CN108109474A - A kind of foot rudder arrangement for simulating big aircraft - Google Patents
A kind of foot rudder arrangement for simulating big aircraft Download PDFInfo
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- CN108109474A CN108109474A CN201810154870.2A CN201810154870A CN108109474A CN 108109474 A CN108109474 A CN 108109474A CN 201810154870 A CN201810154870 A CN 201810154870A CN 108109474 A CN108109474 A CN 108109474A
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- 230000007246 mechanism Effects 0.000 claims abstract description 50
- 238000012937 correction Methods 0.000 claims abstract description 18
- 238000004088 simulation Methods 0.000 claims abstract description 8
- 230000005540 biological transmission Effects 0.000 claims description 9
- 230000033001 locomotion Effects 0.000 claims description 6
- 230000001360 synchronised effect Effects 0.000 claims description 3
- 241001347978 Major minor Species 0.000 abstract description 5
- 238000012549 training Methods 0.000 abstract description 5
- 230000009286 beneficial effect Effects 0.000 abstract description 2
- 230000015556 catabolic process Effects 0.000 abstract description 2
- 238000012423 maintenance Methods 0.000 abstract description 2
- 201000009482 yaws Diseases 0.000 description 6
- 230000000694 effects Effects 0.000 description 5
- 238000010586 diagram Methods 0.000 description 2
- 238000005516 engineering process Methods 0.000 description 2
- 230000009471 action Effects 0.000 description 1
- 230000008901 benefit Effects 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
- 238000013461 design Methods 0.000 description 1
- 239000000686 essence Substances 0.000 description 1
- 238000004880 explosion Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
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Classifications
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- 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
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- 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
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- Aviation & Aerospace Engineering (AREA)
- Business, Economics & Management (AREA)
- Physics & Mathematics (AREA)
- Educational Administration (AREA)
- Educational Technology (AREA)
- General Physics & Mathematics (AREA)
- Braking Elements And Transmission Devices (AREA)
Abstract
The present invention provides a kind of foot rudder arrangements for simulating big aircraft, including by left risers, the fixing bracket that right risers and two connecting plates surround, pedal gear, yaw correction mechanism, braking mechanism, two yaw back middle strut and two middle struts that brake back, the pedal gear is arranged on by mandrel on fixing bracket, the yaw correction mechanism and braking mechanism are separately positioned on support bracket fastened both ends, strut is arranged between pedal gear and yaw correction mechanism during yaw described in two is returned, strut is arranged between pedal gear and braking mechanism during brake described in two is returned.The present invention is simulation foot rudder arrangement that can be similar to the foot rudder arrangement of prototype in terms of prototype dynamics, shape, speed and accuracy, aircraft handling trainee can be effectively increased and obtain more prototype senses of reality on ground, also it can realize that major-minor drives while operates simultaneously, save training time and cost, it is rational in infrastructure, the degree of modularity is high, is beneficial for disassembly and assembly and Breakdown Maintenance.
Description
Technical field
The invention belongs to flight simulator technical field, more particularly, to a kind of foot rudder arrangement for simulating big aircraft.
Background technology
For current domestic flight simulator field, belong to the starting stage, it is low that most of simulator belongs to profiling foreign countries
The similar product stage is held, also has larger gap with emulation.The trainee for causing aircraft handling cannot really realize very on ground
Machine rises, drop, the sense of reality of airflight, increases ground training and the fly technology and lead time of gradient, therefore have must
Design a kind of simulation foot that can be similar to the foot rudder arrangement of prototype in terms of prototype dynamics, shape, speed and accuracy
Rudder arrangement obtains more prototype senses of reality to be effectively increased aircraft handling trainee on ground, save the training time and into
This.
The effect of foot rudder is control direction rudder (rudder is steerable airfoil portion in vertical tail), and effect is pair
Aircraft carries out yaw control, brake, ground small range Nose Wheel Steering, mainly should be in terrestrial operation
The content of the invention
In view of this, the present invention is directed to propose a kind of foot rudder arrangement for simulating big aircraft, no matter foot rudder profile or operate
Mode and dynamics are emulated with prototype height, are different from amusement device completely.Make the driving experience of trainee more close to prototype,
It is the preferred device that ground training large aircraft drives the talent.
