Aviation electromechanical equipment maintenance device

Abstract

The utility model relates to the technical field of electromechanical maintenance equipment, in particular to an aviation electromechanical equipment maintenance device which comprises a storage box and a movable spraying assembly, the movable spraying assembly comprises a supporting frame, a bottom plate, movable wheels, a rubber pad and a liquid outlet pipe, and the supporting frame is detachably connected with the storage box and located on the outer surface of the storage box; the bottom plate is detachably connected with the supporting frame and located below the supporting frame, the moving wheels are detachably connected with the bottom plate and located below the bottom plate, the rubber pad is detachably connected with the moving wheels and located on one side of the moving wheels, and the liquid outlet pipe penetrates through the supporting frame, is detachably connected with the storage box and located at an output port of the storage box. The problems that in long-time use, dust can be accumulated on the aviation equipment, a shell coating of the aviation equipment is damaged to a certain degree, and current maintenance equipment cannot repair and maintain the coating are effectively solved.

Description

Technical Field

[0001] The utility model relates to the technical field of electromechanical maintenance equipment, and particularly relates to a maintenance device for aviation electromechanical equipment. Background Art

[0002] After long-term use, the electromechanical equipment in aerospace needs to be maintained. Due to the long-term use of the equipment, a large amount of dust and stains will accumulate on the surface of the equipment. At this time, if it is cleaned manually, the labor intensity of the workers will be relatively large, and if it is washed with a water gun, the stubborn stains on the equipment cannot be effectively removed, resulting in inconvenient maintenance of the electromechanical equipment.

[0003] In the prior art, a patent number (CN202223326467.4) mentions a maintenance device for electromechanical equipment, including a base, a U-shaped frame fixed on the base, a plurality of high-pressure nozzles fixedly arranged on the inner bottom surface of the U-shaped frame, two oppositely arranged vertical plates slidably arranged on the base, a clamping plate rotatably arranged on one side where the two vertical plates are close to each other, a cross bar arranged on the side surfaces of the two vertical plates, and a cleaning cotton slidably arranged on one side of the cross bar close to the vertical plate. The high-pressure nozzles can spray liquid on the equipment, and the cleaning cotton can scrub the equipment fixed between the two clamping plates. It can facilitate the maintenance of electromechanical equipment for aerospace use, effectively improve the dust cleaning effect of the electromechanical equipment, and effectively reduce the labor intensity of workers.

[0004] In the prior art, the addition of a U-shaped frame, high-pressure nozzles and a transmission mechanism effectively solves the problems that manual cleaning will cause relatively high labor intensity of workers, and washing with a water gun cannot effectively remove stubborn stains on the equipment, resulting in inconvenient maintenance of the electromechanical equipment. However, during long-term use, not only will dust accumulate, but the outer shell coating of the aviation equipment will also be damaged to a certain extent, and the current maintenance equipment cannot repair and maintain the coating. Content of the Utility Model

[0005] The purpose of the utility model is to provide a maintenance device for aviation electromechanical equipment, which solves the problems that during long-term use, not only will dust accumulate on the aviation equipment, but the outer shell coating of the aviation equipment will also be damaged to a certain extent, and the current maintenance equipment cannot repair and maintain the coating.

[0006] To achieve the above object, a maintenance device for aviation electromechanical equipment adopted by the present utility model includes a storage box and a mobile spraying assembly. The mobile spraying assembly includes a support frame, a bottom plate, moving wheels, rubber pads and a liquid outlet pipe. The support frame is detachably connected to the storage box and is located on the outer surface of the storage box. The bottom plate is detachably connected to the support frame and is located below the support frame. The moving wheels are detachably connected to the bottom plate and are located below the bottom plate. The rubber pads are detachably connected to the moving wheels and are located on one side of the moving wheels. The liquid outlet pipe passes through the support frame and is detachably connected to the storage box and is located at the output port of the storage box.

[0007] Wherein, the mobile spraying assembly further includes an extension plate, a handle, a cover and a support plate. The extension plate is detachably connected to the support frame and is located on the upper side of the support frame. The handle is detachably connected to the extension plate and is located on the side of the extension plate away from the support frame. One end of the support plate is detachably connected to the support frame and is located on the lower side of the support frame. The other end of the support plate is detachably connected to the handle and is located below the handle. The cover is detachably connected to the storage box and is located on the upper side of the storage box.

