CN202869495U - Safe operation management auxiliary system for aircraft communication location and navigation used for general aviation field - Google Patents
Safe operation management auxiliary system for aircraft communication location and navigation used for general aviation field Download PDFInfo
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- CN202869495U CN202869495U CN 201220579448 CN201220579448U CN202869495U CN 202869495 U CN202869495 U CN 202869495U CN 201220579448 CN201220579448 CN 201220579448 CN 201220579448 U CN201220579448 U CN 201220579448U CN 202869495 U CN202869495 U CN 202869495U
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Abstract
The utility model discloses a safe operation management auxiliary system for aircraft communication location and navigation used for a general aviation field, belonging to navigation equipment applied to the general aviation field. The auxiliary navigation system comprises a central processor (1), a positioning module (3), a gesture measuring module (4), an aircraft data input interface (5), a display touch control module (2), a communication interface (6) and a video and voice module (7), wherein the positioning module (3), the gesture measuring module (4) and the aircraft data input interface (5) are connected with a data input end of the central processor; the display touch control module (2), the communication interface (6) and the video and voice module (7) are connected with a dual-direction data transmission end of the central processor (1). The safety operation management auxiliary system disclosed by the utility model is applicable to general aviation operating aircrafts, and can be used for relieving the workload of a pilot, improving the working efficiency of the aircraft and strengthening safe flight guarantees, so that the command center can know the specific location information, the course and the height of the operating aircrafts within the range of the command center at any time, thereby solving the difficult problem that the locations of the general aviation operation aircrafts cannot be grasped due to limited wireless communication.
Description
Technical field
The Wing Newsletter location navigation safe operation management backup system that is used for the navigation field belongs to the navigator that is applied in the General Aviation field.
Background technology
Often drive aviation operation aircraft, can make driver's working strength very big, and complicated data manipulation has increased driver's working load, in order to alleviate driver's work load, improve aircraft operation efficient, strengthen the safe flight guarantee, need command centre can understand at any time jurisdiction operation aircraft more specific location information, coursespeed, the information such as height need that solution exists at present always because the difficult problem that the limited navigation operation aircraft position that causes of wireless communication can't be grasped.
The utility model content
In order to address the above problem, the utility model discloses the Wing Newsletter location navigation safe operation management backup system for the navigation field, this system is applicable to General Aviation operation aircraft, can alleviate driver workload, improve aircraft operation efficient, strengthen the safe flight guarantee, make command centre can understand at any time jurisdiction operation aircraft more specific location information, coursespeed, the information such as height, solved exist at present always because the difficult problem that the wireless communication limited navigation operation aircraft position that causes can't be grasped.
The purpose of this utility model is achieved in that
Be used for the Wing Newsletter location navigation safe operation management backup system in navigation field, comprise central processing unit, connect locating module, attitude measurement module, the airplane data input interface of central processing unit data input pin; The demonstration touch-control module, communication interface and the video voice module that connect central processing unit bidirectional data transfers end.
Above-mentioned Wing Newsletter location navigation safe operation management backup system for the navigation field, described demonstration touch-control module comprises display screen and touch-screen, and touch-screen is configured in the display screen upper surface; Wherein, display screen is LCDs.
Above-mentioned Wing Newsletter location navigation safe operation management backup system for the navigation field, described demonstration touch-control module is 4.3 cun, 5 cun, 5.3 cun, 7 cun or 8 cun touch-screens, resolution is 800 * 480 or 960 * 540.
Above-mentioned Wing Newsletter location navigation safe operation management backup system for the navigation field, described locating module is the Big Dipper/GPS bimodulus locating module.
Above-mentioned Wing Newsletter location navigation safe operation management backup system for the navigation field, described attitude measurement module comprises three axis accelerometer, three-axis gyroscope and three axle magnetoresistive transducers.
Above-mentioned Wing Newsletter location navigation safe operation management backup system for the navigation field, described airplane data input interface matches with existing device on the aircraft, and described airplane data input interface is USB interface, PS/2 interface, SATA interface, 1394 interfaces, RS-232 interface or RS-485 interface.
Above-mentioned Wing Newsletter location navigation safe operation management backup system for the navigation field, described communication interface comprises wireless signal transmitter and wireless signal receiver.
Above-mentioned Wing Newsletter location navigation safe operation management backup system for the navigation field, described video voice module comprise and show display screen that touch-control module shares and personal loudspeaker.
Because the utility model is used for the Wing Newsletter location navigation safe operation management backup system in navigation field, comprise central processing unit, and the demonstration touch-control module that is connected with central processing unit, locating module, attitude measurement module, airplane data input interface, communication interface and video voice module; This design is so that this assisting navigation equipment is applicable to General Aviation operation aircraft, can alleviate driver workload, improve aircraft operation efficient, strengthen the safe flight guarantee, make command centre can understand at any time jurisdiction operation aircraft more specific location information, coursespeed, the information such as height, solved exist at present always because the difficult problem that the wireless communication limited navigation operation aircraft position that causes can't be grasped.
Description of drawings
Fig. 1 is the utility model safe operation management circuit of auxiliary system connection diagram.
Among the figure: 1 central processing unit, 2 shows touch-control module, 3 locating modules, 4 attitude measurement modules, 41 three axis accelerometers, 42 three-axis gyroscopes, 43 3 axle magnetoresistive transducers, 5 airplane data input interfaces, 6 communication interfaces, 7 video voice modules.
Embodiment
Below in conjunction with accompanying drawing the utility model embodiment is described in further detail.