In order to achieve the above objectives, the technical proposal of the invention is realized in this way：
A kind of foot rudder arrangement for simulating big aircraft, including the fixed branch surrounded by left risers, right risers and two connecting plates
Frame, pedal gear, yaw correction mechanism, braking mechanism, two yaw back middle strut and two middle struts that brake back, described steps on
Trigger structure is arranged on by mandrel on fixing bracket, and the yaw correction mechanism and braking mechanism are separately positioned on fixing bracket
Both ends, strut is arranged between pedal gear and yaw correction mechanism during yaw described in two is returned, the brake described in two
Strut is arranged between pedal gear and braking mechanism in returning.
Further, the pedal gear includes left-hand tread plate, right-hand tread plate and two groups of transmission components, the left-hand tread plate and the right side
Pedal is connected respectively with one group of transmission component, and the transmission component described in every group includes foot pedal lever, the first pedal connector and the
Two pedal connectors, the left-hand tread plate and right-hand tread plate by pedal turn round axostylus axostyle successively with one end of foot pedal lever and first
One end activity of one end flexible connection of pedal connector, the other end of the foot pedal lever and the second pedal connector is even
It connects, the other end of the first pedal connector is flexibly connected with yaw correction mechanism, the second pedal connector
The other end is flexibly connected with braking mechanism.
Further, the yaw correction mechanism includes two yaw drive links and yaw linkage, the yaw
Linkage includes the bottom plate being fixed between left risers and right risers, the yaw sliding tooth for being separately positioned on bottom plate front and rear sides
Wheel and supporting rack, the yaw drive gear and castellated plates have flank engagement to set, and the castellated plates are around being installed in support
Fixing axle rotary setting between frame and bottom plate, one end of each yaw drive link connect with each first pedal
The other end flexible connection of fitting, the other end of the yaw drive link described in two and connecting without the activity of flank both ends for castellated plates
It connects, the yaw drive gear is rotated coaxially with yaw potentiometer and is arranged on bottom plate.
Further, the braking mechanism includes the strut gear being arranged in pairs, brake drive gear and limited block, each
The non-gear end of the strut gear is flexibly connected with the other end of each second pedal connector, each branch
The gear end of bar gear engage with each brake drive gear, it is each it is described brake drive gear respectively with a brake potentiometer
It rotates coaxially and is arranged on corresponding riser, two strut gears both pass through mandrel setting, and two limited blocks are symmetrical
It is arranged on respective riser, the non-gear end of each strut gear passes through respective limited block.
Further, the other end of each described one end for yawing back middle strut with respective first pedal connector is fixed
Connection, each other end for yawing back middle strut are fixedly connected with supporting rack.
Further, each described one end for braking back middle strut is fixedly connected with respective strut gear, each described
The other end of strut is fixedly connected with the first support plate in braking back, first support plate be fixed at left risers and
Between right risers.
Further, described device further includes two brake drive links, equal one end of brake drive link described in two with it is each
It is flexibly connected from strut gear, the other end is flexibly connected with brake connecting rod mechanism.
Further, the brake connecting rod mechanism includes being fixed on the second support plate between left risers and right risers, the
Angular convolution flap and the second quarter-turn plate, two quarter-turn plates pass through a fixing axle and the second support plate in right angle crook always
It connects and forms cross, two right angles end of each quarter-turn plate is connecting pin, the brake drive link described in two
The other end is flexibly connected with two connecting pins of the left and right directions of two quarter-turn plates.
Further, described device further includes the head rod that synchronously foot rudder arrangement described in two groups corrects yawing rotation,
The head rod both ends are flexibly connected respectively with the connecting seat being installed in castellated plates in foot rudder arrangement described in two groups.
Further, described device further includes the second connecting rod of synchronously foot rudder arrangement brake movement described in two groups, described
The second connecting rod set two altogether, the both ends of the second connecting rod described in two respectively with two in foot rudder arrangement described in two groups
A quarter-turn plate flexible connection.
