Intelligent safety construction monitoring equipment applied to unmanned aerial vehicle

Abstract

The utility model relates to the technical field of detection unmanned aerial vehicles, and provides an intelligent safety construction monitoring device applied to an unmanned aerial vehicle, which comprises an unmanned aerial vehicle main body and a monitoring camera fixedly mounted at the bottom of the unmanned aerial vehicle main body, a protection mechanism is arranged at the bottom of the unmanned aerial vehicle main body, and the protection mechanism comprises a movable shell, a cleaning mechanism is arranged on the inner side wall of the movable shell, an unmanned aerial vehicle falling buffering mechanism is further arranged at the bottom of the unmanned aerial vehicle body, and the cleaning mechanism comprises a semicircular sliding groove formed in the inner side wall of the movable shell and two sliding blocks which are connected into the semicircular sliding groove in a relatively sliding mode. A motor is started to drive a gear to rotate, and a semicircular toothed plate in linkage meshing connection drives a movable shell to slide on a circular sliding rail, so that the movable shell is adjusted out of the interior of a fixed shell and relatively coincides with the fixed shell, sealing protection is effectively performed when the monitoring camera is not used, and the monitoring camera is prevented from being collided and scratched; therefore, the service life of the monitoring camera is prolonged.

Description

TECHNICAL FIELD

[0001] The utility model discloses detection unmanned plane technical field, concretely in an application to the intelligent safe construction monitoring equipment for unmanned plane. BACKGROUND

[0002] The important significance of construction progress monitoring is to monitor the construction progress, timely find the progress deviation and analyze the causes of deviation and its influence on subsequent work and total duration, take corresponding measures if necessary to ensure the realization of progress target.

[0003] For example, the existing public patent: CN215851880U discloses a kind of unmanned plane for construction progress monitoring, including unmanned plane body, the upper surface of unmanned plane body is provided with transmitter, the lower side of unmanned plane body is provided with detection camera, detection camera is fixedly connected with connecting rod on the side surface of unmanned plane body facing, the lower surface of unmanned plane body is fixedly connected with mounting block, the upper end of connecting rod is fixedly connected with first movable ball, the side surface of mounting block facing connecting rod is provided with first movable slot, and unmanned plane body is provided with stabilizing mechanism.

[0004] However, in the implementation of the related technology, the above-mentioned unmanned plane for construction progress monitoring has the following problems: it is difficult to seal and protect the monitoring camera when not in use, and it is not convenient to wipe and clean the monitoring camera, which can easily cause the monitoring camera to collide and scratch, thereby reducing the clarity and service life of the monitoring camera. Therefore, an intelligent safe construction monitoring equipment applied to unmanned plane is proposed. UTILITY MODEL CONTENTS

[0005] The utility model discloses an intelligent safe construction monitoring equipment applied to unmanned plane, which solves the problem of difficult sealing and protection of the monitoring camera when not in use in the related technology, and inconvenient wiping and cleaning of the monitoring camera, which can easily cause the monitoring camera to collide and scratch, thereby reducing the clarity and service life of the monitoring camera.

[0006] The technical scheme of the utility model is as follows: an intelligent safe construction monitoring equipment applied to unmanned plane, comprising: unmanned plane body and monitoring camera fixedly installed at the bottom of the unmanned plane body.

[0007] The bottom of the unmanned plane body is provided with a protection mechanism, the protection mechanism comprises a movable shell, the inner side wall of the movable shell is provided with a cleaning mechanism, and the bottom of the unmanned plane body is further provided with a falling buffer mechanism.

[0008] The cleaning mechanism comprises a semicircular chute formed in the inner side wall of the movable shell, two sliding blocks connected to the inside of the semicircular chute in a sliding manner, an arc-shaped plate fixedly installed between the two sliding blocks, a wiping cotton cloth bonded to the front side of the arc-shaped plate, and a spring one fixedly installed at the rear side of the arc-shaped plate, wherein one end of the spring one away from the arc-shaped plate is fixedly connected to the inner side wall of the movable shell.

[0009] Preferably, the protection mechanism further comprises a fixed shell fixedly installed at the bottom of the unmanned aerial vehicle body, and a circular slide rail fixedly installed at the bottom of the unmanned aerial vehicle body, which is in sliding connection with the movable shell.

[0010] Preferably, the bottom of the unmanned aerial vehicle body is further provided with an L-shaped fixed plate, a motor is fixedly installed on the L-shaped fixed plate, and a gear is fixedly connected to the output end of the motor.

[0011] Preferably, an installation groove is formed in the outer side wall of the movable shell, and a semicircular toothed plate is fixedly installed in the installation groove, which is in meshing connection with the gear.

[0012] Preferably, the landing buffer mechanism comprises four fixed rods fixedly installed at the bottom of the unmanned aerial vehicle body and two ground plates located at the bottom of the four fixed rods.

