阅读说明：本技术 一种地面式飞机表面盐雾高效去除系统 (System is got rid of to ground formula aircraft surface salt fog high efficiency ) 是由 马云鹏 于 2020-06-30 设计创作，主要内容包括：本发明公开一种地面式飞机表面盐雾高效去除系统,包括总控台和均与所述总控台电连接的全向擦洗装置、全向喷淋干燥装置、固定喷淋装置和回收检测装置,飞机可解除式位于所述固定喷淋装置上,所述固定喷淋装置纵向可拆卸式固定于所述回收检测装置的顶部中间位置处,所述全向擦洗装置和所述全向喷淋干燥装置均间隔设置于所述回收检测装置的上方左右两侧,所述全向擦洗装置和所述全向喷淋干燥装置均包括全向可调式固定于顶部的视觉导航组件和第二喷嘴组件。本发明的一种地面式飞机表面盐雾高效去除系统结构简单、操作方便、更加适用于飞机表面沉积污物的去除和清理、保证飞行安全、延长飞机使用寿命和减少维护成本。(The invention discloses a ground type airplane surface salt mist efficient removing system which comprises a master control console, an omnidirectional scrubbing device, an omnidirectional spraying drying device, a fixed spraying device and a recovery detecting device, wherein the omnidirectional scrubbing device, the omnidirectional spraying drying device, the fixed spraying device and the recovery detecting device are all electrically connected with the master control console, an airplane can be located on the fixed spraying device in a detachable mode, the fixed spraying device is longitudinally and detachably fixed at the middle position of the top of the recovery detecting device, the omnidirectional scrubbing device and the omnidirectional spraying drying device are arranged on the left side and the right side above the recovery detecting device at intervals, and the omnidirectional scrubbing device and the omnidirectional spraying drying device both comprise an omnidirectional adjustable visual navigation assembly and a second nozzle assembly which are fixed on the top. The ground type airplane surface salt mist efficient removing system is simple in structure, convenient to operate, more suitable for removing and cleaning deposited dirt on the surface of an airplane, capable of guaranteeing flight safety, long in service life of the airplane and low in maintenance cost.)

1. The utility model provides a system is got rid of to ground formula aircraft surface salt fog high efficiency which characterized in that: the all-directional scrubbing device, the all-directional spraying drying device, the fixed spraying device and the recovery detection device are electrically connected with the general control console, an airplane can be positioned on the fixed spraying device in a removable way, the fixed spraying device is longitudinally and detachably fixed at the middle position of the top of the recovery detection device, the all-directional scrubbing device and the all-directional spraying drying device are arranged at the left side and the right side above the recovery detection device at intervals, the all-directional scrubbing device and the all-directional spraying drying device respectively comprise an all-directionally adjustable visual navigation component and a second nozzle component which are fixed at the top, the visual navigation component is electrically connected with the general control console, the water outlet end of the second nozzle component faces towards the airplane body, the water inlet end of the second nozzle component is communicated with a water supply pipe, and the all-directional scrubbing device also comprises an all-directionally adjustable roller component which is fixed at the top, the roller assembly is detachably abutted to the airplane body, the omni-directional spray drying device further comprises a detachable drying air pipe fixed at the top, and an air port of the drying air pipe faces the airplane body.

2. The system of claim 1, wherein the system comprises: the omnidirectional scrubbing device and the omnidirectional spraying drying device comprise mechanical arms which are detachably fixed on the upper portion, the mechanical arms are electrically connected with the general control console, and the second nozzle assembly, the visual navigation assembly and the drying air pipe are all arranged along the direction of the mechanical arms from bottom to top, extend from the bottom of the mechanical arms to the top and are detachably fixed with the mechanical arms.

3. The system of claim 2, wherein the system comprises: the omnidirectional spraying drying device is provided with at least one first fixer along the direction of the mechanical arm, and the middle section of the drying air pipe is detachably fixed on the outer surface of the mechanical arm through the first fixer.

4. The system of claim 2, wherein the system comprises: the omnidirectional scrubbing device and the omnidirectional spraying drying device further comprise an omnidirectional moving type box body which is detachably fixed on the lower part, the omnidirectional moving type box body is movably arranged on the recovery detection device, and the mechanical arm is detachably fixed on the omnidirectional moving type box body.

5. The system of claim 4, wherein the system comprises: the omnidirectional spraying drying device and the omnidirectional scrubbing device further comprise an electric control module, the electric control module is detachably fixed in the omnidirectional moving type box body, the electric control module is electrically connected with the master console, and the mechanical arm is electrically connected with the electric control module.

6. The system of claim 1, wherein the system comprises: the recycling detection device comprises a recycling tank, a fixing plate, a first circulator and a detection cabinet, wherein the recycling tank is arranged at the bottom, the fixing plate is longitudinally arranged at the left side and the right side of the inside of the recycling tank, the water inlet end of the first circulator is arranged at the lowest horizontal point of the recycling tank, the water outlet end of the first circulator is communicated with the water inlet end of the detection cabinet, and the water outlet end of the detection cabinet is communicated with a water discharge pipe.

7. The system of claim 6, wherein the system comprises: the recycling tank comprises a detachable fixed waterproof layer and a framework, the waterproof layer is laid on the ground or the operation surface, the framework is detachably fixed on the waterproof layer, the workbench and the left side and the right side of the workbench are all arranged above the waterproof layer and are detachably fixed with the framework.

