CN220933070U - Unmanned aerial vehicle airborne light weight chemical examination electric installation - Google Patents
Unmanned aerial vehicle airborne light weight chemical examination electric installation Download PDFInfo
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- CN220933070U CN220933070U CN202322745510.9U CN202322745510U CN220933070U CN 220933070 U CN220933070 U CN 220933070U CN 202322745510 U CN202322745510 U CN 202322745510U CN 220933070 U CN220933070 U CN 220933070U
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- 238000004458 analytical method Methods 0.000 claims abstract description 18
- 238000004891 communication Methods 0.000 claims abstract description 16
- 238000012360 testing method Methods 0.000 claims abstract description 16
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- 239000003990 capacitor Substances 0.000 claims description 7
- 229920001903 high density polyethylene Polymers 0.000 claims description 7
- 239000004700 high-density polyethylene Substances 0.000 claims description 7
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 claims description 6
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- 241000463219 Epitheca Species 0.000 description 2
- 230000003321 amplification Effects 0.000 description 2
- QVFWZNCVPCJQOP-UHFFFAOYSA-N chloralodol Chemical compound CC(O)(C)CC(C)OC(O)C(Cl)(Cl)Cl QVFWZNCVPCJQOP-UHFFFAOYSA-N 0.000 description 2
- 238000010586 diagram Methods 0.000 description 2
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- VYPSYNLAJGMNEJ-UHFFFAOYSA-N Silicium dioxide Chemical compound O=[Si]=O VYPSYNLAJGMNEJ-UHFFFAOYSA-N 0.000 description 1
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- 239000000741 silica gel Substances 0.000 description 1
- 229910002027 silica gel Inorganic materials 0.000 description 1
- 238000006467 substitution reaction Methods 0.000 description 1
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- Shielding Devices Or Components To Electric Or Magnetic Fields (AREA)
Abstract
The utility model belongs to the technical field of power construction and maintenance, and discloses an unmanned aerial vehicle-mounted light-weight test electric device which comprises a lower shell, wherein an upper shell is arranged on the lower shell, the lower shell and the upper shell are both made of metal materials, an induction module is arranged on the upper shell, and a collection and analysis module is arranged in the upper shell. According to the utility model, the induction module is integrated into the structural design of the device shell, and the metal coating is added to the induction module, so that the device shell has an induction function, and the communication module and the acquisition and analysis module are packaged into the metal cavity in the shell, and are distributed in a layered structure so as to be matched with the induction module, thereby the electricity inspection device is designed in a lightweight manner, and the induction module can effectively sense the electromagnetic field environment and shield the electromagnetic field of the circuit structure, so that the safety performance of the device is improved.
Description
Technical Field
The utility model belongs to the technical field of power construction and maintenance, and particularly relates to an unmanned aerial vehicle-mounted light-weight test electric device.
Background
With the increase of overhead transmission line maintenance tasks, the detection of line live state directly relates to the personal safety of operation personnel, and traditional electricity inspection mode consumes time, needs many people to cooperate, and inefficiency carries electricity inspection device through unmanned aerial vehicle and carries out line live state detection very big promotion detection efficiency, how to make the unmanned aerial vehicle of electricity inspection device adaptation basic unit line maintenance team become urgent need.
The chinese patent with the patent number of CN202221942582.1 discloses an airborne non-contact electricity testing device, the device comprises an unmanned aerial vehicle main body and an electroscope, one end bolted connection at the top of the unmanned aerial vehicle main body has a connecting piece, the top of the connecting piece is fixed with a fixed shell, the outside sliding connection at the top of the fixed shell has an assembly shell, the inside of the bottom of the assembly shell is fixed with a fixed block, and the fixed block is in sliding connection with the fixed shell, so that the technical problem that the current electricity testing process needs to be contacted and tested is solved.
According to the technical scheme, although the technical problem that contact electricity test is needed in the existing electricity test process is solved, the device is higher in important requirement on an unmanned aerial vehicle, and poor in electromagnetic interference resistance, and the unmanned aerial vehicle equipped by a basic circuit overhaul team is lower in bearing capacity and cannot be completely matched with the device, so that in the actual use process, the stability of the device is poor, and certain potential safety hazards exist.
Disclosure of utility model
The utility model aims to provide an unmanned aerial vehicle-mounted lightweight test electric device, which is used for solving the problems in the background technology.
