A road navigation flight emergency alarm system

Abstract

The present invention provides a road navigation flight emergency alarm system, including a control module, a flight data acquisition module, a flight data analysis module, a warning instruction generation module, an in-cabin alarm module, a wireless communication module, a body light component and a storage module; wherein the flight data acquisition module is electrically connected and signal-connected with the flight data analysis module, the flight data analysis module is electrically connected and signal-connected with the warning instruction generation module, the warning instruction generation module is electrically connected and signal-connected with the in-cabin alarm module, and the in-cabin alarm module is electrically connected and signal-connected with the body light component and the body light component, respectively. The present invention enables the ground pick-up staff to know that the aircraft has a fault according to the flashing of the warning light, and the command and control end can know the fault of the aircraft according to the warning code, so that people in other fields will not panic when they know the fault of the aircraft.

Description

Technical Field

[0001] The present invention relates to the technical field of flight alarms, and in particular to a flight emergency alarm system. Background Art

[0002] Flight failures may sometimes occur during flight, preparation for takeoff, takeoff or descent. Failures caused by the aircraft body are sometimes very low-level problems that can be solved by some pilots, and sometimes they are higher-level problems that pilots need to rely on experience and on-the-spot reaction measures to solve safely, or they are difficult for pilots to solve easily. Generally, only the pilots know about the failure caused by the aircraft body at the first time, or communicate with the ground command and control to let the ground command know about the failure caused by the aircraft body, but the ground staff cannot know about it and can only take measures through communication with the ground command. Summary of the invention

[0003] In order to solve the above-mentioned deficiencies of the prior art, the purpose of the present invention is to provide a navigation flight emergency alarm system to overcome the defects in the prior art.

[0004] In order to achieve the above-mentioned purpose, the present invention provides a road navigation flight emergency alarm system, including a control module, a flight data acquisition module, a flight data analysis module, a warning instruction generation module, an in-cabin alarm module, a wireless communication module, an aircraft body lighting component and a storage module; wherein the control module is respectively electrically connected and signal-connected with the flight data acquisition module, the flight data analysis module, the in-cabin alarm module, the wireless communication module and the storage module, the flight data acquisition module is electrically connected and signal-connected with the flight data analysis module, the flight data analysis module is electrically connected and signal-connected with the warning instruction generation module, the warning instruction generation module is electrically connected and signal-connected with the in-cabin alarm module, and the in-cabin alarm module is respectively electrically connected and signal-connected with the wireless communication module and the aircraft body lighting component. connection; wherein, the flight data acquisition module collects flight data and transmits the flight data to the flight data analysis module; the flight data analysis module analyzes the received flight data, packages the abnormal flight data to generate warning information, and transmits the warning information to the warning instruction generation module; the warning instruction generation module determines the warning level according to the warning information and generates a warning instruction, and transmits the warning instruction to the cabin alarm module; the cabin alarm module generates a warning code according to the warning level of the warning instruction, and transmits the warning code to the body lighting component and the wireless communication module; the body lighting component controls different warning lights to flash according to the warning code; the wireless communication module sends the warning code to the command and control end.

[0005] Through the above technical solution, the flight data acquisition module collects real-time flight data, the flight data analysis module compares the real-time flight data with the normal flight data to obtain abnormal flight data, the early warning instruction generation module generates specific early warning instructions for the abnormal flight data according to the pre-set early warning level, the cabin alarm module generates early warning codes according to the early warning instructions to control the body lighting components to produce different early warning light flashes, and at the same time the wireless communication module sends the early warning code to the command and control end, so that the staff who pick up the plane on the ground can know that the aircraft has a malfunction according to the flashing early warning lights, and the command and control end can know the malfunction of the aircraft according to the early warning code, so that people in other fields will not panic when they know that the aircraft has a malfunction.

