Intelligent civil aircraft comprehensive monitoring device
The intelligent civil aircraft integrated monitoring device integrates communication and remote monitoring modules and data processing modules to collect and analyze multiple parameters in real time, solving the problem of lag in traditional monitoring devices and improving flight safety and efficiency.
Patent Information
- Application Number
- CN202423275861.9
- Authority / Receiving Office
- CN · China
- Patent Type
- Utility models(China)
- Current Assignee / Owner
- Filing Date
- 2024-12-30
- Publication Date
- 2025-11-07
- Estimated Expiration
- 2034-12-30
AI Technical Summary
Traditional civil aircraft monitoring devices are insufficient to meet the needs of modern flight. The increased number of parameters leads to pilot fatigue, and manual judgment is subject to lag, affecting flight safety and efficiency.
Design an intelligent civil aircraft integrated monitoring device that integrates a communication and remote monitoring module, a data processing module, and multiple sensors to collect and analyze flight, engine, structural health, meteorological, and navigation parameters in real time, providing intuitive parameter display and alarm functions, and realizing remote monitoring and data exchange.
It improves the accuracy and timeliness of pilots' flight decisions, ensures flight safety and efficiency, reduces pilot fatigue, and enables remote monitoring and real-time dispatch.
Smart Images
Figure CN223521040U_ABST
Abstract
Description
TECHNICAL FIELD
[0001] The utility model relates to an airplane monitoring technical field, concretely is a kind of intelligent civil aviation airplane comprehensive monitoring device. BACKGROUND
[0002] In traditional civil aviation airplane monitoring technology, the parameters of the aircraft are usually monitored by the pilot through the instrument panel and various indicators, however, with the continuous development of flight technology and the increasing complexity of the aircraft system, the number of parameters that the pilot needs to monitor increases significantly, and the traditional instrument panel and indicator have been difficult to meet the needs of modern flight, in addition, the traditional monitoring technology often relies on manual judgment and experience, and there is a lag in the discovery and handling of potential faults, which makes it difficult to ensure the safety and efficiency of flight, at the same time, the pilot needs to handle a large amount of information during flight, and relying on the traditional monitoring method is easy to make the pilot feel tired, increasing the risk of flight.
[0003] Therefore, it is particularly important to design an intelligent civil aviation airplane comprehensive monitoring device to change the above technical defects and improve the overall practicality. INVENTION CONTENTS
[0004] The utility model aims at providing an intelligent civil aviation airplane comprehensive monitoring device to solve the problems raised in the background technology.
[0005] To achieve the above-mentioned purpose, the utility model provides the following technical scheme:
[0006] An intelligent civil aviation airplane comprehensive monitoring device, comprising a body and a console, the interior of the console is provided with a control panel, the control panel is connected with a communication and remote monitoring module, the control panel is connected with a data processing module, the data processing module comprises a data acquisition, data storage, data fusion analysis and diagnosis module, the data fusion analysis and diagnosis module is composed of a fault diagnosis algorithm, a health assessment module, an alarm and a warning;
[0007] The data acquisition is connected with a sensor module, the sensor module is composed of a flight parameter sensor, an engine parameter sensor, a structural health parameter sensor, a meteorological parameter sensor and a navigation parameter sensor, wherein the flight parameter sensor comprises an airspeed tube, an altimeter, a heading gyroscope and an attitude sensor, the engine parameter sensor is composed of a speed sensor, a temperature monitor, a pressure sensor and a fuel flow sensor, the structural health parameter sensor comprises a piezoelectric sensor and an optical fiber flow sensor, the meteorological parameter sensor comprises a temperature detector, a humidity sensor and a wind speed and direction sensor, and the navigation parameter sensor comprises a GPS receiver, an inertial navigation system and a radio navigation sensor.
[0008] As the preferred scheme of the utility model, the control panel further includes a touch screen, control buttons, an interface, and a loudspeaker for displaying parameters and giving warnings.
[0009] As the preferred scheme of the utility model, the airspeed tube is arranged at the front of the fuselage for measuring airspeed, the altimeter is arranged at the top of the fuselage, the fuselage is provided with a stable platform, and the heading gyroscope and the attitude sensor are usually arranged on the stable platform of the fuselage for providing accurate heading and attitude information.
