CN208706086U - 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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- CN208706086U CN208706086U CN201820263494.6U CN201820263494U CN208706086U CN 208706086 U CN208706086 U CN 208706086U CN 201820263494 U CN201820263494 U CN 201820263494U CN 208706086 U CN208706086 U CN 208706086U
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- 230000007246 mechanism Effects 0.000 claims abstract description 58
- 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 7
- 201000009482 yaws Diseases 0.000 claims description 7
- 230000001360 synchronised effect Effects 0.000 claims description 4
- 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
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- 238000012423 maintenance Methods 0.000 abstract description 2
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- 238000010586 diagram Methods 0.000 description 3
- 238000005516 engineering process Methods 0.000 description 2
- 230000007547 defect Effects 0.000 description 1
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Abstract
The utility model provides a kind of foot rudder arrangement for simulating big aircraft, including by left risers, the fixation 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 fixed bracket by mandrel, the yaw correction mechanism and braking mechanism are separately positioned on support bracket fastened both ends, yaw described in two returns middle strut setting between pedal gear and yaw correction mechanism, brake described in two is returned middle strut and is arranged between pedal gear and braking mechanism.The utility model is the simulation foot rudder arrangement similar with 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 operating simultaneously, save training time and cost, it is structurally reasonable, the degree of modularity is high, is beneficial for disassembly and assembly and Breakdown Maintenance.
Description
Technical field
The utility model belongs to flight simulator technical field, more particularly, to a kind of foot rudder arrangement for simulating big aircraft.
Background technique
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, there are also larger gaps with emulation.Cause the trainee of aircraft handling that cannot really realize very on ground
Machine, drop, the sense of reality of airflight, increase the technology and lead time of ground training with gradient of flying, therefore having must
Design it is a kind of can in terms of prototype dynamics, shape, speed and accuracy simulation foot similar with the foot rudder arrangement of prototype
Rudder arrangement obtains more prototype senses of reality to effectively increase aircraft handling trainee on ground, save the training time and at
This.
The effect of foot rudder is control 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
Summary of the invention
In view of this, the utility model is directed to a kind of foot rudder arrangement for simulating big aircraft, no matter foot rudder profile or
Mode of operation and dynamics and prototype height emulate, and are different from amusement device completely.Make the driving experience of trainee more close to
Prototype is the preferred device that ground training large aircraft drives the talent.
In order to achieve the above objectives, the technical solution of the utility model is achieved in that
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 fixed bracket by mandrel, and the yaw correction mechanism and braking mechanism are separately positioned on fixed bracket
Both ends, yaw described in two return in strut setting pedal gear and yaw correction mechanism between, 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 connect with one group of transmission component respectively, and transmission component described in every group includes foot pedal lever, the first pedal connector and
Two pedal connectors, the left-hand tread plate and right-hand tread plate by pedal turn round shaft successively with one end of foot pedal lever and first
One end of pedal connector is flexibly connected, and one end activity of the other end of the foot pedal lever and the second pedal connector connects
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 rods and yaw link mechanism, the yaw
Link mechanism 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 support frame, the described yaw driving gear and castellated plates have flank to be engaged, and the castellated plates are around being installed in support
One end of fixing axle rotary setting between frame and bottom plate, each yaw drive rod connects with each first pedal
The other end of fitting is flexibly connected, and the other end of drive rod and connecting without the activity of flank both ends for castellated plates are yawed described in two
It connects, the yaw driving gear and yaw potentiometer rotate coaxially and be arranged on bottom plate.
Further, the braking mechanism includes the strut gear being arranged in pairs, brake driving 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 respective brake driving gear, each brake drive gear respectively with a brake potentiometer
It rotates coaxially and is arranged on corresponding vertical plate, two strut gears both pass through mandrel setting, and two limited blocks are symmetrical
It is arranged on respective vertical plate, 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 support frame.