[0006] As a further explanation of the Luhang flight emergency alarm system of the present invention, preferably, the flight data analysis module includes a transmission module, an extraction module, an analysis module and a warning information generation module, the transmission module and the extraction module are electrically connected and signal-connected with the storage module through the control module, the extraction module is electrically connected and signal-connected with the analysis module, and the analysis module is electrically connected and signal-connected with the warning information generation module; wherein the storage module stores comparison data, the comparison data is normal flight data, and the flight data includes aircraft trajectory data, aircraft status data, environmental factor data, and accident data; the transmission module transmits the flight data to the storage module through the control module for storage, and the extraction module retrieves the comparison data corresponding to the flight data from the storage module through the control module, the comparison data carries a preset data level, and the extraction module transmits the comparison data to the analysis module; the analysis module parses the comparison data to obtain its data level, compares the flight data with the comparison data, and transmits the abnormal flight data and the corresponding data level to the warning information generation module; the warning information generation module packages the abnormal flight data according to the data level to generate warning information, and the warning information carries the corresponding warning level.

[0007] Through the above technical solution, the flight data analysis module adopts dual data transmission channels to realize the data transmission path between the flight data analysis module and the storage module, thereby increasing the data transmission speed. The warning information generation module embeds the pre-set warning level into the warning information, thereby realizing different warning processing operations according to the warning level.

[0008] As a further description of the Luhang flight emergency alarm system described in the present invention, preferably, the transmission module is electrically and signal-connected with the wireless communication module through the control module; wherein, the transmission module transmits the flight data to the wireless communication module through the control module and directly sends it to the command and control end.

[0009] Through the above technical solution, the transmission module sends the flight data directly to the command and control end through the wireless communication module, so that the command and control end can understand the flight status of the aircraft at the first time, and analyze the potential problems of the aircraft in a timely and effective manner through big data based on the flight data.

[0010] As a further explanation of the Luhang flight emergency alarm system described in the present invention, preferably, the warning instruction generation module includes a parsing module and an instruction synthesis module, and the parsing module is electrically and signal-connected to the instruction synthesis module; wherein the parsing module receives the warning information, and obtains the warning level carried by it through the warning information, generates an instruction level and transmits it to the instruction synthesis module; the instruction synthesis module synthesizes the instruction level and the warning information into a warning instruction and transmits it to the in-cabin alarm module.

[0011] Through the above technical solution, the analysis module obtains the warning level, and the warning instruction generation module embeds the preset instruction level into the warning information according to the warning level, so that the cabin alarm module can perform different instruction operations according to the instruction level.

[0012] As a further explanation of the Luhang flight emergency alarm system described in the present invention, preferably, the in-cabin alarm module includes an alarm command processing module and a voice prompt module, and the alarm command processing module is electrically and signal-connected with the body lighting assembly, the wireless communication module and the voice prompt module, respectively; wherein the alarm command processing module controls the voice prompt module according to the command level in the warning command, or randomly generates a warning code, and transmits the warning code to the body lighting assembly and the wireless communication module.

[0013] Through the above technical solution, the alarm command processing module can inform the pilot of low-level flight warnings through the voice prompt module according to the command level, and will make high-level flight warnings produce different warning light flashes through the fuselage lighting components to let the ground staff see and take timely measures.

[0014] As a further explanation of the Luhang flight emergency alarm system described in the present invention, preferably, at least two flight data acquisition modules are set, and each flight data acquisition module is electrically and signal-connected to the clock module; wherein the clock module sends a clock pulse to the flight data acquisition module so that the flight data acquisition module collects flight data at a certain frequency, and multiple flight data acquisition modules collect flight data at different frequencies.

[0015] Through the above technical solution, multiple flight data collection modules are used to collect flight data, which not only ensures the timeliness of data collection, but also reduces the workload of data collection of a single flight data collection module.

[0016] The beneficial effects of the present invention are as follows:

[0017] 1. The present invention collects real-time flight data through the flight data collection module, and the flight data analysis module compares the real-time flight data with the normal flight data to obtain abnormal flight data. The early warning instruction generation module generates a specific early warning instruction for the abnormal flight data according to the preset early warning level. The cabin alarm module generates an early warning code according to the early warning instruction to control the body lighting component to generate different early warning light flashes. At the same time, the wireless communication module sends the early warning code to the command and control end, so that the staff who meet the plane on the ground can know that the aircraft has a malfunction according to the flashing of the early warning light, and the command and control end can know the malfunction of the aircraft according to the early warning code, so that people in other fields will not panic when they know the malfunction of the aircraft.

