An aircraft centralized idle deicing dangerous area detection calibration device, method and application

Abstract

The present application belongs to the technical field of aircraft centralized deicing ground danger warning, and discloses a kind of aircraft centralized idling deicing danger zone detection calibration device, method and application.The device collects the information of temperature, air pressure, wind speed external environment around idling deicing aircraft, and the main control system identifies the wind speed data of surrounding idling deicing danger zone to control the danger alarm device to alarm;Then, the idling danger zone is calibrated, the position is determined by the Beidou positioning system and ultrasonic range finder, the idling deicing danger zone around the idling deicing aircraft is determined by the main control system controlling the track type walking system to measure the idling deicing danger zone, and the idling deicing danger zone is calibrated at the same time.The present application has great significance for ensuring the efficiency of aircraft ground deicing and the safety of deicing personnel.

Description

TECHNICAL FIELD

[0001] The present application belongs to the technical field of aircraft centralized deicing ground danger warning, and particularly relates to an aircraft centralized deicing danger zone detection and calibration device, method and application. BACKGROUND

[0002] With the continuous progress of society, people's living standards are improving, and airplanes are becoming the most convenient way of transportation for people. The safety of airplanes is becoming more and more important. Airports in cold winter areas have poor take-off conditions, and ice attached to the surface of the aircraft seriously affects the safety of the aircraft. An aircraft is a transportation tool that flies by using air lift. Ice accumulation can damage the air dynamic performance of the aircraft in flight. If ice and snow are attached to the surface of the aircraft body, the resistance will increase; if ice layers appear on the wings, the lift will decrease sharply; in addition, ice layers can also block the control surfaces, reducing the handling quality of the aircraft. Uneven distribution of ice accumulation can damage the stability of the aircraft, causing the flight to enter an unstable state. These can lead to very serious consequences, even crashes.

[0003] The most common deicing method in the civil aviation industry is to spray deicing liquid, which is commonly known as "aircraft hot water bath" for passengers. After preheating, the liquid is sprayed on the aircraft body at a temperature of about 82 degrees Celsius, and the ice and snow on the aircraft is removed by high-temperature and high-speed spraying. In addition, the main components of the deicing liquid are ethylene glycol and propylene glycol, which can lower the freezing point to below minus 50 degrees when mixed with water, and can prevent secondary ice accumulation. The specific maintenance time depends on the grade of the deicing liquid used at the time. However, since the time for deicing liquid to prevent secondary ice accumulation is limited, the deiced aircraft should take off as soon as possible, otherwise, secondary deicing will be required when the deicing liquid loses its effectiveness. This is why airlines cannot remove ice and snow from aircrafts in advance, but must wait until the passengers have boarded and the cabin doors have been closed before deicing can begin. Many countries with year-round snow and ice use centralized deicing, which is a special area for aircraft deicing at the entrance of the runway. The take-off aircraft enters the deicing area in turn. Centralized deicing can ensure that the deicing liquid does not lose its effectiveness, and it also saves the trouble of adding liquid to the deicing vehicle. The efficiency of this deicing method is significantly improved. During the deicing process at idle speed, the airflow generated by the aircraft engine can pose a safety hazard to the deicing personnel and the deicing vehicle.

[0004] Through the above analysis, the problems and defects of the prior art are: (1) the existing technology of various sensors has low precision and high cost, and is difficult to be widely applied; (2) the existing danger zone calibration device has high precision requirements and is greatly affected by environmental factors, resulting in poor detection and calibration precision of the deicing danger zone.

[0005] The difficulty of solving the above problems and defects is that as long as the sensor is used for measuring data, it will be affected by the environment, and the stability and accuracy of the calibration device are greatly required.

[0006] The significance of solving the above problems and defects is that as long as the calibration device measures around the idling deicing aircraft, the dangerous area of the idling deicing aircraft can be measured, and the dangerous area is calibrated. The aircraft itself will not have a great impact and the cost is low. Therefore, an idling deicing aircraft dangerous calibration device is invented to calibrate the dangerous area of the idling deicing aircraft, which is of great significance to protect the safety of deicing personnel. SUMMARY

[0007] In order to overcome the problems in the related art, the embodiments of the present application provide a kind of aircraft centralized idling deicing dangerous area detection calibration device, method and application.

