CN208043851U - A kind of airspeed-indicator suitable for flight simulator - Google Patents
A kind of airspeed-indicator suitable for flight simulator Download PDFInfo
- Publication number
- CN208043851U CN208043851U CN201820560607.9U CN201820560607U CN208043851U CN 208043851 U CN208043851 U CN 208043851U CN 201820560607 U CN201820560607 U CN 201820560607U CN 208043851 U CN208043851 U CN 208043851U
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- meter panel
- indicating meter
- airspeed
- gear wheel
- uniform light
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- 238000004088 simulation Methods 0.000 abstract description 5
- 230000000694 effects Effects 0.000 abstract description 2
- 238000009434 installation Methods 0.000 description 8
- 230000007812 deficiency Effects 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 230000000007 visual effect Effects 0.000 description 1
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Abstract
The utility model is related to aircraft flight simulation device technical fields, a kind of especially airspeed-indicator suitable for flight simulator, including dial plate, the first indicating meter panel, the second indicating meter panel, gear wheel, uniform light board, light-emitting backplane and needle pivot, uniform light board is arranged in the upper end of light-emitting backplane, gear wheel is clamped between the second indicating meter panel and uniform light board, first indicating meter panel is arranged in the upper end of the second indicating meter panel, and the lower part of needle pivot connects stepper motor or steering engine by fingerstall.The utility model advantageous effect：The utility model is provided with including dial plate, the first indicating meter panel, the second indicating meter panel, gear wheel, uniform light board, light-emitting backplane and needle pivot, it can see the indicating graduation value of instrument through transparent cover, adjusting knob is meshed with gear wheel, and the location point of pointer instruction can be adjusted by adjusting knob.
Description
Technical field
The utility model is related to aircraft flight simulation device technical fields, especially a kind of air speed suitable for flight simulator
Table.
Background technology
Airspeed-indicator is the instrument for measuring and showing aircraft flight medium velocity, by the flying speed of aircraft in the form of visual signal
It is reflected to aircrew.Professional equipment of the flight simulator as flight training, it is desirable that flight simulator airspeed-indicator flies in simulation
Row training when and true tool of aircraft airspeed indicator coupled possessed function being consistent property as possible in flight, helped in fly simulation training
In the sense of reality for increasing training, enhance user experience.
Therefore, for the above problem, it is necessary to propose a kind of airspeed-indicator suitable for flight simulator.
Utility model content
In view of the above-mentioned deficiencies in the prior art, the purpose of this utility model is to provide one kind being suitable for flight mould
The airspeed-indicator of quasi- device.
A kind of airspeed-indicator suitable for flight simulator, including dial plate, the first indicating meter panel, the second indicator surface
Plate, gear wheel, uniform light board, light-emitting backplane and needle pivot, the uniform light board are arranged in the upper end of light-emitting backplane, the gear wheel folder
It holds between the second indicating meter panel and uniform light board, the first indicating meter panel is arranged in the second indicating meter panel
The lower part of upper end, the needle pivot connects stepper motor or steering engine by fingerstall.
Preferably, the top of the needle pivot is sequentially passed through in light-emitting backplane, uniform light board, gear wheel, the second indicating meter
Panel, the first indicating meter panel and dial plate center and be connected with pointer.
Preferably, the pointer is arranged on dial plate.
Preferably, the upper end of the dial plate is provided with transparent cover.
Preferably, dial plate a side therein is provided with adjusting knob.
Preferably, the adjusting knob is engaged with gear wheel.
Due to the adoption of the above technical scheme, the utility model advantageous effect：The utility model is provided with including dial plate, first
Indicating meter panel, the second indicating meter panel, gear wheel, uniform light board, light-emitting backplane and needle pivot, can be with through transparent cover
See that the indicating graduation value of instrument, adjusting knob are meshed with gear wheel, the position of pointer instruction can be adjusted by adjusting knob
Point, it is simple in structure, securely and reliably.
Description of the drawings
Fig. 1 is the structure chart of the utility model；
Fig. 2 is the unfolding assumption diagram of the utility model；
Reference numeral in figure：1. transparent cover, 2. pointers, 3. installation panels, 4. adjusting knobs, instrument board on 5., under 6.
Instrument board, 7. gear wheels, 8. uniform light boards, 9. light-emitting backplanes, 10. needle pivots, 11. connector sleeves.
Specific implementation mode
The embodiments of the present invention are described in detail below in conjunction with attached drawing, but the utility model can be by right
It is required that the multitude of different ways for limiting and covering is implemented.
As shown in Figure 1, a kind of airspeed-indicator suitable for flight simulator, including installation panel 3, upper instrument board 5, lower instrument
Disk 6, gear wheel 7, uniform light board 8, light-emitting backplane 9 and needle pivot 10, the uniform light board 8 is arranged in the upper end of light-emitting backplane 9, described
Gear wheel 7 is clamped between lower instrument board 6 and uniform light board 8, and the upper instrument board 5 is arranged in the upper end of lower instrument board 6, the finger
The lower part of needle shaft 10 connects stepper motor or steering engine by fingerstall.
