Vertical take-off and landing aircraft with inspection function

Abstract

The utility model relates to the technical field of inspection aircrafts, and discloses a vertical take-off and landing aircraft with an inspection function, the bottom of an unmanned aerial vehicle body is fixedly connected with a base, the middle side of the bottom of the base is fixedly connected with a mounting seat, and the bottom of the mounting seat is provided with a mounting groove; a mounting block is slidably connected to the interior of the mounting groove, mounting holes are formed in the two sides of the mounting block, a holder is fixedly connected to the bottom of the mounting block, a high-definition camera is fixedly connected to the right side of the holder, an illuminating lamp is fixedly connected to the middle side of the holder, and a night vision camera is fixedly connected to the left side of the holder; the unmanned aerial vehicle body, the high-definition camera, the illuminating lamp and the like are arranged to be used in cooperation, the unmanned aerial vehicle body is made to approach a bridge by controlling movement and hovering of the unmanned aerial vehicle body, the high-definition camera shoots and collects videos and pictures of the bridge in multiple directions, manual inspection is not needed, the difficulty and danger of inspection are greatly reduced, and workers can conveniently use the device.

Description

TECHNICAL FIELD

[0001] The utility model relates to the technical field of inspection aircraft, concretely to a vertical take-off and landing aircraft with inspection function. BACKGROUND

[0002] Bridge inspection is the basic work to ensure the safe operation of the bridge and improve the installation reliability, and most of the artificial inspection mode is used, the artificial is transported to the support position through the bridge detection vehicle, elevator and other equipment, and then the support working state is checked through visual inspection and simple measurement.

[0003] The traditional artificial inspection mode has the problems of high labor intensity, low efficiency, high bridge pier, complex structure and auxiliary facilities, and many other factors, which increase the difficulty and danger of artificial inspection, and are inconvenient to use. UTILITY MODEL CONTENT

[0004] In view of the defects of the prior art, the utility model provides a vertical take-off and landing aircraft with inspection function to solve the problems of the traditional artificial inspection mode, such as high labor intensity, low efficiency, high bridge pier, complex structure and auxiliary facilities, and many other factors, which increase the difficulty and danger of artificial inspection, and are inconvenient to use.

[0005] To achieve the above purpose, the utility model provides the following technical scheme: a vertical take-off and landing aircraft with inspection function, including unmanned aerial vehicle body, the bottom of unmanned aerial vehicle body is fixedly connected with base, the both sides of base are fixedly connected with electric push rod, the bottom of electric push rod is fixedly connected with lower pressing block, the both sides of base bottom are fixedly connected with support frame, the inner side top of support frame is provided with counterweight, the bottom of counterweight is provided with clamping groove, the top of counterweight is provided with positioning groove, the middle side of base bottom is fixedly connected with mounting seat, the bottom of mounting seat is provided with mounting groove, the outer side of mounting seat is screw connected with hand screw bolt, the inside of mounting groove is slidably connected with mounting block, the both sides of mounting block are provided with mounting hole, the bottom of mounting block is fixedly connected with holder, the right side of holder is fixedly connected with high-definition camera, the middle side of holder is fixedly connected with illuminating lamp, the left side of holder is fixedly connected with night vision camera.

[0006] Preferably, the shape and size of the mounting block are matched with the shape and size of the mounting groove, and the mounting block is tightly combined with the inner wall of the mounting groove.

[0007] By setting the mounting block, the mounting groove and the like, the gimbal and the unmanned aerial vehicle body can be separated by sliding the mounting block out of the mounting groove, so that the staff can conveniently disassemble and maintain the unmanned aerial vehicle body.

[0008] Preferably, the number of the positioning grooves is two, the positions of the two positioning grooves correspond to the position of the pressing block, the diameter of the pressing block is matched with the diameter of the positioning grooves, and the pressing block is tightly combined with the positioning grooves.

[0009] By setting the positioning grooves, the pressing block and the like and cooperating with the counterweight block, the counterweight block can be installed on the support frame by pushing the pressing block into the positioning groove through the electric push rod, so that the weight of the unmanned aerial vehicle body is increased, the wind resistance of the unmanned aerial vehicle body is improved, the unmanned aerial vehicle body can be normally used in strong wind weather, and the applicability is improved.

[0010] Preferably, the number of the clamping grooves is two, the positions of the two clamping grooves correspond to the positions of the two support frames, and the two support frames are tightly combined with the inner walls of the clamping grooves.

[0011] Preferably, the number of the hand screws is two, the two hand screws are symmetrically distributed on the two sides of the mounting seat, and the two hand screws are both extended into the mounting holes.

