CN208922535U - A kind of horizon instrument suitable for flight simulator - Google Patents
A kind of horizon instrument suitable for flight simulator Download PDFInfo
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- CN208922535U CN208922535U CN201820561865.9U CN201820561865U CN208922535U CN 208922535 U CN208922535 U CN 208922535U CN 201820561865 U CN201820561865 U CN 201820561865U CN 208922535 U CN208922535 U CN 208922535U
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- pitching
- horizon
- flight simulator
- hollow shaft
- connects
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- 238000009434 installation Methods 0.000 claims abstract description 17
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 claims description 14
- 238000005096 rolling process Methods 0.000 claims description 11
- 229910052742 iron Inorganic materials 0.000 claims description 7
- 238000004088 simulation Methods 0.000 abstract description 9
- 210000000515 tooth Anatomy 0.000 description 22
- 230000007812 deficiency Effects 0.000 description 1
- 238000005474 detonation Methods 0.000 description 1
- 230000005611 electricity Effects 0.000 description 1
- 238000005259 measurement Methods 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 230000000007 visual effect Effects 0.000 description 1
Abstract
The utility model relates to aircraft flight simulation device technical fields, especially a kind of horizon instrument suitable for flight simulator, including inclined scale disk, pitching dial, pitch arm, Sloped rotating arm, pitching rack gear, flange hollow shaft, mounting plate and Horizon meter housing, the upper end of Horizon meter housing is arranged in mounting plate, the lower end of installation panel is arranged in background board, flange hollow shaft is connected to the center of mounting plate, the upper end of flange hollow shaft connects Sloped rotating arm by pitching rack gear, Sloped rotating arm connects pitching dial by pitch arm, the upper end of pitching dial connects inclined scale disk, the upper end of inclined scale disk connects background board.The utility model is the utility model has the advantages that the pitching of the utility model flight simulator horizon instrument and inclination indicating mechanism are mounted on flange hollow shaft, entire indicating mechanism can realize 360 ° of rotations, and so as to realize, aircraft aircraft flight attitude in tumbling flight is more accurately indicated in fly simulation training.
Description
Technical field
The utility model relates to aircraft flight simulation device technical field, especially a kind of Horizon suitable for flight simulator
Instrument.
Background technique
Horizon instrument is the instrument of posture in measurement and display aircraft flight, by the pitching in aircraft flight, inclined angle
Aircrew is reflected in the form of visual signal.Professional equipment of the flight simulator as flight training, it is desirable that flight simulator
Horizon instrument possessed function being consistent property as far as possible in simulated training flight and when actual airplane horizon instrument is in flight.In this way
Facilitate to increase the trained sense of reality in fly simulation training, enhances user experience.
Therefore, it is necessary to propose a kind of horizon instrument suitable for flight simulator in response to the above problems.
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 to be suitable for flight mould
The horizon instrument of quasi- device.
A kind of horizon instrument suitable for flight simulator, including installation panel, background board, inclined scale disk, pitching scale
Disk, pitch arm, Sloped rotating arm, pitching rack gear, flange hollow shaft, mounting plate and Horizon meter housing, the mounting plate setting exist
The lower end of installation panel is arranged in the upper end of Horizon meter housing, the background board, and the flange hollow shaft is connected to mounting plate
The upper end of center, the flange hollow shaft connects Sloped rotating arm by pitching rack gear, and the Sloped rotating arm is by bowing
Arm connection pitching dial is faced upward, the upper end of the pitching dial connects inclined scale disk, and the upper end of the inclined scale disk connects
Connect background board.
Preferably, the upper end of the installation panel is provided with transparent cover, wherein a side setting of the installation panel
There is knob.
Preferably, the inclined scale disk is provided with flivver fixing groove, and the flivver fixing groove is provided with flivver
Rack gear.
Preferably, the knob connects flivver rack gear by adjustment gear.
Preferably, the Sloped rotating arm is provided with the first pin shaft, the second pin shaft, pitching Jie tooth and pivoted arm hinge.
Preferably, the lower part of the flange hollow shaft is respectively arranged with pitching sliding tooth, pitching driven tooth, sliding block, limit
Plate, rolling driven tooth, rolling sliding tooth, nut seat and plectrum.
Preferably, failure flag, failure flag shaft, failure flag only support and electromagnet hinge are additionally provided in the Horizon meter housing
Chain, the failure flag are all connected with failure flag by failure flag shaft and only hold in the palm and electromagnetism iron hinge.
Due to the adoption of the above technical scheme, the utility model is the utility model has the advantages that the utility model flight simulator horizon instrument
Pitching and inclination indicating mechanism are mounted on flange hollow shaft, and entire indicating mechanism can realize 360 ° of rotations, so as to realize
Aircraft aircraft flight attitude in tumbling flight more accurately indicates that structure is simple in fly simulation training, securely and reliably.
