Protection pad for airplane maintenance worker

Abstract

An aircraft maintenance worker action protection pad is characterized by comprising a fixing pad, an anti-skid pad, anti-skid rubber strip suction cups and a warning assembly, the interior of the fixing pad is of a cavity structure, a plurality of suction cups and anti-skid rubber strips are arranged below the fixing pad at intervals, and air outlet holes in the tops of the suction cups communicate with an inner cavity of the fixing pad; the protective pad laid on the surface of the airplane is divided into two layers, the lower layer of the protective pad is connected with the fixed pad used for the surface of the airplane, the upper layer of the protective pad is an anti-skid pad, the suckers and the anti-skid rubber strips are arranged below the fixed pad at intervals, and the protective pad is arranged on the lower layer of the protective pad. After the protection points are laid on the surface of the aircraft, air extraction equipment is connected with the air extraction connecting pipe on the side face of the fixing pad for air extraction, so that the suction cups below the fixing pad are sucked to the surface of the aircraft, and the stability of connection between the protection pad and the surface of the aircraft is enhanced.

Description

Technical Field

[0001] The utility model relates to the technical field of auxiliary equipment for aircraft maintenance, in particular to a protective pad for aircraft maintenance work. Background Art

[0002] In recent years, more and more types of aircraft have appeared in my country, and the frequency of use of military aircraft has also increased. With the continuous development and research of my country's military aircraft, its main maintenance technical means are changing components. In the future, military fighter jets and other military aircraft will be safer, more reliable, more flexible and easier to deploy and maintain.

[0003] With the continuous development of social economy, the development level of my country's transportation industry has been significantly improved. As an important part of my country's transportation system, civil aviation has received more and more attention from all walks of life. With the continuous increase in business, some faults will occur during the operation of the aircraft, which will directly affect the safety of the aircraft. Therefore, improving the quality and efficiency of maintenance is very necessary to protect the flight safety of civil aviation aircraft.

[0004] As aircraft fly more and more frequently, the aircraft themselves are getting older, malfunctions occur more and more frequently, and maintenance is required more and more frequently. When maintenance personnel board the wings and fuselage of the aircraft, the surface of the aircraft is too smooth and they can easily slip and get injured. In addition, the stealth coating on the surface of the aircraft can be easily scratched off, and if there is dirt on the soles of shoes, it can easily get on the surface of the aircraft, making the aircraft more prone to rust. For this reason, anti-slip mats are now laid on the surface of the aircraft to avoid slipping and injuries and to prevent maintenance personnel from bringing dirt to damage the aircraft surface.

[0005] However, when the anti-skid mat is directly laid on the surface of the aircraft, the maintenance personnel may fall when walking on the anti-skid mat due to the poor connection between the anti-skid mat and the aircraft. In order to solve this problem, a protective mat for aircraft maintenance work is proposed. Utility Model Content

[0006] In response to the above technical problems, the utility model provides a protective mat for aircraft maintenance work. The protective mat laid on the aircraft surface is designed to be divided into two layers, the lower layer is a fixed mat for connecting to the aircraft surface, and the upper layer is an anti-skid non-slip mat. Suction cups and anti-skid rubber strips are arranged at intervals under the fixed mat, so that the suction cups under the fixed mat are sucked onto the aircraft surface, thereby enhancing the stability of the connection between the protective mat and the aircraft surface.

[0007] To achieve the above purpose, the technical solution of the utility model is as follows:

[0008] A protective mat for aircraft maintenance work, characterized by comprising a fixed mat, an anti-skid mat, an anti-skid rubber strip suction cup, and a warning component. The fixed mat has a cavity structure, a plurality of suction cups and anti-skid rubber strips are arranged at intervals below the fixed mat, an air outlet on the top of the suction cup is connected to the inner cavity of the fixed mat, an anti-skid mat is arranged above the fixed mat, and a warning component is installed on one side of the fixed mat.

[0009] The air extraction hole provided on one side of the fixed pad is connected to the air extraction connecting pipe, a one-way valve is provided on the air extraction connecting pipe, and the air extraction hole of the fixed pad is connected to the inner cavity of the fixed pad.

[0010] The warning assembly consists of a fixed seat, a rotating shaft, a limiting part, a connecting block, a mounting rod and a warning flag. The fixed seat is fixedly connected to the fixed pad. The rotating shaft is installed on the bearing of the fixed seat. The upper end of the rotating shaft is connected to the fixed seat through the limiting part. The rotating shaft is connected to the connecting block. The connecting block is connected to the mounting rod. A warning flag is provided on the mounting rod.

[0011] The limiting portion includes a protruding plate and a limiting stud. The protruding plate is fixedly connected to the rotating shaft. A limiting hole is provided on the protruding plate. The limiting stud passes through the limiting hole on the protruding plate and is threadedly connected to a threaded hole provided on the fixing seat.