[0008] The technical scheme is as follows: a kind of aircraft centralized idling deicing dangerous area detection calibration device, by collecting the temperature, air pressure, wind speed information around idling deicing aircraft, by the identification of surrounding idling deicing dangerous area wind speed data to the main control system, control dangerous alarm device alarm;Again, the idling dangerous area is calibrated, the position is judged by the Beidou positioning system and ultrasonic range finder, and the idling deicing dangerous area around the idling deicing aircraft is determined by the main control system control tracked walking system to measure, and is calibrated simultaneously.

[0009] The device further comprises:

[0010] The upper and lower telescopic probe structure is used to install the vertical telescopic rod, and the sensing system is retracted when not working;

[0011] The tracked walking system moves according to different climate conditions and aircraft types, combined with the measurement data analysis results;

[0012] The anti-rollover system automatically adjusts the chassis height and center position according to the wind speed of the idling deicing dangerous area;

[0013] The lead-acid battery is used to provide stable current;

[0014] The sensing system is used to test the wind speed and the distance of the idling deicing dangerous area from the aircraft, and the control cable is connected with the intelligent control unit;

[0015] The calibration device performs sound and light indication and ground spray indication according to the analysis results of the main control system;

[0016] The intelligent control unit sends the calibration position information to the master control system by using cooperative positioning, networking and information exchange, and combining with the Beidou positioning system, and forms a three-dimensional guidance map of the aircraft idling deicing dangerous area to guide the operation vehicle.

[0017] The master control system is used for analyzing different wind speed data collected, and analyzing and alarming through a danger alarm device.

[0018] The Beidou positioning system is used for positioning different idling dangerous area positions, and identifying and calibrating the idling deicing aircraft dangerous area.

[0019] The terminal system positions each idling dangerous area through the Beidou positioning system, and determines the position of the dangerous area.

[0020] In one embodiment, the sensing system comprises:

[0021] The wind speed tester is used for testing the wind speed of the idling deicing dangerous area.

[0022] The ultrasonic range finder is used for measuring the distance of the idling deicing dangerous area from the aircraft.

[0023] The temperature sensor is used for measuring the external temperature.

[0024] The infrared thermal imaging sensor is used for acquiring external real-time images.

[0025] Another object of the present application is to provide a method for detecting and calibrating the idling deicing dangerous area of an aircraft, which is realized by using the device for detecting and calibrating the idling deicing dangerous area of an aircraft, and the method comprises the following steps:

[0026] S1, a signal is sent through a remote control system, and after receiving the instruction signal, the signal is transmitted to a tracked walking system through a master control system, and the tracked walking system rotates through the track to detect and collect data of the idling deicing aircraft.

[0027] S2, historical data is collected and transmitted to the remote control system through a data transmission system, and the remote control system analyzes the data.

[0028] S3, the signal instruction is re-sent, the wind speed around the aircraft and the position are calibrated and measured, and the wind speed and air pressure are collected for each position.

[0029] S4, the wind speed of the idling dangerous area position is measured through the wind speed tester, and the distance of each idling dangerous area position from the aircraft is calibrated by using the ultrasonic range finder.

[0030] S5, the surroundings of the idling deicing aircraft are measured, and the data about the distance from the aircraft and the wind speed of each idling dangerous area position are collected.

[0031] S6, for different positions, the telescopic probe structure is controlled to be telescoped by the master control system, so that the height perpendicular to the idling dangerous area is collected;

[0032] S7, the data of the wind speed of each idling dangerous area position is collected, and the boundary of each idling dangerous area is alarmed by a danger alarm device;

[0033] S8, the idling dangerous area of the airplane is obtained by connecting the edges of the idling dangerous area and the safe area.

[0034] Another object of the present application is to provide a remote control detection device for implementing the airplane concentrated idling deicing dangerous area detection calibration method.

[0035] Another object of the present application is to provide a real-time data collection and processing analysis device for implementing the airplane concentrated idling deicing dangerous area detection calibration method.

[0036] Another object of the present application is to provide a storage medium receiving a user input program, the computer program stored in the storage medium enabling an electronic device to execute the airplane concentrated idling deicing dangerous area detection calibration method.

[0037] Another object of the present application is to provide a computer device including a memory and a processor, the memory storing a computer program, the computer program being executed by the processor to enable the processor to execute the airplane concentrated idling deicing dangerous area detection calibration method.

[0038] Another object of the present application is to provide an information data processing terminal installed on an electronic device to provide a user input interface to implement the airplane concentrated idling deicing dangerous area detection calibration method.

[0039] Another object of the present application is to provide an airplane concentrated idling deicing dangerous area detection calibration robot to implement the airplane concentrated idling deicing dangerous area detection calibration method.