8. The system of claim 1, wherein the system comprises: the fixed spraying device comprises a workbench, a second circulator, a first nozzle component and a first pipeline, the workbench is longitudinally laid in the middle of the recovery detection device, the second circulator is detachably fixed on one side of the workbench, the airplane can be detachably positioned on the workbench, the workbench and the fixed plate are both positioned at the top of the recovery tank, the upper surface of the workbench is flush with the upper surface of the fixed plate, the first pipeline is detachably fixed at the bottom of the workbench, the first nozzle assembly is detachably arranged on the first pipeline at intervals, the workbench is provided with a water outlet hole at the position corresponding to the first nozzle assembly, the water inlet end of the first pipeline is communicated with the water outlet end of the second circulator, and the water inlet end of the second circulator is communicated with a water supply pipe.

9. The system of claim 1, wherein the system comprises: the second nozzle assembly comprises a nozzle mounting seat and at least one nozzle body, the nozzle body is detachably fixed on the front side of the nozzle mounting seat at intervals, and the water inlet end of the nozzle mounting seat is communicated with the water supply pipe.

10. The system of claim 1, wherein the system comprises: the roller assembly comprises a rotating shaft and a roller body, the rotating shaft is rotatably connected with the mechanical arm, the roller body is sleeved on the periphery of the rotating shaft, and a felt is adhered to the surface of the roller body.

Technical Field

The invention relates to the technical field of aviation manufacturing, in particular to a ground type airplane surface salt mist efficient removing system.

Background

The salt fog removing system of the aircraft in the prior art at home and abroad can only remove the seawater salt stain layer on the outer surface of the front windshield glass in the flying process, and provides clear vision for flying personnel in real time.

The existing technical problems are as follows: the system is used for cleaning the windshield of the airplane in the flying process of the airplane, and has the limitations of operation space and operation objects. The seawater salt stain dirt layer on the outer surface of the windshield glass is difficult to remove, and is removed in the flying process of an airplane, so that the seawater salt stain dirt layer can be influenced by the external environment which changes constantly, the safety of the airplane windshield structure and the operation of a pilot are influenced, and certain danger is realized. The system only removes salt stain on the windshield glass, and the salt mist deposited on the actual airplane body is easy to cause surface corrosion, so that the service life and the use safety of the airplane are influenced. If the airplane body is subjected to salt fog removal treatment on the parking apron in a manual mode, the airplane can be frozen due to residual liquid generated in the salt fog removal process, and flight delay is caused; the desalted mist liquid is not easy to clean after the desalted mist operation, and causes pollution to the parking apron of the airport.

In addition, most of the foreign large-scale airlines use large-scale mechanical arms and cleaning robots for cleaning the surfaces of airplanes, which are large and complex in mechanical structure and high in cost, and are often only specific to a certain model, so that the method is not suitable for being widely popularized and used in airports.

Disclosure of Invention

The invention aims to solve the defects in the prior art, and the invention aims to provide a ground type aircraft surface salt mist efficient removing system which is simple in structure, convenient to operate, more suitable for removing and cleaning deposited dirt on the surface of an aircraft, capable of ensuring flight safety, prolonging the service life of the aircraft and reducing maintenance cost.

The invention relates to a ground type airplane surface salt fog high-efficiency removing system, which comprises a master control station, an omnidirectional scrubbing device, an omnidirectional spraying drying device, a fixed spraying device and a recovery detecting device, wherein the omnidirectional scrubbing device, the omnidirectional spraying drying device, the fixed spraying device and the recovery detecting device are all electrically connected with the master control station, an airplane can be positioned on the fixed spraying device in a detachable mode, the fixed spraying device is longitudinally and detachably fixed at the middle position of the top of the recovery detecting device, the omnidirectional scrubbing device and the omnidirectional spraying drying device are arranged at the left side and the right side above the recovery detecting device at intervals, the omnidirectional scrubbing device and the omnidirectional spraying drying device respectively comprise an omnidirectional adjustable visual navigation component and a second nozzle component which are fixed at the top, the visual navigation component is electrically connected with the master control station, the water outlet end of the second nozzle component faces the airplane body, the water inlet end of the second nozzle component is communicated with a water, the omnidirectional scrubbing device further comprises an omnidirectional adjustable roller assembly fixed at the top, the roller assembly is detachably abutted to the airplane body, the omnidirectional spraying drying device further comprises a detachable drying air pipe fixed at the top, and an air port of the drying air pipe faces the airplane body.

The invention also discloses a system for efficiently removing salt fog on the surface of a ground plane, which comprises the following steps:

the omnidirectional scrubbing device and the omnidirectional spraying drying device all comprise detachable mechanical arms fixed on the upper part, the mechanical arms are electrically connected with the master console, the second nozzle assembly, the visual navigation assembly and the drying air pipe are all arranged along the direction from bottom to top of the mechanical arms, the bottom of the mechanical arms extends to the top, and the mechanical arms are detachably fixed.

The omnidirectional spraying drying device is provided with at least one first fixer along the direction of the mechanical arm, and the middle section of the drying air pipe is detachably fixed on the outer surface of the mechanical arm through the first fixer.

