CN115379160A - Unmanned aerial vehicle airborne monitoring device with thermal imaging function and monitoring method thereof - Google Patents
Unmanned aerial vehicle airborne monitoring device with thermal imaging function and monitoring method thereof Download PDFInfo
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- CN115379160A CN115379160A CN202210843508.2A CN202210843508A CN115379160A CN 115379160 A CN115379160 A CN 115379160A CN 202210843508 A CN202210843508 A CN 202210843508A CN 115379160 A CN115379160 A CN 115379160A
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- 238000012544 monitoring process Methods 0.000 title claims abstract description 31
- 238000001931 thermography Methods 0.000 title claims abstract description 26
- 238000012806 monitoring device Methods 0.000 title claims abstract description 25
- 238000000034 method Methods 0.000 title claims abstract description 18
- 238000003331 infrared imaging Methods 0.000 claims abstract description 27
- 230000005540 biological transmission Effects 0.000 claims abstract description 23
- 238000009434 installation Methods 0.000 claims abstract description 12
- 238000003780 insertion Methods 0.000 claims description 12
- 230000037431 insertion Effects 0.000 claims description 12
- 239000000725 suspension Substances 0.000 claims description 10
- 230000000694 effects Effects 0.000 claims description 7
- 238000001179 sorption measurement Methods 0.000 claims description 3
- 230000008878 coupling Effects 0.000 description 4
- 238000010168 coupling process Methods 0.000 description 4
- 238000005859 coupling reaction Methods 0.000 description 4
- 238000005516 engineering process Methods 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 1
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- H—ELECTRICITY
- H04—ELECTRIC COMMUNICATION TECHNIQUE
- H04N—PICTORIAL COMMUNICATION, e.g. TELEVISION
- H04N7/00—Television systems
- H04N7/18—Closed-circuit television [CCTV] systems, i.e. systems in which the video signal is not broadcast
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16M—FRAMES, CASINGS OR BEDS OF ENGINES, MACHINES OR APPARATUS, NOT SPECIFIC TO ENGINES, MACHINES OR APPARATUS PROVIDED FOR ELSEWHERE; STANDS; SUPPORTS
- F16M11/00—Stands or trestles as supports for apparatus or articles placed thereon ; Stands for scientific apparatus such as gravitational force meters
- F16M11/02—Heads
- F16M11/04—Means for attachment of apparatus; Means allowing adjustment of the apparatus relatively to the stand
- F16M11/043—Allowing translations
- F16M11/045—Allowing translations adapted to left-right translation movement
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16M—FRAMES, CASINGS OR BEDS OF ENGINES, MACHINES OR APPARATUS, NOT SPECIFIC TO ENGINES, MACHINES OR APPARATUS PROVIDED FOR ELSEWHERE; STANDS; SUPPORTS
- F16M11/00—Stands or trestles as supports for apparatus or articles placed thereon ; Stands for scientific apparatus such as gravitational force meters
- F16M11/02—Heads
- F16M11/04—Means for attachment of apparatus; Means allowing adjustment of the apparatus relatively to the stand
- F16M11/043—Allowing translations
- F16M11/048—Allowing translations adapted to forward-backward translation movement
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16M—FRAMES, CASINGS OR BEDS OF ENGINES, MACHINES OR APPARATUS, NOT SPECIFIC TO ENGINES, MACHINES OR APPARATUS PROVIDED FOR ELSEWHERE; STANDS; SUPPORTS
- F16M11/00—Stands or trestles as supports for apparatus or articles placed thereon ; Stands for scientific apparatus such as gravitational force meters
- F16M11/02—Heads
- F16M11/18—Heads with mechanism for moving the apparatus relatively to the stand
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16M—FRAMES, CASINGS OR BEDS OF ENGINES, MACHINES OR APPARATUS, NOT SPECIFIC TO ENGINES, MACHINES OR APPARATUS PROVIDED FOR ELSEWHERE; STANDS; SUPPORTS
- F16M11/00—Stands or trestles as supports for apparatus or articles placed thereon ; Stands for scientific apparatus such as gravitational force meters
- F16M11/42—Stands or trestles as supports for apparatus or articles placed thereon ; Stands for scientific apparatus such as gravitational force meters with arrangement for propelling the support stands on wheels
- F16M11/425—Stands or trestles as supports for apparatus or articles placed thereon ; Stands for scientific apparatus such as gravitational force meters with arrangement for propelling the support stands on wheels along guiding means
