CN206303427U - General Aviation regulatory service seat - Google Patents
General Aviation regulatory service seat Download PDFInfo
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- CN206303427U CN206303427U CN201620887679.5U CN201620887679U CN206303427U CN 206303427 U CN206303427 U CN 206303427U CN 201620887679 U CN201620887679 U CN 201620887679U CN 206303427 U CN206303427 U CN 206303427U
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- display
- general aviation
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- regulatory service
- table surface
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Abstract
The utility model provides a kind of General Aviation regulatory service seat, including seat support, seat support is provided with operating table surface, operating table surface upper end is provided with display, mouse, outside line, digital display clock and panel computer, operating table surface lower end is provided with Key board drawer, and Key board drawer is provided with keyboard；Operating table surface lower section is provided with main frame and Ethernet switch, and main frame is connected with display, mouse, keyboard and Ethernet switch respectively, and main frame is also connected with multiple external equipments.The utility model integrates regulatory service, information service and function of voice communication etc., the access of various external datas is provided, possess flight plan and flight information disposal ability, and stabilized structure, reasonable in design, easy for installation, cost are relatively low, the need for complying fully with the General Aviation development of China.
Description
Technical field
The utility model is related to air traffic control service technology field, and in particular to a kind of General Aviation regulatory service seat.
Background technology
At present, China, to the management mode of all purpose aircraft, is control and the pattern for servicing and depositing, and relies primarily on ground line
Reason department and personnel are managed.China low latitude domain support facility is perfect not to the utmost at this stage, and the management to General Aviation Flight is made
Into greatly limitation.All purpose aircraft flying height is low, and existing blank pipe means are difficult to monitor line trace in fact.Permitted in China
More regional, the phenomenon that the flight of generally existing low latitude domain cannot be monitored, " can't see, not join " outstanding problem has had a strong impact on state
Native air defense and flight safety, are monitoring and are controlling especially prominent.
It is that a kind of basic low latitude domain guarantee sets for the regulatory service seat in General Aviation regulatory service system
Apply.In the prior art, use the design of the developed countries such as America and Europe, not only complex structure, integrated design more at the regulatory service seat
High cost, and because the developed countries such as China and America and Europe are different to the management mode of all purpose aircraft, the prosperity such as America and Europe state
The management mode of family is based on servicing, therefore the regulatory service seat can not comply fully with the need of the General Aviation development of China
Will.
Utility model content
The utility model provides a kind of General Aviation regulatory service seat, with the regulatory service for solving to use in the prior art
Seat can not comply fully with the problem of China's General Aviation development need.
The utility model provides a kind of General Aviation regulatory service seat, including seat support, is set on the seat support
There is operating table surface, the operating table surface upper end is provided with display, mouse, outside line, digital display clock and panel computer, institute
State operating table surface lower end and be provided with Key board drawer, the Key board drawer is provided with keyboard；Operating table surface lower section be provided with main frame and
Ethernet switch, the main frame connects with the display, the mouse, the keyboard and the Ethernet switch respectively
Connect, the main frame is also connected with multiple external equipments.
Used as preferred embodiment of the present utility model, the operating table surface includes that a cross section is the arch platform of triangle
Face, and the front end level table and rear end level table being connected with the two ends of the arch table top.
Used as preferred embodiment of the present utility model, the outside line, digital display clock and panel computer are arranged on institute
State on arch table top, the display is arranged on the rear end level table, the mouse is arranged on the front end horizontal stand
On face.
Used as preferred embodiment of the present utility model, the display is supported by display bracket, the display bracket
Function with lifting and rotation.
Used as preferred embodiment of the present utility model, the operating desk lower section is provided with equipment compartment, and the equipment compartment can by one
The frame of closing and two computer support brackets in the frame are constituted；The main frame and the Ethernet switch are distinguished
In each self-corresponding equipment compartment.
The utility model provides a kind of General Aviation regulatory service seat, collection regulatory service, information service and voice communication
Function etc. is in one, there is provided the access of various external datas, possesses flight plan and flight information disposal ability, and take into full account
Various objective factors of controller, facilitate controller to use.The utility model stabilized structure, reasonable in design, easy for installation, cost
It is relatively low, the need for complying fully with the General Aviation development of China.
Brief description of the drawings
In order to illustrate more clearly of the technical scheme in the utility model embodiment, below will be to needed for embodiment description
The accompanying drawing to be used is briefly described, it should be apparent that, drawings in the following description are only some realities of the present utility model
Example is applied, for those of ordinary skill in the art, on the premise of not paying creative work, can also be according to these accompanying drawings
Obtain other accompanying drawings.
