Thickness measuring equipment capable of flying

Abstract

The utility model discloses a thickness measuring device capable of flying, which relates to the field of thickness measuring equipment and comprises an aircraft, a fixed ring is sleeved on the outer wall of a gauge rod, a movable plate is arranged in the fixed ring, one side of the movable plate is connected with a connecting rod, a contact ring is fixed at the end part of the connecting rod, and the contact ring is connected with the aircraft. A driving rod is connected to one side of the moving plate, four sets of stretching rods are arranged on one side of the moving column, and warning cloth is fixed to the ends of the stretching rods. In the process that the aircraft gets close to the ship body, a contact ring pushes a moving column to slide in a moving bin through a driving rod, when a moving plate moves to the end of the inner wall of a fixing ring, a detection head is attached to the surface of the ship body, a connecting ring moves to a port of a containing bin at the moment, and an extension rod is extruded by extension of a second spring; therefore, the warning cloth is completely unfolded by the four groups of extension rods, and a detector can know whether the detection head is in contact with the surface of the ship body or not according to the unfolding condition of the warning cloth.

Description

TECHNICAL FIELD

[0001] The utility model relates to the field of thickness measuring equipment, specifically to a kind of flight thickness measuring equipment. BACKGROUND

[0002] Thickness measuring equipment is a kind of professional equipment for accurately measuring the thickness of an object, widely used in industrial production, quality detection and many other fields, which can quickly and accurately obtain the thickness data of materials or structures, plays a vital role in ensuring product quality and safe operation of equipment. In manufacturing, detecting parts by thickness measuring equipment can effectively avoid performance degradation or failure caused by thickness deviation.

[0003] Currently, there is a flight thickness measuring equipment that combines unmanned aerial vehicles and detectors. When detecting the thickness of a ship's hull, the operator controls the unmanned aerial vehicle to fly near the ship to be detected, then tightly attaches the detection rod at the end of the unmanned aerial vehicle to the surface of the ship hull. The detection rod has a sensor inside. According to the principle of mechanics, when the sensor contacts the surface of the ship material, it will be affected by the thickness of the material, and then the sensor inside the detection rod will detect the thickness of the ship surface.

[0004] Since the detection rod on the flight thickness measuring equipment needs to be tightly attached to the surface of the ship hull when detecting the thickness of the ship hull, if it is not tightly attached, the sensor inside the detection rod will have difficulty accurately measuring the thickness of the ship hull. Since the unmanned aerial vehicle flies at a high altitude, the operator cannot easily observe whether the detection rod is tightly attached to the surface of the ship hull. UTILITY MODEL CONTENTS

[0005] Therefore, the utility model aims to provide a flight thickness measuring equipment to solve the technical problem of the operator's difficulty in clearly observing whether the detection rod of the unmanned aerial vehicle flying at a high altitude is tightly attached to the surface of the ship hull.

[0006] To achieve the above-mentioned purpose, the utility model provides the following technical solution: a flight thickness measuring equipment, comprising an aircraft, a signal pole mounted on the top of the aircraft, a detection rod connected to the top of the aircraft, a detection head provided at the end of the detection rod, a fixed ring sleeved on the outer wall of the detection rod, a moving plate provided inside the fixed ring, a connecting rod connected to one side of the moving plate, a contact ring fixed at the end of the connecting rod, a drive rod connected to one side of the moving plate, a moving column fixed at the end of the drive rod, a moving bin provided on the outer wall of the moving column, a storage bin connected to one side of the moving bin, four sets of extension rods provided on one side of the moving column, and warning cloth fixed at the end of the extension rods.