[0040] In combination with all the above technical solutions, the present application has the advantages and positive effects as follows: in order to solve the safety hazard problem of the engine wake to the deicing personnel in the existing airplane idling deicing process, the present application designs a calibration device for the idling deicing dangerous area of the airplane in combination with the idling deicing process of the airplane engine. In order to solve the identification and calibration problems in the idling deicing dangerous area of the airplane, the present application designs an idling deicing dangerous calibration device of the airplane in combination with the idling deicing process of the airplane, which has practical significance.

[0041] The application provides a device for detecting and calibrating a dangerous area of a centralized idling deicing aircraft, which collects data around the idling deicing aircraft, analyzes the data through a main control system, and calibrates and identifies the dangerous area through a positioning system and a danger alarm device; the device is provided with an anti-toppling system to adapt to various weather conditions and improve the stability of the device; the device is provided with a track-type self-propelled system, which can be controlled by the main control system to enable the device to walk by itself; the device is provided with a Beidou positioning system, which can send the position of the device to a terminal system and enable real-time monitoring; the device is provided with lead-acid batteries that can be charged by solar energy; the device is provided with a wind speed measuring instrument and an ultrasonic range finder, which can transmit data collected by a data collection system to the main control system of the device; the device is provided with an up-down telescopic probe structure, which can measure and calibrate the wind speed at the vertical height; and the danger alarm device can alarm in dangerous situations and mark the position. BRIEF DESCRIPTION OF DRAWINGS

[0042] The accompanying drawings, which are incorporated herein and form a part of the specification, illustrate embodiments consistent with the present disclosure and, together with the description, further serve to explain the principles of the present disclosure;

[0043] Figure 1 FIG. 1 is a schematic diagram of a device for detecting and calibrating a dangerous area of a centralized idling deicing aircraft according to an embodiment of the present application;

[0044] Figure 2 FIG. 2 is a flowchart of a method for detecting and calibrating a dangerous area of a centralized idling deicing aircraft according to an embodiment of the present application;

[0045] In the figure: 1, up-down telescopic probe structure; 2, track-type walking system; 3, anti-toppling system; 4, lead-acid battery pack; 5, sensing system; 5-1, wind speed measuring instrument; 5-2, ultrasonic range finder; 5-3, temperature sensor; 5-4, infrared thermal imaging sensor; 6, calibration device; 7, intelligent control unit; 8, main control system; 9, Beidou positioning system; 10, danger alarm device; 11, terminal system. DETAILED DESCRIPTION

[0046] To make the above objectives, features and advantages of the present application more apparent and easy to understand, the specific embodiments of the present application are described in detail below in conjunction with the accompanying drawings. In the following description, a large number of specific details are set forth in order to fully understand the present application. However, the present application can be implemented in many other ways different from those described herein, and those skilled in the art can make similar improvements without departing from the scope of the present application, so the present application is not limited to the specific implementation disclosed below.

[0047] Embodiment 1, the method for detecting and calibrating a dangerous area of a centralized idling deicing aircraft according to an embodiment of the present application comprises:

[0048] The aircraft centralized idling de-icing hazard zone detection and calibration device provided by the present invention collects information on the external environment around the aircraft during idling de-icing, such as temperature, air pressure, and wind speed, and uses the main control system 8 to identify and control the hazard alarm device 10 to issue an alarm based on the wind speed data of the surrounding idling de-icing hazard zone.

[0049] Next, the idling danger zone is calibrated. The location is determined by the Beidou positioning system 9 and the ultrasonic rangefinder 5-2. The main control system 8 controls the tracked walking system 2 to measure the idling de-icing danger zone, thereby determining the idling danger zone around the idling de-icing aircraft and calibrating it.

[0050] Example 2, as Figure 1 As shown, the aircraft idling de-icing idling danger zone calibration device provided in this embodiment of the invention includes: a telescopic probe structure 1, a tracked walking system 2, an anti-rollover system 3, a lead-acid battery pack 4, a sensing system 5, a calibration device 6, an intelligent control unit 7, a main control system 8, and a Beidou positioning system 9.

[0051] The telescopic probe structure 1 provides a vertical telescopic function, allowing the sensing system 5 to be retracted when not in use.

[0052] The tracked walking system 2 has a self-propelled movement function, which can intelligently move its position according to different climate conditions and different models, combined with the results of measurement data analysis; the tracks are made of rubber material, which will not damage the apron surface.

