阅读说明：本技术 一种用于飞机整机的自动洗消系统 (Automatic decontamination system for complete airplane ) 是由 马云鹏 于 2020-05-11 设计创作，主要内容包括：本发明公开一种用于飞机整机的自动洗消系统,包括洗消装置和飞机拖动装置,其中,洗消装置包括运动轨道、轨道车和设置于轨道车上的臂型机器人、第一干燥风机、第一洗消泵；飞机拖动装置包括全向移动平台、第二洗消泵、第二干燥风机和第二喷头。飞机停在全向移动平台上,洗消装置往复运动,臂型机器人能够带动第一喷头对飞机机身的不同位置进行洗消,同时,全向移动平台上设置第二喷头,通过第二喷头能够对飞机腹部进行洗消,实现飞机整机全方位洗消,提高飞机整机洗消工作效率,另外,本发明设置了第一干燥风机和第二干燥风机,能够向飞机输送干燥气流,以便在飞机清洗消毒杀菌完成后对飞机进行干燥,避免水渍残留造成二次污染。(The invention discloses an automatic decontamination system for an aircraft complete machine, which comprises a decontamination device and an aircraft dragging device, wherein the decontamination device comprises a moving track, a railcar, an arm type robot, a first drying fan and a first decontamination pump, wherein the arm type robot, the first drying fan and the first decontamination pump are arranged on the railcar; the aircraft dragging device comprises an omnidirectional moving platform, a second decontamination pump, a second drying fan and a second spray head. The airplane stops on the omnidirectional moving platform, the decontamination device reciprocates, the arm-shaped robot can drive the first spray head to decontaminate different positions of the airplane body, meanwhile, the omnidirectional moving platform is provided with the second spray head, the belly of the airplane can be decontaminated through the second spray head, the complete machine of the airplane can be decontaminated in an omnidirectional way, the decontamination working efficiency of the complete machine of the airplane is improved, in addition, the first drying fan and the second drying fan are arranged, the drying airflow can be conveyed to the airplane, the airplane can be dried after the airplane is cleaned, disinfected and sterilized, and secondary pollution caused by residual water stains is avoided.)

1. An automatic decontamination system for an aircraft, comprising:

the decontamination device comprises a moving track, a rail car, an arm type robot, a first drying fan and a first decontamination pump, wherein the arm type robot, the first drying fan and the first decontamination pump are arranged on the rail car;

the aircraft dragging device comprises an omnidirectional moving platform, a second decontamination pump, a second drying fan and a second spray head, wherein the omnidirectional moving platform can support the whole aircraft, the bottom of the omnidirectional moving platform is provided with a dragging wheel, the dragging wheel can drive the omnidirectional moving platform to rotate and slide, the second decontamination pump can be slidably arranged on one side of the omnidirectional moving platform, the second spray head is arranged on the omnidirectional moving platform, the second decontamination pump is communicated with the second spray head, the second drying fan is connected with a second blowing pipe, the second spray head can spray decontamination liquid to the belly of the aircraft, and the second blowing pipe can convey dry airflow to the aircraft;

the decontamination device is arranged on one side of the aircraft dragging device.

2. The automatic decontamination system for an aircraft crew of claim 1, wherein: the first sprayer is also provided with a radar sensor, the radar sensor is arranged on the arm type robot, and the radar sensor can sense the distance between the first sprayer and the airplane; the omnidirectional mobile platform is provided with a laser radar sensor, and the laser radar sensor can sense the distance between the omnidirectional mobile platform and the decontamination device.

3. The automatic decontamination system for an aircraft crew of claim 2, wherein: the first spray head is a fan-shaped spray head.

4. The automatic decontamination system for an aircraft crew of claim 1, wherein: the aircraft dragging device is also connected with a lifting mechanism, the lifting mechanism is arranged at one end of the omnidirectional moving platform, and the lifting mechanism can lift one end of the omnidirectional moving platform; the lifting mechanisms are arranged at the two ends of the omnidirectional moving platform.