In order to achieve the above object, the present utility model provides the following technical solutions: the unmanned aerial vehicle-mounted light-weight test electric device comprises a lower shell, wherein an upper shell is arranged on the lower shell, the lower shell and the upper shell are both made of metal, an induction module is arranged on the upper shell, an acquisition and analysis module is arranged in the upper shell, the induction module is connected with the acquisition and analysis module through a connection type transmission channel, and a communication module is arranged on the lower shell;
The induction module comprises an antenna housing arranged on the upper side of the upper shell, a capacitor plate is embedded in the antenna housing, and a metal coating is arranged on the upper surface of the capacitor plate.
Preferably, the radome is made of high-density polyethylene.
Preferably, the collection and analysis module comprises a control board arranged in the upper shell, a switch, a light guide column and a rola board are arranged on the lower surface of the control board, and an SMA seat is arranged on the rola board.
Preferably, the communication module includes a battery mounted inside a lower case connected to an upper case through a plurality of metal posts, and an antenna is mounted on an outer surface of the lower case.
Preferably, the metal pillar is a copper pillar.
Preferably, the lower shell is connected with the lower ends of the corresponding metal struts through a plurality of first screws, a plurality of mounting holes are formed in the upper shell, and the radome is connected with the corresponding mounting holes through a plurality of second screws.
Preferably, the number of the first screws and the number of the second screws are four.
The beneficial effects of the utility model are as follows:
According to the utility model, the induction module is integrated into the structural design of the device shell, and the metal coating is added to the induction module, so that the device shell has an induction function, and the communication module and the acquisition and analysis module are packaged into the metal cavity in the shell, and are distributed in a layered structure so as to be matched with the induction module, thereby the electricity inspection device is designed in a lightweight manner, and the induction module can effectively sense the electromagnetic field environment and shield the electromagnetic field of the circuit structure, so that the safety performance of the device is improved.
Drawings
FIG. 1 is a schematic perspective view of the present utility model;
FIG. 2 is an exploded view of the present utility model;
FIG. 3 is a schematic diagram showing a three-dimensional structure of an induction module according to the present utility model;
FIG. 4 is a schematic diagram showing a three-dimensional structure of an acquisition and analysis module according to the present utility model;
fig. 5 is a schematic perspective view illustrating a communication module according to the present utility model.
In the figure: 1. a lower case; 2. an upper case; 3. a docking-type transmission channel; 4. an antenna housing; 41. a capacitive plate; 42. a metal plating layer; 5. a control board; 51. a switch; 52. a light guide column; 53. rola plates; 54. an SMA seat; 6. a battery; 61. a metal pillar; 62. an antenna; 7. a first screw; 8. and a second screw.
Detailed Description
The following description of the embodiments of the present utility model will be made clearly and completely with reference to the accompanying drawings, in which it is apparent that the embodiments described are only some embodiments of the present utility model, but not all embodiments. 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.
As shown in fig. 1 to 5, the embodiment of the utility model provides an unmanned aerial vehicle-mounted light-weight test electric device, which comprises a lower shell 1, wherein an upper shell 2 is arranged on the lower shell 1, the lower shell 1 and the upper shell 2 are both made of metal materials, an induction module is arranged on the upper shell 2, an acquisition and analysis module is arranged in the upper shell 2, the induction module is connected with the acquisition and analysis module through a connection type transmission channel 3, a communication module is arranged on the lower shell 1, the induction module comprises a radome 4 arranged on the upper side of the upper shell 2, a capacitor plate 41 is embedded in the radome 4, and a metal coating 42 is arranged on the upper surface of the capacitor plate 41.
The working principle and beneficial effects of the technical scheme are as follows: the induction module of this device has shell and sensor's function concurrently, through adding the metal coating in the induction module and realizing electromagnetic induction function, the metal coating on the capacitive plate 41 can induce the variation of electromagnetic field, and pass through the input port of leading out the coating with signal transmission to the transmission passageway 3 top of plugging into, the transmission passageway 3 of plugging into is through the input port connection induction module, the collection analysis module is connected to the delivery outlet, the inside data transmission of passing through connector probe, the cladding of radome 4 of high density polyethylene makes simultaneously, the protect function of sensor and device has also been realized, and reduce volume and weight by a wide margin, this device after making the lightweight, unmanned aerial vehicle that basic unit circuit maintenance team has been equipped can be adapted, stability when in order to improve the staff operation.