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16M—FRAMES, CASINGS OR BEDS OF ENGINES, MACHINES OR APPARATUS, NOT SPECIFIC TO ENGINES, MACHINES OR APPARATUS PROVIDED FOR ELSEWHERE; STANDS; SUPPORTS
- F16M13/00—Other supports for positioning apparatus or articles; Means for steadying hand-held apparatus or articles
- F16M13/02—Other supports for positioning apparatus or articles; Means for steadying hand-held apparatus or articles for supporting on, or attaching to, an object, e.g. tree, gate, window-frame, cycle
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- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Multimedia (AREA)
- Signal Processing (AREA)
- Closed-Circuit Television Systems (AREA)
- Studio Devices (AREA)
Abstract
The invention discloses an unmanned aerial vehicle airborne monitoring device with a thermal imaging function and a monitoring method thereof, relates to the technical field of unmanned aerial vehicle monitoring, and aims to solve the problems that the existing unmanned aerial vehicle monitoring device only can monitor real-time pictures of an area where an unmanned aerial vehicle is located in the using process, the monitoring range is small, and the installation adjustability is poor. The intelligent remote control display device comprises a main body carrier, a remote control handle and a screen divider, wherein two movable upright rods are arranged at the lower end of the main body carrier, and an alternating current mobile power supply and a switch button are arranged on the front end surface of the main body carrier; further comprising: the wireless network camera and the infrared imaging camera are respectively installed on the lower end positions of the two movable vertical rods, the positioning motors are arranged above the two movable vertical rods, transmission shafts are arranged on the output ends of the positioning motors, connecting shafts are arranged at the tops of the movable vertical rods, couplers are arranged inside the main body carrier frame, and the transmission shafts are movably connected with the connecting shafts through the couplers.
Description
Technical Field
The invention relates to the technical field of unmanned aerial vehicle monitoring, in particular to an unmanned aerial vehicle airborne monitoring device with a thermal imaging function and a monitoring method thereof.
Background
The unmanned plane is an unmanned plane operated by a radio remote control device and a self-contained program control device, or is completely or intermittently and autonomously operated by a vehicle-mounted computer, and the unmanned plane monitoring technology is widely applied to industries such as military police, city management, agriculture, geology, meteorology, electric power, emergency rescue and relief, video shooting and the like.
For example, application No.: 202111194820.5 (named as an unmanned aerial vehicle monitoring device), which comprises a bod, the both sides of organism are rotated and are connected with the support, the lower surface sliding connection of support has anti-drop mechanism, anti-drop mechanism's back swing joint has control mechanism, control mechanism is located the bottom of organism, the organism includes slewing mechanism, slewing mechanism's front is rotated and is connected with chucking mechanism, slewing mechanism includes the snap ring, the ring channel has been seted up on the front of snap ring, the internal surface sliding connection of ring channel has hydraulic pressure mechanism, hydraulic pressure mechanism is located chucking mechanism's outside.
The unmanned aerial vehicle monitoring device can only monitor the real-time image of the area where the unmanned aerial vehicle is located in the using process, the monitoring range is small, and the installation adjustability is poor, so that the unmanned aerial vehicle onboard monitoring device with the thermal imaging function and the monitoring method thereof are provided
Disclosure of Invention
The invention aims to provide an unmanned aerial vehicle airborne monitoring device with a thermal imaging function and a monitoring method thereof, and aims to solve the problems that the existing unmanned aerial vehicle monitoring device provided in the background technology only can monitor real-time pictures of an area where an unmanned aerial vehicle is located in the using process, the monitoring range is small, and the installation adjustability is poor.