5. The automatic decontamination system for an aircraft crew of claim 4, wherein: the slope device is arranged in an inclined mode, the higher end of the slope device is connected with the omnidirectional mobile platform, the two slope devices are respectively connected with the two ends of the omnidirectional mobile platform, and the slope device is detachably connected with the omnidirectional mobile platform.

6. The automatic decontamination system for an aircraft crew of claim 5, wherein: the included angle between the slope device and the horizontal plane is 2.5 degrees.

7. The automatic decontamination system for an aircraft crew of claim 1, wherein: the number of the second spray heads is multiple, and the second spray heads are arranged in a rectangular array.

8. The automatic decontamination system for an aircraft crew of claim 1, wherein: the decontamination device is provided with a first controller, the rail car, the arm type robot, the first drying fan, the first decontamination pump and the first spray head are all connected with the first controller, the arm type robot is provided with a photoelectric sensor, and the photoelectric sensor is connected with the first controller; the aircraft dragging device is provided with a second controller, and the omnidirectional moving platform, the second decontamination pump, the second drying fan and the second spray head are all connected with the second controller.

9. The automatic decontamination system for an aircraft crew of claim 1, wherein: drag chains are arranged between the track and the track car and between the second decontamination pump and the omnidirectional mobile platform; the dragging wheel is a Mecanum wheel.

10. An automatic decontamination system for an aircraft complete machine according to any one of claims 1 to 9, characterized in that: the number of the decontamination devices is twelve, and the twelve decontamination devices are uniformly distributed on two sides of the omnidirectional mobile platform.

Technical Field

The invention relates to the technical field of aviation equipment supporting facilities, in particular to an automatic decontamination system for an aircraft complete machine.

Background

In daily use, an aircraft is often exposed to various pollutants, such as wind sand, dust, aerosol and nuclear chemical contamination in the air, which not only affect the appearance of the aircraft, corrosion or destruction of the fuselage structure and materials caused by the contamination, but also directly affect its ability to perform various flight tasks, and even cause accidents or disasters. As the latest passenger transport cargo aircraft and military aircraft are continuously equipped in all countries of the world, the number of the aircraft is continuously increased, so that the complete machine decontamination of the aircraft becomes a heavy, time-consuming and costly work. Improper decontamination methods can cause new hidden dangers to the airplane.

Meanwhile, the airplane is huge in size, thirty meters long, thirty meters wide and dozens of meters high. The existing airplane decontamination mode is a washing method for high-altitude downward shooting through a single large decontamination vehicle, so that the efficiency is low, time is consumed, the problem that local positions are not in place for decontamination is easy to exist, and secondary pollution to a machine body is easily caused by residual water stains after decontamination.

The Chinese patent application with the publication number of CN108657464A discloses a large-scale aircraft decontamination vehicle with multiple cleaning modes, which comprises a vehicle body, a high-lift cantilever, a cleaning liquid supply mechanism, a power pump mechanism and a control system, wherein the high-lift cantilever comprises a base supporting arm, a multi-stage middle arm and a front end arm which are sequentially connected, telescopic supporting rods are arranged at the joints of the base supporting arm, the multi-stage middle arm and the front end arm, the power pump mechanism comprises a plurality of power pumps with different powers, the number of the power pumps is the same as the number of cleaning modes which can be completed by the decontamination vehicle, the cleaning liquid supply mechanism comprises a liquid storage tank, a liquid supply pipeline and a liquid outlet gun which are sequentially connected, the power pump is connected with the liquid supply pipeline, the control system comprises a P L C control computer, the angle sensor is arranged at the joint of the high-lift cantilever, the distance sensors are arranged around the vehicle body, the output ends of the angle sensors and the distance sensors are connected with the input end of the P L C control computer, the output ends of the power pump or the telescopic supporting rods of the support rods are connected with the P L C control computer, but the control system is not in place where the decontamination vehicle, and the existing technology is not capable of solving the problems of.