[0008] Wherein, the mobile spraying assembly further includes a pressure ring and a telescopic tube. The pressure ring is detachably connected to the liquid outlet pipe and is located on the side of the liquid outlet pipe away from the storage box. The telescopic tube is detachably connected to the pressure ring and is located on the side of the pressure ring away from the liquid outlet pipe.

[0009] Wherein, the mobile spraying assembly further includes a grip and a nozzle. The grip is detachably connected to the telescopic tube and is located on the side of the telescopic tube away from the pressure ring. The nozzle is detachably connected to the grip and is located on the side of the grip away from the telescopic tube.

[0010] Wherein, the maintenance device for aviation electromechanical equipment further includes an observation and protection assembly. The observation and protection assembly includes a protection pad, an observation port, a pull handle and a push groove. The protection pad is detachably connected to the cover and is located on the upper side of the cover. The observation port is detachably connected to the protection pad and is located inside the protection pad. The pull handle is detachably connected to the protection pad and is located on the upper side of the protection pad. The push groove is fixedly connected to the pull handle and is located on the outer surface of the pull handle.

[0011] An aviation electromechanical equipment maintenance device of the present utility model includes a storage box and a mobile spraying component. The mobile spraying component includes a support frame, a bottom plate, moving wheels, rubber pads, and a liquid outlet pipe. The support frame is detachably connected to the storage box and is located on the outer surface of the storage box. The bottom plate is detachably connected to the support frame and is located below the support frame. The moving wheels are detachably connected to the bottom plate and are located below the bottom plate. The rubber pads are detachably connected to the moving wheels and are located on one side of the moving wheels. The liquid outlet pipe passes through the support frame and is detachably connected to the storage box and is located at the output port of the storage box. Due to the addition of the mobile spraying component, it effectively solves the problem that not only will dust accumulate on aviation equipment during long-term use, but the outer shell coating of the aviation equipment will also be damaged to a certain extent, and the current maintenance equipment cannot repair and maintain the coating. BRIEF DESCRIPTION OF THE DRAWINGS

[0012] In order to more clearly illustrate the technical solutions in the embodiments of the present utility model or the prior art, the following will briefly introduce the drawings required for use in the description of the embodiments or the prior art. Obviously, the following drawings are only some embodiments of the present utility model. For those of ordinary skill in the art, without creative efforts, other drawings can also be obtained based on these drawings.

[0013] Figure 1 It is a schematic structural diagram of the whole of the first embodiment of the present utility model.

[0014] Figure 2 It is a front view of the whole of the first embodiment of the present utility model.

[0015] Figure 3 It is a side view of the whole of the first embodiment of the present utility model.

[0016] Figure 4 It is a schematic structural diagram of the whole of the second embodiment of the present utility model.

[0017] 101 - storage box, 102 - support frame, 103 - bottom plate, 104 - moving wheels, 105 - rubber pads, 106 - extension plate, 107 - handle, 108 - support plate, 109 - cover, 110 - liquid outlet pipe, 111 - pressure ring, 112 - telescopic pipe, 113 - grip, 114 - nozzle, 201 - protection pad, 202 - observation port, 203 - pull handle, 204 - push groove. DETAILED DESCRIPTION OF THE EMBODIMENTS

[0018] Embodiments of the present utility model will be described in detail below. Examples of the embodiments are shown in the accompanying drawings, where the same or similar reference numerals represent the same or similar elements or elements with the same or similar functions throughout. The embodiments described below with reference to the accompanying drawings are exemplary and are intended to explain the present utility model, and should not be construed as limiting the present utility model.

[0019] First Embodiment

[0020] Please refer to Figures 1 to 3 , Figure 1 which is a schematic structural diagram of the overall of the first embodiment of the present utility model, Figure 2 which is a front view of the overall of the first embodiment of the present utility model, Figure 3 which is a side view of the overall of the first embodiment of the present utility model.