The omnidirectional scrubbing device and the omnidirectional spraying drying device further comprise an omnidirectional moving type box body which is detachably fixed on the lower part, the omnidirectional moving type box body is movably arranged on the recovery detection device, and the mechanical arm is detachably fixed on the omnidirectional moving type box body.

The omnidirectional spraying drying device and the omnidirectional scrubbing device further comprise an electric control module, the electric control module is detachably fixed in the omnidirectional moving type box body, the electric control module is electrically connected with the master control console, and the mechanical arm is electrically connected with the electric control module.

The recycling detection device comprises a recycling tank, a fixing plate, a first circulator and a detection cabinet, wherein the recycling tank is arranged at the bottom, the fixing plate is longitudinally arranged at the left side and the right side of the inside of the recycling tank, the water inlet end of the first circulator is arranged at the lowest horizontal point of the recycling tank, the water outlet end of the first circulator is communicated with the water inlet end of the detection cabinet, and the water outlet end of the detection cabinet is communicated with a water discharge pipe.

The recycling tank comprises a detachable fixed waterproof layer and a framework, the waterproof layer is laid on the ground or the operation surface, the framework is detachably fixed on the waterproof layer, the workbench and the left side and the right side of the workbench are all arranged above the waterproof layer, and the framework is detachably fixed.

The fixed spraying device comprises a workbench, a second circulator, a first nozzle component and a first pipeline, the workbench is longitudinally laid at the middle position of the recovery detection device, the second circulator is detachably fixed on one side of the workbench, the airplane is detachably positioned on the workbench, the workbench and the fixed plate are both positioned at the top of the recovery tank, the upper surface of the workbench is flush with the upper surface of the fixed plate, the first pipeline is detachably fixed at the bottom of the workbench, the first nozzle assembly is detachably arranged on the first pipeline at intervals, the workbench is provided with a water outlet hole at the position corresponding to the first nozzle assembly, the water inlet end of the first pipeline is communicated with the water outlet end of the second circulator, and the water inlet end of the second circulator is communicated with a water supply pipe.

The second nozzle assembly comprises a nozzle mounting seat and at least one nozzle body, the nozzle body is detachably fixed on the front side of the nozzle mounting seat at intervals, and the water inlet end of the nozzle mounting seat is communicated with the water supply pipe.

The roller assembly comprises a rotating shaft and a roller body, the rotating shaft is rotatably connected with the mechanical arm, the roller body is sleeved on the periphery of the rotating shaft, and a felt is adhered to the surface of the roller body.

The invention relates to a ground type airplane surface salt fog high-efficiency removing system, which comprises a master control station, an omnidirectional scrubbing device, an omnidirectional spraying drying device, a fixed spraying device and a recovery detecting device, wherein the omnidirectional scrubbing device, the omnidirectional spraying drying device, the fixed spraying device and the recovery detecting device are all electrically connected with the master control station, an airplane can be positioned on the fixed spraying device in a detachable mode, the fixed spraying device is longitudinally and detachably fixed at the middle position of the top of the recovery detecting device, the omnidirectional scrubbing device and the omnidirectional spraying drying device are arranged at the left side and the right side above the recovery detecting device at intervals, the omnidirectional scrubbing device and the omnidirectional spraying drying device respectively comprise an omnidirectional adjustable visual navigation component and a second nozzle component which are fixed at the top, the visual navigation component is electrically connected with the master control station, the water outlet end of the second nozzle component faces the airplane body, the water inlet end of the second nozzle component is communicated with a water, the omnidirectional scrubbing device further comprises an omnidirectional adjustable roller assembly fixed at the top, the roller assembly is detachably abutted to the airplane body, the omnidirectional spraying drying device further comprises a detachable drying air pipe fixed at the top, and an air port of the drying air pipe faces the airplane body. Thus, the airplane can be positioned on the fixed spray device in a detachable way, the fixed spray device is longitudinally and detachably fixed at the middle position of the top of the recovery detection device, the omnidirectional scrubbing device and the omnidirectional spray drying device are arranged at the left side and the right side above the recovery detection device at intervals, the omnidirectional scrubbing device and the omnidirectional spray drying device respectively comprise an omnidirectional adjustable visual navigation component fixed at the top, the visual navigation component is electrically connected with the general control console, package protection work is carried out on the key position of the airplane after the airplane reaches the fixed spray device, when salt mist removal work starts, the general control console sends an instruction to start one of the omnidirectional scrubbing devices to move to the vicinity of the airplane, and the rest of the omnidirectional scrubbing devices and the omnidirectional spray drying device are stopped in situ, the visual navigation assembly is used for collecting and transmitting the airplane appearance information to the master control console, the master control console plans a moving path, a collaborative operation flow, a scrubbing force, a spray head pressure, a drying time, a desalting expected effect and the like, then transmits instructions to the omnidirectional scrubbing device, the omnidirectional spray drying device and the fixed spray device, the omnidirectional scrubbing device, the omnidirectional spray drying device and the fixed spray device respectively carry out collaborative operation on the airplane, the omnidirectional scrubbing device further comprises an omnidirectional adjustable roller assembly fixed at the top, the roller assembly is in releasable contact with the airplane body, the roller assembly rubs and cleans the serious salt fog deposition part on the outer surface of the airplane body according to the instructions, and the master control console simultaneously starts the recovery detection device to carry out component detection and analysis on the waste and polluted liquid after the salt fog removal operation, and the salt content after the desalination is detected to meet the specification, so that the quality of the desalination work is ensured. And after the detection is qualified, the drying air pipe is communicated with the fan, and the fan is started to dry the surface of the airplane, so that the secondary pollution of the surface of the airplane caused by residual moisture after the salt mist removal operation is prevented. The omnidirectional spray drying device further comprises a detachable drying air pipe fixed at the top, the air port of the drying air pipe faces the airplane body, after the detection is qualified, the drying air pipe dries the airplane body according to an instruction, salt mist removal and drying cleaning work are completed, the omnidirectional spray drying device moves to an initial safe position and stops working, the fixed spray device stops working with the recovery detection device, and the airplane leaves the workbench. Wherein the electrical connection includes a wireless electrical connection and a wired electrical connection.