Therefore, how to change the current situations that the decontamination efficiency of the aircraft decontamination vehicle is low, the local decontamination is not in place and the risk of secondary pollution exists in the prior art becomes a problem to be solved by technical personnel in the field.

Disclosure of Invention

The invention aims to provide an automatic decontamination system for an aircraft complete machine, which is used for solving the problems in the prior art, improving the decontamination working efficiency of the aircraft and reducing the risk of secondary pollution.

In order to achieve the purpose, the invention provides the following scheme: the invention provides an automatic decontamination system for an aircraft complete machine, which comprises:

the decontamination device comprises a moving track, a rail car, an arm type robot, a first drying fan and a first decontamination pump, wherein the arm type robot, the first drying fan and the first decontamination pump are arranged on the rail car;

the aircraft dragging device comprises an omnidirectional moving platform, a second decontamination pump, a second drying fan and a second spray head, wherein the omnidirectional moving platform can support the whole aircraft, the bottom of the omnidirectional moving platform is provided with a dragging wheel, the dragging wheel can drive the omnidirectional moving platform to rotate and slide, the second decontamination pump can be slidably arranged on one side of the omnidirectional moving platform, the second spray head is arranged on the omnidirectional moving platform, the second decontamination pump is communicated with the second spray head, the second drying fan is connected with a second blowing pipe, the second spray head can spray decontamination liquid to the belly of the aircraft, and the second blowing pipe can convey dry airflow to the aircraft;

the decontamination device is arranged on one side of the aircraft dragging device.

Preferably, a radar sensor is further arranged at the first spray head and arranged on the arm robot, and the radar sensor can sense the distance between the first spray head and the airplane; the omnidirectional mobile platform is provided with a laser radar sensor, and the laser radar sensor can sense the distance between the omnidirectional mobile platform and the decontamination device.

Preferably, the first nozzle is a fan nozzle.

Preferably, the aircraft dragging device is further connected with a lifting mechanism, the lifting mechanism is arranged at one end of the omnidirectional mobile platform, and the lifting mechanism can lift one end of the omnidirectional mobile platform; the lifting mechanisms are arranged at the two ends of the omnidirectional moving platform.

Preferably, the automatic decontamination system for the whole aircraft further comprises slope devices, the slope devices are arranged in an inclined mode, the higher ends of the slope devices are connected with the omnidirectional mobile platform, the two slope devices are respectively connected with the two ends of the omnidirectional mobile platform, and the slope devices are detachably connected with the omnidirectional mobile platform.

Preferably, the ramp means is angled at 2.5 ° to the horizontal.

Preferably, the number of the second spray heads is multiple, and the multiple second spray heads are arranged in a rectangular array.

Preferably, the decontamination device is provided with a first controller, the rail car, the arm robot, the first drying fan, the first decontamination pump and the first spray head are all connected with the first controller, the arm robot is provided with a photoelectric sensor, and the photoelectric sensor is connected with the first controller; the aircraft dragging device is provided with a second controller, and the omnidirectional moving platform, the second decontamination pump, the second drying fan and the second spray head are all connected with the second controller.

Preferably, drag chains are arranged between the track and the track car and between the second decontamination pump and the omnidirectional mobile platform; the dragging wheel is a Mecanum wheel.

Preferably, the number of the decontamination devices is twelve, and the twelve decontamination devices are uniformly distributed on two sides of the omnidirectional mobile platform.