[0012] Specifically, the anti-slip pad is provided with anti-slip convex patterns.

[0013] Specifically, the anti-slip rubber strip is on the same horizontal line as the suction cup.

[0014] Beneficial effects of the utility model:

[0015] The utility model designs the protective pad laid on the aircraft surface into two layers, the lower layer is a fixed pad for connecting to the aircraft surface, and the upper layer is a non-slip non-slip pad. Suction cups and non-slip rubber strips are arranged at intervals below the fixed pad. After the protection point is laid on the aircraft surface, air is extracted by connecting the air extraction device to the air extraction connecting pipe on the side of the fixed pad, so that the suction cup under the fixed pad is sucked to the aircraft surface, thereby enhancing the stability of the connection between the protective pad and the aircraft surface. A one-way valve is provided on the air extraction connecting pipe to prevent air from being extracted and then entering.

[0016] The utility model provides an installation warning component on one side of the fixed pad. The installation rod for installing the warning flag can adjust its placement angle according to the laying situation. The limiting stud in the limiting part is removed to release the limit of the rotating shaft. After directly rotating the installation rod and adjusting it to the corresponding angle, the limiting stud is inserted from the limiting hole of the protruding plate on one side of the rotating shaft and connected to the corresponding threaded hole on the fixing seat. The position of the installation rod at this time can be fixed, and the warning flag is adjusted to a suitable position for easy observation by staff, preventing maintenance personnel from forgetting to remove the protective pad when the aircraft is dispatched. BRIEF DESCRIPTION OF THE DRAWINGS

[0017] Figure 1 This is a schematic diagram of the overall structure of a protective pad for aircraft maintenance work in the utility model;

[0018] Figure 2 This is a bottom view schematic diagram of the overall structure of a protective pad for aircraft maintenance work according to the present invention;

[0019] Figure 3 This is a partial structural diagram of a warning component of a protective mat for aircraft maintenance work according to the present invention;

[0020] Figure 4 This is a schematic structural diagram of position A of a protective pad for aircraft maintenance work in the utility model;

[0021] Figure 5 This is a schematic cross-sectional view of a fixing pad of a protective pad for aircraft maintenance work according to the present invention;

[0022] As shown in the figure: 1. Anti-slip pad, 11. Anti-slip ridges, 2. Fixing pad, 21. Cavity, 22. Anti-slip rubber strip, 23. Suction cup, 24. Exhaust connection pipe, 25. One-way valve, 31. Fixing seat, 311. Threaded hole, 32. Rotating shaft, 34. Mounting rod, 341. Connecting block, 35. Warning flag, 36. Limit stud. DETAILED DESCRIPTION

[0023] The following is a clear and complete description of the technical solution of the present invention in conjunction with the accompanying drawings. Obviously, the embodiments described are only some of the embodiments of the present invention, not all of them. Based on the embodiments of the present invention, all other embodiments obtained by ordinary technicians in this field without making any creative efforts are within the scope of protection of the present invention.

[0024] In the description of this utility model, it should be noted that the terms "center," "upper," "lower," "left," "right," "vertical," "horizontal," "inner," and "outer," etc., indicating positions or relationships, are based on the positions or relationships shown in the accompanying drawings and are intended solely to facilitate the description of this utility model and simplify the description. They do not indicate or imply that the devices or components referred to must have a specific orientation, be constructed, or operate in a specific orientation. Therefore, they should not be construed as limitations on this utility model. Furthermore, the terms "first," "second," and "third" are used for descriptive purposes only and should not be construed as indicating or implying relative importance.

[0025] In the description of the present invention, it should be noted that, unless otherwise clearly specified and limited, the terms "installed", "connected", and "connected" should be understood in a broad sense. For example, it can be a fixed connection, a detachable connection, or an integral connection; it can be a mechanical connection or an electrical connection; it can be a direct connection, or it can be indirectly connected through an intermediate medium, or it can be internal communication between two components. For ordinary technicians in this field, the specific meanings of the above terms in the present invention can be understood according to specific circumstances. In addition, the technical features involved in the different embodiments of the present invention described below can be combined with each other as long as they do not conflict with each other. Example 1

[0026] As shown in the figure, the protective pad consists of two layers: a fixed pad 2 and an anti-skid pad 1. The anti-skid pad 2 is arranged above the fixed pad 2, and the protective pad 1 is provided with anti-skid ridges 11.

[0027] A cavity 21 is provided in the fixing pad 2, and a plurality of suction cups 23 and anti-slip rubber strips 22 are provided at intervals below the fixing pad 2, wherein the anti-slip rubber strips 22 are on the same horizontal line as the suction cups 23, the air outlet on the top of the suction cup 23 is connected to the inner cavity 21 of the fixing pad 2, and the air extraction hole provided on one side of the fixing pad 2 is also connected to the inner cavity 21 of the fixing pad 2, and the air extraction hole is connected to the air extraction connecting pipe 24, and a one-way valve 25 is provided on the air extraction connecting pipe 24.