In order to achieve the purpose, the invention provides the following technical scheme: an unmanned aerial vehicle airborne monitoring device with a thermal imaging function comprises a main body carrier, a remote control handle and a screen dividing display, wherein two movable vertical rods are arranged at the lower end of the main body carrier, and an alternating-current mobile power supply and a switch button are arranged on the front end face of the main body carrier;
further comprising:
the wireless network camera and the infrared imaging camera are respectively arranged at the lower ends of the two movable vertical rods, a positioning motor is arranged above the two movable vertical rods, a transmission shaft is arranged at the output end of the positioning motor, a connecting shaft is arranged at the top of each movable vertical rod, a coupler is arranged in the main body carrier, and the transmission shaft is movably connected with the connecting shaft through the coupler;
the suspension plate is arranged at the upper end of the main body carrier, the suspension plate and the main body carrier are integrally formed, an internal connecting sliding groove is formed in the suspension plate, and a connecting bottom block is arranged in the internal connecting sliding groove;
the horizontal hack lever is arranged at the upper end of the connecting bottom block, the horizontal hack lever and the connecting bottom block are integrally formed, an end surface groove is formed in the horizontal hack lever, a guide slide rail is arranged in the end surface groove, two sleeve connection sliding blocks are arranged outside the guide slide rail, an extension rod is arranged at the upper end of each sleeve connection sliding block, an installation top plate is arranged at the top of each extension rod, and the installation top plate and the extension rods are integrally formed with the sleeve connection sliding blocks;
the router and the hard disk video recorder are arranged on one side of the screen dividing display, the output ends of the wireless network camera and the infrared imaging camera are in transmission connection with the input end of the router, the output end of the router is in transmission connection with the input end of the hard disk video recorder, and the output end of the hard disk video recorder is in transmission connection with the input end of the screen dividing display.
Preferably, be provided with the screens groove on the inner wall of inscription spout, screens groove and inscription spout integrated into one piece set up, the inside in screens groove is provided with the inside lining fixture block, inside lining fixture block with connect bottom block integrated into one piece set up.
Preferably, the bottom of connecting the bottom block is provided with the support and carries the kerve, the inside that the support carried the kerve is provided with the gyro wheel, all be provided with the bearing on the both sides inner wall of support year kerve, the pivot on the outer wall of gyro wheel both sides all with bearing swing joint.
Preferably, all install two screens cover frames on the both ends position of cup jointing the slider, all be provided with the inserting groove on the both sides outer wall of direction slide rail, the inserting groove sets up with direction slide rail integrated into one piece, the inside of inserting groove is provided with to be connected participates in, connects to participate in and screens cover frame integrated into one piece setting.
Preferably, the connection position of the connection pin and the insertion groove is provided with a positive magnet and a negative magnet, and the positive magnet and the negative magnet are respectively integrally formed with the connection pin and the insertion groove.
Preferably, a receiver is arranged in the shell of the positioning motor, the output end of the remote control handle is in transmission connection with the input end of the receiver, and the output end of the receiver is in transmission connection with the input end of the positioning motor.
Preferably, the inner wall of the internal connection sliding groove is provided with an electromagnet panel, the output end of the alternating-current mobile power supply is electrically connected with the input ends of the positioning motor, the switch button, the wireless network camera and the infrared imaging camera, and the output end of the switch button is electrically connected with the input end of the electromagnet panel.
Preferably, a through inner groove is formed outside the coupling, and the through inner groove and the main body carrier are integrally formed.
Preferably, two the bottom of activity pole setting all is provided with the connecting bottom plate, and connecting bottom plate and activity pole setting integrated into one piece set up, two connecting bottom plates pass through the screw respectively with wireless network camera and infrared imaging camera fixed connection.
Preferably, the monitoring method of the monitoring device on board of the unmanned aerial vehicle with the thermal imaging function includes the following steps:
the method comprises the following steps: the horizontal frame rod is longitudinally adjusted in a mode that the connecting bottom block moves in the internal sliding chute, and after the longitudinal adjustment is finished, a switch button is pressed to supply power to the electromagnet panel to generate magnetic force so as to adsorb and fix the idler wheel;
step two: after the longitudinal adjustment is finished, the mounting top plate is driven to move to a proper position for transverse adjustment through the sliding sleeve of the sleeve sliding block and the guide sliding rail, and the mounting top plate is connected to the bottom connecting frame of the unmanned aerial vehicle after the adjustment is finished;
step three: then two clamping sleeve frames are arranged on the guide slide rail in a group, so that the clamping sleeve frames limit the adjusting position of the sleeve slide block, and the connecting pins are fixedly connected with the cathode magnet inside the inserting groove in an adsorption manner through the anode magnet during installation;
step four: after all the installation is finished, the wireless network camera and the infrared imaging camera are driven by the unmanned aerial vehicle to carry out mobile flight monitoring, and the wireless network camera and the infrared imaging camera respectively upload a real-time picture and an infrared thermal imaging picture to the screen splitting display for screen splitting display;
step five: in the monitoring process, the position adjusting motor is controlled to rotate through the remote control handle, and then the movable vertical rod is driven to rotate and adjust, so that the wireless network camera and the infrared imaging camera move to the direction to be monitored to perform real-time monitoring.
