CN219428396U

CN219428396U - Unmanned automatic inspection device

Info

Publication number: CN219428396U
Application number: CN202320857611.2U
Authority: CN
Inventors: 任伟; 尹必勇; 朱彬
Original assignee: Shanghai Hyatt Construction Consulting And Supervision Co ltd
Current assignee: Shanghai Hyatt Construction Consulting And Supervision Co ltd
Priority date: 2023-04-14
Filing date: 2023-04-14
Publication date: 2023-07-28
Anticipated expiration: 2033-04-14

Abstract

The application discloses unmanned automatic tour device relates to unmanned tour equipment technical field. The utility model provides an aircraft main part, the bottom fixedly connected with install bin of aircraft main part, the inside sliding connection of install bin has the inspection glass, and the inside symmetry sliding connection of install bin has the drive plate, the top fixedly connected with of drive plate and the fixture block of inspection glass adaptation, the spout has been seted up to the bottom symmetry of install bin, the inside sliding connection of spout has the slide, the one end of slide is inconsistent with the drive plate. This application is through setting up the cooperation use of drive plate and slide, when the sensor that is out of control induces the aircraft main part and is in out of control the time, through starting the inside that the lift subassembly drive inspection mirror contracted into the mounting box to make two slides receive protection spring's rebound ejecting, form the cover to the mounting box bottom, with this when the aircraft main part is in out of control the state, automatic formation is to the protection of inspection mirror, has effectively improved the security of device.

Description

Unmanned automatic inspection device

Technical Field

The application relates to the technical field of unmanned inspection equipment, in particular to an unmanned automatic inspection device.

Background

The agricultural inspection unmanned aerial vehicle comprises two types of unmanned aerial vehicles, namely a direct-drive unmanned aerial vehicle and a multi-rotor unmanned aerial vehicle, and can be controlled by ground remote control or navigation flight control. Along with the development of science and technology, especially the development of battery technology has driven unmanned aerial vehicle market's expansion rapidly, and more people begin to use unmanned aerial vehicle to carry out pesticide and spray the operation, because unmanned aerial vehicle sprays pesticide not only labour saving and time saving, practice thrift the cost moreover, receive vast peasant's liking.

Because the area is comparatively broad in modern farmland inspection area, it is also comparatively complicated to relate to the topography, inspection unmanned aerial vehicle flies out controllable scope easily when carrying out the work to lead to unmanned aerial vehicle to appear the condition out of control, and general agricultural inspection unmanned aerial vehicle's inspection lens is direct fixation in the bottom of aircraft, so as to obtain better inspection field of vision, just so makes inspection unmanned aerial vehicle drive inspection lens when out of control and produce violent collision so as to damage the camera lens easily, produces great loss.

Disclosure of Invention

The purpose of the present application is: for solving general agricultural inspection unmanned aerial vehicle's inspection lens is the direct fixation in the bottom of aircraft, just so makes inspection unmanned aerial vehicle drive inspection lens when out of control and produce violent collision like this to damage the camera lens, produce the problem of great loss, this application provides an unmanned automatic inspection device.

The application specifically adopts the following technical scheme for realizing the purposes:

the utility model provides an unmanned automatic device of patrolling, includes the aircraft main part, the bottom fixedly connected with mounting box of aircraft main part, the inside sliding connection of mounting box has the inspection mirror, just the inside symmetry sliding connection of mounting box has the drive plate, the top fixedly connected with of drive plate and the fixture block of inspection mirror adaptation, the spout has been seted up to the bottom symmetry of mounting box, the inside sliding connection of spout has the slide, the one end and the drive plate of slide are in contact, just the other end fixedly connected with a plurality of protection spring of slide, protection spring installs the inside at the spout, the mounting groove with the inside intercommunication of mounting box has been seted up to the one end of aircraft main part, the internally mounted of mounting groove has lifting unit, the sensor out of control is installed at the top of aircraft main part.

Through adopting above-mentioned technical scheme, through setting up the cooperation use of drive plate and slide, when the sensor that out of control sensed the aircraft main part and be in out of control the inside that the installation case was gone into in the drive of lift subassembly, and make two slides receive protection spring's resilience ejecting, form the cover to the installation case bottom, with this when the aircraft main part is in out of control the protection to the inspection glass of automatic formation, effectively improved the security of device.

Further, the lifting assembly comprises a lifting motor fixedly connected inside the mounting groove, a gear is fixedly connected to the output end of the lifting motor, and a rack meshed with the gear is fixedly connected to one end of the inspection glass.