[0053] The anti-rollover system 3 can automatically adjust the height and center position of the chassis (not shown) according to the wind speed;

[0054] The lead-acid battery pack 4 can be charged by solar energy, providing a stable current for the entire device;

[0055] The sensing system 5 includes: an anemometer 5-1 for testing wind speed, an ultrasonic rangefinder 5-2 for measuring distance, a temperature sensor 5-3 for measuring the ambient temperature, and an infrared thermal imaging sensor 5-4 for acquiring real-time external images, and is connected to the intelligent control unit 7 via a control cable.

[0056] The calibration device 6 can provide audio-visual indication and ground spraying indication based on the data analysis results.

[0057] The intelligent control unit 7 has functions such as collaborative positioning, networking, and information exchange. It combines with the Beidou positioning system 9 to send calibration location information to the main control system 8, forming a three-dimensional guidance map of the aircraft idling de-icing danger zone, and accurately guiding the operating vehicle.

[0058] The track walking system 2 is controlled by the main control system 8 to walk, the height is continuously adjusted by the up-down telescopic probe structure 1, the height of the airflow generated by the engine of the airplane is tested, and the wind speed is measured by the wind speed measuring instrument 5-1;

[0059] The collected different wind speeds are analyzed by the program of the main control system 8, the dangerous alarm device 10 connected with the main control system 8 is used for alarm analysis, the distance between the idle speed dangerous area distance from the airplane collected by the ultrasonic range finder 5-2 is positioned by the Beidou positioning system 9, and different idle speed dangerous area positions are positioned.

[0060] As shown in Figure 2 The idle speed dangerous area calibration method under the airplane idle speed deicing state provided by the embodiment of the application specifically comprises the following steps:

[0061] S101, a signal is sent to the device by a remote system, the device receives the instruction signal, the main control system 8 is conducted to the track walking system 2, the track walking system 2 is rotated by the track, and the airplane deiced by the idle speed is detected and data is collected;

[0062] S102, the historical data in step S101 is collected and processed, and the data is transmitted to a remote control system by a data transmission system for analysis;

[0063] S103, a signal instruction is re-sent, the wind speed around the airplane and the position of the device are calibrated and measured by the device, and the wind speed v and the air pressure p are collected for each position;

[0064] S104, step S103 is repeated, the wind speed of the idle speed dangerous area position is measured by the wind speed measuring instrument 5-1 on the device, and the distance of each idle speed dangerous area position from the airplane is calibrated by the ultrasonic range finder 5-2;

[0065] S105, step S104 is repeated, the surrounding of the airplane deiced by the idle speed is measured, and the related data about the distance from the airplane (x, y) and the related wind speed of each idle speed dangerous area position are collected;

[0066] S106, step S103 is repeated, the extension of the up-down telescopic probe structure 1 is controlled by the main control system 8 for different positions, so that the vertical height z of the idle speed dangerous area is collected;

[0067] S107, the data of the related wind speed of each position is collected by repeating steps S105 and S106, and the boundary of each idle speed dangerous area is alarmed by the dangerous alarm device 10 of the device;

[0068] S108, the dangerous area of the airplane idling deicing is obtained by connecting the edge of the idling dangerous area and the safe area.

[0069] In the embodiment 4, the detection device can be remotely controlled, and the ultrasonic range finder 5-2 and the wind speed detector 5-1 can complete the measurement under the control of the main control system 8 and transmit to the terminal system 11.

[0070] The terminal system 11 locates each idling dangerous area through the Beidou positioning system 9, so as to determine the position of the danger. The operation is repeated, so as to identify the idling dangerous area around the idling deicing. The idling dangerous area of the idling deicing is found and calibrated, so as to obtain a three-dimensional danger schematic diagram. The safety of the related deicing personnel is ensured.

[0071] In the embodiment 5, the device for collecting and processing analysis of real-time data is provided. The information data is processed, the main control system 8 stores the computer program, and the crawler walking system 2 and the danger alarm device 10 can alarm and mark the dangerous position. The whole idling dangerous area calibration device based on the airplane idling deicing state identifies the idling dangerous area of the airplane idling deicing.

[0072] In the embodiment 6, the idling dangerous area calibration method based on the airplane idling deicing state in the embodiment 3 is described. In a preferred embodiment, the step S101 collects the height of the up-down telescopic probe structure 1, and the wind speed at different heights is measured by the wind speed detector 5-1. The collected wind speed is transmitted to the main control system 8, and the data collection, judgment and interaction are performed through the program of the main control system 8. The wind speed is judged, and the dangerous area is identified and calibrated through the interaction with the terminal system 11.