The front view structure figure at the General Aviation regulatory service seat that Fig. 1 is provided for the utility model embodiment；
The side block diagram at the General Aviation regulatory service seat that Fig. 2 is provided for the utility model embodiment；
The overlooking structure figure at the General Aviation regulatory service seat that Fig. 3 is provided for the utility model embodiment.
Wherein, 1, seat support, 2, arch table top, 3, front end level table, 4, rear end level table, 5, display, 6,
Display bracket, 7, mouse, 8, outside line, 9, digital display clock, 10, panel computer, 11, Key board drawer, 12, keyboard,
13rd, main frame, 14, Ethernet switch, 15, equipment compartment.
Specific embodiment
It is new to this practicality below in conjunction with accompanying drawing to make the purpose of this utility model, technical scheme and advantage clearer
Type implementation method is described in further detail.
The utility model embodiment discloses a kind of General Aviation regulatory service seat, is mainly used in General Aviation field
Management, possess air situation information monitoring, flight management, control zone flow dynamics monitoring, flight track control, flight plan pipe
The functions such as reason, all purpose aircraft information and data monitoring, are responsible for the flight dispatch of all purpose aircraft, it is ensured that all kinds of airborne vehicle peaces
Full flight.
The seat relate to global design according to《Civil aviation approach tower air traffic control set is configured》(MT/H 4005-
1997) standard,《Civil aviation Air Traffic Control Automation System》(MT/H 4029-2010) standard and《General Aviation Flight
Regulations》It is the General Aviation regulatory service seat for meeting China's actual conditions and existing use condition etc. the standard and specification that are related to
Position.
Shown in reference picture 1, Fig. 2 and Fig. 3, the seat includes seat support 1, and the seat support 1 is overall using shaped steel as frame
Frame structure, based on riveting.Seat support 1 is provided with operating table surface, and operating table surface upper end is provided with display 5, mouse 7, outside line electricity
Words 8, digital display clock 9 and panel computer 10.Operating table surface lower end be provided with can plug-type Key board drawer 11, on Key board drawer 11
Keyboard 12 is provided with, it is necessary to Key board drawer 11 be pulled out during using keyboard 12.Operating table surface lower section is provided with main frame 13 and ether
Network switch 14, wherein main frame 13 are connected with display 5, mouse 7, keyboard 12 and Ethernet switch 14 respectively, main frame 13
Also it is connected with multiple external equipments.
The various equipment being arranged in operating table surface are observed or used for convenience of controller, the centre of operating table surface
Position Design is into an arch.Specifically, the operating table surface includes that a cross section is the arch table top 2, Yi Jiyu of triangle
The front end level table 3 and rear end level table 4 of the two ends connection of arch table top 2.Wherein, outside line 8, digital display clock
9 and panel computer 10 be arranged on arch table top 2 towards the side of controller, display 5 is arranged on rear end level table 4,
Mouse 7 is arranged on front end level table 3.
This seat is equipped with an outside line 8, realize between each seat and with outside call；It is equipped with a number
Read clock 9, synchronous UTC time, the time synchronized and time showing of the other equipment for being set on seat；It is equipped with one 10
Inch touchscreen can be conversed panel computer 10, for realizing the functions such as flight plan application, inquiry and management, and can realize a key
Dialing and call function.
In the present embodiment, the seat can use for two controllers simultaneously, thus be equipped with two main frames, 13, two displays
5, two mouses 7 of device and two keyboards 12, the two main frames 13 are distinguished corresponding display 5, mouse 7 and keyboard 12 and are connected
Connect, be also connected with Ethernet switch 14 respectively, for realizing network connection.
The content such as various air situation information of display on display 5 is checked for convenience of controller, 30 inches of large-size screen monitors are employed
High resolution display.Simultaneously, it is contemplated that the objective factor such as controller's height, display 5 is by having the work(for lifting and rotating
The display bracket 6 of energy is supported, and is capable of achieving the rotation in direction up and down, meets multi-angle and the wide area viewing of display 5, is begun
An optimal comfortable viewing angle can be provided to controller eventually.Additionally, the display bracket 6 is also equipped with expanded function, according to
Need the installation of achievable single row or multiple rows display 5.
After the corresponding display 5 of main frame 13, mouse 7 and keyboard 12 are connected, that is, form the control used for controller
Member's work station.After main frame 13 is connected with multiple external equipments, it is possible to provide ADS-B, primary radar, secondary radar and Big Dipper RDSS
Etc. the access of the various external datas of multichannel, therefore whole controller's work station can provide electronic map data and show and control, ATC
Synthesis display and human-computer interaction interface, air situation data storage, time data synchronization, early warning and alerting service, data readback control
With the function such as display and audio playback control and display.Using controller's work station, controller can process radar and ADS-B
The monitoring data that equipment is brought, can be managed and control, and prevent to the overall process that Flight device flies to landing from
Only bump against between each aircraft and between aircraft and barrier, so as to safeguard air traffic order, improve the flight time and
The utilization rate in space.