[0028] A warning assembly is installed on one side of the fixed pad 2. The fixed seat 31 in the warning assembly is fixed on the fixed pad 2. The bearing on the fixed seat 31 is used to install the rotating shaft 32. A protruding plate 321 is provided on one side of the upper end of the rotating shaft 32. A limiting hole is provided on the protruding plate 321. The limiting stud 36 passes through the limiting hole on the protruding plate 321 and is threadedly connected to the threaded hole 311 provided on the fixed seat 31. Among them, a plurality of threaded holes 311 are provided on the fixed seat 3. The rotating shaft 32 is connected to the connecting block 341, the connecting block 341 is connected to the mounting rod 34, and a warning flag 35 is provided on the mounting rod 34. Example 2

[0029] When using the present invention, the protection point is laid on the surface of the aircraft. The lower fixed pad 2 is used to connect to the aircraft surface, and the upper layer is for maintenance personnel to walk on it. The anti-skid pad 1 with anti-skid ridges 11 is provided on the bottom surface of the fixed pad 2. Suction cups 23 and anti-skid rubber strips 22 are arranged at intervals. After the protection pad is laid on the aircraft surface, an air extraction device is connected to the air extraction connecting pipe 24 on the side of the fixed pad 2 to extract air from the cavity 21 of the fixed pad 2, so that the space formed between the suction cup 23 below the fixed pad 2 and the aircraft surface is negative pressure, so that the suction cup 23 is sucked on the aircraft surface, thereby enhancing the stability of the connection between the protection pad and the aircraft surface. A one-way valve 25 is provided on the air extraction connecting pipe 24 to prevent the gas from entering the air extraction connecting pipe 24 after being extracted. The air extraction device can be an existing air extraction device such as an air extractor.

[0030] A warning assembly is installed on one side of the fixed pad 2. The installation rod 34 for installing the warning flag 35 can adjust its angle according to the laying conditions. When adjusting the angle, first remove the limiting stud 36 in the limiting part to release the limit on the rotating shaft 32. After directly rotating the installation rod 34 and adjusting it to the corresponding angle, the limiting stud 36 is inserted from the limiting hole of the protruding plate 321 on the upper side of the rotating shaft 32 and connected to the corresponding threaded hole 311 on the fixing seat 31. The position of the installation rod 34 at this time can be fixed, and the warning flag 35 is adjusted to a suitable position for easy observation by the staff, so as to prevent the maintenance personnel from forgetting to remove the protective pad when the aircraft is dispatched. Among them, the warning flag 35 can be installed on the installation rod 34 in a hanging manner.

[0031] The above shows and describes the basic principles, main features and advantages of the present invention. The various components mentioned in the present invention are common technologies in the existing field. Those skilled in the art should understand that the present invention is not limited to the above embodiments. The above embodiments and descriptions are merely illustrative of the principles of the present invention. Various changes and improvements may be made to the present invention without departing from the spirit and scope of the present invention. Such changes and improvements fall within the scope of the present invention. The scope of protection claimed in this utility model is defined by the appended claims and their equivalents.

Claims

1. A protective mat for aircraft maintenance work, characterized in that It includes a fixed pad, an anti-slip pad, an anti-slip rubber strip suction cup and a warning component. The fixed pad has a cavity structure. Multiple suction cups and anti-slip rubber strips are arranged at intervals below the fixed pad. The air outlet on the top of the suction cup is connected to the inner cavity of the fixed pad. An anti-slip pad is arranged above the fixed pad, and a warning component is installed on one side of the fixed pad.

2. The protective pad for aircraft maintenance work according to claim 1, characterized in that The air extraction hole provided on one side of the fixed pad is connected to the air extraction connecting pipe, a one-way valve is provided on the air extraction connecting pipe, and the air extraction hole of the fixed pad is communicated with the inner cavity of the fixed pad.

3. The protective pad for aircraft maintenance work according to claim 1, characterized in that The warning assembly consists of a fixed seat, a rotating shaft, a limiting part, a connecting block, a mounting rod and a warning flag. The fixed seat is fixedly connected to the fixed pad, the rotating shaft is mounted on the bearing of the fixed seat, the upper end of the rotating shaft is connected to the fixed seat through the limiting part, the rotating shaft is connected to the connecting block, the connecting block is connected to the mounting rod, and a warning flag is provided on the mounting rod.

4. The protective pad for aircraft maintenance work according to claim 3, characterized in that The limiting portion includes a protruding plate and a limiting stud. The protruding plate is fixedly connected to the rotating shaft. A limiting hole is provided on the protruding plate. The limiting stud passes through the limiting hole on the protruding plate and is threadedly connected to a threaded hole provided on the fixing seat.

5. The protective pad for aircraft maintenance work according to claim 1, characterized in that The anti-slip pad is provided with anti-slip convex patterns.

Images