Detailed description of the invention
Fig. 1 is the front view of the utility model；
Fig. 2 is the assembly detonation configuration figure of the utility model；
Fig. 3 is the assembly cross section view of the utility model；
Appended drawing reference in figure: 1. transparent covers, 2. installation panels, 3. knobs, 4. adjustment gears, 5. flivver fixing grooves,
6. flivver rack gear, 7. background boards, 8. inclined scale disks, 9. pitching dials, 10. pitch arms, 11. first pin shafts, 12. pitching
Jie's tooth, 13. second pin shafts, 14. pivoted arm hinges, 15. Sloped rotating arms, 16. pitching rack gears, 17. flange hollow shafts, 18. installations
Plate, 19. pitching sliding tooths, 20. pitching driven tooths, 21. sliding blocks, 22. limit plates, 23. rolling driven tooths, 24. rolling sliding tooths,
25. nut seat, 26. plectrums, 27. Horizon meter housings, 28. failure flags, 29. failure flag shafts, 30. failure flags are only held in the palm, 31. electromagnetism
Iron hinge.
Specific embodiment
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.
Such as Fig. 1 is simultaneously combined shown in Fig. 2 and Fig. 3, a kind of horizon instrument suitable for flight simulator, including installation panel 2, back
Scape plate 7, inclined scale disk 8, pitching dial 9, pitch arm 10, Sloped rotating arm 15, pitching rack gear 16, flange hollow shaft 17,
The upper end of Horizon meter housing 27 is arranged in mounting plate 18 and Horizon meter housing 27, the mounting plate 18, and the setting of background board 7 exists
The lower end of panel 2 is installed, the flange hollow shaft 17 is connected to the center of mounting plate 18, the flange hollow shaft 17 it is upper
End connects Sloped rotating arm 15 by pitching rack gear 16, and the Sloped rotating arm 15 connects pitching dial 9 by pitch arm 10,
The upper end of the pitching dial 9 connects inclined scale disk 8, and the upper end of the inclined scale disk 8 connects background board 7.
Further, the upper end of the installation panel 2 is provided with transparent cover 1, wherein a side of the installation panel 2
It is provided with knob 3, the inclined scale disk 8 is provided with flivver fixing groove 5, and the flivver fixing groove 5 is provided with flivver
Rack gear 6.
Wherein, the knob 3 connects flivver rack gear 6 by adjustment gear 4, and the Sloped rotating arm 15 is provided with first
Pin shaft 11, the second pin shaft 13, pitching Jie tooth 12 and pivoted arm hinge 14.
In addition, the lower part of the flange hollow shaft 17 is respectively arranged with pitching sliding tooth 19, pitching driven tooth 20, sliding block
21, limit plate 22, rolling driven tooth 23, rolling sliding tooth 24, nut seat 25 and plectrum 26 are also set in the Horizon meter housing 27
Be equipped with failure flag 28, failure flag shaft 29, failure flag stop support 30 and electromagnetism iron hinge 31, the failure flag 28 passes through failure flag and turns
Axis 29 is all connected with failure flag and stops support 30 and electromagnetism iron hinge 31.
The pitching of the utility model flight simulator horizon instrument and inclination indicating mechanism are mounted on flange hollow shaft, entirely
Indicating mechanism can realize 360 ° of rotations, so as to realize aircraft aircraft flight appearance in tumbling flight in fly simulation training
State more accurately indicates that structure is simple, securely and reliably.
The utility model simulated flight device in training have in-flight identical flight attitude is shown with actual airplane, allow
User has the impression of live flying when operating, redesign structure according to prior art condition, to show that flight simulator is instructed
Flight pitching in white silk, lateral attitude.
The executing agency that this flight simulator horizon instrument is selected is stepper motor or steering engine, uses two stepper motors or rudder
Machine respectively drives corresponding pitching and tilts mechanical gear mechanism, to make the pitch angle of aircraft in horizon instrument instruction flight simulation
The inclination angle and.In this way, the horizon instrument of flight simulator is made intuitively to show the flight attitude of aircraft, and should
Horizon instrument has the function of indicating fault
To realize that technical solution used by above-mentioned flight simulation horizon instrument function is such that through stepper motor or rudder
Machine respectively drives rolling sliding tooth and pitching sliding tooth, by driving corresponding pitch angle gear mechanism and inclination angle gear mechanism
Structure makes the pitching dial for indicating aircraft flight attitude and the rotation of inclined scale disk, eventually by Horizon instrument board indication mechanism
Intuitively show aircraft flight pitching and lateral attitude.The indicating fault is when receiving fault data by control electricity
Failure flag is popped up or is withdrawn by magnet control indicating fault mechanism by the on-off of magnet current.
The pitching of this flight simulator horizon instrument and inclination indicating mechanism are entirely referred to by being installed on flange hollow shaft
Show that mechanism can realize 360 ° of rotations, so as to realize aircraft aircraft flight attitude in tumbling flight in fly simulation training
More accurately instruction.
