CN108074435A - A kind of flight simulator duplex steering apparatus - Google Patents
A kind of flight simulator duplex steering apparatus Download PDFInfo
- Publication number
- CN108074435A CN108074435A CN201810104502.7A CN201810104502A CN108074435A CN 108074435 A CN108074435 A CN 108074435A CN 201810104502 A CN201810104502 A CN 201810104502A CN 108074435 A CN108074435 A CN 108074435A
- Authority
- CN
- China
- Prior art keywords
- pressure sensor
- flange seat
- electric cylinders
- control stick
- synchronous belt
- 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
- 230000001360 synchronised effect Effects 0.000 claims abstract description 23
- 230000005540 biological transmission Effects 0.000 claims abstract description 11
- 238000004804 winding Methods 0.000 claims abstract description 3
- 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 claims description 10
- 238000000034 method Methods 0.000 claims description 3
- 239000007787 solid Substances 0.000 claims 1
- 230000000694 effects Effects 0.000 abstract description 9
- 238000004088 simulation Methods 0.000 abstract description 6
- 238000009434 installation Methods 0.000 abstract description 4
- 238000012423 maintenance Methods 0.000 abstract description 3
- 238000013016 damping Methods 0.000 description 2
- RZVHIXYEVGDQDX-UHFFFAOYSA-N 9,10-anthraquinone Chemical compound C1=CC=C2C(=O)C3=CC=CC=C3C(=O)C2=C1 RZVHIXYEVGDQDX-UHFFFAOYSA-N 0.000 description 1
- 230000007812 deficiency Effects 0.000 description 1
- 238000013461 design Methods 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 238000012549 training Methods 0.000 description 1
- 238000012546 transfer Methods 0.000 description 1
- 230000009466 transformation Effects 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
- G09B9/12—Motion systems for aircraft simulators
-
- 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
-
- 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
Abstract
The present invention relates to a kind of flight simulator duplex steering apparatus, handle joint is both provided at the top of left and right operation lever；Vertical flange seat transverse flange seat is respectively connected in left and right operation lever；Vertical flange seat lower end is mounted on synchronizing wheel；Winding is equipped with synchronous belt between synchronizing wheel；Universal driving shaft is equipped with by bearing between transverse flange seat；The side of universal driving shaft is connected by transmission arm with the front end of the first pull pressure sensor；The rear end of first pull pressure sensor is connected with longitudinal extension bar；Longitudinal extension bar is mounted in zigzag tread patterns electric cylinders；Transversal stretching bar is provided in laterally driven electric cylinders；The end of transversal stretching bar after the second pull pressure sensor by being connected with sliding block；The front end of sliding block is also mounted on by clamping plate clamping on synchronous belt.The present invention be capable of providing a kind of simple in structure, convenient for installation and maintenance, transmission and simulation effect be good and control stick dynamics can dynamic change flight simulator duplex steering apparatus.
Description
Technical field
The present invention relates to flight simulation machinery technical fields more particularly to a kind of flight simulator duplex handling maneuver to fill
It puts.
Background technology
Flight simulator duplex steerable system is driven for simulating the control stick of aircraft, is realized the linkage of control stick and is moved
State load controls, and pitching and the handling maneuver of aircraft are controlled in simulated flight.The control stick of aircraft is pilot manipulation aircraft
Important medium, pilot changes the state of flight of aircraft by control stick.It mushes, pushes away when pilot draws control stick
Aircraft declines during control stick, and aircraft turns to during swivel lever.Flight simulator will realize the function of control stick, and simulation is really driven
Manipulation experience when sailing.In flight simulator, the control stick of positive co-pilot is linkage, and two control sticks send identical
Flight directive.The linkage of control stick is divided into the linkage on front and rear push-and-pull direction and the linkage in left rotation and right rotation direction.Usually using bullet
Spring or damping spring connection linkage structure and frame, to simulate the resistance of yoke, and realize the reset of control stick.But
During practical flight, the resistance on flight control bar can constantly change with the change of state of flight.Using spring without
Method embodies the dynamic change of resistance exactly, can not also simulate the Function for Automatic Pilot of aircraft.
The content of the invention
A kind of simple in structure, convenient for installation and maintenance, biography is provided the invention aims to overcome the deficiencies in the prior art
Dynamic and simulation effect is good and control stick dynamics can dynamic change flight simulator duplex steering apparatus.
In order to achieve the above objectives, present invention employs following technical solutions.