Through adopting above-mentioned technical scheme, through setting up the cooperation use of gear and rack for start elevator motor can drive the inspection glass and remove along the length direction of install bin.

Further, the top of the clamping block is symmetrically and fixedly connected with an ejection spring, and one end of the ejection spring is fixedly connected with the mounting box.

Through adopting above-mentioned technical scheme, through setting up ejecting spring, effectively strengthened the conflict effect of drive plate and slide.

Further, rubber pads are symmetrically and fixedly connected inside the mounting box.

Through adopting above-mentioned technical scheme, can form the protection to the both sides of inspection glass through setting up the rubber pad, alleviate the vibrations that inspection glass received, improved the protection effect of device.

Further, the inspection glass includes the mirror body of sliding connection in the installation box inside, the camera lens is installed to the bottom of mirror body, just the bottom symmetry rotation of mirror body is connected with the connecting block, arc scraper blade is installed to the one end of connecting block, the outer wall laminating of arc scraper blade and camera lens, the bottom fixedly connected with driving motor of mirror body, the output of driving motor and the connecting axle head fixed connection of elasticity fixture block.

Through adopting above-mentioned technical scheme, through setting up the cooperation use of driving motor and connecting block for start driving motor and can drive arc scraper blade and scrape the clearance along the surface of camera lens, effectively reduce the foreign matter adhesion at the surface of camera lens.

Further, one side of the connecting block is fixedly connected with an elastic clamping block, and clamping holes matched with the elastic clamping block are symmetrically formed in one end of the arc-shaped scraping plate.

Through adopting above-mentioned technical scheme, through setting up the cooperation use of elasticity fixture block and draw-in hole, be convenient for realize the change to arc scraper blade, improved the practicality of device.

Further, the binding face of the arc scraping plate and the lens is fixedly connected with a wool pad.

Through adopting above-mentioned technical scheme, through setting up the cooperation of wool pad and arc scraper blade and using, effectively alleviateed the wearing and tearing of arc scraper blade to the camera lens.

Further, supporting legs are symmetrically and fixedly connected to the bottom of the mounting box, and foot rest shock pads are arranged at the bottoms of the supporting legs.

Through adopting above-mentioned technical scheme, through setting up the cooperation use of supporting legs and foot rest shock pad, effectively improved the stability of aircraft main part when the landing.

In summary, the present application includes at least one of the following beneficial effects:

1. through setting up the cooperation use of drive plate and slide, when the sensor that is out of control induces the aircraft main part and is in out of control the inside that the sight glass contracted into the mounting box is driven through starting lifting unit to make two slides receive protection spring's resilience ejecting, form the cover to the mounting box bottom, with this when the aircraft main part is in out of control the state, automatic formation is to the protection of sight glass, has effectively improved the security of device.

2. Through setting up the cooperation use of driving motor and connecting block for start driving motor and can drive the arc scraper blade and scrape the clearance along the surface of camera lens, effectively reduce the adhesion of foreign matter on the surface of camera lens.

Drawings

Fig. 1 is a schematic perspective view of a device body in the present application.

Fig. 2 is a side cross-sectional view of the aircraft body of the present application.

Fig. 3 is a schematic view of the internal structure of the mounting box in the present application.

Fig. 4 is a schematic perspective view of the inspection mirror in the present application.

Reference numerals illustrate:

1. an aircraft body; 2. a mounting box; 3. a viewing mirror; 4. a drive plate; 5. a clamping block; 6. a chute; 7. a slide plate; 8. a protective spring; 9. a mounting groove; 10. a lifting assembly; 11. a runaway sensor; 12. an ejector spring; 13. a rubber pad; 14. a connecting block; 15. an arc-shaped scraping plate; 16. a drive motor; 17. an elastic clamping block; 18. a clamping hole; 19. a wool pad; 20. supporting feet; 31. a mirror body; 32. a lens; 101. a lifting motor; 102. a gear; 103. a rack.

Detailed Description

The present application is described in further detail below in conjunction with figures 1-4.

The embodiment of the application discloses an unmanned automatic inspection device.