[0018] 2. The flight data analysis module of the present invention adopts a dual data transmission channel to realize the data transmission path between the storage module and the storage module, thereby increasing the data transmission speed. The warning information generation module embeds the preset warning level into the warning information to realize different warning processing operations according to the warning level; the analysis module obtains the warning level, and the warning instruction generation module embeds the preset instruction level into the warning information according to the warning level, thereby realizing that the cabin alarm module performs different instruction operations according to the instruction level; the alarm instruction processing module can let the pilot know the flight warning of a low instruction level through the voice prompt module according to the instruction level, and will let the ground staff see the high-level flight warning through the fuselage lighting component to produce different warning lights flashing, so that timely measures can be taken. BRIEF DESCRIPTION OF THE DRAWINGS

[0019] Figure 1 It is a structural schematic diagram of the Luhang flight emergency alarm system of the present invention;

[0020] Figure 2 It is a structural schematic diagram of the flight data analysis module of the present invention;

[0021] Figure 3 It is a structural schematic diagram of the early warning instruction generation module and the cabin alarm module of the present invention. DETAILED DESCRIPTION

[0022] In order to further understand the structure, features and other purposes of the present invention, the preferred embodiments are described in detail with reference to the accompanying drawings as follows. The embodiments described in the drawings are only used to illustrate the technical solutions of the present invention and are not intended to limit the present invention.

[0023] like Figure 1As shown, a road navigation flight emergency alarm system includes a control module 1, a flight data acquisition module 2, a flight data analysis module 3, a warning instruction generation module 4, an in-cabin alarm module 5, a wireless communication module 6, an aircraft body light component 7 and a storage module 8; wherein the control module 1 is electrically connected and signal-connected with the flight data acquisition module 2, the flight data analysis module 3, the in-cabin alarm module 5, the wireless communication module 6 and the storage module 8 respectively, the flight data acquisition module 2 is electrically connected and signal-connected with the flight data analysis module 3, the flight data analysis module 3 is electrically connected and signal-connected with the warning instruction generation module 4, the warning instruction generation module 4 is electrically connected and signal-connected with the in-cabin alarm module 5, and the in-cabin alarm module 5 is electrically connected and signal-connected with the wireless communication module 6 and the aircraft body light component 7 respectively.

[0024] The flight data collection module 2 is used to collect flight data, and the flight data collection module 2 transmits the flight data to the flight data analysis module 3. Preferably, at least two flight data collection modules 2 are provided, and each flight data collection module 2 is electrically and signal-connected to the clock module; wherein the clock module sends a clock pulse to the flight data collection module 2, so that the flight data collection module 2 collects flight data at a certain frequency, and multiple flight data collection modules 2 collect flight data at different frequencies. Using multiple flight data collection modules to collect flight data not only ensures the timeliness of data collection, but also reduces the workload of data collection of a single flight data collection module.

[0025] The flight data analysis module 3 is used to analyze the received flight data, package the abnormal flight data to generate warning information, and the flight data analysis module 3 transmits the warning information to the warning instruction generation module 4. The warning instruction generation module 4 is used to determine the warning level according to the warning information and generate a warning instruction, and the warning instruction generation module 4 transmits the warning instruction to the cabin alarm module 5. The cabin alarm module 5 is used to generate a warning code according to the warning level of the warning instruction, and the cabin alarm module 5 transmits the warning code to the body lighting component 7 and the wireless communication module 6. The body lighting component 7 is used to control different warning light flashes according to the warning code. The wireless communication module 6 is used to send the warning code to the command and control terminal 9. The flight data acquisition module collects real-time flight data, and the flight data analysis module compares the real-time flight data with the normal flight data to obtain abnormal flight data. The early warning instruction generation module generates specific early warning instructions for abnormal flight data according to the pre-set early warning level. The cabin alarm module generates early warning codes according to the early warning instructions to control the body lighting components to produce different early warning light flashes. At the same time, the wireless communication module sends the early warning code to the command and control end, so that the staff who pick up the plane on the ground can know that the aircraft has a malfunction based on the flashing early warning lights, and the command and control end can know the aircraft malfunction based on the early warning code, so that people in other fields will not panic when they learn about the aircraft malfunction.

