CN208044872U - A kind of General Aviation airborne surveillance system - Google Patents

A kind of General Aviation airborne surveillance system Download PDF

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Publication number
CN208044872U
CN208044872U CN201820371021.8U CN201820371021U CN208044872U CN 208044872 U CN208044872 U CN 208044872U CN 201820371021 U CN201820371021 U CN 201820371021U CN 208044872 U CN208044872 U CN 208044872U
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CN
China
Prior art keywords
way electric
electric connection
wireless data
transceiving device
general aviation
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Expired - Fee Related
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CN201820371021.8U
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Chinese (zh)
Inventor
叶玉妹
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Zhengzhou Dongli Optical Mechanical And Electrical Technology Co ltd
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Individual
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Priority to CN201820371021.8U priority Critical patent/CN208044872U/en
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Expired - Fee Related legal-status Critical Current
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Abstract

The utility model discloses a kind of General Aviation airborne surveillance systems, including central processing unit and wireless data transceiving device, the central processing unit and the two-way electric connection of wireless data transceiving device, the central processing unit and the two-way electric connection of notice to airmen service terminal, the wireless data transceiving device and the two-way electric connection of onboard services terminal, the wireless data transceiving device and the two-way electric connection of Scout and survey on-board terminal, the wireless data transceiving device and the two-way electric connection of Beidou II, the wireless data transceiving device and the two-way electric connections of GPS, the wireless data transceiving device and the two-way electric connection of iridium satellite, the wireless data transceiving device and the two-way electric connection of ground receiving wastewater facility.The utility model obtains information in several ways, ensure that the accuracy of monitoring data, and information can not be obtained in several ways by solving existing monitoring system, thus the problem of can not ensureing to monitor the accuracy of data.