Referring to fig. 1-3, an unmanned automatic inspection device comprises an aircraft main body 1, wherein an installation box 2 is fixedly connected to the bottom of the aircraft main body 1, an inspection mirror 3 is connected to the inside of the installation box 2 in a sliding manner, a transmission plate 4 is symmetrically and slidingly connected to the inside of the installation box 2, a clamping block 5 adapted to the inspection mirror 3 is fixedly connected to the top of the transmission plate 4, a sliding groove 6 is symmetrically formed in the bottom of the installation box 2, a sliding plate 7 is slidingly connected to the inside of the sliding groove 6, one end of the sliding plate 7 is abutted to the transmission plate 4, a plurality of protection springs 8 are fixedly connected to the other end of the sliding plate 7, the protection springs 8 are installed in the sliding groove 6, an installation groove 9 communicated with the inside of the installation box 2 is formed in one end of the aircraft main body 1, a lifting assembly 10 is installed in the inside of the installation groove 9, an out-of-control sensor 11 is installed at the top of the aircraft main body 1, and a rubber pad 13 is symmetrically and fixedly connected to the inside of the installation box 2. Firstly, whether the flying gesture of the aircraft main body 1 is out of control or not is sensed by the out-of-control sensor 11, when the flying gesture of the aircraft main body 1 is out of control, a lifting signal is automatically sent to the lifting component 10, the inspection mirror 3 is driven to retract into the inside of the installation box 2 through the lifting component 10, meanwhile, the inspection mirror 3 forms interference to the clamping block 5 when retracting into the inside of the installation box 2, one end of the driving plate 4 is pushed by the clamping block 5 to separate from the interference with the sliding plate 7 along the length direction of the installation box 2, then the protection spring 8 is enabled to rebound to push out the sliding plate 7 along the length direction of the sliding groove 6, and the two sliding plates 7 are enabled to do mutual approaching movements along the length direction of the sliding groove 6, so that the bottom of the installation box 2 is covered, the inspection mirror 3 can be automatically retracted into the inside of the installation box 2 when the aircraft main body 1 is out of control, meanwhile, the bottom of the installation box 2 is covered by reducing foreign matters, damage is caused to the inspection mirror 3, and the safety of the device is effectively improved.

Referring to fig. 2 and 3, the lifting assembly 10 includes a lifting motor 101 fixedly connected to the inside of the installation groove 9, a gear 102 is fixedly connected to an output end of the lifting motor 101, and a rack 103 engaged with the gear 102 is fixedly connected to one end of the inspection glass 3. The lifting motor 101 is started to drive the gear 102 to rotate, the gear 102 is meshed with the rack 103, and meanwhile the rack 103 drives the inspection mirror 3 to move along the length direction of the installation box 2, so that lifting driving of the inspection mirror 3 is completed.

Referring to fig. 1 and 2, the top of the clamping block 5 is symmetrically and fixedly connected with an ejection spring 12, and one end of the ejection spring 12 is fixedly connected with the mounting box 2. The ejection spring 12 can form interference to the clamping block 5, so that the situation that the transmission plate 4 is loosened due to interference with the sliding plate 7 is reduced.

Referring to fig. 3 and 4, the inspection glass 3 includes a glass body 31 slidably connected inside the installation box 2, a lens 32 is installed at the bottom of the glass body 31, a connecting block 14 is symmetrically and rotatably connected to the bottom of the glass body 31, an arc-shaped scraping plate 15 is installed at one end of the connecting block 14, the arc-shaped scraping plate 15 is attached to the outer wall of the lens 32, a driving motor 16 is fixedly connected to the bottom of the glass body 31, and the output end of the driving motor 16 is fixedly connected with the connecting shaft end of the elastic clamping block 17. Can drive connecting block 14 through starting driving motor 16 and drive arc scraper blade 15 and rotate around the handing-over axle to make the inside and the camera lens 32 laminating of arc scraper blade 15 scrape the foreign matter of camera lens 32 surface adhesion simultaneously, so that the realization is clear away camera lens 32 surface foreign matter, make the inspection of camera lens 32 more clear.

Referring to fig. 3 and 4, an elastic clamping block 17 is fixedly connected to one side of the connecting block 14, and clamping holes 18 adapted to the elastic clamping block 17 are symmetrically formed in one end of the arc-shaped scraping plate 15. The elastic clamping blocks 17 are separated from the inside of the clamping holes 18 by extrusion, so that the clamping connection between the arc-shaped scraping plates 15 and the connecting blocks 14 is released, the arc-shaped scraping plates 15 are replaced conveniently, and the practicability of the device is improved.

Referring to fig. 3 and 4, a pile pad 19 is fixedly connected to the contact surface of the arcuate blade 15 and the lens 32. By providing the flock pad 19 such that the arcuate blade 15 is in flexible contact with the surface of the lens 32, wear of the lens 32 is reduced.

