CN202795061U - Rotor unmanned aircraft ground station - Google Patents
Rotor unmanned aircraft ground station Download PDFInfo
- Publication number
- CN202795061U CN202795061U CN 201220395866 CN201220395866U CN202795061U CN 202795061 U CN202795061 U CN 202795061U CN 201220395866 CN201220395866 CN 201220395866 CN 201220395866 U CN201220395866 U CN 201220395866U CN 202795061 U CN202795061 U CN 202795061U
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- CN
- China
- Prior art keywords
- display module
- unmanned aircraft
- rotor unmanned
- top cover
- electric supply
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Fee Related
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Abstract
The utility model discloses a control device of a rotor aircraft, especially relates to a rotor unmanned aircraft ground station comprising a case body. A main controller, a first power supply device, a second power supply device, voltage stabilization modules, a TV display module, and a video wireless receiving module are disposed in the case body. The first power supply device is electrically connected with the main controller, and the second power supply device can be used to supply power to the TV display module and the video wireless receiving module. The connection line between the second power supply device and the TV display module and the connection line between the second power supply device and the video wireless receiving module are provided with the voltage stabilization modules. A main line of the second power supply device is provided with a voltage display module. The TV display module and the video wireless receiving module are connected together by a video line and an audio line. The video wireless receiving module is connected with a nixie tube display module. The rotor unmanned aircraft ground station has advantages of portability, intelligible image display, functional diversity, and simple control.
Description
Technical field
The utility model relates to a kind of rotor craft control device, particularly relates to rotor unmanned aircraft land station.
Background technology
Rotor wing unmanned aerial vehicle when the operation of outfield, be placed on the desk by various communication apparatus or frame at tripod or lie in ground and control and finish, this mode can affect operating personnel to the accurate operation of machine, maloperation appears easily, and control gear is directly perceived not for the effector, can't accomplish precision, long working can produce fatigue to the people, has a strong impact on handling safety, and device carries inconvenience.
The utility model content
Rotor unmanned aircraft of the present utility model land station has overcome the deficiency that prior art exists, and provides a kind of when making rotor wing unmanned aerial vehicle go out operation, makes control device rotor unmanned aircraft land station easy to carry.
In order to solve the problems of the technologies described above, the technical solution adopted in the utility model is: rotor unmanned aircraft land station, comprise casing, be provided with master controller, the first electric supply installation, the second electric supply installation, Voltage stabilizing module, TV display module and video wireless receiving module in the described casing;
Described the first electric supply installation is electrically connected with described master controller;
Described the second electric supply installation is TV display module and the power supply of video wireless receiving module, circuit at described the second electric supply installation and described TV display module and video wireless receiving module is provided with Voltage stabilizing module, is provided with voltage display module on the main line of described the second electric supply installation;
Described TV display module is connected with tone frequency channel wire by video line with described video wireless receiving module, and described video wireless receiving module is connected with the charactron display module.
Described casing comprises top cover and is positioned at the bottom of described top cover lower end, and a side of described top cover and described bottom is flexibly connected, described top cover be connected the bottom opposite side and connect by locking device, described top cover and described bottom form one and place cavity volume.
The outside of described casing is provided with handle.
Described casing is plastic box, is compounded with the covering composite bed in the inside of described casing.
Described the first electric supply installation and the second electric supply installation are lithium polymer battery, are arranged on the bottom.
Described voltage display module is voltage display, is arranged on the described top cover.
Described TV display module is display, is arranged on the described top cover, is provided with light shield around described display.
Be provided with gauge tap on the described bottom.
Also be provided with socket for subsequent use on the described top cover.
Compared with prior art the beneficial effects of the utility model are: owing to be provided with master controller, the first electric supply installation, the second electric supply installation, Voltage stabilizing module, TV display module and video wireless receiving module in casing, like this electronic display module and master controller are incorporated into one, integrated ground surface station with multichannel communication function has being convenient for carrying, schemes aobvious clear, diverse in function, the simple characteristics of control.
Description of drawings
Fig. 1 is the connection synoptic diagram of rotor unmanned aircraft land station in the utility model.
Fig. 2 is the structural representation of rotor unmanned aircraft land station in the utility model.
Fig. 3 is top cover inner structure synoptic diagram in the utility model.
Fig. 4 is bottom inner structure synoptic diagram in the utility model.
Embodiment
Below in conjunction with drawings and Examples, embodiment of the present utility model is described in further detail.Following examples are used for explanation the utility model, but are not used for limiting scope of the present utility model.
Referring to Fig. 1-Fig. 4, comprise casing 1, be provided with master controller 2 in the casing 1, the first electric supply installation 3, the second electric supply installation 4, Voltage stabilizing module 5, TV display module 6 and video wireless receiving module 7, the first electric supply installation 3 is electrically connected with master controller 1, the second electric supply installation 4 is TV display module 6 and 7 power supplies of video wireless receiving module, circuit at the second electric supply installation 4 and TV display module 6 and video wireless receiving module 7 is provided with Voltage stabilizing module 5, be provided with voltage display module 9 on the main line of the second electric supply installation 4, voltage display module 9 is voltage display 15, TV display module 6 is connected with tone frequency channel wire by video line with video wireless receiving module 7, TV display module 6 is display 14, video wireless receiving module 7 is connected with charactron display module 8, display 14 adopts high definition all-colour LED display, like this owing to adopt high definition all-colour LED display, the flat cooperation and foldable light shade 20, efficiently solve the at any time clear demonstration problem of section of ground image, voltage display 15 can be monitored 5v-30v voltage, can effectively show the current last voltage of this land station, but can effectively computable go out this land station operational use time also, master controller 2 adopts the 72M telechirics, use PCM1024 numerical coding mode, without blocking 1500 meters of effective controls, owing to adopt the PCM standard, can reduce significantly electronic interferences, the first electric supply installation 3 and the second electric supply installation 4 are large capacity lithium polymer battery 22, can effectively prolong land station's working time.