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 rods, equal one end of brake drive rod described in two and 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 the second support plate being fixed between left risers and right risers,
Angular convolution rotating plate and the second quarter-turn plate always, two quarter-turn plates pass through a fixing axle and the second support plate in right angle crook
It connects and forms cross, two right angles end of each quarter-turn plate is connecting pin, brake drive rod 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 first connecting rod of the amendment yawing rotation of foot rudder arrangement described in two groups of synchronization,
The first connecting rod both ends are flexibly connected with the attachment base being installed in castellated plates in foot rudder arrangement described in two groups respectively.
Further, described device further includes the second connecting rod of the brake movement of foot rudder arrangement described in two groups of synchronization, described
The second connecting rod two, two are arranged altogether described in the second connecting rod both ends respectively with two in foot rudder arrangement described in two groups
A quarter-turn plate is flexibly connected.
Compared with the existing technology, a kind of foot rudder arrangement for simulating big aircraft described in the utility model has the advantage that
A kind of foot rudder arrangement for simulating big aircraft described in the utility model, mainly there is following characteristics:
The first, it is emulated in the shape of foot rudder with the ratio of 1:1, embodies the operating space spaciousness characteristic of prototype, it is main
The characteristics of copilot respectively has enough motion spaces, embodies big aircraft；
The second, using module placement.Major-minor drives two sets of foot rudders, and the yaw and brake of every set foot rudder are applied equipped with complete
Power component (pedal gear, yaw correction mechanism, braking mechanism) He Huizhong power component (yaws back middle strut and support of braking back
Bar) and one module of self-contained, while two sets of foot rudders and tight association, so that entire mechanism is fused to a complete system, makes
Make to coordinate it is accurate, be beneficial for disassembly and assembly setting with Breakdown Maintenance；
Third, the setting for yawing back middle strut and the middle strut that brakes back can apply the pedal gear in operation corresponding
Resistance is equivalent to prototype pedal force, and simulation effect is good, and trainee is simulated to a greater extent when ground is practiced
Prototype operation；
4th, the setting of link mechanism, brake connecting rod mechanism and multiple connecting rods is yawed, guarantees 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.
Detailed description of the invention
The attached drawing for constituting a part of the utility model is used to provide a further understanding of the present invention, this is practical new
The illustrative embodiments and their description of type are not constituteed improper limits to the present invention for explaining the utility model.?
In attached drawing:
Fig. 1 is a kind of Structure explosion diagram of the foot rudder arrangement of the big aircraft of simulation described in the utility model embodiment；
Fig. 2 is a kind of structural schematic diagram of the foot rudder arrangement of the big aircraft of simulation described in the utility model embodiment；
Fig. 3 is to yaw linkage arrangement in a kind of foot rudder arrangement of the big aircraft of simulation described in the utility model embodiment
Schematic diagram；
Fig. 4 shows for a kind of foot rudder arrangement brake connecting rod mechanism structure of the big aircraft of simulation described in the utility model embodiment
It is intended to.
Description of symbols:
1- left risers, 2- strut gear, 3- the second pedal connector, 4- brake potentiometer, 5- attachment base, the first pedal of 6-
Connector, 7- brake driving gear, 8- limited block, 9- brake back middle strut；The first support plate of 10-；11- mandrel；12- joint shaft
It holds；13- left-hand tread plate；14- right-hand tread plate；15- right risers；16- brake connecting rod mechanism；The second support plate of 1601-；1602- first is straight
Angular convolution rotating plate；1603- the second quarter-turn plate；17- yaws link mechanism；1701- bottom plate；1702- support frame；1703- tooth form
Plate；18- yaws potentiometer；19- yaw driving gear；20- brake drive rod；21- yaws back middle strut；22- yaws drive rod；
23- pedal turns round shaft；24- foot pedal lever.
Specific embodiment
It should be noted that in the absence of conflict, the feature in the embodiments of the present invention and embodiment can
To be combined with each other.
The utility model will be described in detail below with reference to the accompanying drawings and 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
Fixation bracket that fishplate bar surrounds, pedal gear, yaw correction mechanism, braking mechanism, two yaw back middle strut 21 and two are stopped
Che Huizhong strut 9, the pedal gear are arranged on fixed bracket by mandrel 11, the yaw correction mechanism and brake
Mechanism is separately positioned on support bracket fastened both ends, and yaw described in two returns the middle setting of strut 21 in pedal gear and yaw amendment
Between mechanism, brake described in two is returned middle strut 9 and is arranged between pedal gear and braking mechanism.