The Wing Newsletter location navigation safe operation management backup system that is used for the navigation field of present embodiment, the circuit connection diagram of this safe operation management backup system as shown in Figure 1, this safe operation management backup system comprises central processing unit 1, connects locating module 3, attitude measurement module 4, the airplane data input interface 5 of central processing unit 1 data input pin; The demonstration touch-control module 2, communication interface 6 and the video voice module 7 that connect central processing unit 1 bidirectional data transfers end.
Described demonstration touch-control module 2 comprises display screen and touch-screen, and touch-screen is configured in the display screen upper surface; Wherein, show that it is 800 * 480 demonstration touch screen that touch-control module 2 is preferably 8 cun resolution, can also select other size, such as 4.3 cun, 5 cun, 5.3 cun, 7 cun or 8 cun, and other resolution, such as 960 * 540.
Described locating module 3 is preferably the Big Dipper/GPS bimodulus locating module, can also select locating module of the Big Dipper.
Described attitude measurement module 4 comprises three axis accelerometer 41, three-axis gyroscope 42 and three axle magnetoresistive transducers 43.And the quantity of three axis accelerometer 41 is no less than two, and the quantity of three-axis gyroscope 42 is no less than two, and the quantity of three axle magnetoresistive transducers 43 is no less than two, has only drawn one of them in accompanying drawing 1.
Described airplane data input interface 5 matches with existing device on the aircraft, and described airplane data input interface 5 is preferably USB interface; This interface can also be chosen as PS/2 interface, SATA interface, 1394 interfaces, RS-232 interface or RS-485 interface.
Described communication interface 6 comprises wireless signal transmitter and wireless signal receiver.
Described video voice module 7 comprises and shows display screen that touch-control module 2 shares and personal loudspeaker.
The utility model safe operation management backup system is applied to the General Aviation field, can alleviate driver workload, improve aircraft operation efficient, strengthen the safe flight guarantee, make command centre can understand at any time jurisdiction operation aircraft more specific location information, coursespeed, the information such as height, solved exist at present always because the difficult problem that the wireless communication limited navigation operation aircraft position that causes can't be grasped.
Claims (8)
1. the Wing Newsletter location navigation safe operation management backup system that is used for the navigation field, it is characterized in that comprising central processing unit (1), connect locating module (3), attitude measurement module (4), the airplane data input interface (5) of central processing unit (1) data input pin; The demonstration touch-control module (2), communication interface (6) and the video voice module (7) that connect central processing unit (1) bidirectional data transfers end.
2. the Wing Newsletter location navigation safe operation management backup system for the navigation field according to claim 1 it is characterized in that described demonstration touch-control module (2) comprises display screen and touch-screen, and touch-screen is configured in the display screen upper surface; Wherein, display screen is LCDs.
3. backup system is managed in the Wing Newsletter location navigation safe operation for the navigation field according to claim 2, it is characterized in that described demonstration touch-control module is 4.3 cun, 5 cun, 5.3 cun, 7 cun or 8 cun touch-screens, resolution is 800 * 480 or 960 * 540.
4. the Wing Newsletter location navigation safe operation management backup system for the navigation field according to claim 1 is characterized in that described locating module (3) is the Big Dipper/GPS bimodulus locating module.
5. the Wing Newsletter location navigation safe operation management backup system for the navigation field according to claim 1 is characterized in that described attitude measurement module (4) comprises three axis accelerometer (41), three-axis gyroscope (42) and three axle magnetoresistive transducers (43).
6. backup system is managed in the Wing Newsletter location navigation safe operation for the navigation field according to claim 1, it is characterized in that described airplane data input interface (5) matches with existing device on the aircraft, described airplane data input interface (5) is USB interface, PS/2 interface, SATA interface, 1394 interfaces, RS-232 interface or RS-485 interface.
7. the Wing Newsletter location navigation safe operation management backup system for the navigation field according to claim 1 is characterized in that described communication interface (6) comprises wireless signal transmitter and wireless signal receiver.
8. the Wing Newsletter location navigation safe operation management backup system for the navigation field according to claim 1 is characterized in that described video voice module (7) comprises and shows display screen that touch-control module (2) shares and personal loudspeaker.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 201220579448 CN202869495U (en) | 2012-11-06 | 2012-11-06 | Safe operation management auxiliary system for aircraft communication location and navigation used for general aviation field |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 201220579448 CN202869495U (en) | 2012-11-06 | 2012-11-06 | Safe operation management auxiliary system for aircraft communication location and navigation used for general aviation field |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN202869495U true CN202869495U (en) | 2013-04-10 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN 201220579448 Expired - Fee Related CN202869495U (en) | 2012-11-06 | 2012-11-06 | Safe operation management auxiliary system for aircraft communication location and navigation used for general aviation field |
Country Status (1)
| Country | Link |
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| CN (1) | CN202869495U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102914305A (en) * | 2012-11-06 | 2013-02-06 | 哈尔滨盈盛翔科技开发有限公司 | Aircraft communication, positioning and navigation safety operation management auxiliary system for general aviation field |
-
2012
- 2012-11-06 CN CN 201220579448 patent/CN202869495U/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102914305A (en) * | 2012-11-06 | 2013-02-06 | 哈尔滨盈盛翔科技开发有限公司 | Aircraft communication, positioning and navigation safety operation management auxiliary system for general aviation field |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| 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: 20130410 Termination date: 20141106 |
|
| EXPY | Termination of patent right or utility model |