CN219257690U - A fault alarm device for unmanned aerial vehicle - Google Patents
A fault alarm device for unmanned aerial vehicle Download PDFInfo
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- CN219257690U CN219257690U CN202222513255.0U CN202222513255U CN219257690U CN 219257690 U CN219257690 U CN 219257690U CN 202222513255 U CN202222513255 U CN 202222513255U CN 219257690 U CN219257690 U CN 219257690U
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- 230000005540 biological transmission Effects 0.000 claims description 6
- 238000005516 engineering process Methods 0.000 description 6
- 238000007689 inspection Methods 0.000 description 5
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- 238000004891 communication Methods 0.000 description 3
- 238000012545 processing Methods 0.000 description 3
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Abstract
The utility model provides a fault alarm device for an unmanned aerial vehicle. The fault alarm device for the unmanned aerial vehicle comprises a mounting seat, a protective shell, an annular plate, an alarm, a buzzer, a sensor and four limit groups, wherein the mounting seat, the protective shell, the annular plate, the alarm, the buzzer, the sensor and the four limit groups are arranged on the unmanned aerial vehicle body; the mounting seat is arranged on the unmanned aerial vehicle main body, and the mounting seat and the unmanned aerial vehicle main body can be connected through bolts; the protective shell is arranged on the top of the mounting seat in a threaded manner; the annular plate is arranged in the protective shell, and the bottom of the annular plate is connected with the top of the mounting seat; the alarm is fixedly arranged on the top of the annular plate. The fault alarm device for the unmanned aerial vehicle is simple to operate, is convenient to disassemble and assemble the alarm, can avoid damage to the unmanned aerial vehicle main body, can send a short message to a user, and can remind the user of overhauling.
Description
Technical Field
The utility model belongs to the technical field of unmanned aerial vehicle inspection fault processing, and particularly relates to fault alarm equipment for an unmanned aerial vehicle.
Background
The unmanned aerial vehicle technology is combined with the photogrammetry technology, so that a high-efficiency inspection operation mode, such as electric power inspection, is an important means for ensuring safe operation of a power grid, and based on powerful unmanned aerial vehicle hardware and professional photogrammetry software, the unmanned aerial vehicle integrated inspection system is provided, so that the unmanned aerial vehicle electric power inspection system is more efficient, high-precision and safe and reliable, is solved, is based on a mature fixed wing and rotor unmanned aerial vehicle platform, and provides the most efficient automatic strip line according to the flight requirement of an electric power strip on the line design, and is suitable for a high-altitude line of mountain terrain; in terms of data processing, the advantages of a strip space three and vegetation dense area space three algorithm, a software and hardware integrated image-free control technology, an image-based dense matching technology, a space three-based efficient semi-automatic wire fitting method and the like are brought into play, a power line ground surface channel and wires can be digitally reconstructed in three dimensions, quantitative channel obstacle detection is achieved, a set of integrated solution from data acquisition, processing to analysis and report output is finally formed, the scheme also has three advantages of high efficiency, high precision and safety and reliability, a global unmanned aerial vehicle network is sourced here, the existing unmanned aerial vehicle is prone to faults in long-time use, a set of fault communication alarm equipment is needed at the moment, through retrieval, in the related technology, an unmanned aerial vehicle fault communication alarm device is disclosed, the unmanned aerial vehicle fault communication alarm device comprises a mounting base, a fixing screw is fixedly connected to the upper surface of the mounting base, a connecting ring is fixedly connected to the outer surface of the alarm, a connecting hole is fixedly connected to the outer surface of the connecting ring, a buzzer is fixedly connected to the top of the alarm, a connector is fixedly connected to the inside of the connecting hole, one end of the connecting wire is fixedly connected to the connecting wire, a connecting wire is fixedly connected to the inside of the sensor, and the inside of the alarm body is fixedly connected to the inside of the alarm hole. The utility model is convenient for disassembly and detection of the unmanned aerial vehicle when faults occur by arranging the simple installation structure of the novel fault alarm device, is convenient for disassembly of workers and installation of the alarm device, but has the following defects in actual life, especially has inconvenience when the alarm on the unmanned aerial vehicle is disassembled and assembled, because the alarm is generally fixedly connected with the installation base, and the installation base is fixedly connected with the machine body through the fixing screw, when the alarm is required to be disassembled and assembled, the fixing screw is required to be repeatedly rotated, but the mode not only easily causes sliding wires, so that the disassembly and assembly work is difficult, but also the machine body is easily damaged, and information cannot be sent to a user.