Wherein, the top of the needle pivot 10 sequentially pass through in light-emitting backplane 9, uniform light board 8, gear wheel 7, lower instrument board 6,
The center of upper instrument board 5 and installation panel 3 is connected with pointer 2, and the setting of the pointer 2 is on installation panel 3.
In addition, the upper end of the installation panel 3 is provided with installation panel transparent cover 1, the installation panel 3 therein one
Side is provided with adjusting knob 4, and the adjusting knob 4 is engaged with gear wheel 7.
The utility model make simulated flight device in training with the flying speed with model identical in aircraft flight
It has been shown that, there is the impression of live flying when user being allowed to operate, structure is redesigned according to prior art condition, to show flight mould
Flying speed in quasi- device training.
The executing agency that this flight simulator airspeed-indicator is selected is stepper motor or steering engine, stepper motor or steering engine and instrument
Pointer is connected, and the instruction of aircraft flight speed in fly simulation training is completed by controlling stepper motor or steering engine.
Stepper motor or steering engine are by being connected to connector sleeve 11, and needle pivot 10 is connected with connector sleeve 11 and pointer 2 is installed
On needle pivot 10, the rotation of stepper motor or steering engine drives the rotation of pointer 2, and installation 3 high scale of panel is directed toward by pointer 2
Position instruction go out corresponding simulated flight speed.The airspeed-indicator indicating section includes：Transparent cover 1, pointer 2, mounting surface
Plate 3, upper instrument board 5, lower instrument board 6, uniform light board 8, through transparent cover 1 it can be seen that the indicating graduation value of instrument.Adjust rotation
Button 4 is meshed with gear wheel 7, can adjust the location point that pointer 2 indicates by adjusting knob 4.
The above is only the preferred embodiment of the present invention, and it does not limit the scope of the patent of the present invention,
Equivalent structure or equivalent flow shift made by using the description of the utility model and the drawings, is directly or indirectly transported
Used in other related technical areas, it is equally included in the patent within the scope of the utility model.
Claims (6)
1. a kind of airspeed-indicator suitable for flight simulator, it is characterised in that：Including dial plate, the first indicating meter panel, second
Indicating meter panel, gear wheel, uniform light board, light-emitting backplane and needle pivot, the uniform light board are arranged in the upper end of light-emitting backplane, institute
It states gear wheel to be clamped between the second indicating meter panel and uniform light board, the first indicating meter panel setting is in the second instruction
The lower part of the upper end of instrument face plate, the needle pivot connects stepper motor or steering engine by fingerstall.
2. a kind of airspeed-indicator suitable for flight simulator according to claim 1, it is characterised in that：The needle pivot
Top is sequentially passed through in light-emitting backplane, uniform light board, gear wheel, the second indicating meter panel, the first indicating meter panel and dial plate
Center and be connected with pointer.
3. a kind of airspeed-indicator suitable for flight simulator according to claim 2, it is characterised in that：The pointer setting
On dial plate.
4. a kind of airspeed-indicator suitable for flight simulator according to claim 1, it is characterised in that：The dial plate it is upper
End is provided with transparent cover.
5. a kind of airspeed-indicator suitable for flight simulator according to claim 1, it is characterised in that：The dial plate is wherein
A side be provided with adjusting knob.
6. a kind of airspeed-indicator suitable for flight simulator according to claim 5, it is characterised in that：The adjusting knob
It is engaged with gear wheel.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820560607.9U CN208043851U (en) | 2018-04-19 | 2018-04-19 | A kind of airspeed-indicator suitable for flight simulator |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820560607.9U CN208043851U (en) | 2018-04-19 | 2018-04-19 | A kind of airspeed-indicator suitable for flight simulator |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN208043851U true CN208043851U (en) | 2018-11-02 |
Family
ID=63927751
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201820560607.9U Active CN208043851U (en) | 2018-04-19 | 2018-04-19 | A kind of airspeed-indicator suitable for flight simulator |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN208043851U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN114627719A (en) * | 2022-02-17 | 2022-06-14 | 北京世纪晨数据技术有限责任公司 | Simulation cockpit for simulation aeronautical instrument and simulator |
-
2018
- 2018-04-19 CN CN201820560607.9U patent/CN208043851U/en active Active
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN114627719A (en) * | 2022-02-17 | 2022-06-14 | 北京世纪晨数据技术有限责任公司 | Simulation cockpit for simulation aeronautical instrument and simulator |
| CN114627719B (en) * | 2022-02-17 | 2024-04-02 | 北京世纪晨数据技术有限责任公司 | Simulation aviation instrument and simulator simulation cabin |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| TR01 | Transfer of patent right | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20240418 Address after: No. 10, 13th Floor, Building 1, No. 51 Qinglong Street, Qingyang District, Chengdu City, Sichuan Province, 610000 Patentee after: Sichuan Pan American Smart Industry Co.,Ltd. Country or region after: China Address before: No. 1609, 16th floor, Tianfu Jingrong building, 2039 Tianfu Avenue South, Tianfu New District, Chengdu, Sichuan 610000 Patentee before: FAME VISTA TECHNOLOGIES, LTD. Country or region before: China |