[0013] The top of each of the two ground plates is fixedly provided with a sleeve, the sleeve is inserted to the lower end of the fixed rod through a piston, the bottom end of the fixed rod is fixedly provided with a spring two, the lower end of the spring two is fixedly connected to the inner bottom end of the sleeve, and an exhaust hole is formed in the outer side wall of the sleeve.

[0014] The working principle and beneficial effects of the utility model are as follows:

[0015] 1. The motor is started to drive the gear to rotate, the semicircular toothed plate in meshing connection is driven to slide the movable shell on the circular slide rail, the movable shell is adjusted out of the fixed shell and overlaps the fixed shell, the sealing protection is effectively realized when the monitoring camera is not used, the monitoring camera is prevented from being collided and scratched, and the service life of the monitoring camera is prolonged.

[0016] 2. When the movable shell moves, the wiping cotton cloth contacts the monitoring camera, the wiping cotton cloth presses the arc-shaped plate, the spring one is compressed, and the sliding block is slid in the semicircular chute, so that the purpose of automatically cleaning the monitoring camera is realized, and the definition of the monitoring camera is effectively improved. BRIEF DESCRIPTION OF DRAWINGS

[0017] The utility model will be further explained in detail in combination with the drawings and specific embodiments.

[0018] Figure 1 The whole three-dimensional structure schematic view is provided for the utility model;

[0019] Figure 2 The side view three-dimensional structure schematic view is provided for the utility model;

[0020] Figure 3 The sectional view three-dimensional structure schematic view of the fixed shell is provided for the utility model;

[0021] Figure 4 The sectional view three-dimensional structure schematic view of the sleeve is provided for the utility model;

[0022] In the drawing: 1, unmanned aerial vehicle main body; 2, monitoring camera; 3, protection mechanism; 31, movable shell; 32, L-shaped fixed plate; 33, motor; 34, gear; 35, installation groove; 36, semicircular toothed plate; 37, circular slide rail; 38, fixed shell; 4, cleaning mechanism; 41, semicircular sliding groove; 42, sliding block; 43, arc-shaped plate; 44, wiping cotton cloth; 45, spring one; 5, machine falling buffer mechanism; 51, fixed rod; 52, grounding plate; 53, sleeve; 54, spring two; 55, exhaust hole. DETAILED DESCRIPTION

[0023] The technical scheme in the embodiments of the utility model will be clearly and completely described below in conjunction with the embodiments of the utility model. Obviously, the described embodiments are only part of the embodiments of the utility model, rather than all the embodiments. Based on the embodiments in the utility model, all other embodiments obtained by those skilled in the art without creative labor are involved in the protection scope of the utility model.

[0024] Embodiment one

[0025] Please refer to Figure 1 - Figure 4 An intelligent safety construction monitoring equipment applied to an unmanned aerial vehicle, comprising: an unmanned aerial vehicle main body 1 and a monitoring camera 2 fixedly installed at the bottom of the unmanned aerial vehicle main body 1.

[0026] The bottom of the unmanned aerial vehicle main body 1 is provided with a protection mechanism 3, and the protection mechanism 3 comprises a movable shell 31. An inner side wall of the movable shell 31 is provided with a cleaning mechanism 4. The bottom of the unmanned aerial vehicle main body 1 is further provided with a machine falling buffer mechanism 5.

[0027] The cleaning mechanism 4 comprises a semicircular sliding groove 41 opened in the inner side wall of the movable shell 31, two sliding blocks 42 connected in opposite sliding manner inside the semicircular sliding groove 41, an arc-shaped plate 43 fixedly installed between the two sliding blocks 42, a wiping cotton cloth 44 bonded to the front side of the arc-shaped plate 43, a spring one 45 fixedly installed at the rear side of the arc-shaped plate 43, and an end of the spring one 45 away from the arc-shaped plate 43 fixedly connected with the inner side wall of the movable shell 31.

[0028] The protection mechanism 3 further comprises a fixed shell 38 fixedly installed at the bottom of the unmanned aerial vehicle body 1, a circular slide rail 37 fixedly installed at the bottom of the unmanned aerial vehicle body 1, the circular slide rail 37 being slidably connected with the movable shell 31, an L-shaped fixed plate 32 fixedly installed at the bottom of the unmanned aerial vehicle body 1, a motor 33 fixedly installed on the L-shaped fixed plate 32, a gear 34 fixedly connected with the output end of the motor 33, an installation groove 35 formed in the outer side wall of the movable shell 31, and a semicircular toothed plate 36 fixedly installed in the installation groove 35 and meshingly connected with the gear 34.

[0029] The intelligent safety construction monitoring equipment applied to the unmanned aerial vehicle is provided, the motor 33 is started, the motor 33 drives the gear 34 to rotate, the semicircular toothed plate 36 connected in linkage is driven to slide the movable shell 31 on the circular slide rail 37, the movable shell 31 is adjusted out of the fixed shell 38 and meets the fixed shell 38 again, the sealing protection is effectively performed when the monitoring camera 2 is not used, the collision and scratching of the monitoring camera 2 are prevented, and the service life of the monitoring camera 2 is prolonged.

