CN209118545U - The flight control simulator that stroke and stick force and maneuverability pattern adaptively adjust - Google Patents
The flight control simulator that stroke and stick force and maneuverability pattern adaptively adjust Download PDFInfo
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- CN209118545U CN209118545U CN201820961066.0U CN201820961066U CN209118545U CN 209118545 U CN209118545 U CN 209118545U CN 201820961066 U CN201820961066 U CN 201820961066U CN 209118545 U CN209118545 U CN 209118545U
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Abstract
The utility model discloses the flight control simulators that a kind of stroke and stick force and maneuverability pattern adaptively adjust comprising control stick simulation unit and pedal simulation unit；The control stick simulation unit is formed by handle, the body of rod, pole socket and with somoothing board；The handle is connected to the top of the body of rod, which is connected on pole socket, is arranged below the pole socket with somoothing board.The pedal simulation unit includes foot pedal component, rocker arm assembly, pedal pedestal and adjustment/shifting system；The pedal assembly is mounted on pedal pedestal by rocker arm assembly；Adjustment/shifting system is used to adjust the position of pedal stroke and pedal simulation unit.The utility model can adaptively adjust control stick and pedal stroke, control stick stick force and control stick maneuverability pattern, therefore the utility model is applicable to the control stick to Multiple Type aircraft, pedal carries out analog simulation；And the utility model has the characteristics that occupy little space, easy to assembly, easy maintenance.
Description
Technical field
The utility model relates to flight simulator driver trainings, science popularization air training technical field, more particularly to one kind
The flight control simulator that stroke and stick force and maneuverability pattern can be adjusted adaptively.
Background technique
In flight control system, control stick and rudder foot pedal are the most key a part；Will have a direct impact on makes
The operating experience of user and impression, and the control response of these components and stick force feature etc. will have a direct impact on the journey true to nature of simulation
Degree.Therefore reduction actual airplane control stick, the handling characteristic of pedal and stick force feature become the crucial ring in simulator research and development
Section.
And current flight simulator is usually present following problems:
1, simulator stick force feature cannot reach the behaviour consistent or close with the stick force in really manipulation for operator
The control stick construction of vertical impression, simple simulation system is simple and crude, can only achieve most basic manipulation demand, active strokes, stick force
Feature is completely inconsistent with truth, cannot reach true manipulation experience.Mould is used for even with aircraft primitive part
It is quasi-, FORCE FEEDBACK variation and the variation of handling quality under different flight state to control stick can not be reached；
2, various model control sticks, pedal can not compatible exchange, control stick, pedal currently used for plane simulation are all one
One bar of type, one bar of a machine, the control stick of a certain model aircraft are only used for the simulation of the type simulator.Traditional bar rudder can not be real
The existing compatible various types of functions of the same framework；
3, traditional control stick, the associated components volume of pedal be big, structure disperses, is not easy to modularization and independently dismounts and tie up
Shield, is unsuitable for using on multipurpose small platform.Some simulators use true control stick, pedal parts on aircraft, are
Simulator volume, can only be made greatly, therefore can occupy much room by the installation requirement for adapting to these components.