[0021] The present utility model provides a maintenance device for aviation electromechanical equipment, including a storage box 101 and a mobile spraying assembly. The mobile spraying assembly includes a support frame 102, a bottom plate 103, moving wheels 104, rubber pads 105, a liquid outlet pipe 110, an extension plate 106, a handle 107, a cover 109, a support plate 108, a pressure ring 111, a telescopic pipe 112, a grip 113 and a spray head 114. Through the foregoing solution, the problem that not only dust will accumulate on the aviation equipment during long-term use, but also the outer shell coating of the aviation equipment will be damaged to a certain extent, and the current maintenance equipment cannot repair and maintain the coating is solved. It can be understood that when maintaining the outer shell coating of the aviation equipment, the storage box 101 and the support frame 102 will cooperate with the moving wheels 104, and then the staff will move the storage box 101 to the designated location. Then, the staff will hold the grip 113 and stretch the telescopic pipe 112. The maintenance liquid in the storage box 101 will be transmitted through the liquid outlet pipe 110, and then the pressure ring 111 will pressurize the maintenance liquid and spray it from the spray head 114 onto the outer shell of the aviation equipment. Thus, the problem that not only dust will accumulate on the aviation equipment during long-term use, but also the outer shell coating of the aviation equipment will be damaged to a certain extent, and the current maintenance equipment cannot repair and maintain the coating is effectively solved.

[0022] For this specific embodiment, the support frame 102 is detachably connected to the storage box 101 and is located on the outer surface of the storage box 101. The bottom plate 103 is detachably connected to the support frame 102 and is located below the support frame 102. The moving wheels 104 are detachably connected to the bottom plate 103 and are located below the bottom plate 103. The rubber pads 105 are detachably connected to the moving wheels 104 and are located on one side of the moving wheels 104. The liquid outlet pipe 110 passes through the support frame 102 and is detachably connected to the storage box 101 and is located at the output port of the storage box 101. The storage box 101 is a place for storing the maintenance liquid, and the support frame 102 is the main structural component for supporting the whole. The bottom plate 103 and the moving wheels 104 are functional structural components that effectively endow the whole with the function of free movement. The rubber pads 105 are auxiliary components for extending the service life of the moving wheels 104.

[0023] Among them, the extension plate 106 is detachably connected to the support frame 102 and is located on the upper side of the support frame 102. The handle 107 is detachably connected to the extension plate 106 and is located on the side of the extension plate 106 away from the support frame 102. One end of the support plate 108 is detachably connected to the support frame 102 and is located on the lower side of the support frame 102. The other end of the support plate 108 is detachably connected to the handle 107 and is located below the handle 107. The cover 109 is detachably connected to the storage box 101 and is located above the storage box 101. The extension plate 106, the support plate 108 and the handle 107 are auxiliary functional components for facilitating the staff to push the whole.

[0024] Secondly, the pressure ring 111 is detachably connected to the liquid outlet pipe 110 and is located on the side of the liquid outlet pipe 110 away from the storage box 101. The telescopic pipe 112 is detachably connected to the pressure ring 111 and is located on the side of the pressure ring 111 away from the liquid outlet pipe 110. The pressure pipe is a functional component for pressurizing the maintenance liquid, and the telescopic pipe 112 is a functional component for facilitating the staff to extend the spray head 114.

[0025] At the same time, the grip 113 is detachably connected to the telescopic pipe 112 and is located on the side of the telescopic pipe 112 away from the pressure ring 111. The spray head 114 is detachably connected to the grip 113 and is located on the side of the grip 113 away from the telescopic pipe 112. The grip 113 is an auxiliary component for facilitating the staff to hold the spray head 114.

[0026] When using the present utility model to maintain the coating of the housing of aviation equipment, the storage box 101 and the support frame 102 cooperate with the moving wheels 104, and then the staff moves the storage box 101 to the designated position. Then, the staff holds the grip 113 and stretches the telescopic tube 112, and the maintenance liquid in the storage box 101 is transmitted out through the liquid outlet pipe 110. Then, the pressurizing ring 111 pressurizes the maintenance liquid and sprays it from the nozzle 114 onto the housing of the aviation equipment. Thus, it effectively solves the problem that not only dust will accumulate on the aviation equipment during long-term use, but also the coating of the housing of the aviation equipment will be damaged to a certain extent, and the current maintenance equipment cannot repair and maintain the coating.