[0030] When the movable shell 31 is adjusted and moved, the wiping cotton cloth 44 contacts the monitoring camera 2, after the contact, the wiping cotton cloth 44 extrudes the arc-shaped plate 43, the spring one 45 is compressed, the linkage sliding block 42 slides in the semicircular sliding groove 41, the whole wiping cotton cloth 44 wipes the monitoring camera 2, and the purpose that the monitoring camera 2 is automatically cleaned is achieved, and the definition of the monitoring camera 2 in shooting is improved.

[0031] Embodiment two

[0032] Based on the embodiment one, in the embodiment, the landing buffer mechanism 5 comprises four fixed rods 51 fixedly installed at the bottom of the unmanned aerial vehicle body 1 and two ground plates 52 located at the bottom of the four fixed rods 51, the top of each of the two ground plates 52 is fixedly installed with a sleeve pipe 53, the sleeve pipe 53 is insertedly connected with the bottom end of the fixed rod 51 through a piston, the bottom end of the fixed rod 51 is fixedly installed with a spring two 54, the bottom end of the spring two 54 is fixedly connected with the inner bottom end of the sleeve pipe 53, and an exhaust hole 55 is formed in the outer side wall of the sleeve pipe 53.

[0033] The technical scheme provided in the embodiment is as follows: when the unmanned aerial vehicle body 1 lands, the ground plate 52 contacts the ground, the force generated by the ground and the ground plate 52 is brought to the fixed rod 51 through the spring two 54, the fixed rod 51 is telescoped in the sleeve pipe 53 through the piston, the gas generated by the telescoping is discharged from the exhaust hole 55, the force of landing is effectively slid, and the stability of the unmanned aerial vehicle body 1 in landing is improved.

[0034] The above merely describes the preferred embodiments of the present application, and is not intended to limit the present application, and any modification, equivalent replacement, improvement, etc. made within the spirit and principle of the present application shall be included in the protection scope of the present application.

Claims

1. An intelligent safety construction monitoring device applied to a UAV, characterized in that, The utility model relates to a kind of unmanned aerial vehicle, including: Unmanned aerial vehicle body (1) and monitoring camera (2) fixedly installed in the bottom of the unmanned aerial vehicle body (1); The bottom of the unmanned aerial vehicle body (1) is provided with a protection mechanism (3), the protection mechanism (3) includes a movable shell (31), the inner side wall of the movable shell (31) is provided with a cleaning mechanism (4), and the bottom of the unmanned aerial vehicle body (1) is also provided with a machine falling buffer mechanism (5); The cleaning mechanism (4) includes a semicircular chute (41) opened in the inner side wall of the movable shell (31), two sliders (42) slidably connected inside the semicircular chute (41), an arc-shaped plate (43) fixedly installed between the two sliders (42), a wiping cotton cloth (44) bonded to the front side of the arc-shaped plate (43), a spring (45) fixedly installed at the rear side of the arc-shaped plate (43), and the end of the spring (45) away from the arc-shaped plate (43) is fixedly connected with the inner side wall of the movable shell (31). 2.The intelligent safety construction monitoring device applied to the unmanned aerial vehicle according to claim 1, wherein: The protection mechanism (3) further includes a fixed shell (38) fixedly installed at the bottom of the unmanned aerial vehicle body (1), a circular slide rail (37) fixedly installed at the bottom of the unmanned aerial vehicle body (1), and the circular slide rail (37) is slidably connected with the movable shell (31). 3.The intelligent safety construction monitoring device applied to the unmanned aerial vehicle according to claim 2, characterized in that: The bottom of the unmanned aerial vehicle body (1) is also fixedly installed with an L-shaped fixed plate (32), the L-shaped fixed plate (32) is fixedly installed with a motor (33), and the output end of the motor (33) is fixedly connected with a gear (34). 4.The intelligent safety construction monitoring device applied to the unmanned aerial vehicle according to claim 3, characterized in that: A mounting groove (35) is opened in the outer side wall of the movable shell (31), and a semicircular toothed plate (36) is fixedly installed inside the mounting groove (35), and the semicircular toothed plate (36) is meshingly connected with the gear (34). 5.The intelligent safety construction monitoring device applied to the unmanned aerial vehicle according to claim 1, characterized in that: The machine falling buffer mechanism (5) includes four fixed rods (51) fixedly installed at the bottom of the unmanned aerial vehicle body (1) and two ground plates (52) located at the bottom of the four fixed rods (51); The top of the two ground plates (52) is fixedly installed with a sleeve (53), the sleeve (53) and the bottom end of the fixed rod (51) are inserted by a piston, the bottom end of the fixed rod (51) is fixedly installed with a spring (54), the bottom end of the spring (54) is fixedly connected with the inner bottom end of the sleeve (53), and the outer side wall of the sleeve (53) is penetrated with an exhaust hole (55).

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