Drawings

FIG. 1 is a schematic structural diagram of a system for efficiently removing salt fog from the surface of a ground plane.

FIG. 2 is a schematic view of a recovery detection device of the ground-type airplane surface salt fog efficient removal system.

FIG. 3 is a schematic view of an omnidirectional scrubbing device of a ground-based airplane surface salt fog efficient removal system.

FIG. 4 is an enlarged view of the top of an omnidirectional scrubbing device of a ground-based aircraft surface salt spray efficient removal system of the present invention.

FIG. 5 is a schematic diagram of an omnidirectional spray drying device of a ground-type airplane surface salt fog efficient removal system.

FIG. 6 is an enlarged top view of the omnidirectional spray drying device of the efficient salt spray removal system on the surface of the ground plane.

FIG. 7 is a schematic diagram of a part of a recovery detection device of a ground-type airplane surface salt fog efficient removal system.

FIG. 8 is a schematic illustration of a system for efficiently removing salt spray from the surface of a surface-mounted aircraft, shown in FIG. 7 with a portion of the work bench removed.

Description of the figures

1 … fixed plate 2 … workbench 3 … omnidirectional scrubbing device

4 … omnidirectional spray drying device 5 … detection cabinet 6 … first circulator

7 … second circulator 8 … first line 9 … first nozzle assembly

10 … Mecanum wheel body 11 … Mecanum wheel base 12 … second conduit

13 … second nozzle Assembly 14 … rear mechanical arm 15 … front mechanical arm

16 … roller assembly 17 … second holder 18 … visual navigation camera

19 … Omni-directional movable box 20 … first fixer 21 … dry air pipe

22 … water booster 23 … nozzle body 24 … nozzle mounting seat

25 … planetary motor reducer 26 … coupling 27 … bearing

28 … roller body 29 … rotating shaft

Detailed Description

In the description of the present invention, it should be noted that the terms "upper", "lower", "left", "right", "inner", "outer", "vertical", "horizontal", etc., indicating the orientation or positional relationship, are used as the orientation or positional relationship shown in the drawings only for the convenience of describing the present invention and simplifying the description, and do not indicate or imply that the device or element referred to must have a specific orientation, be constructed and operated in a specific orientation, and thus, should not be construed as limiting the present invention. Furthermore, the terms "first," "second," and "third" are used for descriptive purposes only and are not to be construed as indicating or implying relative importance.

The efficient salt fog removing system for the surface of the ground-type airplane is further described in detail with reference to fig. 1 to 8 of the accompanying drawings.