A kind of flight simulator duplex steering apparatus, including left control stick, right control stick, handle joint, rotation axis,
It is vertical flange seat, transverse flange seat, synchronizing wheel, synchronous belt, universal driving shaft, bearing, transmission arm, the first pull pressure sensor, vertical
To telescopic rod, zigzag tread patterns electric cylinders, fixed pedestal, laterally driven electric cylinders, transversal stretching bar, the second pull pressure sensor, guiding
Bar, sliding block and clamping plate are both provided with handle joint at the top of the left control stick and right operation lever；The left control stick and right behaviour
The bottom for making bar is connected with vertical flange seat by rotation axis；The left control stick and right operation lever are close to the side of lower part
It has been fixedly connected with transverse flange seat；The vertical flange seat lower end is mounted on synchronizing wheel；Peace is wound between the synchronizing wheel
Equipped with synchronous belt；Universal driving shaft is equipped with by bearing between the transverse flange seat；The side of the universal driving shaft passes through transmission
Arm is connected with the front end of the first pull pressure sensor；The rear end of first pull pressure sensor is connected with longitudinal extension bar；Institute
Longitudinal extension bar is stated in zigzag tread patterns electric cylinders；With being equipped in the synchronous belt parallel direction by fixed pedestal
Laterally driven electric cylinders；Transversal stretching bar is provided in the laterally driven electric cylinders；The end of the transversal stretching bar passes through second
Sliding block is connected with after pull pressure sensor；The guiding parallel with the transversal stretching bar is additionally provided in front of the fixed pedestal
Bar；The guide rod passes through the through hole of sliding block side；The front end of the sliding block is also mounted on the synchronous skin by clamping plate clamping
It takes.
As a further improvement on the present invention, also it is socketed with protection safety cover in the left control stick and right operation lever.
As a further improvement on the present invention, set on the medial surface of the periphery of the synchronizing wheel and the synchronous belt
There is the driving cog for being mutually matched occlusion.
The advantageous effects having due to the utilization of above-mentioned technical proposal, the present invention：Technical scheme uses
Left and right operation lever, and universal driving shaft is provided with by bearing and transverse flange seat between them, have and facilitate two operations of realization
The advantageous effects of the real-time synchronization of the push pull maneuver of bar；The technical program is also provided with together in the bottom of left or right operation lever
Step wheel, and be connected between two synchronizing wheels using synchronous belt, the rotation of two operation levers can be realized by synchronous belt
The synchronization of action has the advantageous effects that design is reasonable, rotation synchronous effect is good and convenient for installation and maintenance；The technical program
Longitudinal extension bar and zigzag tread patterns electric cylinders are connected with by transmission arm on universal driving shaft, has and is provided when can be swung to universal driving shaft
Need feedback force, the body-sensing of closer practical flight operation lever, the advantageous effects of promotion simulated operation real experiences；This skill
Art scheme also uses and sliding block is installed on synchronous belt, and is equipped with guide rod, transversal stretching bar and laterally driven electric cylinders,
It thus can be by the way that sliding block and transversal stretching bar, the movement real-time delivery of synchronous belt being realized, laterally driven electric cylinders can root
Corresponding resistance is provided according to different scenes, there are the advantageous effects for improving simulation validity, expanding the scene scope of application；This
Technical solution also by being both provided with pull pressure sensor in the end of lateral control column and longitudinal operation lever, can so pass through
Sensor gathers the push-and-pull of simulated operator and rotational steps parameter information, such as passes it to the control system of simulator and matches somebody with somebody
Hardware device device is covered, can not only realize that the damping feedback force of different scenes is adjusted, can also realize and simulated training person is grasped
It judges and gives a mark and be alternatively arranged as the Transfer Parameters basis for realizing simulation automatic Pilot.
Description of the drawings
Technical solution of the present invention is described further below in conjunction with the accompanying drawings.
Accompanying drawing 1 is the structural representation of the present invention.
In figure：1. left control stick；2. right control stick；3. handle joint；4. rotation axis；5. vertical flange seat；6. horizontal method
Blue seat；7. synchronizing wheel；8. synchronous belt；9. universal driving shaft；10. bearing；11. transmission arm；12. the first pull pressure sensor；It is 13. vertical
To telescopic rod；14. zigzag tread patterns electric cylinders；15. fixed pedestal；16. laterally driven electric cylinders；17. transversal stretching bar；18. second draws
Pressure sensor；19. guide rod；20. sliding block；21. clamping plate；22. protection safety cover；23. driving cog.
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 duplex steering apparatus of the present invention as shown in Figure 1, including left control stick
1st, right control stick 2, handle joint 3, rotation axis 4, vertical flange seat 5, transverse flange seat 6, synchronizing wheel 7, synchronous belt 8, linkage
Axis 9, bearing 10, transmission arm 11, the first pull pressure sensor 12, longitudinal extension bar 13, zigzag tread patterns electric cylinders 14, fixed pedestal
15th, laterally driven electric cylinders 16, transversal stretching bar 17, the second pull pressure sensor 18, guide rod 19, sliding block 20, clamping plate 21, protection
The top of safety guard 22 and driving cog 23, the left control stick 7 and right operation lever 8 is both provided with handle joint 3；The left manipulation
The bottom of bar 7 and right operation lever 8 is connected with vertical flange seat 5 by rotation axis 4；The left control stick 7 and right operation lever 8 exist
Transverse flange seat 6 has been fixedly connected with close to the side of lower part；5 lower end of vertical flange seat is mounted on synchronizing wheel 7；It is described
Winding is equipped with synchronous belt 8 between synchronizing wheel 7；Universal driving shaft 9 is equipped with by bearing 10 between the transverse flange seat 6；Institute
The side for stating universal driving shaft 9 is connected by transmission arm 11 with the front end of the first pull pressure sensor 12；The first pressure sensing
The rear end of device 12 is connected with longitudinal extension bar 13；The longitudinal extension bar 13 is mounted in zigzag tread patterns electric cylinders 14；With it is described
Laterally driven electric cylinders 16 are equipped with by fixed pedestal 15 in 8 parallel direction of synchronous belt；It is set in the laterally driven electric cylinders 16
It is equipped with transversal stretching bar 17；The end of the transversal stretching bar 17 after the second pull pressure sensor 18 by being connected with sliding block 20；
15 front of fixed pedestal is additionally provided with the guide rod 19 parallel with the transversal stretching bar 17；The guide rod 19 passes through
The through hole of 20 side of sliding block；The front end of the sliding block 20 is also mounted on by the clamping of clamping plate 21 on the synchronous belt 8；The left side
Protection safety cover 22 is also socketed in control stick 7 and right operation lever 8；The periphery of the synchronizing wheel 7 and the synchronous belt 8
The driving cog 23 for being mutually matched occlusion is provided on medial surface.
The technical program realizes the linkage of two control sticks using universal driving shaft and synchronizing wheel, and transmission effect is good, simple in structure,
Facilitate installation, safeguard；Using motor is controlled, the steering force of dynamic change is provided to control stick, driving experience is truer, simultaneously
It can also realize automatic Pilot；Electric cylinders service life is long, substantially increases the reliability and service life of flight simulator.
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 duplex steering apparatus, it is characterised in that：Including left control stick（1）, right control stick（2）、
Handle joint（3）, rotation axis（4）, vertical flange seat（5）, transverse flange seat（6）, synchronizing wheel（7）, synchronous belt（8）, linkage
Axis（9）, bearing（10）, transmission arm（11）, the first pull pressure sensor（12）, longitudinal extension bar（13）, zigzag tread patterns electric cylinders
（14）, fixed pedestal（15）, laterally driven electric cylinders（16）, transversal stretching bar（17）, the second pull pressure sensor（18）, guide rod
（19）, sliding block（20）And clamping plate（21）, the left control stick（7）With right operation lever（8）Top be both provided with handle joint
（3）；The left control stick（7）With right operation lever（8）Bottom pass through rotation axis（4）It is connected with vertical flange seat（5）；It is described
Left control stick（7）With right operation lever（8）Transverse flange seat has been fixedly connected in the side close to lower part（6）；The vertical method
Blue seat（5）Lower end is mounted on synchronizing wheel（7）；The synchronizing wheel（7）Between winding synchronous belt is installed（8）；The transverse direction
Flange seat（6）Between pass through bearing（10）Universal driving shaft is installed（9）；The universal driving shaft（9）Side pass through transmission arm（11）With
First pull pressure sensor（12）Front end be connected；First pull pressure sensor（12）Rear end be connected with longitudinal extension bar
（13）；The longitudinal extension bar（13）Mounted on zigzag tread patterns electric cylinders（14）It is interior；With the synchronous belt（8）In parallel direction
Pass through fixed pedestal（15）Laterally driven electric cylinders are installed（16）；The laterally driven electric cylinders（16）On be provided with transversal stretching bar
（17）；The transversal stretching bar（17）End pass through the second pull pressure sensor（18）After be connected with sliding block（20）；It is described solid
Determine pedestal（15）Front is additionally provided with and the transversal stretching bar（17）Parallel guide rod（19）；The guide rod（19）It wears
Cross sliding block（20）The through hole of side；The sliding block（20）Front end also pass through clamping plate（21）Clamping is mounted on the synchronous belt
（8）On.