Accordingly, there is a need to provide a new malfunction alerting device for unmanned aerial vehicles that solves the above-mentioned technical problems.
Disclosure of Invention
The utility model solves the technical problem of providing the fault alarm equipment for the unmanned aerial vehicle, which is simple to operate, is convenient to disassemble and assemble the alarm, can avoid damaging the unmanned aerial vehicle main body, can send a short message to a user, and can remind the user to overhaul.
In order to solve the technical problems, the fault alarm equipment for the unmanned aerial vehicle provided by the utility model comprises a mounting seat, a protective shell, an annular plate, an alarm, a buzzer, a sensor and four limit groups, wherein the mounting seat, the protective shell, the annular plate, the alarm, the buzzer, the sensor and the four limit groups are arranged on the unmanned aerial vehicle main body;
the mounting seat is arranged on the unmanned aerial vehicle main body, and the mounting seat and the unmanned aerial vehicle main body can be connected through bolts;
the protective shell is arranged on the top of the mounting seat in a threaded manner;
the annular plate is arranged in the protective shell, and the bottom of the annular plate is connected with the top of the mounting seat;
the alarm is fixedly arranged on the top of the annular plate;
the buzzer is fixedly arranged on the top of the protective shell;
the sensor is arranged above the alarm and is electrically connected with the alarm and the buzzer through leads respectively;
the four limit groups are all arranged in the protective shell, and the four limit components are distributed in an annular array.
As a further scheme of the utility model, the limiting group comprises a fixed block, an installation inserting block, a first connecting rod, a moving block, a telescopic spring and a second connecting rod, wherein the fixed block is fixedly installed on the top of the installation seat, a groove is formed in the outer wall of one side of the fixed block, the installation inserting block is slidably installed on the fixed block, the first connecting rod is fixedly installed in the groove, the moving block is slidably installed on the first connecting rod, one side of the moving block extends out of the groove, the telescopic spring is slidably sleeved on the first connecting rod, the top end of the telescopic spring is fixedly connected with the bottom of the moving block, the bottom end of the telescopic spring is fixedly connected with the inner wall of the bottom of the groove, the second connecting rod is hinged to the top of the installation inserting block, and the top end of the second connecting rod is hinged with the moving block.
As a further scheme of the utility model, four slots are formed in the outer wall of the annular plate, the four slots are distributed in an annular array, and the slots are matched with the mounting plug blocks.
As a further scheme of the utility model, the top of the mounting seat is provided with a limit groove, the bottom of the annular plate is fixedly provided with a limit rod, and the limit rod is in sliding connection with the limit groove.
As a further scheme of the utility model, the top of the mounting seat is provided with an annular thread groove, the bottom of the protective shell is provided with external threads, and the bottom of the protective shell extends into the annular thread groove and is connected with the inner wall of the annular thread groove in a screwing way.
As a further scheme of the utility model, four pressing plates are fixedly arranged on the inner wall of the protective shell, the four pressing plates are distributed in an annular array, rubber pads are fixedly arranged at the bottoms of the four pressing plates, and the rubber pads are connected with the tops of the annular plates.
As a further scheme of the utility model, a circular ring is movably sleeved on the circular plate, four supporting rods are fixedly arranged at the bottom of the circular ring, the four supporting rods are distributed in an annular array, the bottoms of the supporting rods are fixedly connected with the top of the moving block, and the circular ring is in sliding connection with the fixed block.
As a further scheme of the utility model, the unmanned aerial vehicle main body is provided with an information transmission group, the information transmission group comprises a detection module, a control module, a real-time clock module, a GPS positioning module and a GSM module, the detection module is connected with the control module, the real-time clock module and the GPS positioning module are both connected with the control module, and the control module is connected with the GSM module.