Compared with the prior art, the invention has the beneficial effects that:
1. the wireless network camera and the infrared imaging camera are driven by the unmanned aerial vehicle to carry out mobile flight monitoring, the wireless network camera and the infrared imaging camera respectively upload a real-time picture and an infrared thermal imaging picture to the screen splitting display to be displayed in a split screen mode, in the monitoring process, the positioning motor is controlled to rotate through the remote control handle, and then the movable vertical rod is driven to rotate and adjust, so that the wireless network camera and the infrared imaging camera move to the direction needing to be monitored to carry out real-time monitoring, and the problems that the existing unmanned aerial vehicle monitoring device only can monitor the real-time picture of the area where the unmanned aerial vehicle is located in the using process, and the monitoring range is small are solved.
2. Carry out vertical regulation with horizontal hack lever through the mode of connecting the bottom block in the inside activity of internal connection spout, vertically adjust the back of accomplishing, press shift knob and produce magnetic force for the power supply of electro-magnet panel, adsorb fixed roller, earlier carry out vertical regulation with horizontal hack lever through the mode of connecting the bottom block in the inside activity of internal connection spout, vertically adjust the back of accomplishing, press shift knob and produce magnetic force for the power supply of electro-magnet panel, adsorb fixed roller, reach the effect of horizontal regulation and vertical regulation be convenient for and unmanned aerial vehicle connection installation, the problem that current unmanned aerial vehicle monitoring device is relatively poor at the in-process installation adjustability that uses has been overcome
Drawings
Fig. 1 is a schematic view of the overall structure of an on-board monitoring device of an unmanned aerial vehicle with a thermal imaging function according to the invention;
FIG. 2 is a schematic view of the internal structure of the inscribed chute of the present invention;
FIG. 3 is a schematic view of the internal structure of the horizontal frame rod of the present invention;
FIG. 4 is a schematic view of the positioning frame of the present invention;
FIG. 5 is a schematic view of the connection structure of the positioning motor of the present invention;
fig. 6 is a schematic view of a working flow of the on-board monitoring apparatus of the unmanned aerial vehicle with thermal imaging function according to the present invention;
in the figure: 1. a main body carrier; 2. a movable vertical rod; 3. connecting the bottom plate; 4. a wireless network camera; 5. an infrared imaging camera; 6. a positioning motor; 7. an alternating current mobile power supply; 8. a switch button; 9. a suspension plate; 10. the sliding groove is connected in an internal manner; 11. connecting the bottom block; 12. a horizontal frame bar; 13. an end face groove; 14. sleeving a sliding block; 15. an extension rod; 16. installing a top plate; 17. a clamping groove; 18. lining a fixture block; 19. a supporting bottom groove; 20. a roller; 21. an electromagnet panel; 22. a bearing; 23. a guide slide rail; 24. a clamping sleeve frame; 25. inserting grooves; 26. connecting pins; 27. a positive magnet; 28. a negative magnet; 29. the inner groove is penetrated; 30. a drive shaft; 31. a connecting shaft; 32. a coupling; 33. a remote control handle; 34. a receiver; 35. a router; 36. a hard disk video recorder; 37. and (5) displaying the split screen.
Detailed Description
The technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only a part of the embodiments of the present invention, and not all of the embodiments.