[0010] As the preferred scheme of the utility model, the engine parameter sensor is arranged on the engine, the meteorological parameter sensor is arranged at the top of the fuselage for measuring external meteorological conditions, the GPS receiver is arranged at the top of the fuselage for receiving signals from satellites, and the inertial navigation system and the radio navigation sensor are integrated in the console.
[0011] As the preferred scheme of the utility model, the control panel is embedded on the console and communicates and transmits data with the console through a cable, the communication and remote monitoring module is a functional module of the control panel, is responsible for communication and data exchange with ground stations and other aircraft, and is connected and communicates with the control panel through the interface provided by the control panel.
[0012] As the preferred scheme of the utility model, the data processing module is a functional module of the control panel, is responsible for receiving data from the sensor module, and processes, analyzes and diagnoses the data, and is connected and communicates with the control panel through a special interface of the control panel.
[0013] Compared with the prior art, the utility model has the beneficial effects that:
[0014] 1. The utility model discloses an intelligent civil aviation aircraft comprehensive monitoring device, utilize the structure of communication and remote monitoring module, data processing module, sensor module, through the real -time collection of all kinds of sensor module setting flight parameter, engine parameter, structure health parameter, meteorological parameter and navigation parameter, these sensor data are transmitted to the data processing module in the control cabinet, and this module is responsible for the receiving, storage, fusion analysis and diagnosis of data, and the data processing module uses fault diagnosis algorithm, health evaluation module and alarm and early warning function, in -depth analysis is carried out to sensor data, and potential failure is discovered and handled in time, simultaneously, the touch -sensitive screen, control button, interface and loudspeaker etc. Component on the control panel provides the intuitive parameter display, warning information and operation interface for the pilot, in addition, communication and remote monitoring module makes the aircraft can communicate and data exchange with the ground station and other aircraft, realizes remote monitoring and real -time scheduling, and the pilot can make more accurate and timely flight decision according to the data and analysis result handled, ensures the safety and efficiency of flight, solves the problem that traditional monitoring device is not comprehensive, only relies on the pilot's observation, cannot better grasp the flight state of the aircraft, makes more accurate and timely flight decision, thereby ensures the safety and efficiency of flight. BRIEF DESCRIPTION OF DRAWINGS
[0015] Fig. 1 It is the overall structural drawing of the utility model;
[0016] Fig. 2 It is the machine body schematic view of the utility model;
[0017] Fig. 3 It is the schematic diagram of sensor module of the utility model.
[0018] In the drawing: 1, control panel; 101, communication and remote monitoring module; 102, data processing module; 103, data acquisition; 104, data storage; 105, data fusion analysis and diagnosis module; 1051, fault diagnosis algorithm; 1052, health evaluation module; 1053, alarm and early warning; 2, sensor module; 201, flight parameter sensor; 2011, pitot tube; 2012, altimeter; 2013, heading gyroscope; 2014, attitude sensor; 202, engine parameter sensor; 2021, speed sensor; 2022, temperature monitor; 2023, pressure sensor; 2024, fuel flow sensor; 203, structure health parameter sensor; 2031, piezoelectric sensor; 2032, optical fiber flow sensor; 204, meteorological parameter sensor; 2041, temperature detector; 2042, humidity sensor; 2043, wind speed and direction sensor; 205, navigation parameter sensor; 2051, GPS receiver; 2052, inertial navigation system; 2053, radio navigation sensor; 3, control cabinet; 4, machine body. DETAILED DESCRIPTION
[0019] The technical solutions in the embodiments of the present application will be apparently and completely described below with reference to the drawings. Obviously, the described embodiments are only a part of the embodiments of the present application, rather than all the embodiments of the present application. Based on the embodiments of the present application, all the other embodiments obtained by those skilled in the art without any creative work fall within the scope of the present application.
[0020] In order to facilitate the understanding of the present application, the present application will be described more fully below with reference to the accompanying drawings. Several embodiments of the present application are given. However, the present application can be realized in many different forms and is not limited to the embodiments described herein. On the contrary, the purpose of providing these embodiments is to make the disclosure of the present application more thorough and comprehensive.