[0007] By adopting the above technical scheme, the problem that the detection personnel cannot clearly observe whether the unmanned aerial vehicle detection rod with high flight height is closely attached to the surface of the ship body is solved, in the process that the aircraft approaches the ship body, the contact ring pushes the moving column to slide in the moving bin through the driving rod, when the moving plate moves to the end of the inner wall of the fixed ring, the detection head is attached to the surface of the ship body, and at this time, the connecting ring moves to the port of the storage bin, the stretching rods are extruded due to the stretching of the second spring, so that the four groups of stretching rods completely expand the warning cloth, and the detection personnel can know whether the detection head contacts the surface of the ship body through the expansion of the warning cloth.

[0008] The utility model further sets up, one side of mobile board is provided with first spring, when first spring is in completely compressed state, one side surface of contact ring is in same vertical plane with one side of detection head.

[0009] As preferred, when the detection head is in close contact with the surface of the ship body, the moving plate is displaced to the end of the inner wall of the fixed ring, and at this time, the outer wall of the contact ring and the detection head are in the same vertical plane, thereby avoiding the detection head end damage caused by excessive extrusion of the ship body when the aircraft approaches the ship body.

[0010] The utility model further sets up, one side of mobile column is fixed with connecting ring, and the end of stretching rod is movably installed on the connecting ring.

[0011] As preferred, the connecting ring connects and fixes the four groups of stretching rods, and the stretching rods can be flipped by a certain angle with the connecting ring as the center.

[0012] The utility model further sets up, one side of connecting ring is fixed with fixed rod, and the length of fixed rod is less than the length of stretching rod.

[0013] As preferred, the end of the fixed rod is connected with one side of the warning cloth, and when the warning cloth is completely expanded, the connection of the fixed rod makes the warning cloth present a funnel shape, so that the warning cloth is easily observed by the detection personnel located below the aircraft.

[0014] The utility model further sets up, the outer wall of fixed rod is provided with second spring, and the second spring is in a compressed state.

[0015] As preferred, when the stretching rod moves to the outside of the storage bin, the second spring extrudes and pushes the stretching rod to flip with the connecting ring as the center, so that the warning cloth at the end of the stretching rod can be expanded.

[0016] The utility model further sets up, two sides of warning cloth are provided with cloth of different colors, and the colors of the two sides of the cloth are respectively set as red and green.

[0017] As preferably, in optics, red and green are complementary colors, which are matched together with strong contrast, thereby facilitating the detection personnel to identify the warning cloth.

[0018] The utility model further sets up, the inner wall of the storage compartment is set to conical, and the diameter of the storage compartment port is less than the diameter of the warning cloth.

[0019] As preferably, when the warning cloth is completely unfolded, the warning cloth can cover the port of the storage compartment, and the storage compartment is set to conical, facilitating the collection of the extension rod by the moving column.

[0020] The utility model further sets up, the outer wall of the driving rod is equipped with two sets of limit blocks, and the limit blocks are fixedly installed on the outer wall of the aircraft.

[0021] As preferably, the two sets of limit blocks facilitate the movement of the driving rod from the vertical direction and the horizontal direction, so that the driving rod does not deviate when moving.

[0022] The utility model further sets up, the outer wall of the aircraft is provided with four protective sleeves, and the inner wall of the protective sleeve is provided with a wing.

[0023] As preferably, the high-speed rotation of the four wings provides sufficient flight power for the aircraft, and the protective sleeve protects the wing from being collided by external objects.

[0024] In summary, the utility model mainly has the following beneficial effects:

[0025] 1、The utility model discloses a flying device, a detection rod, a detection head, a contact ring, a driving rod, a moving column, an extension rod and a warning cloth are arranged, which solve the problem that detection personnel cannot clearly observe whether the unmanned aerial vehicle detection rod closely adheres to the ship surface when the flying height is high, in the process that the flying device approaches the ship body, the contact ring drives the moving column to slide in the moving compartment through the driving rod, when the moving plate moves to the end of the inner wall of the fixed ring, the detection head adheres to the ship surface, and the connecting ring moves to the port of the storage compartment at this time, the extension rod is extruded due to the extension of the second spring, so that the four extension rods completely unfold the warning cloth, and the detection personnel know whether the detection head contacts the ship surface by the unfolding condition of the warning cloth.

