阅读说明：本技术 一种航空ai视觉自检多场景通用除防冰云台喷涂系统 (Aviation AI vision self-checking multi-scene universal deicing holder spraying system ) 是由 王伟刚 谭建聪 王彤彤 于 2021-08-06 设计创作，主要内容包括：本发明公开了一种航空AI视觉自检多场景通用除防冰云台喷涂系统,包括高空破冰车本体,高空破冰车本体上设有破冰枪和用于控制破冰枪的中央控制器。破冰枪通过机械臂安装在高空车顶部云台。伺服电机与中央控制器连接,中央控制器可通过伺服电机控制机械臂与破冰枪旋转。异物检测模块安装在高空破冰车本体上,异物检测模块可在破冰枪工作前扫描飞机表面判断异物的尺寸和大小。流量检测模块与中央控制器连接,中央控制器通过流量检测模块控制破冰枪除冰液的流出量。液压检测模块与中央控制器连接。视觉自检模块与中央控制器连接并可在破冰枪工作完成后对比设定图像信息判断飞机表面是否正常。(The invention discloses an aviation AI visual self-inspection multi-scene universal deicing holder spraying system which comprises a high-altitude deicing vehicle body, wherein an ice breaking gun and a central controller for controlling the ice breaking gun are arranged on the high-altitude deicing vehicle body. The ice breaking gun is installed on a cloud deck of the overhead vehicle through a mechanical arm. The servo motor is connected with the central controller, and the central controller can control the mechanical arm and the ice breaking gun to rotate through the servo motor. The foreign matter detection module is installed on the high altitude ice-breaking vehicle body, and the size of foreign matter can be judged on the foreign matter detection module scan aircraft surface before the ice-breaking rifle work. The flow detection module is connected with the central controller, and the central controller controls the outflow of the deicing liquid of the ice breaking gun through the flow detection module. The hydraulic detection module is connected with the central controller. The vision self-checking module is connected with the central controller and can compare the set image information to judge whether the surface of the airplane is normal or not after the ice breaking gun finishes working.)

1. The utility model provides a general deicing cloud platform paint finishing that removes of aviation AI vision self-checking multiscope which characterized in that includes:

the high-altitude ice breaking vehicle comprises a high-altitude ice breaking vehicle body, wherein an ice breaking gun and a central controller for controlling the ice breaking gun are arranged on the high-altitude ice breaking vehicle body;

the ice breaking gun is mounted on a top cloud deck of the high-altitude vehicle through a mechanical arm;

the servo motor is connected with the central controller, and the central controller can control the mechanical arm and the ice breaking gun to rotate through the servo motor;

the foreign matter detection module is mounted on the high-altitude ice breaking vehicle body and can scan the surface of the airplane to judge the size and the size of foreign matters before the ice breaking gun works;

the flow detection module is connected with the central controller, and the central controller controls the outflow of the deicing liquid of the ice breaking gun through the flow detection module;

the hydraulic detection module is connected with the central controller, and the central controller controls the liquid spraying pressure of the ice breaking gun through the hydraulic detection module so as to adjust the spraying height of the ice breaking gun;

the vision self-checking module is connected with the central controller and can compare and set image information to judge whether the surface of the airplane is normal after the ice breaking gun works, and if not, the vision self-checking module sends an abnormal signal to the central controller.

2. The aviation AI visual self-inspection multi-scene general deicing holder spraying system according to claim 1, wherein the central controller is further connected with an alarm module, and when the central controller receives abnormal signals of the foreign matter detection module, the flow detection module and the hydraulic detection module, the alarm module is started to send an alarm signal.

3. The aerial AI visual self-inspection multi-scene universal deicing pan-tilt spraying system according to claim 1, wherein the central controller is a schneider Logic/motion controller-module M262 programmable controller.

4. The aerial AI visual self-inspection multi-scene universal deicing pan-tilt spraying system according to claim 1, wherein said central controller is a Siemens SIMATIC S7-300 high-end motion controller.

5. The aerial AI visual self-inspection multi-scene universal deicing holder spraying system according to claim 1, wherein the high altitude ice breaking vehicle body is further provided with a dynamic detection module, and the central controller can control the rotation speed of the ice breaking gun through the dynamic detection module so as to adjust the spraying amount of deicing liquid on the unit area of the surface of the aircraft.

6. The aerial AI visual self-inspection multi-scene universal deicing pan-tilt spraying system according to claim 1, wherein said dynamic detection module comprises a fiber coaxial displacement sensor ZW-7000/5000 and a fiber coaxial displacement sensor ZW.