[0073] If the area is dangerous, the danger alarm device 10 needs to be controlled to alarm. The data at different height positions are collected and interacted to the terminal system 11, so as to determine the position of each danger.

[0074] In the above embodiments, the description of each embodiment has its own emphasis, and the part not described or recorded in a certain embodiment can be referred to the related description of other embodiments.

[0075] The information interaction, execution process and the like between the above devices / units are based on the same concept as the method embodiments of the present application, and the specific functions and the technical effects brought by the specific functions can be referred to the method embodiments, which will not be described here.

[0076] Those skilled in the art can clearly understand that, for the convenience and brevity of description, only the above-mentioned division of each functional unit and module is exemplified, and in actual application, the above-mentioned functions can be completed by different functional units and modules according to needs, that is, the internal structure of the device is divided into different functional units or modules to complete all or part of the functions described above. Each functional unit and module in the embodiment can be integrated in one processing unit, or each unit can exist physically, or two or more units can be integrated in one unit, and the integrated unit can be realized in the form of hardware or software. In addition, the specific name of each functional unit and module is only for convenient distinction, and does not limit the protection scope of the present application. The specific working process of the unit and module in the above system can refer to the corresponding process in the foregoing method embodiment.

[0077] The embodiment of the present application further provides a computer device, which comprises at least one processor, a memory and a computer program stored in the memory and executable on the at least one processor, wherein the processor implements the steps in any of the method embodiments described above when executing the computer program.

[0078] The embodiment of the present application further provides a computer readable storage medium, which stores a computer program, wherein the computer program is executable by a processor to implement the steps in any of the method embodiments described above.

[0079] The embodiment of the present application further provides an information data processing terminal, which is used to provide a user input interface to implement the steps in any of the method embodiments described above when executed on an electronic device, and the information data processing terminal is not limited to a mobile phone, a computer or a switch.

[0080] The embodiment of the present application further provides a server, which is used to provide a user input interface to implement the steps in any of the method embodiments described above when executed on an electronic device.

[0081] The embodiment of the present application further provides a computer program product, which, when executed on an electronic device, enables the electronic device to implement the steps in any of the method embodiments described above.

[0082] The integrated unit, if implemented in the form of a software function unit and sold or used as an independent product, can be stored in a computer-readable storage medium. Based on such understanding, all or part of the processes in the above-mentioned embodiment methods can be completed by a computer program instructing related hardware, and the computer program can be stored in a computer-readable storage medium. When the processor executes the computer program, the steps of the above-mentioned various method embodiments can be implemented. The computer program includes computer program code, which can be in the form of source code, object code, executable files, or some intermediate forms, etc. The computer-readable medium at least includes any entity or device capable of carrying the computer program code to the photographing device / terminal equipment, a recording medium, a computer memory, a read-only memory (ROM), a random access memory (RAM), an electrical carrier signal, a telecommunication signal, and a software distribution medium. For example, a U disk, a mobile hard disk, a magnetic disk or an optical disk, etc.

[0083] Through the above embodiments, it is shown that the present application measures parameters such as distance, wind speed, temperature, and wake heat field through a sensor group, and the intelligent control unit 7 performs dangerous area position calibration through photoelectric indication signals. The device has a tracked automatic walking system, can intelligently move positions according to different climate conditions and different machine types in combination with measurement data analysis results, thereby performing accurate calibration and indication. After multiple devices are calibrated, position information is sent in combination with a Beidou / GPS system to a main control system 8, a three-dimensional guidance map of an airplane idling deicing dangerous area is formed, and an operation vehicle is accurately guided. The present application has great significance for guaranteeing airplane ground deicing efficiency and deicing worker safety.

[0084] The above is only a preferred specific embodiment of the present application, but the protection scope of the present application is not limited thereto. Any modification, equivalent replacement, and improvement within the technical range disclosed by the present application and within the spirit and principles of the present application should be covered within the protection scope of the present application.