Compared with the prior art, a kind of foot rudder arrangement for simulating big aircraft of the present invention has the advantage that：
A kind of foot rudder arrangement for simulating big aircraft of the present invention, mainly there is following characteristics：
Firstth, with 1 in the shape of foot rudder：1 ratio is emulated, and embodies the operating space spaciousness characteristic of prototype, main
Copilot respectively has enough motion spaces, the characteristics of embodying big aircraft；
Secondth, using module placement.Major-minor drives two sets of foot rudders, often covers the yaw and brake of foot rudder, is applied equipped with complete
Power component (pedal gear, yaw correction mechanism, braking mechanism) and time middle power component (yaw back middle strut and support of braking back
Bar) and one module of self-contained, while two sets of foot rudders and tight association, entire mechanism is made to be fused to a complete system, is made
Make to coordinate it is accurate, be beneficial for disassembly and assembly setting with Breakdown Maintenance；
3rd, the setting of strut and the middle strut that brakes back in yawing back, can apply the pedal gear in operation corresponding
Resistance, is equivalent to prototype pedal force, and analog simulation effect is good so that trainee can simulate to a greater extent when ground is practiced
Prototype is run；
4th, the setting of linkage, brake connecting rod mechanism and multiple connecting rods is yawed, ensures that major-minor drives two sets of foot rudders
High level of synchronization effectively makes up major-minor cockpit other side's operation error defect, is particularly easy to training teaching.
Description of the drawings
The attached drawing for forming the part of the present invention is used for providing a further understanding of the present invention, schematic reality of the invention
Example and its explanation are applied for explaining the present invention, is not constituted improper limitations of the present invention.In the accompanying drawings：
Fig. 1 is a kind of Structure explosion diagram of the foot rudder arrangement of the big aircraft of simulation described in the embodiment of the present invention；
Fig. 2 is a kind of structure diagram of the foot rudder arrangement of the big aircraft of simulation described in the embodiment of the present invention；
Fig. 3 is that linkage arrangement signal is yawed in a kind of foot rudder arrangement of the big aircraft of simulation described in the embodiment of the present invention
Figure；
Fig. 4 is a kind of foot rudder arrangement brake connecting rod mechanism structure signal of the big aircraft of simulation described in the embodiment of the present invention
Figure.
Reference sign：
1- left risers, 2- strut gears, 3- the second pedal connectors, 4- brake potentiometers, 5- connecting seats, the first pedals of 6-
Connector, 7- brake drive gears, 8- limited blocks, 9- brake back middle strut；The first support plates of 10-；11- mandrels；12- joint shafts
It holds；13- left-hand tread plates；14- right-hand tread plates；15- right risers；16- brake connecting rods mechanism；The second support plates of 1601-；1602- first is straight
Angular convolution flap；1603- the second quarter-turn plates；17- yaws linkage；1701- bottom plates；1702- supporting racks；1703- tooth forms
Plate；18- yaws potentiometer；19- yaws drive gear；20- brake drive links；21- yaws back middle strut；22- yaws drive link；
23- pedals turn round axostylus axostyle；24- foot pedal levers.
Specific embodiment
It should be noted that in the case where there is no conflict, the feature in embodiment and embodiment in the present invention can phase
Mutually combination.
The present invention will be described in detail below with reference to the accompanying drawings and in conjunction with the embodiments.
As Figure 1-Figure 4, a kind of foot rudder arrangement for simulating big aircraft, including by left risers 1, right risers 15 and two companies
Fixing bracket that fishplate bar surrounds, pedal gear, yaw correction mechanism, braking mechanism, two yaw back middle strut 21 and two are stopped
Strut 9 during vehicle returns, the pedal gear are arranged on by mandrel 11 on fixing bracket, the yaw correction mechanism and brake
Mechanism is separately positioned on support bracket fastened both ends, and strut 21 is arranged on pedal gear during the yaw described in two is returned and yaw is corrected
Between mechanism, strut 9 is arranged between pedal gear and braking mechanism during the brake described in two is returned.
The pedal gear includes left-hand tread plate 13, right-hand tread plate 14 and two groups of transmission components, the left-hand tread plate 13 and the right side and steps on
Plate 14 is connected respectively with one group of transmission component, and the transmission component described in every group includes foot pedal lever 24,6 and of the first pedal connector
Second pedal connector 3, the left-hand tread plate 13 and right-hand tread plate 14 by pedal turn round axostylus axostyle 23 successively with foot pedal lever 24
One end and the first pedal connector 6 one end flexible connection, the other end of the foot pedal lever 24 is connected with the second pedal
One end flexible connection of part 3, the other end of the first pedal connector 6 is flexibly connected with yaw correction mechanism, described
The other end of second pedal connector 3 is flexibly connected with braking mechanism.
The yaw correction mechanism includes two yaw drive links 22 and yaw linkage 17, the yaw connecting rod machine
Structure 17 includes the bottom plate 1701 being fixed between left risers 1 and right risers 15, is separately positioned on the inclined of 1701 front and rear sides of bottom plate
Boat drive gear 19 and supporting rack 1702, the yaw drive gear 19 and castellated plates 1703 have flank engagement to set, institute
The castellated plates 1703 stated are around the fixing axle rotary setting being installed between supporting rack 1702 and bottom plate 1701, each yaw
The other end of the one end of drive link 22 with each first pedal connector 6 is flexibly connected, the yaw transmission described in two
The other end of bar 22 is flexibly connected with castellated plates 1703 without flank both ends, the yaw drive gear 19 and yaw potentiometer
18 rotate coaxially and are arranged on bottom plate 1701.
The braking mechanism includes the strut gear 2 being arranged in pairs, brake drive gear 7 and limited block 8, each described
The non-gear end of strut gear 2 is flexibly connected with the other end of each second pedal connector 3, each strut tooth
The gear end of wheel 2 is engaged with each brake drive gear 7, it is each it is described brake drive gear 7 respectively with a brake potentiometer 4
It rotates coaxially and is arranged on corresponding riser, two strut gears 2 both pass through mandrel 11 and set, two limited blocks 8
It is symmetricly set on respective riser, the non-gear end of each strut gear 2 passes through respective limited block 8.
The other end of each described one end for yawing back middle strut 21 with respective first pedal connector 6 is fixedly connected,
Each other end for yawing back middle strut 21 is fixedly connected with supporting rack 1702.
Each described one end for brake back middle strut 9 is fixedly connected with respective strut gear 2, each described to brake back
The other end of strut 9 is fixedly connected with the first support plate 10, and first support plate 10 is fixed at left risers 1 and the right side
Between riser 15.
Described device further includes two brake drive links 20,20 equal one end of brake drive link and respective strut described in two
Gear 2 is flexibly connected, and the other end is flexibly connected with brake connecting rod mechanism 16.
The brake connecting rod mechanism 16 includes being fixed on the second support plate 1601 between left risers 1 and right risers 15, the
1602 and second quarter-turn plate 1603 of angular convolution flap always, two quarter-turn plates pass through a fixing axle and the in right angle crook
Two support plates 1601 connect and form cross, and two right angles end of each quarter-turn plate is connecting pin, described in two
The other end of brake drive link 20 is flexibly connected with two connecting pins of the left and right directions of two quarter-turn plates.
Described device further includes the head rod that foot rudder arrangement described in synchronous two groups corrects yawing rotation, and described first
Connecting rod both ends are flexibly connected respectively with the connecting seat 5 being installed in castellated plates 1703 in foot rudder arrangement described in two groups.
Described device further includes the second connecting rod of synchronously foot rudder arrangement brake movement described in two groups, the described second connection
Bar sets two altogether, the both ends of the second connecting rod described in two respectively with two quarter-turns in foot rudder arrangement described in two groups
Plate is flexibly connected.
The connecting pin of two quarter-turn plates is designed with oscillating bearing 12, two the second connecting rods and two quarter-turn plates
Other two connecting pin connection.
The both ends of support frame as described above 1702 carry out /V to 1703 movement travel of castellated plates.
Several lightening holes are designed in the left risers 1 and right risers 15, the right risers 15 are worn equipped with connecting rod
Outlet.
It is connected between two yaw drive links 22 and castellated plates 1703 by oscillating bearing 12.
The operating principle of the present apparatus is：
1st, yaw is corrected：When aircraft occurs to during left drift, preceding right-hand tread plate 14 of pedaling drives the first pedal connector 6, passes through
Yaw drive link 22 drive castellated plates 1703 rotate counterclockwise, due to castellated plates 1703 with yaw drive gear 19 engage, thus
Yaw drive gear 19 is driven to rotate clockwise, since yaw drive gear 19 and yaw potentiometer 18 are coaxially disposed, so driving
Dynamic yaw 18 mandrel of potentiometer is rotated clockwise.At this time yaw potentiometer 18 to computer export an electric signal, then by
Left drift state is corrected in analog machine display after computer disposal.Since left and right pedal is symmetrically associated with together by yawing drive link 22
On one yaw boat drive gear 19, left-hand tread plate 13 is to driver side to recession at this time；When aircraft yaws to the right, then otherwise grasp
Make；
2nd, brake：When making ground taxi after aircraft landing, aircraft to be made to come to a complete stop as early as possible it is necessary to implementing brake to it.With
Tiptoe crawl left-hand tread plate 13, right-hand tread plate 14, pedal do revolution action around pedal revolution axostylus axostyle 23, then drive connected to it
Foot pedal lever 24 does rotary motion simultaneously, in the same direction, while by the second pedal connector 3 strut gear 2 is driven to do revolution and transported
Dynamic, so as to which 4 mandrel of driving brake potentiometer rotates, the potentiometer 4 that brakes at this time exports an electric signal, computer disposal to computer
Analog machine shows braking state afterwards.When the external force of two feet cancels, under strut 9 acts in braking back, braking state is released；
In addition, the angle of left and right foot rudder revolution is controlled, can also be played a role when aircraft floor is turned.
Major-minor drives two sets of foot rudders and is connected by brake connecting rod mechanism 16 with yaw linkage 17 by connecting rod (not shown),
Ensure that two sets of corresponding mechanisms are synchronous.
The foregoing is merely illustrative of the preferred embodiments of the present invention, is not intended to limit the invention, all essences in the present invention
With within principle, any modifications, equivalent replacements and improvements are made should all be included in the protection scope of the present invention god.
Claims (10)
1. a kind of foot rudder arrangement for simulating big aircraft, it is characterised in that：Including by left risers (1), right risers (15) and two companies
Fixing bracket that fishplate bar surrounds, pedal gear, yaw correction mechanism, braking mechanism, two yaw back middle strut (21) and two
Strut (9) in braking back, the pedal gear are arranged on by mandrel (11) on fixing bracket, the yaw correction mechanism
Be separately positioned on support bracket fastened both ends with braking mechanism, the yaw described in two return in strut (21) be arranged on pedal gear and
Between yawing correction mechanism, strut (9) is arranged between pedal gear and braking mechanism during the brake described in two is returned.
2. a kind of foot rudder arrangement for simulating big aircraft according to claim 1, it is characterised in that：The pedal gear includes
Left-hand tread plate (13), right-hand tread plate (14) and two groups of transmission components, the left-hand tread plate (13) and right-hand tread plate (14) respectively with one group of biography
Dynamic component connection, the transmission component described in every group includes foot pedal lever (24), the first pedal connector (6) is connected with the second pedal
Part (3), the left-hand tread plate (13) and right-hand tread plate (14) by pedal turn round axostylus axostyle (23) successively with foot pedal lever (24)
One end and the flexible connection of one end of the first pedal connector (6), the other end of the foot pedal lever (24) and the second pedal connect
One end flexible connection of fitting (3), the other end of the first pedal connector (6) are flexibly connected with yaw correction mechanism,
The other end of the second pedal connector (3) is flexibly connected with braking mechanism.
3. a kind of foot rudder arrangement for simulating big aircraft according to claim 3, it is characterised in that：The yaw correction mechanism
Including two yaw drive links (22) and yaw linkage (17), the yaw linkage (17) includes being fixed on left vertical
Bottom plate (1701) between plate (1) and right risers (15), the yaw drive gear for being separately positioned on bottom plate (1701) front and rear sides
(19) and supporting rack (1702), the yaw drive gear (19) and castellated plates (1703) has flank engagement to set, described
Castellated plates (1703) around the fixing axle rotary setting being installed between supporting rack (1702) and bottom plate (1701), it is each described
The other end of the one end of yaw drive link (22) with each first pedal connector (6) is flexibly connected, described in two
The other end of yaw drive link (22) is flexibly connected with castellated plates (1703) without flank both ends, the yaw drive gear
(19) rotate coaxially and be arranged on bottom plate (1701) with yaw potentiometer (18).