7. The aerial AI visual self-inspection multi-scene universal deicing holder spraying system according to claim 1, wherein the high altitude icebreaker body is further provided with a liquid detection module for detecting the surplus deicing and anti-icing liquid and whether the liquid detection module is invalid, and the liquid detection module is connected with the central controller.

8. The aerial AI visual self-inspection multi-scene universal deicing pan-tilt spraying system according to claim 1, wherein said foreign object detection module comprises an ohm dragon FH image processor, an ohm dragon ZFV-C visual sensor and an ohm dragon E4C-UDA digital amplifier split ultrasonic sensor.

9. The aerial AI visual self-inspection multi-scene universal deicing pan-tilt spraying system according to claim 1, wherein the visual self-inspection module comprises 2D CMOS laser type ZS-HL, 2D CMOS laser type ZS-L and F-30 visual sensors.

Technical Field

The invention relates to the technical field of aviation equipment, in particular to an aviation AI visual self-inspection multi-scene universal deicing holder spraying system.

Background

The existing aviation industry is basically completed by spraying deicing and anti-icing liquid at the front end of a deicing gun at the top end of a high-altitude vehicle mechanical arm through manual operation. And the long-time manual deicing labor can cause personnel fatigue, and if complex targets are met during manual operation, data cannot be compared in real time for defect judgment. And a large amount of time is needed for contacting with a background engineer for judgment and processing, and meanwhile, the accurate real-time transmission of related detection data is not facilitated. On the other hand, ground crew can not spray the deicing and anti-icing liquid accurately when deicing, and the deicing and anti-icing liquid can be directly sprayed to the air inlet channel, the probe hole, the back spray and exhaust port of the engine and the air inlet and exhaust hole parts of the PAU. When the APU works, the air conditioner component valve, the pressurization valve and the door and window are closed, the air conditioner is opened after deicing is completed for one minute, and the time cannot be accurately measured. The above erroneous operation will cause damage to the aircraft. Therefore, there is a need for an aviation AI visual self-inspection multi-scene universal deicing and anti-icing pan-tilt spraying system for solving the above problems.

Disclosure of Invention

The invention aims to overcome the problems in the prior art and provides an aviation AI visual self-inspection multi-scene universal deicing holder spraying system.

In order to achieve the purpose, the invention adopts the following scheme:

the utility model provides a general deicing cloud platform paint finishing that removes of aviation AI vision self-checking multiscope, includes:

the high-altitude ice breaking vehicle body is provided with an ice breaking gun and a central controller for controlling the ice breaking gun.

The ice breaking gun is mounted on a cloud deck at the top of the high-altitude vehicle through a mechanical arm.

And the servo motor is connected with the central controller, and the central controller can control the mechanical arm and the ice breaking gun to rotate through the servo motor.

The foreign matter detection module is installed on the high-altitude ice breaking vehicle body and can scan the surface of the aircraft before the ice breaking gun works to judge the size of the foreign matter.

And the flow detection module is connected with the central controller, and the central controller controls the outflow of the deicing liquid of the ice breaking gun through the flow detection module.

The hydraulic detection module is connected with the central controller, and the central controller controls the liquid spraying pressure of the ice breaking gun through the hydraulic detection module so as to adjust the spraying height of the ice breaking gun.

And the vision self-checking module is connected with the central controller and can compare set image information after the ice breaking gun finishes working to judge whether the surface of the airplane is normal or not, and if not, an abnormal signal is sent to the central controller.

Furthermore, the central controller is also connected with an alarm module, and the alarm module is started to send out an alarm signal after the central controller receives the abnormal signals of the foreign matter detection module, the flow detection module and the hydraulic detection module.

Further, the central controller is a Schneider Logic/motion controller-Module M262 programmable controller.

Further, the central controller is a Simatic S7-300 high-end motion controller.

Furthermore, the high-altitude ice breaking vehicle body is also provided with a dynamic detection module, and the central controller can control the rotation speed of the ice breaking gun through the dynamic detection module so as to adjust the spraying amount of the deicing fluid on the unit area of the surface of the airplane.

Further, the dynamic detection module comprises a fiber coaxial displacement sensor ZW-7000/5000 and a fiber coaxial displacement sensor ZW.

Further, the high-altitude ice breaking vehicle body is further provided with a liquid detection module for detecting the residual amount of the deicing and anti-icing liquid and whether the deicing and anti-icing liquid is invalid or not, and the liquid detection module is connected with the central controller.