The invention relates to a ground type airplane surface salt fog high-efficiency removing system, which refers to related figures in figures 1 to 8, and comprises a master control station, an omnidirectional scrubbing device 3, an omnidirectional spray drying device 4, a fixed spray device and a recovery detection device which are all electrically connected with the master control station, wherein an airplane can be positioned on the fixed spray device in a release mode, the fixed spray device is longitudinally and detachably fixed at the middle position of the top of the recovery detection device, the omnidirectional scrubbing device 3 and the omnidirectional spray drying device 4 are both arranged at the left side and the right side above the recovery detection device at intervals, the omnidirectional scrubbing device 3 and the omnidirectional spray drying device 4 both comprise an omnidirectional adjustable visual navigation component and a second nozzle component 13 which are fixed at the top, the visual navigation component is electrically connected with the master control station, and the water outlet end of the second nozzle component 13 faces to the airplane body, the water inlet end of the second nozzle assembly 13 is communicated with a water supply pipe, the omnidirectional scrubbing device 3 further comprises a drum assembly 16 which is fixed at the top in an omnidirectional adjustable mode, the drum assembly 16 is in releasable offset with the airplane body, the omnidirectional spraying drying device 4 further comprises a drying air pipe 21 which is fixed at the top in a detachable mode, and an air opening of the drying air pipe 21 faces the airplane body. Thus, the airplane can be positioned on the fixed spray device in a detachable way, the fixed spray device is longitudinally and detachably fixed at the middle position of the top of the recovery detection device, the omnidirectional scrubbing device 3 and the omnidirectional spray drying device 4 are arranged at the left side and the right side above the recovery detection device at intervals, the omnidirectional scrubbing device 3 and the omnidirectional spray drying device 4 comprise omnidirectional adjustable visual navigation components fixed at the top, the visual navigation components are electrically connected with the master control console, the airplane packages and protects the important parts of the airplane after arriving at the fixed spray device, when the work of removing salt mist starts, the master control console sends an instruction to start one of the omnidirectional scrubbing devices 3 to move to the vicinity of the airplane, and the rest of the omnidirectional scrubbing devices 3 and the omnidirectional spray drying device 4 are stopped at the original position, the visual navigation component is used for collecting and transmitting the airplane appearance information to the master control console, the master control console plans a moving path, a cooperative operation flow, a scrubbing force, a spray head pressure, a drying time, an expected desalting effect and the like, then an instruction is transmitted to the omnidirectional scrubbing device 3, the omnidirectional spray drying device 4 and the fixed spray device, the omnidirectional scrubbing device 3, the omnidirectional spray drying device 4 and the fixed spray device respectively perform cooperative operation on the airplane, the omnidirectional scrubbing device 3 further comprises an omnidirectional adjustable roller component 16 fixed at the top, the roller component 16 is in releasable contact with the airplane body, the roller component 16 performs friction cleaning on the serious salt spray deposition part on the outer surface of the airplane body according to the instruction, the master control console simultaneously starts the recovery detection device to perform component detection analysis on the waste and dirty liquid after the salt spray operation, the salt content after the desalination is detected to meet the regulations, and the quality of the desalination work is ensured. After the detection is qualified, the drying air pipe 21 is communicated with the fan, the fan is started to dry the surface of the airplane, and secondary pollution to the surface of the airplane caused by residual moisture after the salt fog removal operation is prevented. The omnidirectional spray drying device 4 further comprises a detachable drying air pipe 21 fixed at the top, an air port of the drying air pipe 21 faces the aircraft body, after the detection is qualified, the drying air pipe 21 dries the aircraft body according to an instruction, salt mist removal and drying cleaning work are completed, the omnidirectional spray drying device 3 and the omnidirectional spray drying device 4 move to an initial safe position and stop working, the fixed spray device stops working after the recovery detection device stops working, and the aircraft leaves the workbench 2. Wherein the electrical connection includes a wireless electrical connection and a wired electrical connection. Compared with the prior art, the ground type airplane surface salt fog efficient removing system has the advantages that: the device has the advantages of simple structure and convenient operation, is more suitable for removing and cleaning deposited dirt on the surface of the airplane, ensures the flight safety, prolongs the service life of the airplane and reduces the maintenance cost.

Referring to the relevant figures in fig. 1 to 8, the system for efficiently removing salt fog on the surface of a ground plane of the present invention may specifically be: the omnidirectional scrubbing device 3 and the omnidirectional spraying drying device 4 comprise detachable mechanical arms fixed on the upper portions, the mechanical arms are electrically connected with the general control console, and the second nozzle assemblies 13, the visual navigation assemblies and the drying air pipes 21 are all arranged along the direction of the mechanical arms from bottom to top, extend from the bottoms of the mechanical arms to the tops, and are detachably fixed with the mechanical arms. Therefore, when the visual navigation component collects the appearance information of the airplane, the motion trail of the mechanical arm moves in all directions according to the instruction of the master console, and when the airplane is subjected to desalting operation, the mechanical arm performs cooperative operation according to the movement path planned by the master console. A further preferred technical scheme is that the omnidirectional spray drying device 4 is provided with at least one first fixer 20 along the direction of the mechanical arm, and the middle section of the drying air pipe 21 is detachably fixed with the outer surface of the mechanical arm through the first fixer 20. Like this, the one end and the fan intercommunication of dry tuber pipe 21, the other end of dry tuber pipe 21 with the front end of arm is detachable fixed, the middle section of dry tuber pipe 21 through first fixer 20 with the surface detachable fixed of arm, it is whole dry tuber pipe 21 depends on the surface of arm prevents dry tuber pipe 21 places at will, avoids dry tuber pipe 21 is easily by the fifty percent discount when bending and takes place the fracture, perhaps dry tuber pipe 21 drags at will lead to being pressed on the recovery detection device and roll over. A further preferred technical solution is that the omnidirectional scrubbing device 3 and the omnidirectional spraying and drying device 4 are provided with at least one second fixer 17 along the direction of the mechanical arm, and the middle section of the second pipeline 12 is detachably fixed to the outer surface of the mechanical arm through the second fixer 17. Like this, the one end of second pipeline 12 with the third circulator intercommunication, the other end of second pipeline 12 with the front end detachable of arm is fixed, the middle section of second pipeline 12 pass through second fixer 17 with the outer surface detachable of arm is fixed, and is whole second pipeline 12 depends on the surface of arm prevents second pipeline 12 places at will, avoids second pipeline 12 is easily by the fifty percent discount when bending and takes place the weeping danger, perhaps second pipeline 12 drags at will lead to being folded by pressure on the recovery detection device. A further preferred technical solution is that the mechanical arm includes a front mechanical arm 15 and a rear mechanical arm 14, a lower end of the rear mechanical arm 14 is rotatably fixed to the omni-directional movement type box 19, an upper end of the rear mechanical arm 14 is rotatably fixed to a rear end of the front mechanical arm 15, the visual navigation camera 18, the roller assembly 16, the second nozzle assembly 13, and the drying duct 21 are detachably fixed to a front end of the front mechanical arm 15 at a position corresponding thereto, and the first holder 20 is detachably fixed to outer surfaces of the front mechanical arm 15 and the rear mechanical arm 14, respectively. Thus, the rear mechanical arm 14 can rotate around the omnidirectional moving type box 19, the front mechanical arm 15 rotates around the top of the rear mechanical arm 14, and then the mechanical arm can be adjusted to various positions, heights and movement tracks preset by the master control console on the omnidirectional moving type box 19, so as to perform fine repeated washing and salt mist removing operation on the airplane, the adaptability is stronger, salt mist removing operation can be performed on various parts of the airplane, the visual navigation camera 18, the roller assembly 16, the second nozzle assembly 13 and the drying air pipe 21 are detachably fixed at the front end of the front mechanical arm 15 at the corresponding position, when the front mechanical arm 15 rotates around the top of the rear mechanical arm 14, and the rear mechanical arm 14 rotates around the omnidirectional moving type box 19, the second pipeline 12 can continuously perform washing and salt mist removing operation on airplanes of various types along with the movement tracks of the mechanical arm .

