CN204740745U - Airborne vehicle flight information acquisition dispensing device - Google Patents
Airborne vehicle flight information acquisition dispensing device Download PDFInfo
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- CN204740745U CN204740745U CN201520502897.8U CN201520502897U CN204740745U CN 204740745 U CN204740745 U CN 204740745U CN 201520502897 U CN201520502897 U CN 201520502897U CN 204740745 U CN204740745 U CN 204740745U
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- 238000004891 communication Methods 0.000 claims abstract description 13
- 238000000034 method Methods 0.000 claims description 9
- 238000012544 monitoring process Methods 0.000 description 4
- 238000005516 engineering process Methods 0.000 description 3
- 238000011835 investigation Methods 0.000 description 3
- 238000012549 training Methods 0.000 description 3
- 230000005540 biological transmission Effects 0.000 description 2
- 206010000369 Accident Diseases 0.000 description 1
- 230000002159 abnormal effect Effects 0.000 description 1
- 238000013480 data collection Methods 0.000 description 1
- 238000011161 development Methods 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
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- 238000010295 mobile communication Methods 0.000 description 1
- 238000007634 remodeling Methods 0.000 description 1
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Abstract
The utility model discloses an airborne vehicle flight information acquisition dispensing device, information collection handles sending module, power module including the location, power module does through power supply management chip location information collection handles the sending module power supply, location information collection handles sending module and includes main control unit, respectively with barometric height information acquisition device that main control unit connects, fly to join pick -up chip, cockpit information acquisition module, gyroscope gesture collector and wireless communication module. The utility model discloses an airborne vehicle flight information acquisition dispensing device can the simultaneous acquisition barometric height, flight geographic coordinates, flying speed, flight height, flight attitude information to send to the ground server through wireless communication module, each electron device is integrated to a circuit board in, takies smallly, especially is fit for the narrow and small small -size aircraft of inner space.
Description
Technical field
The utility model belongs to information acquiring technology field, specifically, relates to a kind of aircraft information acquisition dispensing device.
Background technology
Current all purpose aircraft runs mostly away from control airport, and by flying height and the flight operation area influence of topography, air traffic control service is difficult to utilize existing secondary radar to implement effective monitoring to its aircraft driver standardized operation.
There is solo flight course containing in training flight course in aviation school's training flight, during the button aircraft solo flight of flying cadet's independence, according to the rules whether flight reappearance, course fly, specifying that pilotinstructorpiston cannot control with or without observing flight safety.Existing ADS-B ground base station only has the effective monitoring scope of radius 180 kilometers, and monitoring range is limited, and base station deployment cost is high, and it is unrealistic that General Aviation enterprise independently disposes monitored base stations.
In addition, current aircraft supervision also causes certain supervision difficulty because civil aviaton's flight runs supervisor's resource-constrained, be difficult to implement the supervision of comprehensive operation one line to the ruuning situation of all purpose aircraft away from the trans-regional operation in its main operation base, be difficult to investigate and prosecute and hit the illegal flight of General Aviation, be unfavorable for the sound development of China's aviation safety and domestic General Aviation industry.
And, specific requirement is done because civil aviaton's regulations are not equipped with black box to small-sized navigation aviation, domestic all purpose aircraft does not configure aircraft black box mostly, in addition generally there is aircraft accident away from business district is meagrely-populated once in enforcement flight operation in all purpose aircraft flight operation, and the side's of playing a game air-accident investigation is unfavorable.Meanwhile, the transmission of existing aircraft locating device be flying height under the standard pressure that records of satellite, the flying height that operation cannot be provided to fly under on-the-spot QFE to supervisor, Data Collection is incomplete.
Utility model content
The technical matters that the utility model is not easy to monitor to solve more existing training aircraft information, proposes a kind of aircraft information acquisition dispensing device, can solve the problem.
In order to solve the problems of the technologies described above, the utility model is achieved by the following technical solutions:
A kind of aircraft information acquisition dispensing device, comprise locating information and collect process sending module, power module, described power module is that described locating information collection process sending module is powered by power supply management chip, described locating information is collected process sending module and is comprised master controller, the barometer altitude information acquisition device be connected respectively, flies to join acquisition chip, driving cabin information acquisition module, gyroscope Posture acquisition device and wireless communication module with described master controller.
Further, described driving cabin information acquisition module comprises driving cabin image acquisition device.
Further, described driving cabin information acquisition module also comprises driving cabin sound collector.
Further, described wireless communication module is 4G data communication module.
Compared with prior art, advantage of the present utility model and good effect are: aircraft information acquisition dispensing device of the present utility model, barometer altitude, flight geographic coordinate, flying speed, flying height, flight attitude information can be gathered simultaneously, and be sent to ground-based server by wireless communication module, each electron device is integrated in one piece of circuit board, take volume little, be especially applicable to the narrow and small small aircraft in inner space.
After reading the detailed description of the utility model embodiment by reference to the accompanying drawings, other features of the present utility model and advantage will become clearly.
Accompanying drawing explanation
In order to be illustrated more clearly in the utility model embodiment or technical scheme of the prior art, be briefly described to the accompanying drawing used required in embodiment or description of the prior art below, apparently, accompanying drawing in the following describes is only embodiments more of the present utility model, for those of ordinary skill in the art, under the prerequisite not paying creative work, other accompanying drawing can also be obtained according to these accompanying drawings.