[0026] like Figure 2 As shown, the flight data analysis module 3 includes a transmission module 31, an extraction module 32, an analysis module 33 and a warning information generation module 34. The transmission module 31 and the extraction module 32 are electrically connected and signal-connected with the storage module 8 through the control module 1, the transmission module 31 is electrically connected and signal-connected with the wireless communication module 6 through the control module 1, the extraction module 32 is electrically connected and signal-connected with the analysis module 33, and the analysis module 33 is electrically connected and signal-connected with the warning information generation module 34.

[0027] Among them, the storage module 8 is used to store comparison data, and the comparison data is normal flight data, and the flight data includes aircraft trajectory data, aircraft status data, environmental factor data, and accident data. The transmission module 31 is used to transmit the flight data to the storage module 8 through the control module 1 for storage, and the transmission module 31 is used to transmit the flight data to the wireless communication module 6 through the control module 1 and directly send it to the command and control end 9, so that the command and control end can understand the flight status of the aircraft at the first time, and analyze the potential problems of the aircraft through big data in a timely and effective manner based on the flight data. The extraction module 32 is used to retrieve the comparison data corresponding to the flight data from the storage module 8 through the control module 1, and the comparison data carries a pre-set data level. The extraction module 32 transmits the comparison data to the analysis module 33; the flight data analysis module uses a dual data transmission channel through the transmission module 31 and the extraction module 32 to realize the data transmission path between the storage module and the data transmission module, thereby increasing the data transmission speed. The analysis module 33 is used to analyze the comparison data to obtain its data level, and compare the flight data with the comparison data. The analysis module 33 transmits the abnormal flight data and the corresponding data level to the warning information generation module 34. The warning information generation module 34 is used to package the abnormal flight data according to the data level to generate warning information. The warning information carries the corresponding warning level. The warning information generation module embeds the preset warning level into the warning information to implement different warning processing operations according to the warning level.

[0028] like Figure 3 As shown, the warning instruction generation module 4 includes a parsing module 41 and an instruction synthesis module 42, and the parsing module 41 is electrically connected and signal-connected to the instruction synthesis module 42; wherein the parsing module 41 receives the warning information, obtains the warning level carried by the warning information through the warning information, generates the instruction level and transmits it to the instruction synthesis module 42; the instruction synthesis module 42 synthesizes the instruction level and the warning information into a warning instruction and transmits it to the cabin alarm module 5. The parsing module obtains the warning level, and the warning instruction generation module embeds the pre-set instruction level into the warning information according to the warning level, so that the cabin alarm module can perform different instruction operations according to the instruction level.

[0029] like Figure 3As shown, the cabin alarm module 5 includes an alarm instruction processing module 51 and a voice prompt module 52. The alarm instruction processing module 51 is electrically and signal-connected with the aircraft light assembly 7, the wireless communication module 6 and the voice prompt module 52 respectively; wherein, the alarm instruction processing module 51 controls the voice prompt module 52 according to the instruction level in the warning instruction, or randomly generates a warning code and transmits the warning code to the aircraft light assembly 7 and the wireless communication module 6. According to the instruction level, the alarm instruction processing module can let the pilot know the flight warning of a low instruction level through the voice prompt module, and let the flight warning of a high level generate different warning lights through the aircraft light assembly to let the ground staff see it and take timely measures.

[0030] It should be noted that the above invention content and specific implementation methods are intended to demonstrate the practical application of the technical solution provided by the present invention and should not be interpreted as limiting the scope of protection of the present invention. Those skilled in the art can make various modifications, equivalent substitutions or improvements within the spirit and principles of the present invention. The scope of protection of the present invention shall be subject to the attached claims.