Referring to the relevant figures in fig. 1 to 8, the system for efficiently removing salt fog on the surface of a ground plane of the present invention may further include: the omnidirectional scrubbing device 3 and the omnidirectional spraying drying device 4 further comprise an omnidirectional moving type box body 19 which is detachably fixed on the lower part, the omnidirectional moving type box body 19 is movably arranged on the recovery detection device, and the mechanical arm is detachably fixed on the omnidirectional moving type box body 19. Therefore, the omni-directional mobile box body 19 is fixed at the bottom of the mechanical arm, and part of electrical peripherals and other equipment can be detachably fixed inside the omni-directional mobile box body 19, so that waterproof and other protective measures can be conveniently carried out on the external equipment. A further preferred technical scheme is that the omni-directional mobile box 19 comprises a shell and a support, the support is movably arranged on the recovery detection device, the mechanical arm is detachably fixed at the top of the support, and the periphery of the platform support is fixed with the support. Thus, the electric control module, the visual navigation positioning module, the third circulator and the fan are all detachably fixed on the inner side of the bracket in the corresponding omnidirectional scrubbing device 3 and the omnidirectional spray drying device 4, the outer shell is fixed with the bracket at the periphery of the bracket, the outer shell covers the outer sides of the electric control module, the visual navigation positioning module, the third circulator and the fan, and liquid for washing the surface of the airplane is prevented from splashing to the electric control module, the visual navigation positioning module, the third circulator and the fan, because the electric control module, the visual navigation positioning module, the third circulator and the fan are all electrically connected, liquid splashes to the electric control module, the visual navigation positioning module, the third circulator and the fan, so that a short circuit phenomenon is easily caused, and the whole equipment is burnt. Further preferred technical scheme does the shell is made by the cold-rolled sheet of 2mm thick, the platform support is made by square pipe, moving platform's top with the detachable fixing of bolt is passed through to the bottom of electric lift slip table. Like this, the shell is bent by the cold rolling sheet that 2mm is thick and is welded the back spraying and mould and form, whole the shell forms an overall structure, prevents the shell leads to liquid infiltration because the hole that the concatenation probably arouses. A further preferred technical scheme is that the omnidirectional spray drying device 4 further comprises a fan, the fan is detachably fixed in the omnidirectional movable box 19, and the drying air pipe 21 is communicated with the fan. Like this, retrieve detection device and detect qualified back because dry tuber pipe 21 with the fan intercommunication opens during the fan, the fan improves gas pressure and passes through gas dry tuber pipe 21 discharges to the aircraft surface, and then carries out the drying to the aircraft surface, prevents that the remaining moisture from causing aircraft surface secondary pollution after the desalinization fog work. A further preferable technical solution is that the visual navigation assembly comprises a visual navigation camera 18 and a visual navigation positioning module, the visual navigation camera 18 is detachably fixed at the top of the mechanical arm, the visual navigation positioning module is detachably fixed in the omni-directional mobile box 19, the visual navigation camera 18 is electrically connected with the visual navigation positioning module, and the visual navigation positioning module is electrically connected with the console. In this way, the vision navigation camera 18 is electrically connected with the vision navigation positioning module, the vision navigation positioning module is electrically connected with the master console, the vision navigation camera 18 performs initial survey on the surface of the airplane, transmits the acquired information to the vision navigation positioning module, the vision navigation positioning module synthesizes the information and then transmits the information to the master console, and the master console sends regulation and control commands to the omnidirectional scrubbing device 3, the omnidirectional spray drying device 4, the fixed spray device and the like according to actual conditions.

Referring to the relevant figures in fig. 1 to 8, the system for efficiently removing salt fog on the surface of a ground plane of the present invention may further include: the omnidirectional spraying drying device 4 and the omnidirectional scrubbing device 3 further comprise an electric control module, the electric control module is detachably fixed in the omnidirectional moving type box body 19, the electric control module is electrically connected with the master console, and the mechanical arm is electrically connected with the electric control module. Therefore, the main control console sends the instruction to the electric control module, the electric control module controls the mechanical arm to move according to the instruction of the main control console, the moving track of the mechanical arm is accurately controlled, and salt mist stains of the airplane body are removed in a targeted mode.