The pedal gear includes that 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 are stepped on
Plate 14 is connect with one group of transmission component respectively, and 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 shaft 23 successively with foot pedal lever 24
One end and one end of the first pedal connector 6 be flexibly connected, the other end of the foot pedal lever 24 connect with the second pedal
One end of part 3 is flexibly connected, and 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 rods 22 and yaw link mechanism 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 driving gear 19 and support frame 1702, the yaw driving gear 19 and castellated plates 1703 have flank to be engaged, institute
The castellated plates 1703 stated are around the fixing axle rotary setting being installed between support frame 1702 and bottom plate 1701, each yaw
One end of drive rod 22 is flexibly connected with the other end of each first pedal connector 6, the transmission of yaw described in two
The other end of bar 22 is flexibly connected with castellated plates 1703 without flank both ends, the yaw driving gear 19 and yaw potentiometer
18 rotate coaxially setting on bottom plate 1701.
The braking mechanism includes the strut gear 2 being arranged in pairs, brake driving 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 respectively brake driving gear 7, each brake drive gear 7 respectively with a brake potentiometer 4
It rotates coaxially and is arranged on corresponding vertical plate, two strut gears 2 both pass through the setting of mandrel 11, two limited blocks 8
It is symmetricly set on respective vertical plate, the non-gear end of each strut gear 2 passes through respective limited block 8.
Each described one end for yawing back middle strut 21 is fixedly connected with the other end of respective first pedal connector 6,
Each other end for yawing back middle strut 21 is fixedly connected with support frame 1702.
It is each it is described brake back in one end of strut 9 be fixedly connected with respective strut gear 2, it is 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 vertical plate 15.
Described device further includes two brake drive rods 20, equal one end of brake drive rod 20 described in two and respective strut
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
Angular convolution rotating plate 1602 and the second quarter-turn plate 1603 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 rod 20 is flexibly connected with two connecting pins of the left and right directions of two quarter-turn plates.
Described device further includes the first connecting rod of the amendment yawing rotation of foot rudder arrangement described in synchronous two groups, and described first
Connecting rod both ends are flexibly connected with the attachment base 5 being installed in castellated plates 1703 in foot rudder arrangement described in two groups respectively.
Described device further includes the second connecting rod of the brake movement of foot rudder arrangement described in two groups of synchronization, second connection
Bar two, two are arranged altogether described in the second connecting rod both ends 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 limit 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 rods 22 and castellated plates 1703 by oscillating bearing 12.
The operating principle of the present apparatus is:
1, yaw amendment: when aircraft occurs to when left drift, preceding right-hand tread plate 14 of pedaling drives the first pedal connector 6, passes through
Yaw drive rod 22 drives castellated plates 1703 to rotate counterclockwise, since castellated plates 1703 are engaged with yaw driving gear 19, thus
Yaw driving gear 19 is driven to rotate clockwise, since yaw driving 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
Analog machine display amendment left drift state after computer disposal.It is associated with together since left and right pedal symmetrically passes through yaw drive rod 22
On one yaw boat driving 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；
2, it brakes: when making ground taxi after aircraft landing, to make aircraft 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 movement around pedal revolution shaft 23, then drive connected to it
Foot pedal lever 24 simultaneously, do rotary motion in the same direction, while driving strut gear 2 to do revolution fortune by the second pedal connector 3
Dynamic, so that 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 revocation of the external force of two feet, under strut 9 acts in braking back, braking state is released；
In addition to this, the angle of control left and right foot rudder revolution can also play a role when aircraft floor is turned.
Major-minor drives two sets of foot rudders and is connected with yaw link mechanism 17 by connecting rod (not shown) by brake connecting rod mechanism 16,
Guarantee that two sets of corresponding mechanisms are synchronous.
The above is only the preferred embodiment of the utility model only, is not intended to limit the utility model, all at this
Within the spirit and principle of utility model, any modification, equivalent replacement, improvement and so on should be included in the utility model
Protection scope within.