[0012] Compared with the prior art, the vertical take-off and landing aircraft with the inspection function has the following beneficial effects:

[0013] 1. The vertical take-off and landing aircraft with the inspection function is provided with the unmanned aerial vehicle body, the high-definition camera and the illuminating lamp and the like, and cooperates with each other, the unmanned aerial vehicle body is controlled to move and hover, approaches the bridge, the high-definition camera is used to shoot and collect videos and pictures of the bridge from multiple directions, manual inspection is not needed, the difficulty and danger of the inspection are greatly reduced, and the staff can use it conveniently.

[0014] 2. The vertical take-off and landing aircraft with the inspection function is provided with the positioning grooves, the pressing block and the like and cooperates with the counterweight block, the counterweight block is installed on the support frame by pushing the pressing block into the positioning groove through the electric push rod, the weight of the unmanned aerial vehicle body is increased, the wind resistance of the unmanned aerial vehicle body is improved, the unmanned aerial vehicle body can be normally used in strong wind weather, and the applicability is improved. BRIEF DESCRIPTION OF DRAWINGS

[0015] Figure 1 It is a front view structural schematic diagram of the utility model;

[0016] Figure 2 It is a bottom view structural schematic diagram of the utility model;

[0017] Figure 3A base structure schematic view of the utility model;

[0018] Figure 4 A mounting seat structure schematic view of the utility model;

[0019] Figure 5 A mounting block structure schematic view of the utility model;

[0020] Figure 6 A counterweight block structure schematic view of the utility model;

[0021] Figure 7 A hand screw bolt structure schematic view of the utility model.

[0022] In the drawing: 1, unmanned aerial vehicle body; 2, base; 3, electric push rod; 4, lower pressing block; 5, support frame; 6, clamping groove; 7, counterweight block; 8, positioning groove; 9, mounting seat; 10, mounting groove; 11, hand screw bolt; 12, mounting block; 13, mounting hole; 14, holder; 15, high-definition camera; 16, illuminating lamp; 17, night vision camera. DETAILED DESCRIPTION

[0023] The technical solutions in the embodiments of the utility model will be clearly and completely described below with reference to the drawings in 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 fall within the protection scope of the utility model.

[0024] Embodiment 1:

[0025] Please refer to Figures 1-6A vertical take-off and landing aircraft with inspection function, including unmanned aerial vehicle body 1, the bottom of unmanned aerial vehicle body 1 is fixedly connected with base 2, the two sides of base 2 are fixedly connected with electric push rod 3, the bottom of electric push rod 3 is fixedly connected with lower pressing block 4, the two sides of the bottom of base 2 are fixedly connected with support frame 5, the inner side top of support frame 5 is provided with counterweight 7, the bottom of counterweight 7 is provided with clamping groove 6, the top of counterweight 7 is provided with positioning groove 8, the middle side of the bottom of base 2 is fixedly connected with mounting seat 9, the bottom of mounting seat 9 is provided with mounting groove 10, the outer side of mounting seat 9 is screw-connected with hand screw bolt 11, the inside of mounting groove 10 is slidably connected with mounting block 12, the shape and size of mounting block 12 are adapted to the shape and size of mounting groove 10, and mounting block 12 is tightly attached to the inner wall of mounting groove 10, the two sides of mounting block 12 are provided with mounting hole 13, the number of hand screw bolt 11 is two, and the two hand screw bolts 11 are symmetrically distributed on the two sides of mounting seat 9, and the two hand screw bolts 11 are extended into the inside of mounting hole 13, the bottom of mounting block 12 is fixedly connected with holder 14, the right side of holder 14 is fixedly connected with high-definition camera 15, the middle side of holder 14 is fixedly connected with illuminating lamp 16, and the left side of holder 14 is fixedly connected with night vision camera 17.

[0026] Principle: when in use, the staff first slides mounting block 12 into mounting groove 10, and fixes mounting block 12 by screwing hand screw bolt 11 into mounting hole 13, so as to connect holder 14 with unmanned aerial vehicle body 1, at this time, the staff operates unmanned aerial vehicle body 1 to take off, controls the movement and hovering of unmanned aerial vehicle body 1, makes it close to the bridge, and makes high-definition camera 15 take multi-directional video and picture shooting and collection of the bridge, when the light of the bridge is not good, the staff can start illuminating lamp 16 to supplement light, so as to facilitate high-definition camera 15 to image, through the setting of night vision camera 17, night vision function can be realized, which is convenient for night patrol and improves applicability and facilitates the staff to use.

[0027] Compared with the related art, the vertical take-off and landing aircraft with inspection function has the following beneficial effects: through the cooperation of unmanned aerial vehicle body 1, high-definition camera 15 and illuminating lamp 16, the movement and hovering of unmanned aerial vehicle body 1 are controlled, the unmanned aerial vehicle body 1 is made to close to the bridge, and high-definition camera 15 takes multi-directional video and picture shooting and collection of the bridge, manual inspection is not needed, the difficulty and danger of inspection are greatly reduced, and the staff can use conveniently.