Referring to the relevant figures in fig. 1 to 8, the system for efficiently removing salt fog on the surface of a ground plane of the present invention may further include: the recycling detection device comprises a recycling tank, a fixing plate 1, a first circulator 6 and a detection cabinet 5, wherein the recycling tank is arranged at the bottom, the fixing plate 1 is longitudinally arranged at the left side and the right side of the recycling tank, the water inlet end of the first circulator 6 is arranged at the lowest horizontal point of the recycling tank, the water outlet end of the first circulator 6 is communicated with the water inlet end of the detection cabinet 5, and the water outlet end of the detection cabinet 5 is communicated with a drain pipe. Therefore, the water inlet end of the first circulator 6 is arranged at the lowest horizontal point of the recovery tank, the water outlet end of the first circulator 6 is communicated with the detection cabinet 5, the waste liquid is pumped into the detection cabinet 5 through the first circulator 6, the detection cabinet 5 performs component detection and analysis on the waste liquid, the salt content after the detection and the desalination meet the specification, and the quality of the desalination work is ensured. The fixing plate 1 may be a punched plate or the like. The first circulator 6 may be a suction pump or the like. Further preferred technical scheme does the recovery pond includes fixed waterproof layer of detachable and skeleton, the waterproof layer is laid on ground or the working face, the skeleton is detachable to be fixed in on the waterproof layer, workstation 2 and the left and right sides 1 three of fixed plate all are in the top of waterproof layer and with the skeleton is detachable fixed. Like this, the waterproof layer has fine sealed effect to the waste liquid after washing the aircraft, prevents that waste liquid from passing through the position infiltration soil at recovery pond place, and then to the environment in the regional scope in the vicinity of recovery pond place causes the pollution, arouses a series of environmental degradation etc.. The framework can be made of large section steel and other section materials, because the section materials are objects with certain geometrical shapes made of iron or steel and materials with certain strength and toughness through processes of rolling, extruding, forging and the like, the framework made of the section materials can form certain supporting force in the process of airplane cleaning, and the workbench 2 cannot be directly pressed on the waterproof layer in the process of airplane cleaning. The further preferred technical scheme does the waterproof layer includes the tarpaulin, the tarpaulin is made by airtight membrane material, the waterproof layer with the skeleton passes through the detachable fixed of splint, the movable guide rail workstation 2 with fixed plate 1 all through the bolt with the skeleton detachable fixed. Therefore, the airtight membrane has the characteristics of good sealing performance and high strength, and has good sealing effect on waste liquid. The waterproof layer with the skeleton passes through the detachable fixed of splint, makes the waterproof layer is located all the time the bottom of skeleton, and moving guide the workstation 2 with fixed plate 1 is all fixed in the frame that the skeleton is constituteed, and all is located the waterproof layer top, like this, wash the useless dirty liquid process behind the aircraft workstation 2 with all collect behind the fixed plate on the waterproof layer, made things convenient for the collection of useless dirty liquid then cyclic utilization. In a further preferred embodiment, the first circulator 6 and the second circulator 7 are detachably fixed to the framework. Like this, be located the inside lowest of waterproof layer first circulator 6 is fixed on the skeleton, make first circulator 6's rigidity, and then first circulator 6 is fixed all the time the lowest of waterproof layer is fixed like this can in time be as far as possible with useless waste liquid recovery cyclic utilization, prevent to pollute the surrounding environment. The second circulator 7 is fixed on the framework at one side of the workbench 2, so that the second circulator 7 and the workbench 2 keep relative positions, and the first pipeline 8 is prevented from being broken due to the displacement of the second circulator 7.

Referring to the relevant figures in fig. 1 to 8, the system for efficiently removing salt fog on the surface of a ground plane of the present invention may further include: the fixed spraying device comprises a workbench 2, a second circulator 7, a first nozzle assembly 9 and a first pipeline 8, the workbench 2 is longitudinally laid at the middle position of the recovery detection device, the second circulator 7 is detachably fixed at one side of the workbench 2, the airplane can be positioned on the workbench 2 in a release manner, the workbench 2 and the fixed plate 1 are positioned at the top of the recovery pool, the upper surface of the workbench 2 is flush with the upper surface of the fixed plate 1, the first pipeline 8 is detachably fixed at the bottom of the workbench 2, the first nozzle assembly 9 is detachably arranged on the first pipeline 8 at intervals, the workbench 2 is provided with a water outlet hole at the position corresponding to the first nozzle assembly 9, the water inlet end of the first pipeline 8 is communicated with the water outlet end of the second circulator 7, and the water inlet end of the second circulator 7 is communicated with a water supply pipe. Thus, the working table 2 is longitudinally arranged at the central position of the recovery detection device, the fixed plate 1 is detachably and fixedly arranged at the left side and the right side of the working table 2 respectively, the inner side of the fixed plate 1 is detachably and fixedly connected with the working table 2, the outer side of the fixed plate 1 is detachably and fixedly connected with the recovery tank, so that the upper surface of the fixed plate 1 and the upper surface of the working table 2 are kept on the same horizontal plane, the first pipeline 8 is arranged below the working table 2, the first nozzles are detachably and fixedly arranged on the first pipeline 8 at intervals, the working table 2 is provided with water outlet holes at the positions corresponding to the first nozzles, the water inlet end of the first pipeline 8 is communicated with the first circulator 6, the water inlet end of the first circulator 6 is communicated with a water supply pipe, and when the first circulator 6 is started, the first circulator 6 pumps the liquid in the water supply pipe, the liquid can be sprayed to the bottom of the airplane through the water outlet after being sprayed out of the first nozzle, and the salt stain dirt attached to the surface of the airplane can be removed by the salt mist removing component in the liquid. The second circulator 7 may be a suction pump or the like.