Compared with the related art, the fault alarm device for the unmanned aerial vehicle has the following beneficial effects:
1. the utility model has the advantages that the operation is simple, the alarm is convenient to disassemble, assemble, replace and maintain, and the fixing screw does not need to be repeatedly rotated, so that the damage to the unmanned aerial vehicle main body can be avoided;
2. the utility model can send the short message to the user by setting the information transmission group, so as to remind the user to overhaul in time.
Drawings
The present utility model is further described below with reference to the accompanying drawings for the convenience of understanding by those skilled in the art.
FIG. 1 is a schematic diagram of the structure of the present utility model;
FIG. 2 is a schematic view of a mounting base according to the present utility model;
FIG. 3 is a schematic view of an annular plate of the present utility model.
In the figure: 1. an unmanned aerial vehicle main body; 2. a mounting base; 3. a protective shell; 4. an annular plate; 5. an alarm; 6. a buzzer; 7. a sensor; 8. a fixed block; 9. installing an inserting block; 10. a first connecting rod; 11. a moving block; 12. a telescopic spring; 13. a second connecting rod; 14. a circular ring; 15. a detection module; 16. a control module; 17. a real-time clock module; 18. a GPS positioning module; 19. and a GSM module.
Detailed Description
Referring to fig. 1, fig. 2 and fig. 3 in combination, fig. 1 is a schematic structural diagram of the present utility model; FIG. 2 is a schematic view of a mounting base according to the present utility model; FIG. 3 is a schematic view of an annular plate of the present utility model. The fault alarm device for the unmanned aerial vehicle comprises a mounting seat 2, a protective shell 3, an annular plate 4, an alarm 5, a buzzer 6, a sensor 7 and four limiting groups, wherein the mounting seat 2, the protective shell 3, the annular plate 4, the alarm 5, the buzzer 6 and the four limiting groups are arranged on the unmanned aerial vehicle body 1;
the mounting seat 2 is arranged on the unmanned aerial vehicle main body 1, and the mounting seat 2 and the unmanned aerial vehicle main body 1 can be connected through bolts;
the protective shell 3 is arranged on the top of the mounting seat 2 in a threaded manner;
the annular plate 4 is arranged in the protective shell 3, and the bottom of the annular plate 4 is connected with the top of the mounting seat 2;
the alarm 5 is fixedly arranged on the top of the annular plate 4;
the buzzer 6 is fixedly arranged on the top of the protective shell 3;
the sensor 7 is arranged above the alarm 5, and the sensor 7 is electrically connected with the alarm 5 and the buzzer 6 through leads respectively;
the four limit groups are all arranged in the protective shell 3, and the four limit components are distributed in a ring array.
The limiting group comprises a fixed block 8, an installation inserting block 9, a first connecting rod 10, a moving block 11, a telescopic spring 12 and a second connecting rod 13, wherein the fixed block 8 is fixedly installed on the top of the installation seat 2, a groove is formed in the outer wall of one side of the fixed block 8, the installation inserting block 9 is slidably installed on the fixed block 8, the first connecting rod 10 is fixedly installed in the groove, the moving block 11 is slidably installed on the first connecting rod 10, one side of the moving block 11 extends out of the groove, the telescopic spring 12 is slidably sleeved on the first connecting rod 10, the top end of the telescopic spring 12 is fixedly connected with the bottom of the moving block 11, the bottom end of the telescopic spring 12 is fixedly connected with the bottom inner wall of the groove, the second connecting rod 13 is hinged to be installed on the top of the installation inserting block 9, and the top end of the second connecting rod 13 is hinged to the moving block 11.
Four slots are formed in the outer wall of the annular plate 4 and distributed in an annular array, and the slots are matched with the mounting plug blocks 9.
The top of mount pad 2 has seted up the spacing groove, the bottom fixed mounting of annular plate 4 has the gag lever post, gag lever post and spacing groove sliding connection.
The top of mount pad 2 has seted up annular thread groove, the external screw thread has been seted up to the bottom of protecting crust 3, the bottom of protecting crust 3 extends to in the annular thread groove and the inner wall in annular thread groove closes the connection soon.
Four pressing plates are fixedly arranged on the inner wall of the protective shell 3 and distributed in an annular array, rubber pads are fixedly arranged at the bottoms of the four pressing plates, and the rubber pads are connected with the tops of the annular plates 4.