2. a kind of flight simulator duplex steering apparatus according to claim 1, it is characterised in that：The left manipulation
Bar（7）With right operation lever（8）On be also socketed with protection safety cover（22）.
3. a kind of flight simulator duplex steering apparatus according to claim 1, it is characterised in that：The synchronizing wheel
（7）Periphery and the synchronous belt（8）Medial surface on be provided with the driving cog for being mutually matched occlusion（23）.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810104502.7A CN108074435A (en) | 2018-02-02 | 2018-02-02 | A kind of flight simulator duplex steering apparatus |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810104502.7A CN108074435A (en) | 2018-02-02 | 2018-02-02 | A kind of flight simulator duplex steering apparatus |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN108074435A true CN108074435A (en) | 2018-05-25 |
Family
ID=62157036
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201810104502.7A Pending CN108074435A (en) | 2018-02-02 | 2018-02-02 | A kind of flight simulator duplex steering apparatus |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN108074435A (en) |
Citations (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB396378A (en) * | 1932-01-22 | 1933-07-24 | John Ronald Sturge Whiting | Apparatus for training air pilots on the ground, and providing the sensation of controlled flight for instructional and/or amusement purposes |
| EP0683743A1 (en) * | 1993-02-24 | 1995-11-29 | Altair Corporation | Control system for aircraft |
| CN202855112U (en) * | 2012-10-15 | 2013-04-03 | 昆山航理机载设备有限公司 | Motor-human sense simulation control system motor of helicopter |
| 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 |
| US20160252926A1 (en) * | 2013-10-15 | 2016-09-01 | Sagem Defense Securite | Flight control device for an aircraft |
| CN106205275A (en) * | 2016-07-12 | 2016-12-07 | 徐舒青 | The push-pull effort control system of aviation simulator control lever |
| CN106601070A (en) * | 2016-12-16 | 2017-04-26 | 中仿智能科技（上海）股份有限公司 | Aircraft side stick simulation device |
| CN107507485A (en) * | 2017-08-09 | 2017-12-22 | 上海工程技术大学 | A kind of flight simulator and the gearing of A seating riding manipulation and loading device |
-
2018
- 2018-02-02 CN CN201810104502.7A patent/CN108074435A/en active Pending
Patent Citations (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB396378A (en) * | 1932-01-22 | 1933-07-24 | John Ronald Sturge Whiting | Apparatus for training air pilots on the ground, and providing the sensation of controlled flight for instructional and/or amusement purposes |
| EP0683743A1 (en) * | 1993-02-24 | 1995-11-29 | Altair Corporation | Control system for aircraft |
| CN202855112U (en) * | 2012-10-15 | 2013-04-03 | 昆山航理机载设备有限公司 | Motor-human sense simulation control system motor of helicopter |
| 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 |
| US20160252926A1 (en) * | 2013-10-15 | 2016-09-01 | Sagem Defense Securite | Flight control device for an aircraft |
| CN106205275A (en) * | 2016-07-12 | 2016-12-07 | 徐舒青 | The push-pull effort control system of aviation simulator control lever |
| CN106601070A (en) * | 2016-12-16 | 2017-04-26 | 中仿智能科技（上海）股份有限公司 | Aircraft side stick simulation device |
| CN107507485A (en) * | 2017-08-09 | 2017-12-22 | 上海工程技术大学 | A kind of flight simulator and the gearing of A seating riding manipulation and loading device |
Non-Patent Citations (2)
| Title |
|---|
| 廖峰: "飞行模拟机电动式辅助操纵负荷系统的仿真", 《科学技术与工程》 * |
| 王恒亮 等: "飞行模拟器操纵负荷系统仿真分析与实现", 《航空科学技术》 * |
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| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| RJ01 | Rejection of invention patent application after publication |
Application publication date: 20180525 |
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| RJ01 | Rejection of invention patent application after publication |