[0026] 2、The utility model discloses a contact ring, a connecting rod, a moving plate and a fixed ring are arranged, when the detection head closely contacts the ship surface, the moving plate is displaced to the end of the inner wall of the fixed ring, and the outer wall of the contact ring and the detection head is in the same vertical plane at this time, avoiding that the detection head is damaged at the end when the flying device approaches the ship body due to excessive extrusion of the ship body. BRIEF DESCRIPTION OF DRAWINGS

[0027] Figure 1The device overall schematic view of the utility model;

[0028] Figure 2 The device overall side view of the utility model;

[0029] Figure 3 The storage bin overall section view of the utility model;

[0030] Figure 4 The warning cloth unfolding schematic view of the utility model;

[0031] Figure 5 The utility model Figure 2 Local enlarged view A figure;

[0032] Figure 6 The pulley installation schematic view of the utility model.

[0033] Mark explanation:

[0034] 1, aircraft; 101, probe pole; 102, signal pole; 103, wing; 104, protective sleeve; 105, probe head; 2, contact ring; 201, connecting rod; 202, moving plate; 203, fixed ring; 204, first spring; 3, drive rod; 301, limit block; 4, moving bin; 401, storage bin; 5, moving column; 501, connecting ring; 502, extension rod; 503, second spring; 504, fixed rod; 6, warning cloth; 7, pulley. Specific implementation

[0035] The technical scheme in the embodiment of the utility model will be described clearly and completely in combination with the drawings in the embodiment of the utility model. The embodiment described below is exemplary and is only used for explaining the utility model and can not be understood as the limitation of the utility model.

[0036] The embodiment of the utility model will be described according to the overall structure of the utility model.

[0037] First embodiment:

[0038] Please refer to Figure 1 — Figure 5The utility model provides an unmanned aerial vehicle detection device, including aircraft 1, the top of aircraft 1 is equipped with signal pole 102, the top of aircraft 1 is connected with detection pole 101, the end of detection pole 101 is provided with detection head 105, the outer wall of detection pole 101 is sleeved with fixed ring 203, the inside of fixed ring 203 is provided with moving plate 202, one side of moving plate 202 is connected with connecting rod 201, the end of connecting rod 201 is fixed with contact ring 2, one side of moving plate 202 is connected with drive rod 3, the end of drive rod 3 is fixed with moving column 5, the outer wall of moving column 5 is provided with moving bin 4, one side of moving bin 4 is connected with storage bin 401, one side of moving column 5 is provided with four groups of stretchers 502, the end of stretcher 502 is fixed with warning cloth 6, the problem that the detection personnel is difficult to clearly observe whether the unmanned aerial vehicle detection pole of high flight height is closely attached to the surface of ship is solved, in the process that aircraft 1 approaches the ship body, contact ring 2 pushes moving column 5 to slide in moving bin 4 through drive rod 3, when moving plate 202 moves to the end of the inner wall of fixed ring 203, detection head 105 is attached to the surface of ship, and the connecting ring 501 of this time moves to the port of storage bin 401, and the stretcher 502 is extruded due to the expansion of the second spring 503, so that four groups of stretchers 502 completely unfold warning cloth 6, and the detection personnel knows whether detection head 105 contacts the surface of ship through the unfolding situation of warning cloth 6.

[0039] In the above embodiment, please refer to Figure 5 One side of moving plate 202 is provided with first spring 204, when first spring 204 is in the completely compressed state, one side surface of contact ring 2 is in the same vertical plane with one side of detection head 105, when detection head 105 is closely contacted with the surface of ship, moving plate 202 is displaced to the end of the inner wall of fixed ring 203, and the outer wall of contact ring 2 and detection head 105 is in the same vertical plane at this time, so that the end of detection head 105 is damaged due to excessive extrusion of ship when aircraft 1 approaches the ship body is avoided.