Further, the foreign matter detection module comprises an ohm dragon FH image processor, an ohm dragon ZFV-C visual sensor and an ohm dragon E4C-UDA digital amplifier separated ultrasonic sensor.

Further, the visual self-checking module comprises 2D CMOS laser type ZS-HL, 2D CMOS laser type ZS-L and F-30 visual sensors.

Compared with the prior art, the invention has the following advantages: firstly, the deicing speed of the airplane can be improved, and a large amount of manpower is saved. Secondly, can prevent to remove that anti-icing liquid is invalid to each working phase time prejudgement in advance through this cloud platform spraying system that removes, intelligent automatic check compares data judgement defect and reports to the police in advance, and backstage personnel response mechanism goes on in step, has improved work efficiency. The deicing and anti-icing holder spraying system can judge the condition of foreign matters on the surface of the wing in detail, and prevent the aircraft with high-performance supercritical wing wings from taking off due to pollution and damage to the wing surfaces caused by ice, snow or frost in advance. And fourthly, the deicing and anti-icing liquid is prevented from being directly sprayed to an air inlet channel, a probe hole, a back spray and exhaust port of the engine and an air inlet and exhaust hole of the PAU by strictly controlling the spraying angle and accurately spraying.

Drawings

The present application will be described in further detail with reference to the following drawings and detailed description.

Fig. 1 is a schematic diagram of the overall structure of an aviation AI visual self-inspection multi-scene general deicing holder spraying system.

Detailed Description

The following detailed description of embodiments of the present invention is provided in connection with the accompanying drawings and examples. The following examples are intended to illustrate the invention but are not intended to limit the scope of the invention.

Example one

As shown in fig. 1, an aviation AI vision self-inspection multi-scene universal deicing and anti-icing holder spraying system comprises:

the high-altitude ice breaking vehicle comprises a high-altitude ice breaking vehicle body, wherein an ice breaking gun 3 and a central controller 1 for controlling the ice breaking gun 3 are arranged on the high-altitude ice breaking vehicle body.

The ice breaking gun 3 is arranged on a cloud deck at the top of the high-altitude vehicle through a mechanical arm.

The servo motor 2, servo motor 2 are connected with central controller 1, and central controller 1 accessible servo motor 2 control arm and the rotation of the rifle 3 that opens ice.

Foreign matter detection module 4, foreign matter detection module 4 installs on the high altitude icebreaker body, and foreign matter detection module 4 can scan the aircraft surface before 3 work of ice-breaking rifle and judge the size and the size of foreign matter.

Flow detection module 5, flow detection module 5 is connected with central controller 1, and central controller 1 passes through flow detection module 5 control ice gun 3 deicing fluid's outflow.

The hydraulic detection module 6 is connected with the central controller 1, and the central controller 1 controls the liquid spraying pressure of the ice breaking gun 3 through the hydraulic detection module 6 so as to adjust the spraying height of the ice breaking gun.

And the vision self-checking module 7 is connected with the central controller 1, and can compare the set image information after the ice breaking gun 3 finishes working to judge whether the surface of the airplane is normal or not, and if not, an abnormal signal is sent to the central controller 1.

After confirming the required accurate position of spraying through foreign matter detection module 4, central controller 1 controls arm and the accurate angle of rotation of ice gun 3 through servo motor 2, central controller 1 has adjusted the flow and the accurate blowout deicing fluid of pressure value of ice gun 3 through flow detection module 5 and hydraulic pressure detection module 6, the speed that the blowout volume passes through the shower nozzle detects the back of reminding evenly sprays accurate volume, prevent that corresponding structure and covering and place facility etc. from being corroded by excessive blowout liquid.

Preferably, the central controller 1 is further connected with an alarm module 8, and the alarm module 8 is started to send an alarm signal after the central controller 1 receives the abnormal signals of the foreign matter detection module 4, the flow detection module 5 and the hydraulic pressure detection module 6.

Preferably, the central controller 1 is a Schneider Logic/motion controller-Module M262 programmable controller.

Preferably, the high-altitude ice breaking vehicle body is further provided with a dynamic detection module 9, and the central controller 1 can control the rotation speed of the ice breaking gun 3 through the dynamic detection module 9 so as to adjust the spraying amount of the deicing fluid on the unit area of the surface of the airplane.

Preferably, the dynamic detection module 9 comprises a fiber coaxial displacement sensor ZW-7000/5000 and a fiber coaxial displacement sensor ZW.