Referring to fig. 1-6, an embodiment of the present invention is shown: an unmanned aerial vehicle airborne monitoring device with a thermal imaging function comprises a main body carrier 1, a remote control handle 33 and a screen divider 37, wherein two movable vertical rods 2 are arranged at the lower end of the main body carrier 1, and an alternating current mobile power supply 7 and a switch button 8 are arranged on the front end face of the main body carrier 1;
further comprising:
the wireless network camera 4 and the infrared imaging camera 5 are respectively installed at the lower end positions of the two movable upright stanchions 2, the positioning motors 6 are respectively arranged above the two movable upright stanchions 2, the output ends of the positioning motors 6 are provided with transmission shafts 30, the tops of the movable upright stanchions 2 are provided with connecting shafts 31, the inside of the main body carrier 1 is provided with couplings 32, and the transmission shafts 30 are movably connected with the connecting shafts 31 through the couplings 32;
a suspension plate 9 arranged at the upper end position of the main body carrier 1, wherein the suspension plate 9 and the main body carrier 1 are integrally formed, an internal connecting sliding groove 10 is arranged inside the suspension plate 9, and a connecting bottom block 11 is arranged inside the internal connecting sliding groove 10;
the horizontal hack lever 12 is arranged at the upper end of the connecting bottom block 11, the horizontal hack lever 12 and the connecting bottom block 11 are integrally formed, an end surface groove 13 is arranged inside the horizontal hack lever 12, a guide slide rail 23 is arranged inside the end surface groove 13, two sleeve connection slide blocks 14 are arranged outside the guide slide rail 23, an extension rod 15 is arranged at the upper end of each sleeve connection slide block 14, a mounting top plate 16 is arranged at the top of each extension rod 15, and the mounting top plate 16 and the extension rods 15 are both integrally formed with the sleeve connection slide blocks 14;
the router 35 and the hard disk video recorder 36 are arranged at one side of the sub-screen display 37, the output ends of the wireless network camera 4 and the infrared imaging camera 5 are in transmission connection with the input end of the router 35, the output end of the router 35 is in transmission connection with the input end of the hard disk video recorder 36, and the output end of the hard disk video recorder 36 is in transmission connection with the input end of the sub-screen display 37.
Referring to fig. 2, a locking groove 17 is formed on an inner wall of the inner sliding groove 10, the locking groove 17 and the inner sliding groove 10 are integrally formed, an inner lining locking block 18 is disposed inside the locking groove 17, the inner lining locking block 18 and the connecting bottom block 11 are integrally formed, and the locking groove 17 formed on the inner wall of the inner sliding groove 10 plays a role in locking and releasing.
Referring to fig. 2, a supporting bottom groove 19 is disposed at the bottom of the connecting bottom block 11, a roller 20 is disposed inside the supporting bottom groove 19, bearings 22 are disposed on inner walls of two sides of the supporting bottom groove 19, and rotating shafts on outer walls of two sides of the roller 20 are movably connected to the bearings 22.
Referring to fig. 3 and 4, two clamping sleeve frames 24 are respectively installed at two end positions of the sleeve sliding block 14, insertion grooves 25 are respectively installed on outer walls of two sides of the guide sliding rail 23, the insertion grooves 25 and the guide sliding rail 23 are integrally formed, connecting pins 26 are arranged inside the insertion grooves 25, and the connecting pins 26 and the clamping sleeve frames 24 are integrally formed.
Referring to fig. 4, a positive magnet 27 and a negative magnet 28 are disposed at the connection position of the connection pin 26 and the insertion groove 25, and the positive magnet 27 and the negative magnet 28 are integrally formed with the connection pin 26 and the insertion groove 25, respectively.
Referring to fig. 6, a receiver 34 is disposed inside the housing of the positioning motor 6, an output end of the remote control handle 33 is in transmission connection with an input end of the receiver 34, and an output end of the receiver 34 is in transmission connection with an input end of the positioning motor 6.
Referring to fig. 2 and 6, an electromagnet panel 21 is disposed on an inner wall of the internal connecting chute 10, an output end of the ac mobile power supply 7 is electrically connected to input ends of the positioning motor 6, the switch button 8, the wireless network camera 4 and the infrared imaging camera 5, an output end of the switch button 8 is electrically connected to an input end of the electromagnet panel 21, and the electromagnet panel 21 disposed on the inner wall of the internal connecting chute 10 plays a role of adsorbing the roller 20.
Referring to fig. 5, the coupler 32 is provided with an inner through groove 29 on the outside thereof, the inner through groove 29 is integrally formed with the main body carrier 1, and the inner through groove 29 provided on the outside of the coupler 32 serves to support the coupler 32.
Referring to fig. 1, the bottom of each of the two movable vertical rods 2 is provided with a connecting bottom plate 3, the connecting bottom plates 3 and the movable vertical rods 2 are integrally formed, the two connecting bottom plates 3 are respectively and fixedly connected with a wireless network camera 4 and an infrared imaging camera 5 through screws, and the connecting bottom plates 3 arranged at the bottom of each of the two movable vertical rods 2 play a role in facilitating connection of the wireless network camera 4 and the infrared imaging camera 5.