Claims

1. An aircraft centralized idle de-icing danger zone detection calibration device, characterized in that, The device collects the temperature, air pressure and wind speed information around the idling deicing aircraft, identifies the wind speed data of the surrounding idling deicing dangerous area through the main control system (8), controls the dangerous alarm device (10) to alarm, and then calibrates the idling dangerous area, determines the position through the Beidou positioning system (9) and the ultrasonic range finder (5-2), controls the crawler walking system (2) to measure the idling deicing dangerous area through the main control system (8), and determines the idling deicing dangerous area around the idling deicing aircraft while calibrating; The aircraft centralized idling deicing dangerous area detection and calibration device further comprises: The up-and-down telescopic probe structure (1) is used for installing the vertical telescopic rod and withdrawing the sensing system (5) when not working; The crawler walking system (2) moves the position according to different climate conditions and aircraft types and in combination with the measurement data analysis result; The anti-rollover system (3) automatically adjusts the chassis height and center position according to the wind speed of the idling deicing dangerous area; The lead-acid battery pack (4) is used for providing stable current; The sensing system (5) is used for testing the wind speed and the distance of the idling deicing dangerous area from the aircraft, and the control cable is connected with the intelligent control unit (7); The calibration device (6) performs sound-light indication and ground spray indication according to the analysis result of the main control system (8); The intelligent control unit (7) utilizes cooperative positioning, networking and information exchange, combines the Beidou positioning system (9), sends the calibration position information to the main control system (8), forms a three-dimensional guidance map of the idling deicing dangerous area of the aircraft, and guides the operation vehicle; The main control system (8) is used for analyzing different wind speed data collected and analyzing and alarming through the dangerous alarm device (10); The Beidou positioning system (9) respectively positions different idling dangerous areas and identifies and calibrates the idling deicing dangerous area of the aircraft; The terminal system (11) positions each idling dangerous area through the Beidou positioning system (9) and determines the position of the dangerous area.

2. The aircraft centralized idle speed de-icing danger zone detection calibration device of claim 1, wherein, The sensing system (5) comprises: The wind speed tester (5-1) is used for testing the wind speed of the idling deicing dangerous area; The ultrasonic range finder (5-2) is used for testing the distance of the idling deicing dangerous area from the aircraft; The temperature sensor (5-3) is used for measuring the external temperature; The infrared thermal imaging sensor (5-4) is used for acquiring external real-time images.

3. A method for detecting and calibrating hazardous areas during centralized idling de-icing of aircraft, characterized in that, The method is implemented by using the aircraft centralized idling deicing dangerous area detection and calibration device according to any one of claims 1-2, and the method comprises the following steps: S1, a signal is sent through a remote control system, after receiving the instruction signal, the signal is transmitted to the crawler walking system (2) through the main control system (8), the crawler walking system (2) rotates through the crawler belt, and the idling deicing aircraft is detected and data is collected; S2, historical data is collected, the data is transmitted to the remote control system through a data transmission system, and the remote control system analyzes the data; S3, a signal instruction is re-sent, the wind speed around the aircraft and the position are calibrated and measured, and the wind speed and air pressure of each position are collected. S4, the wind speed of the idle dangerous area position is measured by the wind speed meter (5-1), and the distance between each idle dangerous area position and the airplane is calibrated by the ultrasonic range finder (5-2); S5, the surrounding of the idle deicing airplane is measured, and the distance between the idle deicing dangerous area and the airplane and the wind speed of each idle dangerous area position are collected; S6, the stretching and retracting of the up-and-down retractable probe structure (1) is controlled by the main control system (8) for different positions, so that the vertical height of the idle dangerous area is collected; S7, the data of the wind speed of each idle dangerous area position is collected, and the boundary of each idle dangerous area is alarmed by the danger alarm device (10); S8, the edges of the idle dangerous area and the safe area are connected, and the idle deicing dangerous area of the airplane is obtained.

4. A remotely operated detection device, characterized by, The remote control detection device is used to implement the airplane centralized idle deicing dangerous area detection and calibration method in claim 3.

5. An apparatus for acquisition and processing analysis of real-time data, characterized by, The real-time data collection and processing and analysis device is used to implement the airplane centralized idle deicing dangerous area detection and calibration method in claim 4.

6. A storage medium that receives a user input program, characterized by The computer program stored in the storage medium makes the electronic device execute the airplane centralized idle deicing dangerous area detection and calibration method in claim 3.

7. A computer device, comprising: The computer device includes a memory and a processor, the memory stores a computer program, and the computer program is executed by the processor, so that the processor executes the airplane centralized idle deicing dangerous area detection and calibration method in claim 3.

8. An information data processing terminal, characterized by The information data processing terminal installed on the electronic device provides a user input interface to implement the airplane centralized idle deicing dangerous area detection and calibration method in claim 3.

9. An aircraft centralized idle speed de-icing danger zone detection calibration robot, characterized in that, The airplane centralized idle deicing dangerous area detection and calibration method in claim 3 is implemented.

Images