[0021] It should be noted that when an element is referred to as being "fixedly attached" to another element, it can be directly on the other element or there can be intervening elements. When an element is referred to as being "connected" or "coupled" to another element, it can be directly connected or coupled to the other element or intervening elements can be present. As used herein the terms "vertical", "horizontal", "left", "right" and the like are merely used for the purpose of illustration.
[0022] Unless otherwise defined, all technical and scientific terms used herein have the same meaning as commonly understood by one of ordinary skill in the art to which this application belongs. The terminology used in the description of the application herein is for the purpose of describing particular embodiments only and is not intended to be limiting of the application. As used herein, the term "and / or" includes any and all combinations of one or more of the associated listed items.
[0023] Embodiments, please see Figs. 1-3 The present application provides a technical solution:
[0024] The utility model provides an intelligent civil aviation aircraft comprehensive monitoring device, including body 4, control platform 3, the inside of control platform 3 is equipped with control panel 1, control panel 1 connects communication and remote monitoring module 101, control panel 1 connects data processing module 102, data processing module 102 includes data acquisition 103, data storage 104, data fusion analysis and diagnosis module 105, data fusion analysis and diagnosis module 105 is by fault diagnosis algorithm 1051, health assessment module 1052, alarm and early warning 1053 constitutes, data acquisition 103 connects sensor module 2, and sensor module 2 is by flight parameter sensor 201, engine parameter sensor 202, structural health parameter sensor 203, meteorological parameter sensor 204, navigation parameter sensor 205 constitutes, wherein flight parameter sensor 201 includes airspeed pipe 2011, altimeter 2012, heading gyroscope 2013, attitude sensor 2014 constitutes, and engine parameter sensor 202 is by speed sensor 2021, temperature monitor 2022, pressure sensor 2023, fuel flow sensor 2024 constitutes, and structural health parameter sensor 203 includes piezoelectric sensor 2031, optical fiber flow sensor 2032, and meteorological parameter sensor 204 includes temperature detector 2041, humidity sensor 2042, wind speed and direction sensor 2043, and navigation parameter sensor 205 includes GPS receiver 2051, inertial navigation system 2052, radio navigation sensor 2053, the device is through the various sensor modules 2 on the body, and the key parameters of aircraft are collected in real time, and these parameters include but are not limited to flight parameter 201 such as airspeed, height, heading and attitude, engine parameter 202 such as speed, temperature, pressure and fuel flow, structural health parameter 203 such as stress, vibration of body, meteorological parameter 204 such as temperature, humidity, wind speed and direction and navigation parameter 205 such as GPS position, inertial navigation data and radio navigation signal, sensor module 2 gathers these data, will be transmitted to the data processing module 102 in the control platform 3, and data processing module 102 is a highly integrated system, it is responsible for receiving the original data from sensor module 2, stores, fusion analysis and diagnosis, in this process, data processing module 102 will use advanced fault diagnosis algorithm 1051, and the sensor data is in-depth analyzed to identify any potential failure or abnormal situation, simultaneously, health assessment module 1052 will assess the overall health condition of aircraft, and generates corresponding health report, when data processing module 102 detects potential failure or abnormality, it will immediately trigger alarm and early warning 1053 function, at this time, the touch screen on control panel 1 will show detailed alarm information, including fault type, location and possible solution, simultaneously, the loudspeaker will issue a sound alarm to remind the pilot, and the pilot can confirm and handle these alarm information through the control button and interface on control panel 1, in addition to providing alarm and early warning 1053 information,The control panel 1 also provides an intuitive parameter display and operation interface for the pilot, who can view various parameters of the aircraft at any time to understand the real-time state of the aircraft, which helps the pilot better grasp the flight state of the aircraft and make more accurate and timely flight decisions. In addition, the communication and remote monitoring module 101 is an important component, which enables the aircraft to communicate and exchange data with ground stations and other aircraft, realizes remote monitoring and real-time scheduling, which helps ground personnel to understand the flight state and position information of the aircraft in real time, and provides support and guarantee for the flight decision of the pilot.