[0028] Embodiment 2

[0029] Please refer to Figures 1-7The bottom of the unmanned aerial vehicle body 1 is fixedly connected with a base 2, both sides of the base 2 are fixedly connected with electric push rods 3, the bottom of the electric push rod 3 is fixedly connected with a pressing block 4, both sides of the bottom of the base 2 are fixedly connected with supporting frames 5, the inner side top of the supporting frame 5 is provided with a counterweight 7, the bottom of the counterweight 7 is provided with clamping grooves 6, the number of the clamping grooves 6 is two, the positions of the two clamping grooves 6 correspond to the positions of the two supporting frames 5, and the two supporting frames 5 are tightly combined with the inner walls of the clamping grooves 6, the top of the counterweight (7) is provided with positioning grooves 8, the number of the positioning grooves 8 is two, the positions of the two positioning grooves 8 correspond to the position of the pressing block 4, the diameter of the pressing block 4 is matched with the diameter of the positioning groove 8, and the pressing block 4 is tightly combined with the positioning groove 8.

[0030] Working principle: when the staff needs to carry out the inspection work in the strong wind weather, the staff can place the counterweight 7 on the inner side top of the supporting frame 5, and make the clamping groove 6 at the bottom of the counterweight 7 and the supporting frame 5 are mutually clamped, at this time, the staff starts the electric push rod 3, the electric push rod 3 pushes the pressing block 4 to move downwards, and then the pressing block 4 is clamped into the positioning groove 8 at the top of the counterweight 7, that is, the counterweight 7 is installed on the supporting frame 5, the weight of the unmanned aerial vehicle body 1 is increased, the wind resistance of the unmanned aerial vehicle body 1 is improved, the normal use of the unmanned aerial vehicle body 1 in the strong wind weather is ensured, and the applicability is improved.

[0031] Compared with the related art, the vertical take-off and landing aircraft with the inspection function has the beneficial effects that: the counterweight 7 is installed on the supporting frame 5 by setting the positioning groove 8, the pressing block 4 and the like, the pressing block 4 is clamped into the positioning groove 8 by the electric push rod 3, the weight of the unmanned aerial vehicle body 1 is increased, the wind resistance of the unmanned aerial vehicle body 1 is improved, the normal use of the unmanned aerial vehicle body 1 in the strong wind weather is ensured, and the applicability is improved.

[0032] Although the embodiments of the utility model have been shown and described, it can be understood by those skilled in the art that various changes, modifications, replacements and modifications can be made to these embodiments without departing from the principles and spirits of the utility model, the scope of the utility model is defined by the appended claims and their equivalents.

Claims

1. A vertical take-off and landing aircraft with inspection function, comprising a drone body (1), characterized in that: The bottom of the unmanned aerial vehicle body (1) is fixedly connected with a base (2), both sides of the base (2) are fixedly connected with an electric push rod (3), the bottom of the electric push rod (3) is fixedly connected with a pressing block (4), both sides of the bottom of the base (2) are fixedly connected with a support frame (5), the inner side top of the support frame (5) is provided with a counterweight (7), the bottom of the counterweight (7) is provided with a clamping groove (6), the top of the counterweight (7) is provided with a positioning groove (8), the bottom of the base (2) is fixedly connected with a mounting seat (9), the bottom of the mounting seat (9) is provided with a mounting groove (10), the outer side of the mounting seat (9) is threadedly connected with a hand screw bolt (11), the inside of the mounting groove (10) is slidably connected with a mounting block (12), both sides of the mounting block (12) are provided with mounting holes (13), the bottom of the mounting block (12) is fixedly connected with a holder (14), the right side of the holder (14) is fixedly connected with a high-definition camera (15), the middle side of the holder (14) is fixedly connected with an illuminating lamp (16), the left side of the holder (14) is fixedly connected with a night vision camera (17).

2. The vertical take-off and landing aircraft with a patrol function according to claim 1, characterized in that: The shape and size of the mounting block (12) are matched with the shape and size of the mounting groove (10), and the mounting block (12) is tightly attached to the inner wall of the mounting groove (10).

3. The vertical take-off and landing aircraft with a patrol function according to claim 1, characterized in that: The number of the positioning grooves (8) is two, the positions of the two positioning grooves (8) correspond to the position of the pressing block (4), the diameter of the pressing block (4) is matched with the diameter of the positioning groove (8), and the pressing block (4) is tightly attached to the positioning groove (8).

4. The vertical take-off and landing aircraft with a patrol function according to claim 1, characterized in that: The number of the clamping grooves (6) is two, the positions of the two clamping grooves (6) correspond to the positions of the two support frames (5), and the two support frames (5) are tightly attached to the inner wall of the clamping groove (6).

5. The vertical take-off and landing aircraft with a patrol function according to claim 1, characterized in that: The number of the hand screw bolts (11) is two, the two hand screw bolts (11) are symmetrically distributed on both sides of the mounting seat (9), and the two hand screw bolts (11) extend into the mounting holes (13).

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