CN208298414U - A kind of simulation aircraft wide-angle turning control device - Google Patents
A kind of simulation aircraft wide-angle turning control device Download PDFInfo
- Publication number
- CN208298414U CN208298414U CN201820180971.2U CN201820180971U CN208298414U CN 208298414 U CN208298414 U CN 208298414U CN 201820180971 U CN201820180971 U CN 201820180971U CN 208298414 U CN208298414 U CN 208298414U
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- CN
- China
- Prior art keywords
- gear
- potentiometer
- rotating disc
- pedestal
- fixedly installed
- 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
Links
- 238000004088 simulation Methods 0.000 title abstract description 14
- NJPPVKZQTLUDBO-UHFFFAOYSA-N novaluron Chemical compound C1=C(Cl)C(OC(F)(F)C(OC(F)(F)F)F)=CC=C1NC(=O)NC(=O)C1=C(F)C=CC=C1F NJPPVKZQTLUDBO-UHFFFAOYSA-N 0.000 abstract description 10
- 230000000694 effects Effects 0.000 abstract description 9
- 238000013016 damping Methods 0.000 abstract description 4
- 238000000034 method Methods 0.000 description 3
- 238000006073 displacement reaction Methods 0.000 description 2
- 239000012530 fluid Substances 0.000 description 2
- 238000006243 chemical reaction Methods 0.000 description 1
- 230000006835 compression Effects 0.000 description 1
- 238000007906 compression Methods 0.000 description 1
- 230000007812 deficiency Effects 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 238000007599 discharging Methods 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 238000009434 installation Methods 0.000 description 1
- 238000005259 measurement Methods 0.000 description 1
- 230000008447 perception Effects 0.000 description 1
- 239000007787 solid Substances 0.000 description 1
- 230000009466 transformation Effects 0.000 description 1
- 230000016776 visual perception Effects 0.000 description 1
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- Mechanical Control Devices (AREA)
Abstract
The utility model relates to a kind of simulation aircraft wide-angle turning control devices, and the upper end of frame body is fixedly connected with rotating disc by shaft；The close end position of shaft is equipped with gear；Rotating disc is connected by connection bolt with mounting flange；Handwheel is installed on the lateral surface of mounting flange；The lower edge of rotating disc is provided with wing plate；Connecting plate is fixedly installed on wing plate；Potentiometer is mounted on the upper end of connecting plate；The input terminal of potentiometer is connected with lower gear；Lower gear with gear is mutually ratcheting is installed together；The lower end of frame body is equipped with rotating ball；The lower end of rotating ball is fixedly installed with reset damper rod；It resets and is provided with telescopic rod on damper rod；The lower end of telescopic rod is fixedly installed with pedestal；Mounting hole is provided on pedestal.The technical solution of the utility model be capable of providing it is a kind of it is convenient for disassembly and assembly, at low cost, damping force variation is gentle and simulation effect simulates well aircraft wide-angle turning control device.
Description
Technical field
The utility model relates to flight simulation machinery technical field more particularly to a kind of turning manipulations of simulation aircraft wide-angle
Device.
Background technique
Flight-simulation equipment is to make the driving experience of driver realize high fidelity, and on visual perception, simulation flies
Machine steering external situation, to be played situations such as making pilot judge posture, position, height, speed and the weather of aircraft
To the effect of driver training training, training cost is reduced, training speed is accelerated.Aircraft is by deflecting roller in ground taxi
Change direction to turn, what usually preceding wheel was used to turn to.Aircraft and ground face contact are tires on undercarriage, are led
It falls and erects support and roll-sliding effect, nose-gear plays a part of to balance and turn to.Pilot operator turns to handwheel, before control
Undercarriage deflecting roller, so that it may change the line of travel of aircraft.
It is the device for simulating actual airplane ground handling maneuver that flight simulator, which turns to handwheel, is located at cockpit main driving one
Side.When pilot shakes handwheel counterclockwise, deflecting roller left avertence, aircraft is turned to the left；When pilot shakes handwheel clockwise,
Deflecting roller right avertence, aircraft bend to right.When steering handwheel is generally used for ground low speed slide, the manipulation of aircraft wide-angle turning.
