing in the horizontal direction in the flying process of carrying the monitoring device, so that the unmanned aerial vehicle cannot be frequently leveled due to the swing and cannot be crashed; moreover, anti swing structure 4 is not atress in unmanned aerial vehicle take off back, vertical direction, consequently can not influence monitoring devices's input.
The top of the side face, opposite to the position of the holder controller 412, of the monitoring box body 3 is provided with an anti-swing joint 326, the middle of the edge of the top face of the monitoring box body 3, close to the anti-swing joint 326, is provided with a hanging ring 325, and the hanging ring 325 is provided with a rubber ring for protecting the hanging wire 413 from being broken.
The holder dispenser 411 is connected to the two hanging rings 325 on the monitoring box 3 through two hanging wires 413.
The anti-swing structure 4 comprises a pair of support frames 42, and the support frames 42 are composed of an unmanned aerial vehicle landing gear 421 through a three-way pipe 422 and a limiting rod 423 arranged thereon; the upper end and the cloud platform controller 412 of unmanned aerial vehicle undercarriage 421 are connected, the joint and the anti swing joint 326 joint of gag lever post 423.
In particular, the anti-oscillation structure 4 comprises a pair of support brackets 42; the support frame 42 is a carbon fiber support with a right-angled triangular section, and the carbon fiber support is composed of an unmanned aerial vehicle landing gear 421, an anti-swing support 424 connected with the unmanned aerial vehicle landing gear 421 through a three-way pipe 422, and a limiting rod 423 connected with the unmanned aerial vehicle landing gear 421 and the anti-swing support 424; the small-angle end of the supporting frame 42 is connected with the hinge 414 on the flying platform 41, and the bottom end of the limiting rod 423 is inserted into the anti-swing snap ring 329 of the monitoring box body 3. The takeoff platform 41 can be easily removed from the anti-swing structure 4 by means of the hinge 414 for storage.
EXAMPLE III
The third embodiment is the same as the first embodiment except that:
the direction parallel to the plane where the two solar supports 32 are located is used as the observation direction, the clockwise direction is used as the rotation direction, and the included angle range between the right solar support 32 and the horizontal plane is 55 degrees so as to meet the use requirements of different latitudes and different areas.
Example four
Example four is the same as example one except that:
the direction parallel to the plane where the two solar supports 32 are located is used as the observation direction, the clockwise direction is used as the rotation direction, and the included angle range between the right solar support 32 and the horizontal plane is 60 degrees so as to meet the use requirements of different latitudes and different areas.
Application example one
The first application example is described based on the structure of the first embodiment, and is intended to clarify the use method of the present invention, which is shown in fig. 4 and specifically includes the following steps:
s1, the flying platform 41 is placed on the takeoff platform 5, and the limiting rod 423 of the anti-swing structure 4 is clamped on the anti-swing joint 326 of the monitoring box body 3.
And S2, planning the air route of the unmanned aerial vehicle according to the longitude and latitude of the launching position of the selected monitoring device in advance.
S3, controlling the unmanned aerial vehicle to carry the monitoring device to a throwing place with the longitude and latitude coordinates appointed, and ensuring that the throwing position is correct through a camera carried on the unmanned aerial vehicle flying platform 41.
S4, whether the flying platform 41 is kept horizontal or not is firstly checked by using unmanned aerial vehicle flying control, the flying control holder of the unmanned aerial vehicle is operated, then the limit rod 423 is controlled to be opened through the holder controller 412, so that the limit rod is separated from the anti-swing joint 326, then the state of the holder dispenser 411 is controlled to be changed into 'open', and finally the box 3 is monitored to be naturally dispensed.
And S5, inserting the monitoring device into the ground after obtaining a certain speed through free falling, and fixing the monitoring device.
S6, the unmanned aerial vehicle takes a picture of the monitoring device and then navigates back, and the monitoring cloud platform is used for checking whether the observation data is transmitted back, whether the data quality is normal and whether the monitoring result is available.
Application example two
The second application example is described based on the structure of the second embodiment, and is intended to clarify the method of use of the present invention, and as shown in fig. 8, the specific method of use of the present invention is as follows:
s1, the flying platform 41 is placed on the takeoff platform 5, and the limiting rod 423 of the anti-swing structure 4 is inserted into the anti-swing ring 329 of the monitoring box body 3.
And S2, planning the air route of the unmanned aerial vehicle according to the longitude and latitude of the launching position of the selected monitoring device in advance.
S3, controlling the unmanned aerial vehicle to carry the monitoring device to a throwing place with the longitude and latitude coordinates appointed, and ensuring that the throwing position is correct through a camera carried on the unmanned aerial vehicle flying platform 41.