[0025] The control panel 1 further comprises a touch screen, control buttons, interfaces, speakers for displaying parameters, warnings, the attitude sensor 2014 comprises a pitch angle sensor, a roll angle sensor, the pilot can intuitively view the parameters of the aircraft, obtain warning information in time, and perform necessary operations, the pitot tube 2011 is arranged at the front of the fuselage 4 for measuring airspeed, the altimeter 2012 is located at the top of the fuselage, the fuselage 4 is provided with a stable platform, and the heading gyroscope 2013 and the attitude sensor 2014 are usually located on the stable platform of the fuselage 4 for providing accurate heading and attitude information, ensuring that the aircraft can accurately obtain key information such as airspeed, altitude, heading and attitude during flight. This helps the pilot to better master the flight state of the aircraft, the engine parameter sensor 202 is arranged on the engine, the meteorological parameter sensor 204 is arranged at the top of the fuselage 4 for measuring external meteorological conditions, the GPS receiver 2051 is arranged at the top of the fuselage 4 for receiving signals from satellites, the inertial navigation system 2052 and the radio navigation sensor 2053 are integrated inside the console 3, which can monitor the running state of the engine in real time, discover and handle potential faults in time, the meteorological parameter sensor is arranged at the top of the fuselage, which can accurately measure the external meteorological conditions and provide important basis for the pilot's decision. The setting of the GPS receiver, the inertial navigation system and the radio navigation sensor provides reliable navigation information, ensuring the accuracy and safety of flight, the control panel 1 is embedded on the console 3 and communicates and transmits data with the console 3 through a cable, the communication and remote monitoring module 101 is a functional module of the control panel 1, responsible for communication and data exchange with ground stations and other aircraft, and connected and communicated with the control panel 1 through the interface provided by the control panel 1, which can communicate and exchange data with ground stations and other aircraft. This helps to realize the remote monitoring and real-time scheduling of the aircraft, improves the flexibility and efficiency of flight, the data processing module 102 is a functional module of the control panel 1, responsible for receiving data from the sensor module 2 and processing, analyzing and diagnosing, and connected and communicated with the control panel 1 through the special interface of the control panel 1, responsible for receiving data from the sensor module and processing, analyzing and diagnosing. Through powerful data processing capability, this module can discover and handle potential faults and problems in time, and provide strong data support for the pilot's decision. At the same time, through data analysis and diagnosis, important reference basis can be provided for the maintenance and maintenance of the aircraft, prolonging the service life of the aircraft.
[0026] The utility model discloses a working procedure: when using the intelligent civil aviation aircraft comprehensive monitoring device, first, the device collects the key parameters of the aircraft in real time through various sensor modules 2 on the aircraft body, these parameters include but are not limited to flight parameters 201 such as airspeed, altitude, heading and attitude, engine parameters 202 such as speed, temperature, pressure and fuel flow, structural health parameters 203 such as stress and vibration of the aircraft body, weather parameters 204 such as temperature, humidity, wind speed and direction, and navigation parameters 205 such as GPS position, inertial navigation data and radio navigation signals, the sensor module 2 collects these data, which will be transmitted to the data processing module 102 in the console 3, the data processing module 102 is a highly integrated system, which is responsible for receiving raw data from the sensor module 2, storing, fusion analysis and diagnosis, in this process, the data processing module 102 will use advanced fault diagnosis algorithm 1051 to analyze the sensor data in depth to identify any potential failure or abnormal condition, at the same time, the health assessment module 1052 will assess the overall health condition of the aircraft and generate a corresponding health report, when the data processing module 102 detects potential failure or abnormality, it will immediately trigger the alarm and early warning 1053 function, at this time, the touch screen on the control panel 1 will display detailed alarm information, including fault type, location and possible solution, at the same time, the loudspeaker will sound an audible alarm to remind the pilot, the pilot can confirm and handle these alarm information through the control buttons and interfaces on the control panel 1, in addition to providing alarm and early warning 1053 information, the control panel 1 also provides a visual parameter display and operation interface for the pilot, the pilot can check the parameters of the aircraft at any time to understand the real-time state of the aircraft, which helps the pilot better master the flight state of the aircraft and make more accurate and timely flight decisions. In addition, the communication and remote monitoring module 101 is an important component, which enables the aircraft to communicate and exchange data with the ground station and other aircraft, realizes remote monitoring and real-time scheduling, which helps ground personnel to understand the flight state and position information of the aircraft in real time, provides support and guarantee for the flight decision of the pilot.