Referring to the relevant figures in fig. 1 to 8, the system for efficiently removing salt fog on the surface of a ground plane of the present invention may further include: the second nozzle assembly 13 includes a nozzle mounting seat 24 and at least one nozzle body 23, the nozzle body 23 is detachably fixed to the front side of the nozzle mounting seat 24 at intervals, and the water inlet end of the nozzle mounting seat 24 is communicated with the water supply pipe. Like this, it is a plurality of nozzle body 23 is detachable to be fixed in the front side of nozzle mount pad 24 will salt fog washing liquid and clear water reposition of redundant personnel in the second pipeline 12 become a plurality of little water columns, have increased the coverage area that sprays of salt fog washing liquid and clear water, improve the operating efficiency. A further preferred technical solution is that the omnidirectional spray drying device 4 and the omnidirectional scrubbing device 3 further include a third circulator, the third circulator is detachably fixed in the omnidirectional movable box 19, the second nozzle assembly 13 is communicated with the third circulator through a second pipeline 12, the third circulator is communicated with the water supply pipe, and the third circulator is detachably fixed in the omnidirectional movable box 19. Therefore, the salt spray removing liquid is pumped out of the water supply pipe and sent into the second pipeline 12 by the third circulator and then sent to the second nozzle assembly 13, the water outlet end of the second nozzle assembly 13 faces the airplane body, the salt spray removing liquid can be directly sprayed to the airplane body, and the third circulator provides larger power for the salt spray removing liquid, so that the salt spray removing liquid has certain scouring force when being sprayed to the airplane body. The third circulator may be a suction pump or the like. In a further preferable technical solution, a water pressurizer 22 is disposed at a water inlet end of the second nozzle assembly 13, and a water inlet end and a water outlet end of the water pressurizer 22 are respectively communicated with the third circulator and the nozzle mounting seat 24. In this way, the water pressurizer 22 can pressurize the liquid in the second pipeline 12 to form high-pressure water columns to be sprayed out from the second nozzle assembly 13, so that the liquid has stronger pressure to clean the dirt when washing the surface of the airplane. The water booster 22 may be a high pressure pipe joint pump.

Referring to the relevant figures in fig. 1 to 8, the system for efficiently removing salt fog on the surface of a ground plane of the present invention may further include: the roller assembly 16 comprises a rotating shaft 29 and a roller body 28, the rotating shaft 29 is rotatably connected with the mechanical arm, the roller body 28 is sleeved on the periphery of the rotating shaft 29, and felt is adhered to the surface of the roller body 28. Therefore, when the friction cleaning is carried out on the parts with serious salt mist deposition, the felt prevents the surface of the airplane from being damaged due to the large friction force generated by the roller assembly 16 and the surface of the airplane, and simultaneously, due to the soft characteristic of the surface, each part of the omnidirectional scrubbing device 3 has a certain compression distance with the surface of the airplane, so that the possible damage to the surface of the airplane is reduced. A planetary motor reducer 25 is detachably fixed between the roller assembly 16 and the mechanical arm, the planetary motor reducer 25 is detachably fixed with the mechanical arm, and the roller assembly 16 is detachably fixed with the planetary motor reducer 25 through a coupler 26. Thus, the planetary motor reducer 25 can reduce the rotation speed of the motor while increasing the output torque. The roller assembly 16 has the advantages of attractive overall structure, compact structure, space saving, large output torque and capability of effectively ensuring the strength of the roller assembly 16 for scrubbing the surface of the airplane so as to ensure the effective removal of salt spray.

Referring to the relevant figures in fig. 1 to 8, the system for efficiently removing salt fog on the surface of a ground plane of the present invention may further include: mecanum wheel base 11 is detachably fixed to the bottom of omnidirectional movement formula box 19, each detachably is fixed with mecanum wheel body 10 on four angles of mecanum wheel base 11. Thus, the mecanum wheel body 10 is based on the principle of a central wheel having a number of wheel axles located at the periphery of the wheel, the angled peripheral wheel axles translating a portion of the wheel steering force to a wheel normal force. Depending on the direction and speed of the respective wheels, the resulting combination of these forces produces a resultant force vector in any desired direction, thereby ensuring that the mecanum wheel base 11 can move autonomously in the direction of the resultant force vector without changing the direction of the mecanum wheel body 10 itself. A plurality of small rollers are diagonally distributed on the rim of the mecanum wheel body 10 so that the wheel can slide laterally. The generatrix of the small rollers is particularly so that the envelope of each small roller is cylindrical when the wheel is turned around a fixed wheel spindle, so that the wheel can roll forward continuously. The mecanum wheel body 10 is compact in structure and flexible in movement, and is a successful omnidirectional wheel. Mecanum wheel base 11 has 4 this kind of novel wheels to make up, can be more nimble convenient realization all direction movement function.

The above description is only for the purpose of illustrating a few embodiments of the present invention, and should not be taken as limiting the scope of the present invention, in which equivalent changes, modifications, or scaling up or down, etc. made in accordance with the spirit of the present invention should be considered as falling within the scope of the present invention.