Claims

1. A road navigation flight emergency alarm system, characterized in that: It comprises a control module (1), a flight data collection module (2), a flight data analysis module (3), a warning instruction generation module (4), an in-cabin alarm module (5), a wireless communication module (6), a body lighting component (7) and a storage module (8); wherein: The control module (1) is electrically connected and signal-connected to the flight data acquisition module (2), the flight data analysis module (3), the cabin alarm module (5), the wireless communication module (6) and the storage module (8), respectively; the flight data acquisition module (2) is electrically connected and signal-connected to the flight data analysis module (3), the flight data analysis module (3) is electrically connected and signal-connected to the warning instruction generation module (4), the warning instruction generation module (4) is electrically connected and signal-connected to the cabin alarm module (5), and the cabin alarm module (5) is electrically connected and signal-connected to the wireless communication module (6) and the aircraft body light assembly (7); The flight data collection module (2) collects flight data and transmits the flight data to the flight data analysis module (3); The flight data analysis module (3) analyzes the received flight data, packages the abnormal flight data to generate warning information, and transmits the warning information to the warning instruction generation module (4); the flight data analysis module (3) comprises a transmission module (31), an extraction module (32), an analysis module (33) and a warning information generation module (34); the transmission module (31) and the extraction module (32) are electrically connected and signal-connected to the storage module (8) through the control module (1); the extraction module (32) and the analysis module (33) are electrically connected and signal-connected to the analysis module (33); and the analysis module (33) and the warning information generation module (34) are electrically connected and signal-connected; the transmission module (31) is electrically connected and signal-connected to the wireless communication module (6) through the control module (1); The storage module (8) stores comparison data, the comparison data being normal flight data, the flight data including aircraft trajectory data, aircraft status data, environmental factor data, and accident data; The transmission module (31) transmits the flight data to the storage module (8) through the control module (1) for storage, and the transmission module (31) transmits the flight data to the wireless communication module (6) through the control module (1) and directly sends it to the command and control terminal (9); at the same time, the extraction module (32) retrieves the comparison data corresponding to the flight data from the storage module (8) through the control module (1), the comparison data carrying a preset data level, and the extraction module (32) transmits the comparison data to the analysis module (33); The analysis module (33) analyzes the comparison data to obtain its data level, compares the flight data with the comparison data, and transmits the abnormal flight data and the corresponding data level to the warning information generation module (34); The warning information generation module (34) packages the abnormal flight data according to the data level to generate warning information, wherein the warning information carries the corresponding warning level; The warning instruction generation module (4) determines the warning level according to the warning information and generates a warning instruction, and transmits the warning instruction to the cabin alarm module (5); The cabin alarm module (5) generates a warning code according to the warning level of the warning instruction, and transmits the warning code to the aircraft lighting component (7) and the wireless communication module (6); The body lighting component (7) generates different warning light flashes according to the warning code control; The wireless communication module (6) sends the warning code to the command and control terminal (9).

2. The navigation flight emergency alarm system according to claim 1, characterized in that: The warning instruction generation module (4) comprises a parsing module (41) and an instruction synthesis module (42), wherein the parsing module (41) is electrically connected to the instruction synthesis module (42) and signal-connected to the instruction synthesis module (42); wherein the parsing module (41) receives warning information, obtains the warning level carried by the warning information through the warning information, generates an instruction level and transmits it to the instruction synthesis module (42); the instruction synthesis module (42) synthesizes the instruction level and the warning information into a warning instruction and transmits it to the cabin alarm module (5).

3. The navigation flight emergency alarm system according to claim 2, characterized in that: The cabin alarm module (5) comprises an alarm instruction processing module (51) and a voice prompt module (52), wherein the alarm instruction processing module (51) is electrically connected and signal-connected to the aircraft light assembly (7), the wireless communication module (6) and the voice prompt module (52), respectively; wherein the alarm instruction processing module (51) controls the voice prompt module (52) according to the instruction level in the warning instruction, or randomly generates a warning code, and transmits the warning code to the aircraft light assembly (7) and the wireless communication module (6).

4. The navigation flight emergency alarm system according to claim 1, characterized in that: At least two flight data collection modules (2) are provided, and each flight data collection module (2) is electrically connected and signal-connected to the clock module; The clock module sends a clock pulse to the flight data collection module (2), so that the flight data collection module (2) collects flight data at a certain frequency, and the plurality of flight data collection modules (2) collect flight data at different frequencies.

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