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
Fixation 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 fixed bracket by mandrel (11), the yaw correction mechanism
Be separately positioned on support bracket fastened both ends with braking mechanism, yaw described in two return in strut (21) setting in pedal gear and
It yaws between correction mechanism, brake described in two is returned middle strut (9) and is arranged between pedal gear and braking mechanism.
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, transmission component described in every group include that foot pedal lever (24), the first pedal connector (6) are connected with the second pedal
Part (3), the left-hand tread plate (13) and right-hand tread plate (14) by pedal revolution shaft (23) successively with foot pedal lever (24)
One end and one end of the first pedal connector (6) are flexibly connected, and the other end of the foot pedal lever (24) and the second pedal connect
One end of fitting (3) is flexibly connected, and the other end of the first pedal connector (6) is 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 2, it is characterised in that: the yaw correction mechanism
Including two yaw drive rods (22) and yaw link mechanism (17), the yaw link mechanism (17) includes being fixed on left stand
Bottom plate (1701) between plate (1) and right risers (15), the yaw driving gear for being separately positioned on bottom plate (1701) front and rear sides
(19) and support frame (1702), yaw driving gear (19) and castellated plates (1703) has flank to be engaged, described
Castellated plates (1703) around the fixing axle rotary setting being installed between support frame (1702) and bottom plate (1701), it is each described
One end of yaw drive rod (22) is flexibly connected with the other end of each first pedal connector (6), described in two
The other end of drive rod (22) and being flexibly connected without flank both ends for castellated plates (1703) are yawed, the yaw drives gear
(19) it rotates coaxially and is 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 driving 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 respective brake driving gear (7), each brake driving gear (7) is coaxial with a brake potentiometer (4) respectively
It rotates and is arranged on corresponding vertical plate, two strut gears (2) both pass through mandrel (11) setting, two limited blocks
(8) it is symmetricly set on respective vertical plate, 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: each described to yaw back
One end of strut (21) is fixedly connected with the other end of respective first pedal connector (6), it is each it is described yaw back in strut
(21) the other end is fixedly connected with support frame (1702).
6. a kind of foot rudder arrangement for simulating big aircraft according to claim 5, it is characterised in that: each described to brake back
One end of strut (9) is fixedly connected with respective strut gear (2), it is each it is described brake back in strut (9) the other end 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 rod (20), the one end of brake drive rod (20) 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
It (16) include the second support plate (1601) being fixed between left risers (1) and right risers (15), the first quarter-turn plate
(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) it connects and forms cross, two right angles end of each quarter-turn plate is connecting pin, and 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
Set further include the amendment yawing rotation of foot rudder arrangement described in synchronous two groups first connecting rod, the first connecting rod both ends difference
It is flexibly connected with the attachment base (5) being installed on 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 the brake movement of foot rudder arrangement described in two groups synchronous, second connecting rod are arranged two, described in two altogether
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 |
|---|---|---|---|
| CN201820263494.6U CN208706086U (en) | 2018-02-23 | 2018-02-23 | A kind of foot rudder arrangement for simulating big aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820263494.6U CN208706086U (en) | 2018-02-23 | 2018-02-23 | A kind of foot rudder arrangement for simulating big aircraft |
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| Publication Number | Publication Date |
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| CN208706086U true CN208706086U (en) | 2019-04-05 |
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| CN201820263494.6U Active CN208706086U (en) | 2018-02-23 | 2018-02-23 | A kind of foot rudder arrangement for simulating big aircraft |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108109474A (en) * | 2018-02-23 | 2018-06-01 | 哈尔滨莱特兄弟飞行技术有限公司 | A kind of foot rudder arrangement for simulating big aircraft |
-
2018
- 2018-02-23 CN CN201820263494.6U patent/CN208706086U/en active Active
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108109474A (en) * | 2018-02-23 | 2018-06-01 | 哈尔滨莱特兄弟飞行技术有限公司 | A kind of foot rudder arrangement for simulating big aircraft |
| CN108109474B (en) * | 2018-02-23 | 2024-03-19 | 哈尔滨莱特兄弟科技开发有限公司 | Foot rudder device for simulating large aircraft |
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