As shown in fig. 1, in one embodiment: the radome 4 is made of high-density polyethylene.
The working principle and beneficial effects of the technical scheme are as follows: the radome 4 made of high-density polyethylene material has lighter weight, and can further lighten the weight of the device, thereby improving the stability of the device in use.
As shown in fig. 4, in one embodiment: the acquisition and analysis module comprises a control board 5 arranged in the upper shell 2, a switch 51, a light guide column 52 and a rola board 53 are arranged on the lower surface of the control board 5, and an SMA seat 54 is arranged on the roller board 53.
The working principle and beneficial effects of the technical scheme are as follows: after the acquisition and analysis module receives the data transmitted by the connection type transmission channel 3, under the mutual cooperation of the control board 5, the rola board 53 and the SMA seat 54, a measurement result is formed after data processing such as filtering, signal amplification and the like, and the measurement result is transmitted to the communication module.
As shown in fig. 5, in one embodiment: the communication module includes a battery 6 mounted inside a lower case 1, the lower case 1 is connected to an upper case 2 through a plurality of metal posts 61, and an antenna 62 is mounted on the outer surface of the lower case 1.
The working principle and beneficial effects of the technical scheme are as follows: the communication module adopts a JZX811 spread spectrum wireless data transmission module, the measuring result is sent to the background through the antenna 62 by the Lora radio frequency chip, and the metal support column 61 can be connected with the upper shell 2 and the lower shell 1.
As shown in fig. 1, in one embodiment: the metal support posts 61 are copper support posts.
The working principle and beneficial effects of the technical scheme are as follows: by providing the metal stay 61 as a copper stay, the electromagnetic shielding effect of the present device can be further improved, thereby improving the stability of the present device in use.
As shown in fig. 1, in one embodiment: the lower shell 1 is connected with the lower ends of the corresponding metal support posts 61 through a plurality of first screws 7, a plurality of mounting holes are formed in the upper shell 2, and the radome 4 is connected with the corresponding mounting holes through a plurality of second screws 8.
The working principle and beneficial effects of the technical scheme are as follows: the setting of first screw 7 can connect fixed inferior valve 1 and epitheca 2, and the setting of second screw 8 can connect fixed radome 4 and epitheca 2 to improve the stability of this device.
As shown in fig. 1, in one embodiment: the number of the first screws 7 and the second screws 8 is four.
The working principle and beneficial effects of the technical scheme are as follows: by setting the number of the first screws 7 and the second screws 8 to four, the stability after the installation of the device can be improved.
Working principle and using flow:
Besides the induction module, the whole shielding structure design is adopted, the lower shell 1 and the upper shell 2 are all made of all metal materials, meanwhile, in the structure design, the whole shell is reserved with only 4 interfaces such as an antenna 62, a switch 51, an indicator lamp (namely a light guide column 52), charging and the like, the interfaces of the antenna 62 are coaxial shielding structures, the metal shell of the switch 51 is welded with the device shell, metal shielding connection is realized, the light guide column 52 is closed by adopting a lamp column structure for opening, and the charging interface is closed by matching with a silica gel plug-in.
The induction module has the functions of a shell and a sensor, realizes the electromagnetic induction function by adding a metal coating in a high-density polyethylene material, and simultaneously realizes the protection of the sensor and the protection function of the device by wrapping the radome 4 made of high-density polyethylene, and greatly reduces the volume and the weight, so that the device after light weight can be adapted to an unmanned aerial vehicle equipped by a basic circuit overhaul team, and the stability of the operation of workers is improved.
During measurement, the switch 51 is firstly opened, the whole device is driven to operate by electric power provided by the battery 6, the variable quantity of an electromagnetic field is induced by the metal coating 42 on the capacitor plate 41, signals are transmitted to the input port above the connection type transmission channel 3 through the lead-out coating, the connection type transmission channel 3 is connected with the induction module through the input port, the output port is connected with the acquisition analysis module, the inside is subjected to data transmission through the connector probe, the outside is designed by adopting a shielding structure, the copper shielding layer is coated on the outer side of the connector to ensure the stability of a communication link under a strong electromagnetic environment, the copper shielding layer is welded and fixed with the shielding structure, the acquisition analysis module acquires data from the output port of the connection type transmission channel 3, after the data processing such as filtering, signal amplification and the like is carried out on the control board 5, the rola board 53 and the SMA seat 54, a measurement result is formed, the communication module is transmitted to the communication module, the communication module adopts the JZX811 spread spectrum wireless data transmission module, and the measurement result is transmitted to the background through the Lora radio frequency chip, and the whole current testing process is completed. (wherein the control plates 5, rola, 53, and the SMA seat 54 are all of the prior art, the working principles of which are not described in detail)
According to the utility model, the induction module is integrated into the structural design of the device shell, and the metal coating is added into the induction module, so that the device shell has an induction function, and the communication module and the acquisition and analysis module are packaged into the metal cavity in the shell, and are distributed in a layered structure so as to be matched with the induction module, thereby the electricity inspection device is designed in a lightweight manner, and the induction module can effectively sense the electromagnetic field environment and shield the electromagnetic structure, so that the safety performance of the device is improved.