Referring to fig. 1 and 3, supporting feet 20 are symmetrically and fixedly connected to the bottom of the mounting box 2, and foot rest shock pads are arranged at the bottoms of the supporting feet 20. Through setting up the cooperation use of supporting legs 20 and foot rest shock pad for aircraft main part 1 obtains certain buffering when descending, thereby makes the descending of aircraft main part 1 more stable.

The implementation principle of the unmanned automatic inspection device in the embodiment is as follows: firstly, a runaway sensor 11 is arranged to sense whether the flying gesture of the aircraft body 1 is out of control, when the flying gesture of the aircraft body 1 is out of control, a lifting signal is automatically sent to a lifting assembly 10, a lifting motor 101 is started to drive a gear 102 to rotate, the gear 102 is meshed with a rack 103, meanwhile, the rack 103 drives a patrol mirror 3 to form interference to a clamping block 5 when retracting into the installation box 2, one end of a transmission plate 4 is pushed by the clamping block 5 to be separated from interference with a sliding plate 7 along the length direction of the installation box 2, then a protection spring 8 is enabled to rebound to push out the sliding plate 7 along the length direction of a sliding groove 6, and the two sliding plates 7 are enabled to move close to each other along the length direction of the sliding groove 6, so that the bottom of the installation box 2 is covered;

meanwhile, the driving motor 16 is started in the flight process, the connecting block 14 can be driven to drive the arc scraping plate 15 to rotate around the connecting shaft, the inside of the arc scraping plate 15 is attached to the lens 32, and meanwhile, foreign matters adhered to the surface of the lens 32 are scraped, so that the foreign matters on the surface of the lens 32 are conveniently removed, and the inspection of the lens 32 is clearer.

Claims

1. An unmanned automatic tour device, includes aircraft main part (1), its characterized in that: the utility model provides a bottom fixedly connected with install bin (2) of aircraft main part (1), the inside sliding connection of install bin (2) has inspection glass (3), just the inside symmetry sliding connection of install bin (2) has drive plate (4), the top fixedly connected with of drive plate (4) and fixture block (5) of inspection glass (3) adaptation, spout (6) have been seted up to the bottom symmetry of install bin (2), the inside sliding connection of spout (6) has slide (7), the one end and the drive plate (4) of slide (7) are inconsistent, just the other end fixedly connected with of slide (7) a plurality of protection spring (8), protection spring (8) install the inside at spout (6), mounting groove (9) with inside intercommunication of install bin (2) are seted up to the one end of aircraft main part (1), internally mounted of mounting groove (9) has lifting unit (10), the sensor (11) out of control are installed at the top of aircraft main part (1).

2. An unmanned automatic tour device according to claim 1, wherein: lifting assembly (10) are including fixed connection at inside elevator motor (101) of mounting groove (9), the output fixedly connected with gear (102) of elevator motor (101), the one end fixedly connected with of inspection glass (3) and rack (103) of gear (102) meshing.

3. An unmanned automatic tour device according to claim 1, wherein: the top of the clamping block (5) is symmetrically and fixedly connected with an ejection spring (12), and one end of the ejection spring (12) is fixedly connected with the mounting box (2).

4. An unmanned automatic tour device according to claim 1, wherein: rubber pads (13) are symmetrically and fixedly connected in the installation box (2).

5. An unmanned automatic tour device according to claim 1, wherein: the inspection glass (3) comprises a glass body (31) which is slidably connected inside an installation box (2), a lens (32) is installed at the bottom of the glass body (31), a connecting block (14) is symmetrically connected with the bottom of the glass body (31) in a rotating mode, an arc-shaped scraping plate (15) is installed at one end of the connecting block (14), the arc-shaped scraping plate (15) is attached to the outer wall of the lens (32), a driving motor (16) is fixedly connected to the bottom of the glass body (31), and the output end of the driving motor (16) is fixedly connected with the connecting shaft end of an elastic clamping block (17).

6. An unmanned automatic tour device according to claim 5, wherein: one side of the connecting block (14) is fixedly connected with an elastic clamping block (17), and clamping holes (18) matched with the elastic clamping block (17) are symmetrically formed in one end of the arc-shaped scraping plate (15).

7. An unmanned automatic tour device according to claim 5, wherein: the pile pad (19) is fixedly connected with the joint surface of the arc scraping plate (15) and the lens (32).

8. An unmanned automatic tour device according to claim 1, wherein: the bottom of the installation box (2) is symmetrically and fixedly connected with supporting legs (20), and foot rest shock pads are arranged at the bottoms of the supporting legs (20).