Referring to fig. 1-6, a monitoring method of an on-board monitoring device of an unmanned aerial vehicle with thermal imaging function includes the following steps:
the method comprises the following steps: firstly, the horizontal frame rod 12 is longitudinally adjusted in a mode that the connecting bottom block 11 moves in the internal connecting chute 10, and after the longitudinal adjustment is finished, the switch button 8 is pressed to supply power to the electromagnet panel 21 to generate magnetic force so as to adsorb the fixed idler wheel 20;
step two: after the longitudinal adjustment is finished, the mounting top plate 16 is driven to move to a proper position through the sliding sleeve of the sleeve sliding block 14 and the guide sliding rail 23 for transverse adjustment, and after the adjustment is finished, the mounting top plate 16 is connected to the bottom connecting frame of the unmanned aerial vehicle;
step three: then two clamping sleeve frames 24 are assembled on the guide slide rail 23 in a group, so that the clamping sleeve frames 24 limit the adjusting position of the sleeve sliding block 14, and the connecting pins 26 are fixedly connected with the cathode magnet 28 in the insertion groove 25 through the anode magnet 27 in an adsorption manner during assembly;
step four: after all the installation is finished, the wireless network camera 4 and the infrared imaging camera 5 are driven by the unmanned aerial vehicle to carry out mobile flight monitoring, and the wireless network camera 4 and the infrared imaging camera 5 respectively upload a real-time picture and an infrared thermal imaging picture to the screen splitting display 37 for screen splitting display;
step five: in the monitoring process, the positioning motor 6 is controlled to rotate through the remote control handle 33, and then the movable vertical rod 2 is driven to rotate and adjust, so that the wireless network camera 4 and the infrared imaging camera 5 move to the direction to be monitored to perform real-time monitoring.
It will be evident to those skilled in the art that the invention is not limited to the details of the foregoing illustrative embodiments, and that the present invention may be embodied in other specific forms without departing from the spirit or essential attributes thereof. The present embodiments are therefore to be considered in all respects as illustrative and not restrictive, the scope of the invention being indicated by the appended claims rather than by the foregoing description, and all changes which come within the meaning and range of equivalency of the claims are therefore intended to be embraced therein. Any reference sign in a claim should not be construed as limiting the claim concerned.
Claims (10)
1. An unmanned aerial vehicle airborne monitoring device with a thermal imaging function comprises a main body carrier (1), a remote control handle (33) and a screen divider display (37), wherein two movable upright rods (2) are arranged at the lower end of the main body carrier (1), and an alternating-current mobile power supply (7) and a switch button (8) are arranged on the front end surface of the main body carrier (1);
the method is characterized in that: further comprising:
the wireless network camera (4) and the infrared imaging camera (5) are respectively installed at the lower end positions of the two movable vertical rods (2), a position adjusting motor (6) is arranged above each of the two movable vertical rods (2), a transmission shaft (30) is arranged at the output end of each position adjusting motor (6), a connecting shaft (31) is arranged at the top of each movable vertical rod (2), a coupler (32) is arranged inside the main body carrier frame (1), and the transmission shaft (30) is movably connected with the connecting shaft (31) through the coupler (32);
the suspension plate (9) is arranged at the upper end of the main body carrier (1), the suspension plate (9) and the main body carrier (1) are integrally formed, an internal connection sliding groove (10) is arranged in the suspension plate (9), and a connection bottom block (11) is arranged in the internal connection sliding groove (10);
the horizontal hack lever (12) is arranged at the upper end of the connecting bottom block (11), the horizontal hack lever (12) and the connecting bottom block (11) are integrally formed, an end surface groove (13) is arranged inside the horizontal hack lever (12), a guide slide rail (23) is arranged inside the end surface groove (13), two sleeving sliders (14) are arranged outside the guide slide rail (23), an extension rod (15) is arranged at the upper end of each sleeving slider (14), a mounting top plate (16) is arranged at the top of each extension rod (15), and the mounting top plate (16) and the extension rods (15) are integrally formed with the sleeving sliders (14);
the router comprises a router (35) and a hard disk video recorder (36), wherein the router is arranged on one side of the screen dividing display (37), the output ends of the wireless network camera (4) and the infrared imaging camera (5) are in transmission connection with the input end of the router (35), the output end of the router (35) is in transmission connection with the input end of the hard disk video recorder (36), and the output end of the hard disk video recorder (36) is in transmission connection with the input end of the screen dividing display (37).
2. The on-board monitoring device of a drone with thermal imaging capability of claim 1, characterized in that: be provided with screens groove (17) on the inner wall of inscription spout (10), screens groove (17) and inscription spout (10) integrated into one piece set up, the inside in screens groove (17) is provided with inside lining fixture block (18), and inside lining fixture block (18) set up with being connected bottom block (11) integrated into one piece.