It is noted that relational terms such as first and second, and the like are used solely to distinguish one entity or action from another entity or action without necessarily requiring or implying any actual such relationship or order between such entities or actions. Moreover, the terms "comprises," "comprising," or any other variation thereof, are intended to cover a non-exclusive inclusion, such that a process, method, article, or apparatus that comprises a list of elements does not include only those elements but may include other elements not expressly listed or inherent to such process, method, article, or apparatus.
Although embodiments of the present utility model have been shown and described, it will be understood by those skilled in the art that various changes, modifications, substitutions and alterations can be made therein without departing from the principles and spirit of the utility model, the scope of which is defined in the appended claims and their equivalents.
Claims (7)
1. The utility model provides an unmanned aerial vehicle airborne lightweight chemical examination electric device, includes inferior valve (1), its characterized in that: an upper shell (2) is arranged on the lower shell (1), the lower shell (1) and the upper shell (2) are both made of metal, an induction module is arranged on the upper shell (2), an acquisition and analysis module is arranged in the upper shell (2), the induction module is connected with the acquisition and analysis module through a connection type transmission channel (3), and a communication module is arranged on the lower shell (1);
The induction module comprises an antenna housing (4) arranged on the upper side of an upper shell (2), a capacitor plate (41) is embedded in the antenna housing (4), and a metal coating (42) is arranged on the upper surface of the capacitor plate (41).
2. The unmanned aerial vehicle-mounted lightweight test electric device according to claim 1, wherein: the antenna housing (4) is made of high-density polyethylene.
3. The unmanned aerial vehicle-mounted lightweight test electric device according to claim 1, wherein: the collection analysis module comprises a control board (5) arranged in an upper shell (2), a switch (51), a light guide column (52) and a rola board (53) are arranged on the lower surface of the control board (5), and an SMA seat (54) is arranged on the rola board (53).
4. The unmanned aerial vehicle-mounted lightweight test electric device according to claim 1, wherein: the communication module comprises a battery (6) arranged inside a lower shell (1), wherein the lower shell (1) is connected with an upper shell (2) through a plurality of metal struts (61), and an antenna (62) is arranged on the outer surface of the lower shell (1).
5. The unmanned aerial vehicle-mounted lightweight test electric device of claim 4, wherein: the metal support (61) is a copper support.
6. The unmanned aerial vehicle-mounted lightweight test electric device of claim 4, wherein: the antenna housing is characterized in that the lower shell (1) is connected with the lower ends of the corresponding metal support posts (61) through a plurality of first screws (7), a plurality of mounting holes are formed in the upper shell (2), and the antenna housing (4) is connected with the corresponding mounting holes through a plurality of second screws (8).
7. The unmanned aerial vehicle-mounted lightweight test electric device of claim 6, wherein: the number of the first screws (7) and the number of the second screws (8) are four.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
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CN202322745510.9U CN220933070U (en) | 2023-10-12 | 2023-10-12 | Unmanned aerial vehicle airborne light weight chemical examination electric installation |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
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CN202322745510.9U CN220933070U (en) | 2023-10-12 | 2023-10-12 | Unmanned aerial vehicle airborne light weight chemical examination electric installation |
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Publication Number | Publication Date |
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CN220933070U true CN220933070U (en) | 2024-05-10 |
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CN202322745510.9U Active CN220933070U (en) | 2023-10-12 | 2023-10-12 | Unmanned aerial vehicle airborne light weight chemical examination electric installation |
Country Status (1)
Country | Link |
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CN (1) | CN220933070U (en) |
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2023
- 2023-10-12 CN CN202322745510.9U patent/CN220933070U/en active Active
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