[0040] In the above embodiment, please refer to Figure 3 One side of moving column 5 is fixed with connecting ring 501, the end of stretcher 502 is movably installed on connecting ring 501, connecting ring 501 connects and fixes four groups of stretchers 502, and stretcher 502 can overturn a certain angle with connecting ring 501 as the center.

[0041] In the above embodiment, please refer to Figure 3The fixed rod 504 is fixed on one side of the connecting ring 501, and the length of the fixed rod 504 is less than the length of the stretching rod 502. The end of the fixed rod 504 is connected to one side of the warning cloth 6. When the warning cloth 6 is fully unfolded, the connection of the fixed rod 504 makes the warning cloth 6 present a funnel shape, so that the warning cloth 6 is easy to be observed by the detection personnel located below the aircraft 1.

[0042] In the above embodiment, please refer to Figure 3 The outer wall of the fixed rod 504 is provided with the second spring 503, and the second spring 503 is in a compressed state. When the stretching rod 502 moves outward from the storage bin 401, the second spring 503 pushes and turns the stretching rod 502 around the connecting ring 501 as the center, so that the warning cloth 6 at the end of the stretching rod 502 can be unfolded.

[0043] In the above embodiment, please refer to Figure 3 The two sides of the warning cloth 6 are provided with different colored cloth, and the two sides of the cloth are respectively provided with red and green color. In optics, red and green are complementary colors, and when they are matched together, the contrast is strong, so as to facilitate the detection personnel to identify the front and back of the warning cloth 6.

[0044] In the above embodiment, please refer to Figure 3 The inner wall of the storage bin 401 is provided with a taper, and the diameter of the port of the storage bin 401 is less than the diameter of the warning cloth 6. When the warning cloth 6 is fully unfolded, the warning cloth 6 can cover the port of the storage bin 401, and the storage bin 401 is provided with a taper, which is convenient for the moving column 5 to collect the stretching rod 502.

[0045] In the above embodiment, please refer to Figure 2 The outer wall of the driving rod 3 is provided with two groups of limiting blocks 301, and the limiting blocks 301 are fixedly installed on the outer wall of the aircraft 1. The two groups of limiting blocks 301 facilitate the movement of the driving rod 3 to be limited from the vertical direction and the horizontal direction, so that the driving rod 3 does not deviate when moving.

[0046] In the above embodiment, please refer to Figure 1 The outer wall of the aircraft 1 is provided with four protective sleeves 104, and the inner wall of the protective sleeve 104 is provided with the wing 103. The high-speed rotation of the four wings 103 provides sufficient flight power for the aircraft 1, and the protective sleeve 104 protects the wing 103 from being collided by external objects.

[0047] Second embodiment:

[0048] Please refer to Figure 6The side of the storage bin 401 is provided with four groups of pulleys 7, and the pulleys 7 are arranged at the end of the extension rod 502; when the moving column 5 drives the extension rod 502 to move to the inside of the storage bin 401, the extension rod 502 slides on the outer wall of the pulley 7; the arrangement of the pulley 7 reduces the friction between the extension rod 502 and the inner wall of the storage bin 401 during the contraction movement of the extension rod 502 to the storage bin 401, so that the moving column 5 can easily wind the warning cloth 6 into the storage bin 401 through the extension rod 502.