Fig. 1 is a kind of embodiment functional-block diagram of the aircraft information acquisition dispensing device that the utility model proposes.
Embodiment
Below in conjunction with the accompanying drawing in the utility model embodiment, be clearly and completely described the technical scheme in the utility model embodiment, obviously, described embodiment is only the utility model part embodiment, instead of whole embodiments.Based on the embodiment in the utility model, those of ordinary skill in the art are not making the every other embodiment obtained under creative work prerequisite, all belong to the scope of the utility model protection.
Embodiment one, the present embodiment proposes a kind of aircraft information acquisition dispensing device, as shown in Figure 1, comprise locating information and collect process sending module, power module, described power module is that described locating information collection process sending module is powered by power supply management chip, described locating information is collected process sending module and is comprised master controller, the barometer altitude information acquisition device be connected with described master controller respectively, fly to join acquisition chip, driving cabin information acquisition module, gyroscope Posture acquisition device and wireless communication module, wherein, barometer altitude information acquisition device is for gathering barometer altitude information, and be sent to master controller, driving cabin information acquisition module is for gathering the parameter information in driving cabin, and be sent to master controller, gyroscope Posture acquisition device is for gathering aircraft flight attitude information, and be sent to master controller.The aircraft information acquisition dispensing device of the present embodiment, barometer altitude can be gathered simultaneously, flight geographic coordinate, flying speed, flying height, flight attitude information, and be sent to ground-based server by wireless communication module, each electron device is integrated in one piece of circuit board, take volume little, especially the narrow and small small aircraft in inner space is applicable to, current small aircraft can be solved be not suitable for black box being installed and causing the problem that flight information cannot be grasped, this device can all flying qualities of complete documentation aircraft, once have an accident, help can be played to the investigation of accident.
Described master controller is also connected with storage chip, for storing the above-mentioned parameter data that master controller receives.
As a preferred embodiment, described driving cabin information acquisition module comprises driving cabin image acquisition device, for gathering the image information in driving cabin, whether meets working specification for monitoring driving person's operation.
In addition, preferred described driving cabin information acquisition module also comprises driving cabin sound collector, for recording the sound in driving cabin, comprising in the voice messaging of driver and driving cabin and occurring abnormal sound, being conducive to the investigation of later stage to fault.
Described wireless communication module is 4G data communication module, and master controller is sent to Land-Mobile-Network serving BS by mobile communications network after the data of each module acquires being packed, and is then forwarded to the server of Surveillance center, achieves real-time data transmission.
Certainly; above-mentioned explanation is not to restriction of the present utility model; the utility model is also not limited in above-mentioned citing, the change that those skilled in the art make in essential scope of the present utility model, remodeling, interpolation or replacement, also should belong to protection domain of the present utility model.
Claims (4)
1. an aircraft information acquisition dispensing device, it is characterized in that: comprise locating information and collect process sending module, power module, described power module is that described locating information collection process sending module is powered by power supply management chip, described locating information is collected process sending module and is comprised master controller, the barometer altitude information acquisition device be connected respectively, flies to join acquisition chip, driving cabin information acquisition module, gyroscope Posture acquisition device and wireless communication module with described master controller.
2. aircraft information acquisition dispensing device according to claim 1, is characterized in that: described driving cabin information acquisition module comprises driving cabin image acquisition device.
3. aircraft information acquisition dispensing device according to claim 1 and 2, is characterized in that: described driving cabin information acquisition module also comprises driving cabin sound collector.
4. aircraft information acquisition dispensing device according to claim 1 and 2, is characterized in that: described wireless communication module is 4G data communication module.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520502897.8U CN204740745U (en) | 2015-07-13 | 2015-07-13 | Airborne vehicle flight information acquisition dispensing device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520502897.8U CN204740745U (en) | 2015-07-13 | 2015-07-13 | Airborne vehicle flight information acquisition dispensing device |
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| Publication Number | Publication Date |
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| CN204740745U true CN204740745U (en) | 2015-11-04 |
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| CN201520502897.8U Expired - Fee Related CN204740745U (en) | 2015-07-13 | 2015-07-13 | Airborne vehicle flight information acquisition dispensing device |
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Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105513162A (en) * | 2015-12-01 | 2016-04-20 | 合肥飞友网络科技有限公司 | Intelligent terminal positioning-based airplane flight data system |
| CN107797566A (en) * | 2017-10-20 | 2018-03-13 | 莲花丝路科技有限公司 | A kind of ground controlled approach of unmanned plane |
| CN109413035A (en) * | 2018-09-11 | 2019-03-01 | 陕西千山航空电子有限责任公司 | A kind of winged ginseng wireless network adaptive device of miniaturization |
-
2015
- 2015-07-13 CN CN201520502897.8U patent/CN204740745U/en not_active Expired - Fee Related
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105513162A (en) * | 2015-12-01 | 2016-04-20 | 合肥飞友网络科技有限公司 | Intelligent terminal positioning-based airplane flight data system |
| CN107797566A (en) * | 2017-10-20 | 2018-03-13 | 莲花丝路科技有限公司 | A kind of ground controlled approach of unmanned plane |
| CN109413035A (en) * | 2018-09-11 | 2019-03-01 | 陕西千山航空电子有限责任公司 | A kind of winged ginseng wireless network adaptive device of miniaturization |
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Legal Events
| Date | Code | Title | Description |
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| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20151104 |
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| CF01 | Termination of patent right due to non-payment of annual fee |