The movable sleeve is provided with a circular ring 14 on the annular plate 4, four supporting rods are fixedly arranged at the bottom of the circular ring 14 and distributed in an annular array, the bottom of each supporting rod is fixedly connected with the top of the movable block 11, and the circular ring 14 is slidably connected with the fixed block 8.
When the alarm 5 needs to be disassembled, the protective shell 3 is rotated firstly, the protective shell 3 is separated from the mounting seat 2, so that the protective shell 3 can be opened, then the ring 14 is pressed by hands to move downwards, and then the ring 14 drives the moving block 11 to squeeze the telescopic spring 12 to move downwards, so that the mounting insert 9 is separated from the slot under the action of the second connecting rod 13 and the hinge, and the alarm 5 can be taken out.
Similarly, when the alarm 5 needs to be installed, the ring 14 is pressed to move downwards in the same manner as the operation, and then the ring 14 drives the moving block 11 to extrude the telescopic spring 12 to move downwards, so as to drive the installation insert 9 to move towards the protecting shell 3, then the limiting rod at the bottom of the annular plate 4 is inserted into the limiting groove, then the ring 14 is released, and then the moving block 11 is driven to reset under the action of the telescopic spring 12, so that the installation insert 9 is inserted into the slot under the action of the hinging and the second connecting rod 13 to limit and fix the annular plate 4, thereby limiting and fixing the alarm 5, and finally the protecting shell 3 is inserted into the annular thread groove to rotate and fix the alarm 5, so that the operation is simple, the dismounting and mounting of the alarm 5 are facilitated, the fixing screw is not required to be repeatedly rotated, and the damage to the unmanned aerial vehicle main body 1 can be avoided
The unmanned aerial vehicle is characterized in that an information transmission group is arranged on the unmanned aerial vehicle main body 1 and comprises a detection module, a control module, a real-time clock module, a GPS positioning module and a GSM module, wherein the detection module is connected with the control module, the real-time clock module and the GPS positioning module are both connected with the control module, and the control module is connected with the GSM module.
Firstly, pre-stored numbers are set for a GSM module, wherein the GSM module consists of a UART interface, a GSM radio frequency chip, a memory and a power amplifier device and is provided with an independent operating system, fault information and control information from a control module are received, and the GSM module sends the fault information and the control information to a preset telephone number in a short message mode;
the information transmission system uses a real-time clock module and a GPS positioning module to manage time and position, and is powered by a button battery and a lithium battery.
The unmanned aerial vehicle main body 1 is checked through the detection module, when the detected problem is solved, information is transmitted to the control module, the control module reads the time and the area through the real-time clock module and the GPS positioning module, transmits the information and fault information to the GSM module, and controls the GSM module to send the information to a user in the form of a short message, so that the user is informed of the timely maintenance.
It should be noted that, the device structure and the drawings of the present utility model mainly describe the principle of the present utility model, in terms of the technology of the design principle, the arrangement of the power mechanism, the power supply system, the control system, etc. of the device is not completely described, and on the premise that the person skilled in the art understands the principle of the present utility model, the specific details of the power mechanism, the power supply system and the control system can be clearly known, the control mode of the application file is automatically controlled by the controller, and the control circuit of the controller can be realized by simple programming of the person skilled in the art;
the standard parts used in the method can be purchased from the market, and can be customized according to the description of the specification and the drawings, the specific connection modes of the parts are conventional means such as mature bolts, rivets and welding in the prior art, the machines, the parts and the equipment are conventional models in the prior art, and the structures and the principles of the parts are all known by the skilled person through technical manuals or through conventional experimental methods.
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 may be made therein without departing from the spirit and scope of the utility model as defined by the appended claims and their equivalents, and in other related technical fields, which are equally encompassed by the scope of the present utility model.
Claims (8)
1. The fault alarm device for the unmanned aerial vehicle is characterized by comprising a mounting seat, a protective shell, an annular plate, an alarm, a buzzer, a sensor and four limit groups, wherein the mounting seat, the protective shell, the annular plate, the alarm, the buzzer, the sensor and the four limit groups are arranged on the unmanned aerial vehicle body;
the mounting seat is arranged on the unmanned aerial vehicle main body, and the mounting seat and the unmanned aerial vehicle main body can be connected through bolts;
the protective shell is arranged on the top of the mounting seat in a threaded manner;
the annular plate is arranged in the protective shell, and the bottom of the annular plate is connected with the top of the mounting seat;
the alarm is fixedly arranged on the top of the annular plate;
the buzzer is fixedly arranged on the top of the protective shell;
the sensor is arranged above the alarm and is electrically connected with the alarm and the buzzer through leads respectively;
the four limit groups are all arranged in the protective shell, and the four limit components are distributed in an annular array.