[0049] The utility model discloses in the specific work time: when aircraft 1 flies to the ship body vicinity, the contact ring 2 of detection rod 101 one side first with the ship body surface contact, subsequently equipment personnel control aircraft 1 to approach the ship body, in the process that aircraft 1 approaches the ship body, contact ring 2 pushes mobile plate 202 to move to the inside of fixed ring 203 through connecting rod 201, and the movement of mobile plate 202 extrudes first spring 204 and contracts, in the process that mobile plate 202 moves, mobile plate 202 pushes the moving column 5 in the moving bin 4 and slides to the outside through drive rod 3, and the extension rod 502 connected to one side of moving column 5, because the second spring 503 in the compression state stretches to the outside, so that the extension rod 502 slowly opens in the process of moving to the port of storage bin 401, when mobile plate 202 moves to the inside end of fixed ring 203, detection head 105 is attached to the ship body surface, and the connecting ring 501 of one side of moving column 5 moves to the port of storage bin 401 at this time, four groups of extension rod 502 completely unfold warning cloth 6, and the detection personnel know that detection head 105 has contacted the ship body surface through the unfolding situation of warning cloth 6.

[0050] Although the embodiments of the utility model have been shown and described, the specific embodiments are only the explanation of the utility model, and are not the limitation of the utility model, and the specific features, structures, materials or characteristics described can be combined in any one or more embodiments or examples in a suitable way, and the person skilled in the art can make the modification, replacement and change of the embodiment without creative contribution after reading the specification without departing from the principles and the tenet of the utility model, but as long as in the claim range of the utility model, it is protected by the patent law.

Claims

1. A flying thickness measuring apparatus comprising an aircraft (1), characterized in that: The top of the aircraft (1) is provided with a signal pole (102), the top of the aircraft (1) is connected with a detection rod (101), the end of the detection rod (101) is provided with a detection head (105), the outer wall of the detection rod (101) is sleeved with a fixed ring (203), the inside of the fixed ring (203) is provided with a moving plate (202), one side of the moving plate (202) is connected with a connecting rod (201), the end of the connecting rod (201) is fixedly provided with a contact ring (2), one side of the moving plate (202) is connected with a driving rod (3), the end of the driving rod (3) is fixedly provided with a moving column (5), the outer wall of the moving column (5) is provided with a moving bin (4), one side of the moving bin (4) is connected with a storage bin (401), one side of the moving column (5) is provided with four groups of extension rods (502), the end of the extension rod (502) is fixedly provided with a warning cloth (6).

2. The flyable thickness measuring apparatus of claim 1, wherein: One side of the moving plate (202) is provided with a first spring (204), when the first spring (204) is in a fully compressed state, one side surface of the contact ring (2) is in the same vertical plane with one side of the detection head (105).

3. The flyable thickness measuring apparatus of claim 1, wherein: One side of the moving column (5) is fixedly provided with a connecting ring (501), the end of the extension rod (502) is movably installed on the connecting ring (501).

4. The flyable thickness measuring apparatus of claim 3, wherein: One side of the connecting ring (501) is fixedly provided with a fixed rod (504), and the length of the fixed rod (504) is less than the length of the extension rod (502).

5. The flyable thickness measuring apparatus of claim 4, wherein: The outer wall of the fixed rod (504) is provided with a second spring (503), and the second spring (503) is in a compressed state.

6. The flyable thickness measuring apparatus of claim 1, wherein: Both sides of the warning cloth (6) are provided with cloth of different colors, and the colors of both sides of the cloth are respectively red and green.

7. The flyable thickness measuring apparatus of claim 1, wherein: The inner wall of the storage bin (401) is provided in a conical shape, and the diameter of the port of the storage bin (401) is less than the diameter of the warning cloth (6).

8. The flyable thickness measuring apparatus of claim 1, wherein: The outer wall of the driving rod (3) is sleeved with two groups of limiting blocks (301), and the limiting blocks (301) are installed and fixed on the outer wall of the aircraft (1).

9. The flyable thickness measuring apparatus of claim 1, wherein: The outer wall of the aircraft (1) is provided with four groups of protective sleeves (104), and the inside of the protective sleeve (104) is installed with a wing (103).

10. The flyable thickness measuring apparatus of claim 1, wherein: One side of the storage bin (401) is installed with four groups of pulleys (7), and the pulleys (7) are located at the end of the extension rod (502).

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