Compared with the prior art, the invention has the following technical effects: the invention discloses an automatic decontamination system for an aircraft complete machine, which comprises a decontamination device and an aircraft dragging device, wherein the decontamination device comprises a moving track, a railcar, an arm type robot, a first drying fan and a first decontamination pump, wherein the arm type robot, the first drying fan and the first decontamination pump are arranged on the railcar; the aircraft dragging device comprises an omnidirectional moving platform, a second decontamination pump, a second drying fan and a second spray head, wherein the omnidirectional moving platform can support the whole aircraft, the bottom of the omnidirectional moving platform is provided with a dragging wheel which can drive the omnidirectional moving platform to rotate and slide, the second decontamination pump is slidably arranged on one side of the omnidirectional moving platform, the second spray head is arranged on the omnidirectional moving platform, the second decontamination pump is communicated with the second spray head, the second drying fan is connected with a second blow pipe, the second spray head can spray decontamination liquid to the belly of the aircraft, and the second blow pipe can convey dry airflow to the aircraft; the decontamination device is arranged at one side of the aircraft dragging device. When the automatic decontamination system for the whole aircraft works, the aircraft stops on the omnidirectional moving platform, the omnidirectional moving platform adjusts the safety distance between the omnidirectional moving platform and the decontamination device, the decontamination device reciprocates, the arm-type robot can drive the first spray head to decontaminate different positions of the aircraft body, meanwhile, the second spray head is arranged on the omnidirectional moving platform, and the belly of the aircraft can be decontaminated through the second spray head, so that the comprehensive decontamination of the whole aircraft is realized, and the decontamination working efficiency of the whole aircraft is improved.

Drawings

In order to more clearly illustrate the embodiments of the present invention or the technical solutions in the prior art, the drawings needed to be used in the embodiments will be briefly described below, and it is obvious that the drawings in the following description are only some embodiments of the present invention, and it is obvious for those skilled in the art to obtain other drawings without inventive exercise.

FIG. 1 is a schematic view of an automatic decontamination system for an aircraft complete machine of the present invention;

FIG. 2 is a schematic view of a decontamination apparatus of the automatic decontamination system for an aircraft complete machine of the present invention;

FIG. 3 is a schematic view of an aircraft towing arrangement of the automatic decontamination system for an aircraft complete machine of the present invention;

FIG. 4 is a schematic view of the automatic decontamination system for an aircraft complete machine of the present invention in operation;

the system comprises a decontamination device 1, a moving track 101, a rail car 102, an arm robot 103, a first drying fan 104, a first decontamination pump 105, a first spray head 106, a first blowing pipe 107, an aircraft dragging device 2, an omnidirectional moving platform 201, a second decontamination pump 202, a second spray head 203, a decontamination pipeline 204, a dragging wheel 205, a lifting mechanism 206, a slope device 3 and a drag chain 4.

Detailed Description

The technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only a part of the embodiments of the present invention, and not all of the embodiments. All other embodiments, which can be derived by a person skilled in the art from the embodiments given herein without making any creative effort, shall fall within the protection scope of the present invention.

The invention aims to provide an automatic decontamination system for an aircraft complete machine, which is used for solving the problems in the prior art, improving the decontamination working efficiency of the aircraft and reducing the risk of secondary pollution.

In order to make the aforementioned objects, features and advantages of the present invention comprehensible, embodiments accompanied with figures are described in further detail below.

Referring to fig. 1-4, wherein fig. 1 is a schematic view of an automatic decontamination system for an aircraft complete machine according to the present invention, fig. 2 is a schematic view of a decontamination device of an automatic decontamination system for an aircraft complete machine according to the present invention, fig. 3 is a schematic view of an aircraft dragging device of an automatic decontamination system for an aircraft complete machine according to the present invention, and fig. 4 is a schematic view of an automatic decontamination system for an aircraft complete machine according to the present invention in operation

The invention provides an automatic decontamination system for an aircraft complete machine, which comprises:

the decontamination device 1 comprises a moving track 101, a railcar 102, an arm type robot 103, a first drying fan 104 and a first decontamination pump 105, wherein the arm type robot 103 is arranged on the railcar 102, the railcar 102 is slidably arranged on the moving track 101, the arm type robot 103 is connected with a first spray head 106, the first decontamination pump 105 is communicated with the first spray head 106, the first drying fan 104 is connected with a first blowing pipe 107, the first spray head 106 can spray decontamination liquid to an airplane, and the first blowing pipe 107 can convey dry airflow to the airplane;