Casing 1 is plastic box, be compounded with the covering composite bed in the inside of casing 1, the outside of casing 1 is provided with handle 10, casing 1 comprises top cover 11 and is positioned at the bottom 12 of top cover 11 lower ends, one side of top cover 11 and bottom 12 is flexibly connected, top cover 11 is connected opposite side by locking device 13 connections with bottom, top cover 11 and bottom 12 form one and place cavity volume, be provided with display 14 on the top cover 11, voltage display 15, power light 16, channel selector 17, channel display 18 and socket for subsequent use 19, be provided with light shield 20 around the display 14, be provided with master controller 2 on the bottom 12, gauge tap 21 and battery 22, gauge tap 21 comprises power switch, video switch, communication switch and controller switches, like this owing to adopt plastic box 1, plastic box 1 has waterproof, dustproof, the characteristics such as shatter-resistant, be compounded with the covering composite bed in the inside of casing 1, has lightweight, high-intensity characteristic, placing cavity volume can all be incorporated into original in disorder thing in the chest, as long as open the various data of chest after arriving the outfield, the interface is very clear, can be quick, efficiently, safe carries out the work, and has to be convenient for carrying, diverse in function, control is simple, the sturdy characteristics such as durable.
The above only is preferred implementation of the present utility model; should be understood that; for those skilled in the art; under the prerequisite that does not break away from the utility model know-why; can also make some improvement and modification, these improve and modification also should be considered as protection domain of the present utility model.
Claims (9)
1. rotor unmanned aircraft land station comprises casing, it is characterized in that: be provided with master controller, the first electric supply installation, the second electric supply installation, Voltage stabilizing module, TV display module and video wireless receiving module in the described casing;
Described the first electric supply installation is electrically connected with described master controller;
Described the second electric supply installation is TV display module and the power supply of video wireless receiving module, circuit at described the second electric supply installation and described TV display module and video wireless receiving module is provided with Voltage stabilizing module, is provided with voltage display module on the main line of described the second electric supply installation;
Described TV display module is connected with tone frequency channel wire by video line with described video wireless receiving module, and described video wireless receiving module is connected with the charactron display module.
2. rotor unmanned aircraft as claimed in claim 1 land station, it is characterized in that: described casing comprises top cover and is positioned at the bottom of described top cover lower end, one side of described top cover and described bottom is flexibly connected, described top cover be connected the bottom opposite side and connect by locking device, described top cover and described bottom form one and place cavity volume.
3. rotor unmanned aircraft as claimed in claim 2 land station, it is characterized in that: the outside of described casing is provided with handle.
4. rotor unmanned aircraft as claimed in claim 3 land station, it is characterized in that: described casing is plastic box, is compounded with the covering composite bed in the inside of described casing.
5. rotor unmanned aircraft as claimed in claim 2 land station, it is characterized in that: described the first electric supply installation and the second electric supply installation are lithium polymer battery, are arranged on the bottom.
6. rotor unmanned aircraft as claimed in claim 2 land station, it is characterized in that: described voltage display module is voltage display, is arranged on the described top cover.
7. rotor unmanned aircraft as claimed in claim 2 land station, it is characterized in that: described TV display module is display, is arranged on the described top cover, is provided with light shield around described display.
8. rotor unmanned aircraft as claimed in claim 2 land station is characterized in that: be provided with gauge tap on the described bottom.
9. rotor unmanned aircraft as claimed in claim 2 land station is characterized in that: also be provided with socket for subsequent use on the described top cover.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 201220395866 CN202795061U (en) | 2012-08-11 | 2012-08-11 | Rotor unmanned aircraft ground station |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 201220395866 CN202795061U (en) | 2012-08-11 | 2012-08-11 | Rotor unmanned aircraft ground station |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN202795061U true CN202795061U (en) | 2013-03-13 |
Family
ID=47822296
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN 201220395866 Expired - Fee Related CN202795061U (en) | 2012-08-11 | 2012-08-11 | Rotor unmanned aircraft ground station |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN202795061U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103217983A (en) * | 2013-04-22 | 2013-07-24 | 北京航空航天大学 | Multi-rotor-wing multifunctional aerial robot remote control device |
| CN105404308A (en) * | 2015-11-24 | 2016-03-16 | 中国电子科技集团公司第二十七研究所 | Flight control unit for parafoil type unmanned plane |
-
2012
- 2012-08-11 CN CN 201220395866 patent/CN202795061U/en not_active Expired - Fee Related
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103217983A (en) * | 2013-04-22 | 2013-07-24 | 北京航空航天大学 | Multi-rotor-wing multifunctional aerial robot remote control device |
| CN105404308A (en) * | 2015-11-24 | 2016-03-16 | 中国电子科技集团公司第二十七研究所 | Flight control unit for parafoil type unmanned plane |
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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: 20130313 Termination date: 20160811 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |