CN108109473A - A kind of flight simulator foot rudder linkage - Google Patents
A kind of flight simulator foot rudder linkage Download PDFInfo
- Publication number
- CN108109473A CN108109473A CN201810104503.1A CN201810104503A CN108109473A CN 108109473 A CN108109473 A CN 108109473A CN 201810104503 A CN201810104503 A CN 201810104503A CN 108109473 A CN108109473 A CN 108109473A
- Authority
- CN
- China
- Prior art keywords
- linkage
- swing arm
- operating pedal
- hand tread
- axis
- 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.)
- Pending
Links
- 238000009434 installation Methods 0.000 abstract description 2
- 238000004519 manufacturing process Methods 0.000 abstract description 2
- 230000000694 effects Effects 0.000 description 7
- 238000004088 simulation Methods 0.000 description 3
- 230000005540 biological transmission Effects 0.000 description 2
- 238000010586 diagram Methods 0.000 description 2
- 238000006243 chemical reaction Methods 0.000 description 1
- 238000013016 damping Methods 0.000 description 1
- 230000007812 deficiency Effects 0.000 description 1
- 230000005611 electricity Effects 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 230000001737 promoting effect Effects 0.000 description 1
- 230000009466 transformation Effects 0.000 description 1
- 201000009482 yaws Diseases 0.000 description 1
Classifications
-
- G—PHYSICS
- G09—EDUCATION; CRYPTOGRAPHY; DISPLAY; ADVERTISING; SEALS
- G09B—EDUCATIONAL OR DEMONSTRATION APPLIANCES; APPLIANCES FOR TEACHING, OR COMMUNICATING WITH, THE BLIND, DEAF OR MUTE; MODELS; PLANETARIA; GLOBES; MAPS; DIAGRAMS
- G09B9/00—Simulators for teaching or training purposes
- G09B9/02—Simulators for teaching or training purposes for teaching control of vehicles or other craft
- G09B9/08—Simulators for teaching or training purposes for teaching control of vehicles or other craft for teaching control of aircraft, e.g. Link trainer
- G09B9/28—Simulation of stick forces or the like
-
- G—PHYSICS
- G09—EDUCATION; CRYPTOGRAPHY; DISPLAY; ADVERTISING; SEALS
- G09B—EDUCATIONAL OR DEMONSTRATION APPLIANCES; APPLIANCES FOR TEACHING, OR COMMUNICATING WITH, THE BLIND, DEAF OR MUTE; MODELS; PLANETARIA; GLOBES; MAPS; DIAGRAMS
- G09B9/00—Simulators for teaching or training purposes
- G09B9/02—Simulators for teaching or training purposes for teaching control of vehicles or other craft
- G09B9/08—Simulators for teaching or training purposes for teaching control of vehicles or other craft for teaching control of aircraft, e.g. Link trainer
Abstract
The present invention relates to a kind of flight simulator foot rudder linkage, middle frame is installed in the inside of housing；The both sides of housing are symmetrically arranged with rest pedal；Framework upper both sides are provided with left operating pedal and right operating pedal by mounting rail；The inside edge of left operating pedal is connected to after passing sequentially through upper swing arm, upper connecting rod, lower link and lower swing arm on left-hand tread plate linkage brake axis；The inside edge of right operating pedal is connected to after passing sequentially through upper swing arm, upper connecting rod, lower link and lower swing arm on right-hand tread plate linkage brake axis；Vertical rotation axis is movably connected in by turntable on mounting platform；The both ends of driver plate are connected by the body of rod with mounting rail；The lower sides of vertical rotation axis are equipped with foot rudder interlocking bar by connecting plate.Technical scheme is capable of providing a kind of flight simulator foot rudder linkage rational in infrastructure, linkage performance is good, easy for installation compact and manufacture is at low cost.
Description
Technical field
The present invention relates to flight simulation machinery technical field more particularly to a kind of flight simulator foot rudder linkages.
Background technology
The rudder of aircraft is steerable airfoil portion in vertical tail, and effect is to carry out yaw control to aircraft,
It is turned to for correcting vector and low-angle.When we need to change the course of aircraft, pilot passes through the realization pair of foot rudder
The control of rudder is finally reached the purpose of yaw.
Flight simulator foot rudder linkage is to simulate yaw control, realizes real driving experience.Work as pilot
Before when pedaling Vehicular left pedal, right steps can be retreated with same magnitude, and aircraft is to left drift；When pedaling right steps before pilot,
Vehicular left pedal can be retreated with same magnitude, and aircraft yaws to the right.In addition, when pilot pushes pedal, moreover it is possible to realize
Fall frame brake function.The foot rudder of positive co-pilot is linkage, and identical action is made in synchronization, sends same finger
Order.
Aircraft foot rudder is one of important tool that pilot controls aircraft, in flight simulator, how in narrow and small mould
Intend realizing foot rudder coordinated signals in cabin, mitigate the weight of simulator, reduce cost etc. as problem to be solved.
The content of the invention
There is provided the invention aims to overcome the deficiencies in the prior art it is a kind of it is rational in infrastructure, linkage performance is good, installation
Facilitate flight simulator foot rudder linkage compact and that manufacture is at low cost.
In order to achieve the above objectives, present invention employs following technical solutions.
A kind of flight simulator foot rudder linkage is stepped on including housing, frame, rest pedal, left operating pedal, right operation
Plate, mounting rail, upper swing arm, upper connecting rod, mounting platform, driver plate, turntable, vertical rotation axis, connecting plate, foot rudder interlocking bar, current potential
Device, left-hand tread plate linkage brake axis, right-hand tread plate linkage brake axis, bearing, lower link and lower swing arm, the quantity of the frame is two
And it is symmetrically installed together；The frame is installed in the inside of the housing；The both sides of the housing are symmetrically arranged with rest
Pedal；The framework upper both sides are provided with left operating pedal and right operating pedal by mounting rail；The left operating pedal
Inside edge pass sequentially through upper swing arm, upper connecting rod, lower link and lower swing arm after be connected on left-hand tread plate linkage brake axis；It is described
The inside edge of right operating pedal is connected to right-hand tread plate brake connection after passing sequentially through upper swing arm, upper connecting rod, lower link and lower swing arm
On moving axis；Mounting platform is additionally provided in the frame；The vertical rotation axis is movably connected in the mounting platform by turntable
On；The upper end of the vertical rotation axis is equipped with driver plate；The both ends of the driver plate are connected by the body of rod with mounting rail；It is described to hang down
The lower sides of straight shaft are equipped with foot rudder interlocking bar by connecting plate；The vertical rotation axis, left-hand tread plate linkage brake axis and the right side
The end of pedal linkage brake axis is mounted on potentiometer；The left-hand tread plate linkage brake axis and right-hand tread plate linkage brake axis by
Close end position is respectively connected with bearing.
As a further improvement on the present invention, the end of the connecting plate is also associated with damper rod, and the outer end of damper rod
On be provided with fixed seat.
As a further improvement on the present invention, the surface of the left operating pedal and right operating pedal is uniformly provided with anti-skidding
Through hole.
The advantageous effects having due to the utilization of above-mentioned technical proposal, the present invention：Technical scheme passes through
Using two frames, mounting rail, rotor plate, turntable and the vertical rotation axis being arranged symmetrically, and pass through setting foot rudder connection between frame
Lever can drive foot rudder interlocking bar to swing by the rotation of rotor plate, realize two frame real-time linkage operations, have
Link advantageous effects reliable and stable, that transmission is real-time；The technical program additionally uses left and right operating pedal, the upper bottom
Arm and upper and lower strut, can be by that when being pushed to left or right operating pedal, can drive left or right pedal linkage brake
Axis rotates simultaneously, not only has the advantageous effects that can realize two frames while linkage, but also installs electricity by end
Position device, the foot-operated depth signal of conversion operation person can be gathered and pass it to the brake feedback device of simulator by having, and be risen
To the advantageous effects of real simulation operating experience；The technical program additionally uses passes through connecting rod respectively at the both ends of rotor plate
It is connected with the mounting rail of left and right operating pedal, when thus can reach one side pedal and travelling forward, another pedal will
It moves backward, there is the combined operation for realizing left and right pedal, promote the advantageous effects of the convenience of operation；The technical program
Damper rod is also provided with, there is realize after the action of foot rudder interlocking bar timely automated at the uniform velocity to reset, ensure to step in simulation
The damping sense of plate, the advantageous effects for promoting operation validity.
Description of the drawings
Technical solution of the present invention is described further below in conjunction with the accompanying drawings.
Attached drawing 1 is overall structure diagram of the invention.
Attached drawing 2 is inside enlarged structure schematic diagram of the invention.
In figure：1. housing；2. frame；3. rest pedal；4. left operating pedal；5. right operating pedal；6. mounting rail；On 7.
Swing arm；8. upper connecting rod；9. mounting platform；10. driver plate；11. turntable；12. vertical rotation axis；13. connecting plate；14. foot rudder links
Bar；15. potentiometer；16. left-hand tread plate linkage brake axis；17. right-hand tread plate linkage brake axis；18. bearing；19. lower link；Under 20.
Swing arm；21. damper rod；22. fixed seat；23. anti-skidding through hole.
Specific embodiment
Below in conjunction with the accompanying drawings and specific embodiment the present invention is described in further detail.
A kind of flight simulator foot rudder linkage of the present invention as shown in attached drawing 1,2, including housing 1, frame
2nd, rest pedal 3, left operating pedal 4, right operating pedal 5, mounting rail 6, upper swing arm 7, upper connecting rod 8, mounting platform 9, driver plate
10th, turntable 11, vertical rotation axis 12, connecting plate 13, foot rudder interlocking bar 14, potentiometer 15, left-hand tread plate linkage brake axis 16, right-hand tread plate
Linkage brake axis 17, bearing 18, lower link 19, lower swing arm 20, damper rod 21, fixed seat 22 and anti-skidding through hole 23, the frame 2
Quantity two and to be symmetrically installed together；The frame 2 is installed in the inside of the housing 1；The both sides of the housing 1
It is symmetrically arranged with rest pedal 3；Mounting rail 6 is provided with left operating pedal 4 for the 2 top both sides of frame and right operation is stepped on
Plate 5；The inside edge of the left operating pedal 4 connects after passing sequentially through upper swing arm 7, upper connecting rod 8, lower link 19 and lower swing arm 20
On left-hand tread plate linkage brake axis 16；The inside edge of the right operating pedal 5 passes sequentially through upper swing arm 7, upper connecting rod 8, lower company
It is connected to after bar 19 and lower swing arm 20 on right-hand tread plate linkage brake axis 17；Mounting platform 9 is additionally provided in the frame 2；It is described
Vertical rotation axis 12 is movably connected in by turntable 11 on the mounting platform 9；The upper end of the vertical rotation axis 12 is equipped with transmission
Plate 10；The both ends of the driver plate 10 are connected by the body of rod with mounting rail 6；The lower sides of the vertical rotation axis 12 pass through connection
Plate 13 is equipped with foot rudder interlocking bar 14；The vertical rotation axis 12, left-hand tread plate linkage brake axis 16 and right-hand tread plate linkage brake axis 17
End be mounted on potentiometer 15；The left-hand tread plate linkage brake axis 16 and right-hand tread plate linkage brake axis 17 are by close end position
It puts and is respectively connected with bearing 18；The end of the connecting plate 13 is also associated with damper rod 21, and is provided on the outer end of damper rod 21
Fixed seat 22；The surface of the left operating pedal 4 and right operating pedal 5 is uniformly provided with anti-skidding through hole 23.
It the above is only the concrete application example of the present invention, protection scope of the present invention be not limited in any way.All uses
Equivalent transformation or equivalent replacement and the technical solution formed, all fall within rights protection scope of the present invention.
Claims (3)
1. a kind of flight simulator foot rudder linkage, it is characterised in that：Including housing（1）, frame（2）, rest pedal（3）、
Left operating pedal（4）, right operating pedal（5）, mounting rail（6）, upper swing arm（7）, upper connecting rod（8）, mounting platform（9）, driver plate
（10）, turntable（11）, vertical rotation axis（12）, connecting plate（13）, foot rudder interlocking bar（14）, potentiometer（15）, left-hand tread plate brake connection
Moving axis（16）, right-hand tread plate linkage brake axis（17）, bearing（18）, lower link（19）And lower swing arm（20）, the frame（2）Number
It measures as two and is symmetrically installed together；The frame（2）It is installed in the housing（1）Inside；The housing（1）Two
Side is symmetrically arranged with rest pedal（3）；The frame（2）Top both sides pass through mounting rail（6）It is provided with left operating pedal（4）
With right operating pedal（5）；The left operating pedal（4）Inside edge pass sequentially through upper swing arm（7）, upper connecting rod（8）, lower link
（19）And lower swing arm（20）After be connected to left-hand tread plate linkage brake axis（16）On；The right operating pedal（5）Inside edge according to
It is secondary to pass through upper swing arm（7）, upper connecting rod（8）, lower link（19）And lower swing arm（20）After be connected to right-hand tread plate linkage brake axis（17）
On；The frame（2）Inside it is additionally provided with mounting platform（9）；The vertical rotation axis（12）Pass through turntable（11）It is movably connected in institute
State mounting platform（9）On；The vertical rotation axis（12）Upper end driver plate is installed（10）；The driver plate（10）Both ends lead to
Cross the body of rod and mounting rail（6）Connection；The vertical rotation axis（12）Lower sides pass through connecting plate（13）The linkage of foot rudder is installed
Bar（14）；The vertical rotation axis（12）, left-hand tread plate linkage brake axis（16）With right-hand tread plate linkage brake axis（17）End pacify
Equipped with potentiometer（15）；The left-hand tread plate linkage brake axis（16）With right-hand tread plate linkage brake axis（17）Equal close to end position
It is connected with bearing（18）.
2. a kind of flight simulator foot rudder linkage according to claim 1, it is characterised in that：The connecting plate（13）
End be also associated with damper rod（21）, and damper rod（21）Outer end on be provided with fixed seat（22）.
3. a kind of flight simulator foot rudder linkage according to claim 1, it is characterised in that：The left operating pedal
（4）With right operating pedal（5）Surface be uniformly provided with anti-skidding through hole（23）.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810104503.1A CN108109473A (en) | 2018-02-02 | 2018-02-02 | A kind of flight simulator foot rudder linkage |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810104503.1A CN108109473A (en) | 2018-02-02 | 2018-02-02 | A kind of flight simulator foot rudder linkage |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN108109473A true CN108109473A (en) | 2018-06-01 |
Family
ID=62221634
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201810104503.1A Pending CN108109473A (en) | 2018-02-02 | 2018-02-02 | A kind of flight simulator foot rudder linkage |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN108109473A (en) |
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108597296A (en) * | 2018-06-05 | 2018-09-28 | 珠海高斯科技有限公司 | The pedal manipulation device of flight simulator |
| CN109326170A (en) * | 2018-10-15 | 2019-02-12 | 中仿智能科技（上海）股份有限公司 | A kind of foot-operated simulator of aircraft |