Generally using spring connection handwheel and pedestal, rotary resistance is provided.But the power that spring provides changes greatly, and handwheel resets
When be easy to produce swing, simulation effect is poor.
Utility model content
The utility model aim is for overcome the deficiencies in the prior art and provides a kind of convenient for disassembly and assembly, at low cost, damping
Power variation is gentle and simulation effect simulates well aircraft wide-angle turning control device.
In order to achieve the above objectives, the utility model uses following technical solution.
A kind of simulation aircraft wide-angle is turned control device, including frame body, shaft, gear, rotating disc, connection bolt,
Wing plate, mounting flange, handwheel, connecting plate, lower gear, rotating ball, resets damper rod, telescopic rod, pedestal and installation at potentiometer
The upper end in hole, the frame body is fixedly connected with rotating disc by shaft；The close end position of the shaft is equipped with gear；
The rotating disc is connected by connection bolt with mounting flange；Handwheel is installed on the lateral surface of the mounting flange；It is described
The lower edge of rotating disc is provided with wing plate；Connecting plate is fixedly installed on the wing plate；The potentiometer is mounted on connecting plate
Upper end；The input terminal of the potentiometer is connected with lower gear；The lower gear with the gear is mutually ratcheting is installed together；Institute
The lower end for stating frame body is equipped with rotating ball；The lower end of the rotating ball is fixedly installed with reset damper rod；The reset damping
Telescopic rod is provided on bar；The lower end of the telescopic rod is fixedly installed with pedestal；Mounting hole is provided on the pedestal.
The potentiometer is angle displacement potentiometer as a further improvement of the utility model,.
The driving method for resetting damper rod is that air pressure or fluid pressure type drive as a further improvement of the utility model,
It is dynamic.
Due to the application of the above technical scheme, the advantageous effects that the utility model has: the technology of the utility model
Scheme uses shaft, rotating disc, mounting flange and handwheel, and the operation of simulation aircraft wide-angle turning may be implemented, have structure
Simply, advantageous effects at low cost；The technical program additionally uses gear, lower gear and potentiometer, and by potentiometer
It is mounted on the arm plate of rotating disc, by potentiometer to the rotation angle measurement of rotary shaft, reaches the reality to handwheel work angle
When sensed data collect, realize to operator manipulate be intended to accurate judgement, have wheel measuring precisely, convenient for simulator it is timely
The advantageous effects that perception operation is intended to；The technical program additionally uses air pressure or fluid pressure type resets damper rod, when handwheel revolves
When turning, the telescopic rod in damper rod can be by compression and pressure increases, after discharging handwheel, under air pressure or hydraulic reaction,
Telescopic rod can auto-extending, play the reset again to hand wheel position, have reset at the uniform velocity, damping feedback force is stable, it is imitative to be promoted
The advantageous effects of true simulation true feeling.
Detailed description of the invention
Technical solutions of the utility model are described further with reference to the accompanying drawing.
Attached drawing 1 is the structural schematic diagram of the utility model.
In figure: 1. frame bodies；2. shaft；3. gear；4. rotating disc；5. connecting bolt；6. wing plate；7. potentiometer；8. solid
Determine flange；9. handwheel；10. connecting plate；11. lower gear；12. rotating ball；13. resetting damper rod；14. telescopic rod；15. pedestal；
16. mounting hole.
Specific embodiment
With reference to the accompanying drawing and specific embodiment the utility model is described in further detail.