Preferably, the high-altitude ice breaking vehicle body is further provided with a liquid detection module for detecting the residual amount of the deicing and anti-icing liquid and whether the deicing and anti-icing liquid is invalid or not, and the liquid detection module is connected with the central controller 1.

Preferably, the foreign object detection module 4 includes an Oilon FH image processor, an Oilon ZFV-C vision sensor, and an Oilon E4C-UDA digital amplifier split ultrasonic sensor.

Preferably, the visual self-test module 7 comprises 2D CMOS laser type ZS-HL, 2D CMOS laser type ZS-L and F-30 visual sensors.

Compared with the prior art, the invention has the following advantages: firstly, the deicing speed of the airplane can be improved, and a large amount of manpower is saved. Secondly, can prevent to remove that anti-icing liquid is invalid to each working phase time prejudgement in advance through this cloud platform spraying system that removes, intelligent automatic check compares data judgement defect and reports to the police in advance, and backstage personnel response mechanism goes on in step, has improved work efficiency. The deicing and anti-icing holder spraying system can judge the condition of foreign matters on the surface of the wing in detail, and prevent the aircraft with high-performance supercritical wing wings from taking off due to pollution and damage to the wing surfaces caused by ice, snow or frost in advance. And fourthly, the deicing and anti-icing liquid is prevented from being directly sprayed to an air inlet channel, a probe hole, a back spray and exhaust port of the engine and an air inlet and exhaust hole of the PAU by strictly controlling the spraying angle and accurately spraying.

Example two

As shown in fig. 1, an aviation AI vision self-inspection multi-scene universal deicing and anti-icing holder spraying system comprises:

the high-altitude ice breaking vehicle comprises a high-altitude ice breaking vehicle body, wherein an ice breaking gun 3 and a central controller 1 for controlling the ice breaking gun 3 are arranged on the high-altitude ice breaking vehicle body.

The ice breaking gun 3 is arranged on a cloud deck at the top of the high-altitude vehicle through a mechanical arm.

The servo motor 2, servo motor 2 are connected with central controller 1, and central controller 1 accessible servo motor 2 control arm and the rotation of the rifle 3 that opens ice.

Foreign matter detection module 4, foreign matter detection module 4 installs on the high altitude icebreaker body, and foreign matter detection module 4 can scan the aircraft surface before 3 work of ice-breaking rifle and judge the size and the size of foreign matter. The foreign matter detection module 4 can automatically check and compare data, judge defect conditions and the like, and can accurately detect the icing outside the airplane, particularly the surface of the wing. Even if fine frost particles or ice particles with the diameter of 1-2 mm and the size of salt are sparsely distributed on the upper surface of the wing according to the density of one particle per square centimeter, the measurement can be accurately carried out.

Flow detection module 5, flow detection module 5 is connected with central controller 1, and central controller 1 passes through flow detection module 5 control ice gun 3 deicing fluid's outflow.

The hydraulic detection module 6 is connected with the central controller 1, and the central controller 1 controls the liquid spraying pressure of the ice breaking gun 3 through the hydraulic detection module 6 so as to adjust the spraying height of the ice breaking gun.

After confirming the required accurate position of spraying through foreign matter detection module 4, central controller 1 controls arm and the accurate angle of rotation of ice gun 3 through servo motor 2, central controller 1 has adjusted the flow and the accurate blowout deicing fluid of pressure value of ice gun 3 through flow detection module 5 and hydraulic pressure detection module 6, the speed that the blowout volume passes through the shower nozzle detects the back of reminding evenly sprays accurate volume, prevent that corresponding structure and covering and place facility etc. from being corroded by excessive blowout liquid.

And the vision self-checking module 7 is connected with the central controller 1, and can compare the set image information after the ice breaking gun 3 finishes working to judge whether the surface of the airplane is normal or not, and if not, an abnormal signal is sent to the central controller 1.

Preferably, the central controller 1 is a Simatic S7-300 high-end motion controller.

Preferably, the high-altitude ice breaking vehicle body is further provided with a dynamic detection module 9, and the central controller 1 can control the rotation speed of the ice breaking gun 3 through the dynamic detection module 9 so as to adjust the spraying amount of the deicing fluid on the unit area of the surface of the airplane.

Preferably, the dynamic detection module 9 comprises a fiber coaxial displacement sensor ZW-7000/5000 and a fiber coaxial displacement sensor ZW.

The foregoing is only a preferred embodiment of the present application, and it should be noted that, for those skilled in the art, several modifications and substitutions can be made without departing from the technical principle of the present application, and these modifications and substitutions should also be regarded as the protection scope of the present application.