[0027] Second Embodiment

[0028] Please refer to Figure 4 , Figure 4 which is a schematic diagram of the overall structure of the second embodiment of the present utility model.

[0029] On the basis of the first embodiment, an aviation electromechanical equipment maintenance device of the present utility model further includes an observation and protection component, and the observation and protection component includes a protection pad 201, an observation port 202, a pull handle 203 and a push groove 204.

[0030] For this specific embodiment, the protection pad 201 is detachably connected to the cover 109 and is located above the cover 109. The observation port 202 is detachably connected to the protection pad 201 and is located inside the protection pad 201. The pull handle 203 is detachably connected to the protection pad 201 and is located above the protection pad 201. The push groove 204 is fixedly connected to the pull handle 203 and is located on the outer surface of the pull handle 203. The protection pad 201 is a protective auxiliary component that protects the cover 109 and the storage box 101 from damage from above, and the observation port 202 is an auxiliary functional component that facilitates the staff to observe the amount of maintenance liquid stored inside the storage box 101 in real time. The pull handle 203 and the push groove 204 are functional components that facilitate the staff to disassemble the cover 109 and the storage box 101.

[0031] The above-disclosed is only a preferred embodiment of the present utility model. Of course, it cannot be used to limit the scope of rights of the present utility model. Those of ordinary skill in the art can understand the entire or part of the process of implementing the above embodiments, and the equivalent changes made according to the claims of the present utility model still fall within the scope covered by the utility model.

Claims

1. An aviation electromechanical equipment maintenance device, including a storage box, characterized in that, it further includes a mobile spraying component, the mobile spraying component includes a support frame, a bottom plate, moving wheels, rubber pads and liquid outlet pipes. The support frame is detachably connected to the storage box and is located on the outer surface of the storage box. The bottom plate is detachably connected to the support frame and is located below the support frame. The moving wheels are detachably connected to the bottom plate and are located below the bottom plate. The rubber pads are detachably connected to the moving wheels and are located on one side of the moving wheels. The liquid outlet pipes pass through the support frame and are detachably connected to the storage box and are located at the output port of the storage box.

2. The aviation electromechanical equipment maintenance device according to claim 1, characterized in that, the mobile spraying component further includes an extension plate, a handle, a cover and a support plate. The extension plate is detachably connected to the support frame and is located on the upper side of one side of the support frame. The handle is detachably connected to the extension plate and is located on the side of the extension plate away from the support frame. One end of the support plate is detachably connected to the support frame and is located on the lower side of one side of the support frame. The other end of the support plate is detachably connected to the handle and is located below the handle. The cover is detachably connected to the storage box and is located above the storage box.

3. The aviation electromechanical equipment maintenance device according to claim 2, characterized in that, the mobile spraying component further includes a pressure ring and a telescopic tube. The pressure ring is detachably connected to the liquid outlet pipe and is located on the side of the liquid outlet pipe away from the storage box. The telescopic tube is detachably connected to the pressure ring and is located on the side of the pressure ring away from the liquid outlet pipe.

4. The aviation electromechanical equipment maintenance device according to claim 3, characterized in that, the mobile spraying component further includes a grip and a nozzle. The grip is detachably connected to the telescopic tube and is located on the side of the telescopic tube away from the pressure ring. The nozzle is detachably connected to the grip and is located on the side of the grip away from the telescopic tube.

5. The aviation electromechanical equipment maintenance device according to claim 4, characterized in that, the aviation electromechanical equipment maintenance device further includes an observation and protection component. The observation and protection component includes a protection pad, an observation port, a pull handle and a push groove. The protection pad is detachably connected to the cover and is located above the cover. The observation port is detachably connected to the protection pad and is located inside the protection pad. The pull handle is detachably connected to the protection pad and is located above the protection pad. The push groove is fixedly connected to the pull handle and is located on the outer surface of the pull handle.

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