The pitch angle gear mechanism includes pitching dial 9, pitch arm 10, the first pin shaft 11, pitching Jie tooth 12, second
Pin shaft 13, pivoted arm hinge 14, pitching rack gear 16, mounting plate 18, pitching sliding tooth 19, pitching driven tooth 20, sliding block 22；It is described
Pitch gear mechanism includes: inclined scale disk 8, Sloped rotating arm 15, flange hollow shaft 17, mounting plate 18, limit plate 22, rolling
Driven tooth 23, rolling sliding tooth 24；The indicating fault mechanism includes: failure flag 28, failure flag shaft 29, failure flag only support
30, electromagnetism iron hinge 31.
The display portion mechanism includes transparent cover 1, installation panel 2, knob 3, adjustment gear 4, flivver fixing groove
5, flivver rack gear 6, background board 7.It can indicate that by flivver rack gear 6, background board 7, inclined scale disk 8, pitching dial 9
The flight attitude of aircraft.Pitching dial 9 and flivver rack gear 6 are fixed on installation panel 2 by flivver fixing groove 5, are led to
It crosses knob 3 and flivver rack gear 6 is adjusted relative to horizon position on background board 7.
The above is only the preferred embodiment of the present invention, and therefore it does not limit the scope of the patent of the utility model,
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 also included in the patent protection scope of the utility model.
Claims (7)
1. a kind of horizon instrument suitable for flight simulator, it is characterised in that: including installation panel, background board, inclined scale disk,
Pitching dial, pitch arm, Sloped rotating arm, pitching rack gear, flange hollow shaft, mounting plate and Horizon meter housing, the installation
The upper end of Horizon meter housing is arranged in plate, and the lower end of installation panel is arranged in the background board, and the flange hollow shaft is connected to
The upper end of the center of mounting plate, the flange hollow shaft connects Sloped rotating arm, the Sloped rotating by pitching rack gear
Arm connects pitching dial by pitch arm, and the upper end of the pitching dial connects inclined scale disk, the inclined scale disk
Upper end connect background board.
2. a kind of horizon instrument suitable for flight simulator as described in claim 1, it is characterised in that: the installation panel
Upper end is provided with transparent cover, and wherein a side of the installation panel is provided with knob.
3. a kind of horizon instrument suitable for flight simulator as claimed in claim 2, it is characterised in that: the inclined scale disk
It is provided with flivver fixing groove, the flivver fixing groove is provided with flivver rack gear.
4. a kind of horizon instrument suitable for flight simulator as claimed in claim 3, it is characterised in that: the knob passes through tune
It saves gear and connects flivver rack gear.
5. a kind of horizon instrument suitable for flight simulator as described in claim 1, it is characterised in that: the Sloped rotating arm
It is provided with the first pin shaft, the second pin shaft, pitching Jie tooth and pivoted arm hinge.
6. a kind of horizon instrument suitable for flight simulator as described in claim 1, it is characterised in that: the flange hollow shaft
Lower part be respectively arranged with pitching sliding tooth, pitching driven tooth, sliding block, limit plate, rolling driven tooth, rolling sliding tooth, nut
Seat and plectrum.
7. a kind of horizon instrument suitable for flight simulator as described in claim 1, it is characterised in that: the Horizon meter housing
It is inside additionally provided with failure flag, failure flag shaft, failure flag only support and electromagnetism iron hinge, the failure flag is equal by failure flag shaft
Connecting fault flag is only held in the palm and electromagnetism iron hinge.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820561865.9U CN208922535U (en) | 2018-04-19 | 2018-04-19 | A kind of horizon instrument suitable for flight simulator |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820561865.9U CN208922535U (en) | 2018-04-19 | 2018-04-19 | A kind of horizon instrument suitable for flight simulator |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN208922535U true CN208922535U (en) | 2019-05-31 |
Family
ID=66691934
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201820561865.9U Active CN208922535U (en) | 2018-04-19 | 2018-04-19 | A kind of horizon instrument suitable for flight simulator |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN208922535U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110634351A (en) * | 2019-09-29 | 2019-12-31 | 中仿智能科技（上海）股份有限公司 | Aviation horizon sensor control system of flight simulator |
| CN110745000A (en) * | 2019-10-29 | 2020-02-04 | 上海天马有机发光显示技术有限公司 | Vehicle instrument and display method thereof, and vehicle speed monitoring display system |
-
2018
- 2018-04-19 CN CN201820561865.9U patent/CN208922535U/en active Active
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110634351A (en) * | 2019-09-29 | 2019-12-31 | 中仿智能科技（上海）股份有限公司 | Aviation horizon sensor control system of flight simulator |
| CN110745000A (en) * | 2019-10-29 | 2020-02-04 | 上海天马有机发光显示技术有限公司 | Vehicle instrument and display method thereof, and vehicle speed monitoring display system |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20240328 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 |