S4, whether the flying platform 41 is kept horizontal or not is checked by using unmanned aerial vehicle flight control, the flight control holder of the unmanned aerial vehicle is operated, the state of the holder dispenser 411 is controlled to be changed into 'on', and the monitoring box body 3 is naturally unhooked and dispensed.
And S5, inserting the monitoring device into the ground after obtaining a certain speed through free falling, and fixing the monitoring device.
S6, the unmanned aerial vehicle takes a picture of the monitoring device and then navigates back, and the monitoring cloud platform is used for checking whether the observation data is transmitted back, whether the data quality is normal and whether the monitoring result is available.
Claims (6)
1. The utility model provides a long-range geological disaster monitoring devices that deploys with anti swing structure to by monitoring box (3) to and set up in monitoring box (3), electric connection's GNSS receiver (1) and power supply system (2) are constituteed, power supply system (2) include solar control ware (21) and lithium cell (22), its characterized in that:
an anti-swing structure (4) is arranged on the monitoring box body (3);
the anti-swing structure (4) comprises a flying platform (41) connected with the unmanned aerial vehicle, a tripod head dispenser (411) is arranged at the center of the bottom of the flying platform (41), and tripod head controllers (412) are symmetrically arranged at the bottom of the flying platform (41) by taking the tripod head dispenser (411) as a central line;
anti-swing joints (326) are respectively arranged on the top of the side surface of the monitoring box body (3) opposite to the position of the holder controller (412), and lifting rings (325) are respectively arranged in the middle of the top surface edge of the monitoring box body (3) close to the anti-swing joints (326);
the holder dispenser (411) is respectively connected with two lifting rings (325) on the monitoring box body (3) through two lifting wires (413);
the anti-swing structure (4) comprises a pair of supporting frames (42), wherein each supporting frame (42) is composed of an unmanned aerial vehicle landing gear (421) through a three-way pipe (422) and a limiting rod (423) arranged on the unmanned aerial vehicle landing gear; the upper end and cloud platform controller (412) of unmanned aerial vehicle undercarriage (421) are connected, the joint and the anti swing joint (326) joint of gag lever post (423).
2. A remotely deployed geological disaster monitoring device with sway resistant architecture as claimed in claim 1 wherein:
the top of the monitoring box body (3) is provided with a GNSS satellite antenna (31);
the GNSS satellite antenna (31) comprises an antenna support rod (312), one end of the antenna support rod (312) is vertically connected with the center of the top surface of the monitoring box body (3), and the other end of the antenna support rod (312) is provided with an SMA-KF male head (311); the SMA-KF male head (311) is connected with the GNSS receiver (1) through an antenna connecting line (313) arranged in an antenna supporting rod (312);
two solar supports (32) are arranged on the top surface of the monitoring box body (3) in a mirror image mode by taking the GNSS satellite antenna (31) as a symmetrical position; the upper ends of the two solar brackets (32) can be folded and connected to a butt joint circular ring (314) on the antenna support rod (312); the upper surfaces of the two solar supports (32) are connected with solar films (321) through fixing bolts (323);
four corners of the bottom surface of the monitoring box body (3) are respectively provided with a contact pin (324).
3. The device for monitoring geologic hazards having an anti-sway structure deployed remotely as claimed in claim 2 wherein the right side solar rack (32) is angled from the horizontal in the range of 45 ° to 60 ° with the viewing direction being parallel to the plane of both of said two solar racks (32) and the direction of rotation being clockwise.
4. A remotely deployed geological disaster monitoring device with anti-sway structure as claimed in claim 2 wherein said solar rack (32) is provided with a waterproof junction box (322), and said antenna support pole (312) is provided with a wire access nozzle (315) with a downward opening at the shaft below the docking ring (314); and a solar connecting wire (316) on the solar film (321) is connected with a solar controller (21) in the monitoring box body (3) through a waterproof junction box (322) and a wire connecting nozzle (315).
5. A remotely deployed geological disaster monitoring device with anti-sway structure as claimed in claim 1 wherein the top surface of the monitoring box (3) is provided with a 4G gain antenna (327) connected to GNSS receiver (1).
6. The device for monitoring geological disasters deployed in remote areas with anti-swing structures according to claim 1, wherein the bottom surface of the inner cavity of the monitoring box (3), the corner points of the GNSS receiver (1), the solar controller (21) and the lithium battery (22) are provided with buffer materials (328).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202022473152.7U CN214041742U (en) | 2020-10-30 | 2020-10-30 | Remote deployment geological disaster monitoring device with anti-swing structure |
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202022473152.7U CN214041742U (en) | 2020-10-30 | 2020-10-30 | Remote deployment geological disaster monitoring device with anti-swing structure |
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| CN214041742U true CN214041742U (en) | 2021-08-24 |
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| CN202022473152.7U Active CN214041742U (en) | 2020-10-30 | 2020-10-30 | Remote deployment geological disaster monitoring device with anti-swing structure |
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