4. a kind of foot rudder arrangement for simulating big aircraft according to claim 3, it is characterised in that：The braking mechanism includes
Strut gear (2), brake drive gear (7) and the limited block (8) being arranged in pairs, the non-tooth of each strut gear (2)
Wheel end is flexibly connected with the other end of each second pedal connector (3), the gear end of each strut gear (2)
It is engaged with each brake drive gear (7), each brake drive gear (7) is coaxial with a brake potentiometer (4) respectively
It rotates and is arranged on corresponding riser, two strut gears (2) both pass through mandrel (11) setting, two limited blocks
(8) it is symmetricly set on respective riser, the non-gear end of each strut gear (2) passes through respective limited block (8).
5. a kind of foot rudder arrangement for simulating big aircraft according to claim 4, it is characterised in that：It is each described to yaw back
The other end of the one end of strut (21) with respective first pedal connector (6) is fixedly connected, each described to yaw back middle strut
(21) the other end is fixedly connected with supporting rack (1702).
6. a kind of foot rudder arrangement for simulating big aircraft according to claim 5, it is characterised in that：It is each described to brake back
One end of strut (9) is fixedly connected with respective strut gear (2), the other end of each middle strut (9) that brake back with
First support plate (10) is fixedly connected, first support plate (10) be fixed at left risers (1) and right risers (15) it
Between.
7. a kind of foot rudder arrangement for simulating big aircraft according to claim 6, it is characterised in that：Described device further includes two
A brake drive link (20), brake drive link (20) one end described in two is flexibly connected with respective strut gear (2), another
End is flexibly connected with brake connecting rod mechanism (16).
8. a kind of foot rudder arrangement for simulating big aircraft according to claim 7, it is characterised in that：The brake connecting rod mechanism
(16) the second support plate (1601), the first quarter-turn plate that are fixed between left risers (1) and right risers (15) are included
(1602) and the second quarter-turn plate (1603), two quarter-turn plates pass through a fixing axle and the second support plate in right angle crook
(1601) connect and form cross, two right angles end of each quarter-turn plate is connecting pin, and the brake described in two passes
The other end of lever (20) is flexibly connected with two connecting pins of the left and right directions of two quarter-turn plates.
9. a kind of foot rudder arrangement of the big aircraft of simulation according to any one of claim 3-7, it is characterised in that：The dress
It puts and further includes the head rod that synchronously foot rudder arrangement described in two groups corrects yawing rotation, head rod both ends difference
It is flexibly connected with the connecting seat (5) being installed in castellated plates (1703) in foot rudder arrangement described in two groups.
10. a kind of foot rudder arrangement for simulating big aircraft according to claim 9, it is characterised in that：Described device further includes
Second connecting rod of foot rudder arrangement brake movement, second connecting rod set two, described in two altogether described in two groups synchronous
The both ends of the second connecting rod be flexibly connected respectively with two quarter-turn plates in foot rudder arrangement described in two groups.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810154870.2A CN108109474B (en) | 2018-02-23 | 2018-02-23 | Foot rudder device for simulating large aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810154870.2A CN108109474B (en) | 2018-02-23 | 2018-02-23 | Foot rudder device for simulating large aircraft |
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| Publication Number | Publication Date |
|---|---|
| CN108109474A true CN108109474A (en) | 2018-06-01 |
| CN108109474B CN108109474B (en) | 2024-03-19 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201810154870.2A Active CN108109474B (en) | 2018-02-23 | 2018-02-23 | Foot rudder device for simulating large aircraft |
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| Country | Link |
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| CN (1) | CN108109474B (en) |
Cited By (3)
| 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 |
| 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 |
| CN110147107A (en) * | 2019-05-29 | 2019-08-20 | 南京拓兴智控科技有限公司 | Unmanned plane is sliding to run correction control method, device, unmanned plane and storage medium |
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| CN110147107A (en) * | 2019-05-29 | 2019-08-20 | 南京拓兴智控科技有限公司 | Unmanned plane is sliding to run correction control method, device, unmanned plane and storage medium |
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