Utility model content
Place in view of the above-mentioned deficiencies in the prior art, the utility model provide a kind of stroke and stick force and manipulation side
The flight control simulator that formula adaptively adjusts, for adaptively with group formula flight Simulation System, the trip and stick force and a behaviour
The flight control simulator that vertical mode adaptively adjusts includes control stick simulation unit and pedal simulation unit；
The control stick simulation unit includes handle, the body of rod, pole socket and matches somoothing board；Wherein, the body of rod includes outer
Shell, the interior of shell is installed with high-order roll channel shaft, two wrist bar stick force generate spring assembly and pattern switching
Motor；Wrist bar rocker arm is connected to the body of rod top by high-order roll channel shaft, and passes through boat with the handle
Blind plug is connected with ready-packaged joint；Described two wrist bar stick force generate spring assembly and interlock in the bottom of the wrist bar rocker arm
Distribution；The wrist bar rocker arm compresses two wrist bar stick force respectively and generates spring assembly when rotating；The pattern switching motor
It is connect with lock pin, is provided with the bayonet to match with the lock pin on the wrist bar rocker arm；The bottom of the lock pin and shift
Connecting rod connects, and is disposed with control stick stroke limit sliding block, connector and engaging lug from top to bottom on the shift connecting rod；
The pole socket includes that control stick stroke limit groove seat and cross are set a roof beam in place, and is arranged in the control stick stroke limit groove seat
There is turn away a visitor with some excuse to sail throw of lever limiting slot more, the cross set a roof beam in place on gimbal structure, the bottom end of the body of rod and described ten thousand are installed
It is connected to section structure, is connected with roll channel output shaft and pitch channel output shaft on the connector, the roll channel is defeated
Shaft and the pitch channel output shaft penetrate the control stick limit groove seat setting respectively；Connect respectively on each engaging lug
It is connected to stick force simulation spring assembly, the other end of the stick force simulation spring assembly is connected to the endpoint that the cross is set a roof beam in place；
It is described to be made of with somoothing board the electronic slide unit that two square crossings are stacked, wherein what is be located above is electronic
The bottom that the sliding block of slide unit is set a roof beam in place with the cross is fixed, the sliding block connection of the electronic slide unit of slide unit pedestal and lower section；
The pedal simulation unit includes foot pedal component, rocker arm assembly, pedal pedestal and adjustment/shifting system；Institute
Stating pedal assembly includes foot pedal, foot pedal pillar, sliding block and sliding rail；The foot pedal props up column articulated, institute with the foot pedal
It states sliding block to be fixed below the foot pedal pillar, the sliding rail is arranged on the pedal pedestal, the sliding block and the cunning
Rail is slidably connected；
The rocker arm assembly include the first fork-shaped rocker arm, the first fork-shaped rocker arm both ends respectively with two foot pedal components
Connection；And the first fork-shaped rocker arm is connected on the pedal pedestal by first rotating shaft, setting above the first rotating shaft
There is first angle sensor；Two end side surfaces of the first fork-shaped rocker arm abut respectively has a pedal force to simulate spring assembly；
Adjustment/the shifting system includes pedal range controlling mechanism and pedal position adjusting mechanism；The pedal stroke
Control mechanism includes electronic worm screw, and pedal limit card block is connected on the electronic worm screw, is arranged in the pedal limit card block
There is limit card slot；The pedal position adjusting mechanism includes electric pushrod, and described electric pushrod one end and pedal emulation are single
Member connection, the other end connect on the operational platform, and the pedal simulation unit is slidably connected with the operating platform.
Further, the stick force simulation spring assembly is by the air spring and setting of internal layer on the outside of the air spring
Mechanical spring composition.
Further, set a roof beam in place one end of connection of the mechanical spring and the cross is also connected with the first servo electric cylinders.
Further, roll channel output shaft is two, and two roll channel output shafts are on the connector
Relative distribution, one of roll channel output shaft are connected with third angle sensor, another roll channel exports axis connection
There is the first stick force to adjust component；
The pitch channel output shaft is two, and two pitch channel output shafts Relative distribution on the connector,
One of pitch channel output shaft is connected with fourth angle sensor, another pitch channel output shaft is connected with the second stick force
Adjust component.
Further, it includes: that the second fork-shaped shakes that first stick force, which adjusts component and second stick force adjusting component,
Arm, two stick force adjustment springs and stick force adjust electric cylinders；
The second fork-shaped rocker arm and the rolling channel output shaft or pitch channel export axis connection, and two stick force adjust bullet
Spring is distributed in the two sides of the second fork-shaped rocker arm, and the stick force adjusts electric cylinders and is separately connected with two stick force adjustment springs.