Further, operating table surface lower section is provided with equipment compartment 15, and the equipment compartment 15 is by closed 19 inch rack
Two extension type computer support brackets composition with frame, can simultaneously meet the peace of upper frame type equipment and vertical equipment
Dress is put.In the present embodiment, equipment compartment 15 is provided with three, lay out in parallel, and two main frames 13 and an Ethernet switch 14 are just
It is respectively arranged in each self-corresponding equipment compartment 15.During work, equipment compartment 15 is closed, be effectively reduced main frame 13 and Ethernet is handed over
Change planes 14 operation when the noise that produces.
Whole General Aviation regulatory service seat tailored appearance, easy for installation, flexible configuration is easy to safeguard, using more
Extensively.Whole seat support and table top of feeling ashamed are installed, and other equipment accordingly installs restocking, i.e. operable after energization.
It is to be appreciated that mentioned in above-mentioned implementation method of the present utility model " on ", D score, "left", "right",
On the basis of the direction shown in each figure, these words for being used for limiting direction are intended merely to facilitate for " preceding " and " afterwards " etc.
It is bright, do not represent the limitation to the utility model concrete technical scheme.
Preferred embodiment of the present utility model is the foregoing is only, is not used to limit the utility model, it is all in this practicality
Within new spirit and principle, any modification, equivalent substitution and improvements made etc. should be included in guarantor of the present utility model
Within the scope of shield.
Claims (5)
1. a kind of General Aviation regulatory service seat, it is characterised in that including seat support, the seat support is provided with operation
Table top, the operating table surface upper end is provided with display, mouse, outside line, digital display clock and panel computer, the operation
Table top lower end is provided with Key board drawer, and the Key board drawer is provided with keyboard；The operating table surface lower section is provided with main frame and Ethernet
Interchanger, the main frame is connected with the display, the mouse, the keyboard and the Ethernet switch respectively, institute
Main frame is stated also to be connected with multiple external equipments.
2. General Aviation regulatory service seat according to claim 1, it is characterised in that the operating table surface includes
Cross section is the arch table top of triangle, and the front end level table that is connected with the two ends of the arch table top and rear end level
Table top.
3. General Aviation regulatory service seat according to claim 2, it is characterised in that the outside line, digital aobvious
Show that clock and panel computer are arranged on the arch table top, the display is arranged on the rear end level table, described
Mouse is arranged on the front end level table.
4. General Aviation regulatory service seat according to claim 1, it is characterised in that the display passes through display
Support is supported, and the display bracket has the function of lifting and rotation.
5. General Aviation regulatory service seat according to claim 1, it is characterised in that the operating desk lower section is provided with
Standby cabin, two computer support brackets of the equipment compartment by a closed frame and in the frame are constituted；The master
Machine and the Ethernet switch are respectively arranged in each self-corresponding equipment compartment.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620887679.5U CN206303427U (en) | 2016-08-16 | 2016-08-16 | General Aviation regulatory service seat |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620887679.5U CN206303427U (en) | 2016-08-16 | 2016-08-16 | General Aviation regulatory service seat |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206303427U true CN206303427U (en) | 2017-07-07 |
Family
ID=59241810
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201620887679.5U Active CN206303427U (en) | 2016-08-16 | 2016-08-16 | General Aviation regulatory service seat |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN206303427U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109375644A (en) * | 2018-10-29 | 2019-02-22 | 中国航空无线电电子研究所 | A kind of foldable manipulation seat towards portable integrated transport |
| CN110269413A (en) * | 2019-07-16 | 2019-09-24 | 照彰实业（东莞）有限公司 | Intelligent control tower |
-
2016
- 2016-08-16 CN CN201620887679.5U patent/CN206303427U/en active Active
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109375644A (en) * | 2018-10-29 | 2019-02-22 | 中国航空无线电电子研究所 | A kind of foldable manipulation seat towards portable integrated transport |
| CN110269413A (en) * | 2019-07-16 | 2019-09-24 | 照彰实业（东莞）有限公司 | Intelligent control tower |
| CN110269413B (en) * | 2019-07-16 | 2024-10-01 | 照彰实业（东莞）有限公司 | Intelligent tower |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CP01 | Change in the name or title of a patent holder |
Address after: 710068 Baisha commercial building, 1 Baisha Road, Xi'an, Shaanxi Patentee after: Northwest Limited Company Limited Address before: 710068 Baisha commercial building, 1 Baisha Road, Xi'an, Shaanxi Patentee before: In the research of modern navigation (Xi'an) Technology Co., Ltd. |
|
| CP01 | Change in the name or title of a patent holder |