Description

A kind of General Aviation airborne surveillance system
Technical field
The utility model is related to technical field of aerospace more particularly to a kind of General Aviation airborne surveillance systems.
Background technology
General Aviation refers to being engaged in Civil Aviation Activities other than public air transport using civil aircraft, including be engaged in Industry, agricultural, forestry, fishery and the operation flight of construction industry and health care, rescue and relief work, meteorological detection, marine monitoring, The flying activity of scientific experiment, education and training, culture and sports etc..Continuous development with China's navigation industry and country The continuous release of the low latitude open policy, low by the end of 2013, China shares 1623 frame of all purpose aircraft, it is contemplated that the end of the year 2014 reached To 1800 framves, reach 5000 framves to the year two thousand twenty.Due to all purpose aircraft have it is small, type of aircraft is more, operation height is low, Based on visual flight, cheap, airborne equipment is simple, flight the features such as arbitrariness is also big, be easy to cause flight be difficult to monitor, The safety problems such as national air defense and air-defence critical area.A kind of General Aviation is proposed in Chinese utility model patent CN107038900A Low-altitude surveillance and service system, the utility model can not obtain information in several ways, to ensure to monitor data Accuracy, for this purpose, it is proposed that a kind of General Aviation airborne surveillance system.
Utility model content
Technical problems based on background technology, the utility model proposes a kind of General Aviation airborne surveillance system, The characteristics of obtaining information with various ways, ensureing monitoring data accuracy, solving existing monitoring system can not be by a variety of Mode obtains information, thus the problem of can not ensureing to monitor the accuracy of data.
The utility model provides the following technical solutions:A kind of General Aviation airborne surveillance system, including central processing unit and Wireless data transceiving device, the central processing unit and the two-way electric connection of wireless data transceiving device, the central processing unit With the two-way electric connection of notice to airmen service terminal, the wireless data transceiving device with onboard services terminal is two-way electrically connects It connects, the wireless data transceiving device and the two-way electric connection of Scout and survey on-board terminal, the wireless data transceiving device and the Big Dipper The two-way electric connection of two generations, the wireless data transceiving device and the two-way electric connections of GPS, the wireless data transceiving device with The two-way electric connection of iridium satellite, the wireless data transceiving device and the two-way electric connection of ground receiving wastewater facility, the ground receiver The output end of device draws with data to be connect the input terminal of processing gateway and is unidirectionally electrically connected, and the data draw the output for connecing processing gateway The input terminal with vacant lot system navigation aircraft surveillance database is held unidirectionally to be electrically connected, the central processing unit is supervised with low latitude synthesis The two-way electric connection of viewing system, the central processing unit and the two-way electric connection of General Aviation Flight service system.
Preferably, the General Aviation Flight service system includes General Aviation Flight meteorology processing center, General Aviation Flight Plan Processing Center and General Aviation Flight information handling center.
Preferably, the input terminal of the central processing unit and the output end of pressure altimeter are unidirectionally electrically connected, the gas Press altimeter using one kind in BA5803, BT5611 and BP5607.
Preferably, the input terminal of the central processing unit and the output end of battery are unidirectionally electrically connected, the electricity of the battery Pressure is 5V, electric current 2A.
Preferably, the low latitude comprehensive monitoring system includes low clearance area watchdog subsystem and wide area multiple spot monitoring subsystem System.
Preferably, the ground receiving wastewater facility includes ADS-B ground receivers and GAMS ground receivers, and the data are drawn It includes that ADS-B data draw and connect processing gateway and GAMS data draw and connect processing gateway to connect processing gateway.
The utility model provides a kind of General Aviation airborne surveillance system, is monitored by Beidou II, due to north In two generations of struggling against, belong to global positioning satellite communication system, and using Big Dipper short message correspondence with foreign country means, world flight model may be implemented Interior monitoring, while the monitoring means of integrated ADS-B and GAMS are enclosed, the ADS-B airplane information numbers of transmitting 1090Mhz can be received According to monitoring the airplane information in the certain distance centered on the system, air surveillance ability formed, by being provided with iridium Star, iridium satellite mobile communication system are a kind of global satellite mobile communication systems, by using satellite hand telephone set, through defending Star can on earth from anywhere in transfer to and receive telephone signal, achieve the purpose that global surveillance, obtain in several ways Information ensure that the accuracy of monitoring data.
Description of the drawings
Fig. 1 is Tthe utility model system schematic diagram.
Specific implementation mode
The following will be combined with the drawings in the embodiments of the present invention, carries out the technical scheme in the embodiment of the utility model Clearly and completely describe, it is clear that the described embodiments are only a part of the embodiments of the utility model, rather than whole Embodiment.Based on the embodiments of the present invention, those of ordinary skill in the art are without making creative work The every other embodiment obtained, shall fall within the protection scope of the present invention.
Referring to Fig. 1, the utility model provides a kind of technical solution:A kind of General Aviation airborne surveillance system, including in Central processor and wireless data transceiving device, central processing unit and the two-way electric connection of wireless data transceiving device, central processing Device and the two-way electric connection of notice to airmen service terminal, wireless data transceiving device and the two-way electric connection of onboard services terminal, Wireless data transceiving device and the two-way electric connection of Scout and survey on-board terminal, wireless data transceiving device are two-way electrically with Beidou II Connection, wireless data transceiving device and the two-way electric connections of GPS, wireless data transceiving device and the two-way electric connection of iridium satellite, nothing Line data transmitter-receiver set and the two-way electric connection of ground receiving wastewater facility, output end and the data of ground receiving wastewater facility, which are drawn, connects processing net The input terminal of pass is unidirectionally electrically connected, and data draw the output end and vacant lot system navigation aircraft surveillance database for connecing processing gateway Input terminal is unidirectionally electrically connected, central processing unit and the two-way electric connection of low latitude comprehensive monitoring system, central processing unit with it is general The two-way electric connection of aviation flight service system, General Aviation Flight service system include in the processing of General Aviation Flight meteorology The heart, General Aviation Flight plan processing center and General Aviation Flight information handling center, the input terminal and gas of central processing unit The output end of pressure altimeter is unidirectionally electrically connected, and pressure altimeter uses one kind in BA5803, BT5611 and BP5607, center The input terminal of processor and the output end of battery are unidirectionally electrically connected, and the voltage of battery is 5V, electric current 2A, low latitude integrated supervision System includes low clearance area watchdog subsystem and wide area multiple spot watchdog subsystem, and ground receiving wastewater facility includes ADS-B ground receivers Machine and GAMS ground receivers, data draw that connect processing gateway include that ADS-B data draw and connect processing gateway and GAMS data draw and meet place Manage gateway.
It in the utility model, is monitored by Beidou II, since Beidou II belongs to global positioning satellite communication system The monitoring within the scope of world flight may be implemented using Big Dipper short message correspondence with foreign country means in system, at the same integrated ADS-B and The monitoring means of GAMS can receive the ADS-B airplane information data of transmitting 1090Mhz, monitor centered on the system Airplane information in certain distance forms air surveillance ability, and by being provided with iridium satellite, iridium satellite mobile communication system is a kind of complete Ball satellite mobile communication system, by using satellite hand telephone set, through satellite can on earth from anywhere in transfer to With reception telephone signal, achieve the purpose that global surveillance, obtain information in several ways, ensure that the accurate of monitoring data Property.
The preferable specific implementation mode of the above, only the utility model, but the scope of protection of the utility model is not Be confined to this, any one skilled in the art within the technical scope disclosed by the utility model, according to this practicality Novel technical solution and its utility model design are subject to equivalent substitution or change, should all cover the protection model in the utility model Within enclosing.