A kind of simulation aircraft wide-angle turning control device described in the utility model as shown in Fig. 1, including frame body
1, shaft 2, gear 3, rotating disc 4, connection bolt 5, wing plate 6, potentiometer 7, mounting flange 8, handwheel 9, connecting plate 10, lower tooth
Wheel 11, rotating ball 12 reset damper rod 13, telescopic rod 14, pedestal 15 and mounting hole 16, and the upper end of the frame body 1 passes through shaft 2
It is fixedly connected with rotating disc 4；The close end position of the shaft 2 is equipped with gear 3；The rotating disc 4 passes through connection spiral shell
Bolt 5 is connected with mounting flange 8；Handwheel 9 is installed on the lateral surface of the mounting flange 8；The lower edge of the rotating disc 4 is set
It is equipped with wing plate 6；Connecting plate 10 is fixedly installed on the wing plate 6；The potentiometer 7 is mounted on the upper end of connecting plate 10；It is described
The input terminal of potentiometer 7 is connected with lower gear 11；The lower gear 11 with the gear 3 is mutually ratcheting is installed together；It is described
The lower end of frame body 1 is equipped with rotating ball 12；The lower end of the rotating ball 12, which is fixedly installed with, resets damper rod 13；The reset
Telescopic rod 14 is provided on damper rod 13；The lower end of the telescopic rod 14 is fixedly installed with pedestal 15；It is arranged on the pedestal 15
There is mounting hole 16；The potentiometer 7 is angle displacement potentiometer；The driving method for resetting damper rod 13 is air pressure or hydraulic
Formula driving.
The above is only the specific application examples of the utility model, do not constitute any limit to the protection scope of the utility model
System.Any technical scheme formed by adopting equivalent transformation or equivalent replacement, all fall within the utility model rights protection scope it
It is interior.
Claims (3)
- The control device 1. a kind of simulation aircraft wide-angle is turned, it is characterised in that: including frame body (1), shaft (2), gear (3), rotating disc (4), connection bolt (5), wing plate (6), potentiometer (7), mounting flange (8), handwheel (9), connecting plate (10), under Gear (11), resets damper rod (13), telescopic rod (14), pedestal (15) and mounting hole (16), the frame body at rotating ball (12) (1) upper end is fixedly connected with rotating disc (4) by shaft (2)；The close end position of the shaft (2) is equipped with gear (3)；The rotating disc (4) is connected by connecting bolt (5) with mounting flange (8)；On the lateral surface of the mounting flange (8) Handwheel (9) are installed；The lower edge of the rotating disc (4) is provided with wing plate (6)；Connection is fixedly installed on the wing plate (6) Plate (10)；The potentiometer (7) is mounted on the upper end of connecting plate (10)；The input terminal of the potentiometer (7) is connected with lower gear (11)；The lower gear (11) with the gear (3) is mutually ratcheting is installed together；The lower end of the frame body (1) is equipped with Rotating ball (12)；The lower end of the rotating ball (12), which is fixedly installed with, resets damper rod (13)；On the reset damper rod (13) It is provided with telescopic rod (14)；The lower end of the telescopic rod (14) is fixedly installed with pedestal (15)；It is provided on the pedestal (15) Mounting hole (16).
- The control device 2. a kind of simulation aircraft wide-angle according to claim 1 is turned, it is characterised in that: the potentiometer It (7) is angle displacement potentiometer.
- The control device 3. a kind of simulation aircraft wide-angle according to claim 1 is turned, it is characterised in that: the reset resistance The driving method of Buddhist nun's bar (13) is air pressure or fluid pressure type driving.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820180971.2U CN208298414U (en) | 2018-02-02 | 2018-02-02 | A kind of simulation aircraft wide-angle turning control device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820180971.2U CN208298414U (en) | 2018-02-02 | 2018-02-02 | A kind of simulation aircraft wide-angle turning control device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN208298414U true CN208298414U (en) | 2018-12-28 |
Family
ID=64698108
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201820180971.2U Expired - Fee Related CN208298414U (en) | 2018-02-02 | 2018-02-02 | A kind of simulation aircraft wide-angle turning control device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN208298414U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110702039A (en) * | 2019-10-22 | 2020-01-17 | 国网宁夏电力有限公司经济技术研究院 | Device for measuring wind deflection angle of suspension insulator string |
-
2018
- 2018-02-02 CN CN201820180971.2U patent/CN208298414U/en not_active Expired - Fee Related
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110702039A (en) * | 2019-10-22 | 2020-01-17 | 国网宁夏电力有限公司经济技术研究院 | Device for measuring wind deflection angle of suspension insulator string |
| CN110702039B (en) * | 2019-10-22 | 2021-06-01 | 国网宁夏电力有限公司经济技术研究院 | Device for measuring wind deflection angle of suspension insulator string |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20181228 Termination date: 20220202 |