| CN109407750A (en) * | 2018-12-27 | 2019-03-01 | 宁波慈溪小家电创新设计研究院有限公司 | A kind of foot rudder |
| CN109637263A (en) * | 2018-12-20 | 2019-04-16 | 天津中天翔翼航空科技有限公司 | Flight simulator pedal controller |
| CN112201114A (en) * | 2020-10-12 | 2021-01-08 | 浙江大学 | Big aircraft pedal analogue means based on rack and pinion motion |
| CN113700812A (en) * | 2021-08-25 | 2021-11-26 | 芜湖东旭光电装备技术有限公司 | Synchronous rotation centering device |
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| US4713007A (en) * | 1985-10-11 | 1987-12-15 | Alban Eugene P | Aircraft controls simulator |
| CN102137768A (en) * | 2008-07-28 | 2011-07-27 | 弗莱克健康理念股份有限公司 | Combined air, water and road vehicle |
| CN202189480U (en) * | 2011-07-28 | 2012-04-11 | 北京蓝天航空科技有限责任公司 | General simulation pedal |
| CN202887507U (en) * | 2012-11-14 | 2013-04-17 | 昆山航理机载设备有限公司 | Simulative operation device of aircraft |
| CN103303462A (en) * | 2012-03-09 | 2013-09-18 | 陕西飞机工业（集团）有限公司 | Vertical spindle foot control system |
| CN203753397U (en) * | 2013-12-09 | 2014-08-06 | 陕西飞机工业（集团）有限公司 | Foot manipulation mechanism |
| US20150375721A1 (en) * | 2014-06-26 | 2015-12-31 | Mando Corporation | Pedal simulator |
| CN206021648U (en) * | 2016-05-07 | 2017-03-15 | 福建科德电子科技有限公司 | A kind of flight simulator linkage pin rudder arrangement |
| CN206236311U (en) * | 2016-06-24 | 2017-06-09 | 上海源荀电子技术有限公司 | A kind of tangent flight pin rudder of axis |
| CN107074358A (en) * | 2014-05-07 | 2017-08-18 | Xti飞行器公司 | The aircraft of VTOL |
-
2018
- 2018-02-02 CN CN201810104503.1A patent/CN108109473A/en active Pending
Patent Citations (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4713007A (en) * | 1985-10-11 | 1987-12-15 | Alban Eugene P | Aircraft controls simulator |
| CN102137768A (en) * | 2008-07-28 | 2011-07-27 | 弗莱克健康理念股份有限公司 | Combined air, water and road vehicle |
| CN202189480U (en) * | 2011-07-28 | 2012-04-11 | 北京蓝天航空科技有限责任公司 | General simulation pedal |
| CN103303462A (en) * | 2012-03-09 | 2013-09-18 | 陕西飞机工业（集团）有限公司 | Vertical spindle foot control system |
| CN202887507U (en) * | 2012-11-14 | 2013-04-17 | 昆山航理机载设备有限公司 | Simulative operation device of aircraft |
| CN203753397U (en) * | 2013-12-09 | 2014-08-06 | 陕西飞机工业（集团）有限公司 | Foot manipulation mechanism |
| CN107074358A (en) * | 2014-05-07 | 2017-08-18 | Xti飞行器公司 | The aircraft of VTOL |
| US20150375721A1 (en) * | 2014-06-26 | 2015-12-31 | Mando Corporation | Pedal simulator |
| CN206021648U (en) * | 2016-05-07 | 2017-03-15 | 福建科德电子科技有限公司 | A kind of flight simulator linkage pin rudder arrangement |
| CN206236311U (en) * | 2016-06-24 | 2017-06-09 | 上海源荀电子技术有限公司 | A kind of tangent flight pin rudder of axis |
Cited By (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108597296A (en) * | 2018-06-05 | 2018-09-28 | 珠海高斯科技有限公司 | The pedal manipulation device of flight simulator |
| CN108597296B (en) * | 2018-06-05 | 2024-04-05 | 珠海高斯科技有限公司 | Pedal operating device of flight simulator |
| CN109326170A (en) * | 2018-10-15 | 2019-02-12 | 中仿智能科技（上海）股份有限公司 | A kind of foot-operated simulator of aircraft |
| CN109637263A (en) * | 2018-12-20 | 2019-04-16 | 天津中天翔翼航空科技有限公司 | Flight simulator pedal controller |
| CN109637263B (en) * | 2018-12-20 | 2024-01-26 | 天津中天翔翼航空科技有限公司 | Pedal controller of flight simulator |
| CN109407750A (en) * | 2018-12-27 | 2019-03-01 | 宁波慈溪小家电创新设计研究院有限公司 | A kind of foot rudder |
| CN112201114A (en) * | 2020-10-12 | 2021-01-08 | 浙江大学 | Big aircraft pedal analogue means based on rack and pinion motion |
| CN113700812A (en) * | 2021-08-25 | 2021-11-26 | 芜湖东旭光电装备技术有限公司 | Synchronous rotation centering device |
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