Claims (6)

1. a kind of General Aviation airborne surveillance system, including central processing unit and wireless data transceiving device, it is characterised in that:Institute Central processing unit and the two-way electric connection of wireless data transceiving device are stated, the central processing unit is double with notice to airmen service terminal Electrotropism connects, the wireless data transceiving device and the two-way electric connection of onboard services terminal, the wireless data transceiving dress Set with the two-way electric connection of Scout and survey on-board terminal, the wireless data transceiving device and the two-way electric connection of Beidou II are described Wireless data transceiving device and the two-way electric connections of GPS, the wireless data transceiving device and the two-way electric connection of iridium satellite, it is described Wireless data transceiving device and the two-way electric connection of ground receiving wastewater facility, the output end of the ground receiving wastewater facility draws with data to be connect The input terminal of processing gateway is unidirectionally electrically connected, and the data draw the output end and vacant lot system navigation aircraft prison for connecing processing gateway Input terminal depending on database is unidirectionally electrically connected, the central processing unit and the two-way electric connection of low latitude comprehensive monitoring system, institute State central processing unit and the two-way electric connection of General Aviation Flight service system.
2. a kind of General Aviation airborne surveillance system according to claim 1, it is characterised in that:The General Aviation Flight Service system includes General Aviation Flight meteorology processing center, General Aviation Flight plan processing center and General Aviation Flight feelings Report processing center.
3. a kind of General Aviation airborne surveillance system according to claim 1, it is characterised in that:The central processing unit The output end of input terminal and pressure altimeter is unidirectionally electrically connected, the pressure altimeter using BA5803, BT5611 and One kind in BP5607.
4. a kind of General Aviation airborne surveillance system according to claim 1, it is characterised in that:The central processing unit The output end of input terminal and battery is unidirectionally electrically connected, and the voltage of the battery is 5V, electric current 2A.
5. a kind of General Aviation airborne surveillance system according to claim 1, it is characterised in that:The low latitude integrated supervision System includes low clearance area watchdog subsystem and wide area multiple spot watchdog subsystem.
6. a kind of General Aviation airborne surveillance system according to claim 1, it is characterised in that:The ground receiving wastewater facility Including ADS-B ground receivers and GAMS ground receivers, the data draw that connect processing gateway include that ADS-B data draw and connect processing Gateway and GAMS data, which are drawn, connects processing gateway.
CN201820371021.8U 2018-03-19 2018-03-19 A kind of General Aviation airborne surveillance system Expired - Fee Related CN208044872U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201820371021.8U CN208044872U (en) 2018-03-19 2018-03-19 A kind of General Aviation airborne surveillance system

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201820371021.8U CN208044872U (en) 2018-03-19 2018-03-19 A kind of General Aviation airborne surveillance system

Publications (1)

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CN208044872U true CN208044872U (en) 2018-11-02

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Country Status (1)

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CN (1) CN208044872U (en)

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Date Code Title Description
GR01 Patent grant
GR01 Patent grant
TR01 Transfer of patent right
TR01 Transfer of patent right

Effective date of registration: 20190514

Address after: 450001 No. 11 Changchun Road, Zhengzhou High-tech Zone, Henan Province, 13 buildings, 2 units, 11 floors, 102, 103

Patentee after: Zhengzhou Dongli Optical Mechanical and Electrical Technology Co.,Ltd.

Address before: 323699 Huang Jia 10, Tian Yang village, tight water beach town, Yunhe County, Lishui, Zhejiang

Patentee before: Ye Yumei

CF01 Termination of patent right due to non-payment of annual fee
CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20181102