2. The malfunction alerting device for an unmanned aerial vehicle as claimed in claim 1, wherein: the limiting group comprises a fixed block, an installation insert block, a first connecting rod, a moving block, a telescopic spring and a second connecting rod, wherein the fixed block is fixedly installed on the top of the installation seat, a groove is formed in the outer wall of one side of the fixed block, the installation insert block is slidably installed on the fixed block, the first connecting rod is fixedly installed in the groove, the moving block is slidably installed on the first connecting rod, one side of the moving block extends out of the groove, the telescopic spring is slidably sleeved on the first connecting rod, the top end of the telescopic spring is fixedly connected with the bottom of the moving block, the bottom end of the telescopic spring is fixedly connected with the inner wall of the bottom of the groove, the second connecting rod is hinged to the top of the installation insert block, and the top end of the second connecting rod is hinged to the moving block.
3. The malfunction alerting device for an unmanned aerial vehicle as claimed in claim 1, wherein: four slots are formed in the outer wall of the annular plate and distributed in an annular array, and the slots are matched with the mounting inserting blocks.
4. The malfunction alerting device for an unmanned aerial vehicle as claimed in claim 1, wherein: the top of mount pad has seted up the spacing groove, the bottom fixed mounting of annular plate has the gag lever post, gag lever post and spacing groove sliding connection.
5. The malfunction alerting device for an unmanned aerial vehicle as claimed in claim 1, wherein: the top of mount pad has seted up annular thread groove, the external screw thread has been seted up to the bottom of protecting crust, the bottom of protecting crust extends to in the annular thread groove and the inner wall in annular thread groove closes the connection soon.
6. The malfunction alerting device for an unmanned aerial vehicle as claimed in claim 1, wherein: four pressing plates are fixedly arranged on the inner wall of the protective shell and distributed in an annular array, rubber pads are fixedly arranged at the bottoms of the four pressing plates, and the rubber pads are connected with the tops of the annular plates.
7. The malfunction alerting device for an unmanned aerial vehicle as claimed in claim 1, wherein: the movable sleeve is provided with a circular ring, four supporting rods are fixedly arranged at the bottom of the circular ring and distributed in an annular array, the bottom of each supporting rod is fixedly connected with the top of the movable block, and the circular ring is in sliding connection with the fixed block.
8. The malfunction alerting device for an unmanned aerial vehicle as claimed in claim 1, wherein: the unmanned aerial vehicle is characterized in that an information transmission group is arranged on the unmanned aerial vehicle main body and comprises a detection module, a control module, a real-time clock module, a GPS positioning module and a GSM module, wherein the detection module is connected with the control module, the real-time clock module and the GPS positioning module are both connected with the control module, and the control module is connected with the GSM module.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202222513255.0U CN219257690U (en) | 2022-09-22 | 2022-09-22 | A fault alarm device for unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202222513255.0U CN219257690U (en) | 2022-09-22 | 2022-09-22 | A fault alarm device for unmanned aerial vehicle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN219257690U true CN219257690U (en) | 2023-06-27 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202222513255.0U Active CN219257690U (en) | 2022-09-22 | 2022-09-22 | A fault alarm device for unmanned aerial vehicle |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN219257690U (en) |
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2022
- 2022-09-22 CN CN202222513255.0U patent/CN219257690U/en active Active
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Effective date of registration: 20231208 Address after: No. 555 Renmin Road, Nanyang City, Henan Province, 473299 Patentee after: Nanyang Feilong Power Group Co.,Ltd. Address before: 474350 North 217, Ju Tan Street, Chengguan Town, Neixiang City, Nanyang, Henan. Patentee before: STATE GRID HENAN ELECTRIC POWER COMPANY NEIXIANG COUNTY POWER SUPPLY Co. |