the airplane dragging device 2 comprises an omnidirectional moving platform 201, a second decontamination pump 202, a second drying fan and a second spray head 203, wherein the omnidirectional moving platform 201 can support the whole airplane, the bottom of the omnidirectional moving platform 201 is provided with the dragging wheel 205, the dragging wheel 205 can drive the omnidirectional moving platform 201 to rotate and slide, the second decontamination pump 202 is slidably arranged on one side of the omnidirectional moving platform 201, the second spray head 203 is arranged on the omnidirectional moving platform 201, the omnidirectional moving platform 201 adjusts the safety distance with the decontamination device 1, the second decontamination pump 202 is communicated with the second spray head 203, the second drying fan is connected with a second blowing pipe, the second spray head 203 can spray decontamination liquid to the belly of the airplane, and the second blowing pipe can convey drying airflow to the airplane;

the decontamination device 1 is arranged at one side of the aircraft dragging device 2.

When the automatic decontamination system for the whole aircraft works, the aircraft stops on the omnidirectional moving platform 201, the decontamination device 1 reciprocates, the arm-shaped robot 103 can drive the first spray head 106 to decontaminate different positions of the aircraft body, meanwhile, the omnidirectional moving platform 201 is provided with the second spray head 203, the belly of the aircraft can be decontaminated through the second spray head 203, the omnibearing decontamination of the whole aircraft is realized, and the decontamination working efficiency of the whole aircraft is improved.

Wherein, first shower nozzle 106 department still is provided with radar sensor, and radar sensor sets up on arm type robot 103, and radar sensor can the perception interval between first shower nozzle 106 and the aircraft, and when radar sensor confirmed that the interval between first shower nozzle 106 and the aircraft is suitable to be washed and is disinfected the operation, first shower nozzle 106 carries out cleaning and disinfecting and dry to the aircraft, improves and washes the work efficiency that disappears. Correspondingly, omnidirectional movement platform 201 has the laser radar sensor, and the laser radar sensor can the perception omnidirectional movement platform 201 and wash the interval between the device 1 that disappears, and simultaneously, the laser radar sensor can guarantee in step with the radar sensor of first shower nozzle 106 department with the safe interval of aircraft, guarantees that the aircraft surface does not receive mechanical damage, promotes and washes the factor of safety that disappears.

In this specific embodiment, the first nozzle 106 is a fan-shaped nozzle, so that the first nozzle 106 can perform fan-shaped spraying decontamination on the aircraft body, thereby enlarging the spraying area and improving the working efficiency. In other embodiments of the present invention, the air outlets of the first blowpipe 107 and the second blowpipe can be configured as fan-shaped air outlets, which improves the aircraft drying efficiency.

Specifically, the aircraft dragging device 2 is further connected with a lifting mechanism 206, the lifting mechanism 206 is arranged on two sides of the omnidirectional moving platform 201, the lifting mechanism 206 can be matched with the dragging wheel 205 to cooperatively adjust the position of the aircraft, wherein the lifting mechanism 206 adjusts the height position of the omnidirectional moving platform 201, the dragging wheel 205 adjusts the horizontal position of the omnidirectional moving platform 201, the safe distance between the aircraft and the device is ensured, and meanwhile, the cleaning range of the device can cover the surface of the whole aircraft. In this embodiment, the two ends of the omnidirectional moving platform 201 are both provided with the lifting mechanisms 206, so as to improve the convenience of operation.

In addition, the automatic decontamination system for the whole aircraft further comprises a slope device 3, the slope device 3 is arranged in an inclined mode, the higher end of the slope device 3 is connected with the omnidirectional moving platform 201, the two slope devices 3 are respectively connected with the two ends of the omnidirectional moving platform 201, the aircraft can smoothly run to the omnidirectional moving platform 201 by utilizing the slope device 3, the slope devices 3 are arranged at the two ends of the omnidirectional moving platform 201, the operation convenience is improved, the slope devices 3 are detachably connected with the omnidirectional moving platform 201, the disassembly and assembly are convenient, and the situation that the slope devices 3 influence the movement of the omnidirectional moving platform 201 is avoided.