[0027] In summary, the intelligent civil aviation aircraft comprehensive monitoring device collects, transmits, processes and analyzes the key parameters of the aircraft in real time, provides comprehensive flight information and alarm and early warning functions for the pilot, which helps the pilot better master the flight state of the aircraft and make more accurate and timely flight decisions, thereby ensuring the safety and efficiency of flight.
[0028] The standard parts used in the present application file can be purchased from the market, the specific connection mode of each part adopts the conventional means such as bolt, rivet and welding in the prior art, the mechanical, part and equipment adopt the conventional type in the prior art, the control mode is controlled through the control panel, the control circuit of the control panel can be realized through the simple circuit connection of the person skilled in the art, which belongs to the public knowledge in the art, so the control mode and circuit connection are not explained in detail in the present application.
[0029] Although the embodiments of the present application have been shown and described, it can be understood by those skilled in the art that various changes, modifications, replacements and modifications can be made to these embodiments without departing from the principles and spirits of the present application, the scope of the present application is defined by the appended claims and their equivalents.
Claims
1. An intelligent civil aircraft integrated monitoring device, comprising a fuselage (4), a control console (3), characterized in that: The inside of the control console (3) is provided with a control panel (1), the control panel (1) is connected with a communication and remote monitoring module (101), the control panel (1) is connected with a data processing module (102), the data processing module (102) comprises a data acquisition (103), a data storage (104), a data fusion analysis and diagnosis module (105), the data fusion analysis and diagnosis module (105) is composed of a fault diagnosis algorithm (1051), a health evaluation module (1052), an alarm and early warning (1053); The data acquisition (103) is connected with a sensor module (2), the sensor module (2) is composed of a flight parameter sensor (201), an engine parameter sensor (202), a structure health parameter sensor (203), a meteorological parameter sensor (204), a navigation parameter sensor (205), wherein the flight parameter sensor (201) comprises an airspeed tube (2011), an altimeter (2012), a heading gyroscope (2013), an attitude sensor (2014), the engine parameter sensor (202) is composed of a speed sensor (2021), a temperature monitor (2022), a pressure sensor (2023), a fuel flow sensor (2024), the structure health parameter sensor (203) comprises a piezoelectric sensor (2031), an optical fiber flow sensor (2032), the meteorological parameter sensor (204) comprises a temperature detector (2041), a humidity sensor (2042), a wind speed and direction sensor (2043), the navigation parameter sensor (205) comprises a GPS receiver (2051), an inertial navigation system (2052), a radio navigation sensor (2053). 2.The intelligent civil aircraft integrated monitoring device according to claim 1, characterized in that: The control panel (1) further comprises a touch screen, control buttons, interfaces, speakers for displaying parameters, warnings, the attitude sensor (2014) comprises a pitch angle sensor, a roll angle sensor. 3.The intelligent civil aircraft integrated monitoring device according to claim 1, characterized in that: The airspeed tube (2011) is arranged at the front of the fuselage (4) for measuring airspeed, the altimeter (2012) is located at the top of the fuselage, the fuselage (4) is provided with a stable platform, and the heading gyroscope (2013), the attitude sensor (2014) are usually located on the stable platform of the fuselage (4) for providing accurate heading and attitude information.
4. The intelligent civil aircraft integrated monitoring device according to claim 1, characterized in that: The engine parameter sensor (202) is arranged on the engine, the meteorological parameter sensor (204) is arranged at the top of the fuselage (4) for measuring external meteorological conditions, the GPS receiver (2051) is arranged at the top of the fuselage (4) for receiving signals from satellites, the inertial navigation system (2052), the radio navigation sensor (2053) are integrated inside the control console (3).
5. The intelligent civil aircraft integrated monitoring device according to claim 1, characterized in that: The control panel (1) is embedded on the console (3) and communicates and transmits data with the console (3) through a cable, the communication and remote monitoring module (101) is a functional module of the control panel (1), responsible for communication and data exchange with the ground station and other aircraft, and connected and communicated with the control panel (1) through the interface provided by the control panel (1).
6. The intelligent civil aircraft integrated monitoring device according to claim 1, characterized in that: The data processing module (102) is a functional module of the control panel (1), responsible for receiving data from the sensor module (2), and processing, analyzing and diagnosing, and connected and communicated with the control panel (1) through the special interface of the control panel (1).