3. The on-board monitoring device of a drone with thermal imaging capability of claim 2, characterized in that: the bottom of connecting bottom block (11) is provided with the support and carries kerve (19), the inside that the support carried kerve (19) is provided with gyro wheel (20), all be provided with bearing (22) on the support carries both sides inner wall of kerve (19), pivot on the outer wall of gyro wheel (20) both sides all with bearing (22) swing joint.
4. The airborne monitoring apparatus of unmanned aerial vehicle with thermal imaging function of claim 3, characterized in that: two clamping sleeve frames (24) are installed at two ends of the sleeve connection sliding block (14), insertion grooves (25) are formed in outer walls of two sides of the guide sliding rail (23), the insertion grooves (25) and the guide sliding rail (23) are integrally formed, connection pins (26) are arranged in the insertion grooves (25), and the connection pins (26) and the clamping sleeve frames (24) are integrally formed.
5. The on-board monitoring device of a drone with thermal imaging capability of claim 4, characterized in that: and the connecting position of the connecting pin (26) and the inserting groove (25) is provided with a positive magnet (27) and a negative magnet (28), and the positive magnet (27) and the negative magnet (28) are respectively integrally formed with the connecting pin (26) and the inserting groove (25).
6. The on-board monitoring device of a drone with thermal imaging capability of claim 5, characterized in that: a receiver (34) is arranged in a shell of the positioning motor (6), the output end of the remote control handle (33) is in transmission connection with the input end of the receiver (34), and the output end of the receiver (34) is in transmission connection with the input end of the positioning motor (6).
7. The airborne monitoring apparatus of unmanned aerial vehicle with thermal imaging function of claim 6, characterized in that: the inner wall of the internal connection sliding groove (10) is provided with an electromagnet panel (21), the output end of the alternating-current mobile power supply (7) is electrically connected with the input ends of the positioning motor (6), the switch button (8), the wireless network camera (4) and the infrared imaging camera (5), and the output end of the switch button (8) is electrically connected with the input end of the electromagnet panel (21).
8. The on-board monitoring device of a drone with thermal imaging capability of claim 7, characterized in that: a through inner groove (29) is formed in the outer portion of the coupler (32), and the through inner groove (29) and the main body carrier (1) are integrally formed.
9. The on-board monitoring device of a drone with thermal imaging capability of claim 8, characterized in that: two the bottom of activity pole setting (2) all is provided with connecting bottom plate (3), connects bottom plate (3) and activity pole setting (2) integrated into one piece setting, two connect bottom plate (3) through the screw respectively with wireless network camera (4) and infrared imaging camera (5) fixed connection.
10. The monitoring method of the monitoring device with thermal imaging function on board the unmanned aerial vehicle as claimed in claim 9, comprising the steps of:
the method comprises the following steps: the horizontal frame rod (12) is longitudinally adjusted in a mode that the connecting bottom block (11) moves in the internal sliding chute (10), and after the longitudinal adjustment is finished, a switch button (8) is pressed to supply power to an electromagnet panel (21) to generate magnetic force so as to adsorb a fixed roller (20);
step two: after the longitudinal adjustment is finished, the mounting top plate (16) is driven to move to a proper position for transverse adjustment through the sliding sleeve of the sleeve sliding block (14) and the guide sliding rail (23), and the mounting top plate (16) is connected to the unmanned aerial vehicle bottom connection frame after the adjustment is finished;
step three: then two clamping sleeve frames (24) are arranged on the guide slide rail (23) in a group, so that the clamping sleeve frames (24) limit the adjusting position of the sleeve slide block (14), and the connecting pins (26) are fixedly connected with the cathode magnet (28) in the insertion groove (25) in an adsorption manner through the anode magnet (27) during installation;
step four: after all the installation is finished, the wireless network camera (4) and the infrared imaging camera (5) are driven by the unmanned aerial vehicle to carry out mobile flight monitoring, and the wireless network camera (4) and the infrared imaging camera (5) respectively upload a real-time picture and an infrared thermal imaging picture to the screen display (37) for split screen display;
step five: in the monitoring process, the position adjusting motor (6) is controlled to rotate through the remote control handle (33), and then the movable vertical rod (2) is driven to rotate and adjust, so that the wireless network camera (4) and the infrared imaging camera (5) move to the direction needing to be monitored to perform real-time monitoring.
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