In this embodiment, the included angle between the slope device 3 and the horizontal plane is 2.5 degrees, the slope is gentle, and the climbing difficulty is reduced. It should be noted here that the slope device 3 is made of square steel or pattern steel by welding, and the surface of the slope device 3 is coated with a rust-proof paint to prevent metal corrosion.

More specifically, the number of the second nozzles 203 is multiple, the multiple second nozzles 203 are arranged in a rectangular array, the second decontamination pump 202 is connected with the second nozzles 203 through a decontamination pipeline 204, and the multiple second nozzles 203 can decontaminate different parts of the belly of the aircraft, so that the decontamination work efficiency is improved.

For convenience of control, the decontamination device 1 is provided with a first controller, the rail car 102, the arm type robot 103, the first drying fan 104, the first decontamination pump 105 and the first spray head 106 are all connected with the first controller, the arm type robot 103 is provided with a photoelectric sensor, the photoelectric sensor is connected with the first controller, the aircraft dragging device 2 is provided with a second controller, the omnidirectional moving platform 201, the second decontamination pump 202, the second drying fan and the second spray head 203 are all connected with the second controller, the first controller is installed on the rail car 102, the first controller can plan a motion path for the arm type robot 103 according to the position of the aircraft surface needing decontamination, the first controller and the radar sensor collect distance signals from the aircraft surface through Ethernet communication, the first controller can send decontamination instructions to control the arm type robot 103, the first decontamination pump 105, the first drying fan 104 and the rail car 102 to perform corresponding actions, meanwhile, the first controller can monitor distance signals fed back by the radar sensor to ensure the safety of the aircraft, the second controller can control the arm type robot 103, the first decontamination pump 105, the first drying fan 104 and the rail car 102 to perform corresponding actions according to the artificial guidance of the second omnidirectional moving platform, the unmanned guidance of the aircraft 201, the aircraft is used for controlling the aircraft to adjust the aircraft, the aircraft 201, the aircraft body of the aircraft 201, the aircraft 201, the aircraft is used for performing accurate adjustment of the aircraft, the aircraft is performed by the aircraft, the aircraft is performed by the aircraft, the aircraft is performed by the aircraft.

Furthermore, the towchains 4 are arranged between the track and the track car 102 and between the second decontamination pump 202 and the omnidirectional mobile platform 201, and in the process of movement of the track car 102 and the second decontamination pump 202, the towchains 4 can ensure normal conveying of decontamination liquid, protect the safety of electrical elements and ensure normal operation of decontamination; the dragging wheel 205 is a Mecanum wheel, can rotate 360 degrees and adopt a laser radar sensor for navigation and positioning, and can realize accurate positioning of the position in a compact space for accurate positioning of the aircraft parking position.

In addition, in the present embodiment, the number of the decontamination devices 1 is twelve, the twelve decontamination devices 1 are uniformly distributed on two sides of the omnidirectional moving platform 201, and work simultaneously, so as to improve the decontamination efficiency of the airplane, and in practical application, the number of the decontamination devices 1 can be determined according to the airplane model.

When the automatic decontamination system for the whole aircraft works, the aircraft stops on the omnidirectional moving platform 201, the omnidirectional moving platform 201 can assist the aircraft to accurately position, the rail car 102 reciprocates, the arm robot 103 arranged on the rail car 102 can drive the first spray head 106 to decontaminate different positions of the aircraft body, meanwhile, the second spray head 203 is arranged on the omnidirectional moving platform 201, the belly of the aircraft can be decontaminated through the second spray head 203, the omnibearing decontamination of the whole aircraft is realized, and the working efficiency of the whole aircraft decontamination is improved.

The principle and the implementation mode of the invention are explained by applying a specific example, and the description of the embodiment is only used for helping to understand the method and the core idea of the invention; meanwhile, for a person skilled in the art, according to the idea of the present invention, the specific embodiments and the application range may be changed. In view of the above, the present disclosure should not be construed as limiting the invention.