Further, second angle sensor is installed in the shaft of the high-order roll channel.
Further, the bottom end of the handle is provided with fast-assembling nut, and the top of the wrist bar rocker arm is provided with fast-assembling
Screw socket；The handle is connected by the fast-assembling nut with the fast-assembling screw socket with the wrist bar rocker arm.
Further, two pedal force simulation spring assemblies are connected by link mechanism, and the link mechanism passes through
Second shaft is connected on the pedal pedestal, and the link mechanism is also connected with one second servo electric cylinders.
Further, foot-operated fixing flat spring assembly and the 5th angle sensor are respectively provided with inside each foot pedal pillar
Device.
Further, two pedal force simulation spring assemblies are using block form or the mounting means of staggered.
The utility model relates to control stick, pedal can according to the aircraft of various models switch control stick, pedal row
Journey, the stick force of control stick and channel pattern；And relatively independent, compact-sized, the easy to disassemble maintenance of each unit module.Stroke control
It is the mode using mechanical position limitation, by gearshift, automatically switches the corresponding different trips range of different model aircraft.Stick force
Control in such a way that servo mechanism combines, thus can achieve stepless, unconfined in various models spring assembly
Stick force between free switching.
The utility model has the advantage that compared with the existing technology
1, the flight control simulator of the utility model can switch control stick according to aircraft type, pedal stroke, drive
Sail bar stick force and operation mode；Therefore it can realize that same framework is suitble to the analog simulation of Multiple Type aircraft control stick, pedal, tie
It closes exchangeable panel and corresponding simulation control software achieves that different model, the analog simulation of different type of machines；
2, be greatly decreased the buying expenses of analog machine, legacy analog device substantially just for a kind of model aircraft, and
The a set of basic platform of the simulator of the utility model can correspond to various types of aircrafts, and adaptability is significantly larger than traditional analog and sets
It is standby；
3, it takes up little area and saves space, the utility model uses modularization Integrated design, is suitble to make on various small-sized platforms
With not needing a large amount of many and diverse external equipments and support；
4, easy maintenance, the unit of modularized design can easily realize the replacement of spare module entirety Quick Release ready-package, nothing
Need many and diverse Maintenance and Repair work.
Detailed description of the invention
Fig. 1 is the structural schematic diagram of control stick simulation unit provided by the embodiment of the utility model；
Fig. 2 is another structural schematic diagram of control stick simulation unit provided by the embodiment of the utility model；
Fig. 3 a, the structural schematic diagram that 3b, 3c, 3d are the body of rod provided by the embodiment of the utility model；
Fig. 4 is the structural schematic diagram of pole socket provided by the embodiment of the utility model；
Fig. 5 is the structural schematic diagram provided by the embodiment of the utility model with somoothing board；
Fig. 6 is the scheme of installation that stick force adjusts electric cylinders；
Fig. 7 is the structural schematic diagram that stick force adjusts component；
Fig. 8 is to drive throw of lever gear Principles of Regulation figure；
Fig. 9 is the structural schematic diagram of pedal simulation unit provided by the embodiment of the utility model；
Figure 10 is the structural schematic diagram of foot pedal component provided by the embodiment of the utility model；
Figure 11 is the structural schematic diagram of rocker arm assembly provided by the embodiment of the utility model；
Figure 12 is the schematic illustration that rocker arm assembly adjusts pedal force；
Figure 13 is the schematic view of the mounting position of pedal stroke shift control mechanism；
Figure 14 is the structural schematic diagram of pedal stroke provided by the embodiment of the utility model shift control mechanism；
Figure 15 is the schematic diagram of pedal position limiting slide block provided by the embodiment of the utility model；
Figure 16 is the structural schematic diagram of pedal position adjusting mechanism provided by the embodiment of the utility model.
Description of symbols:
A: handle, B: the body of rod, C: pole socket, D: match somoothing board, 1: wrist bar rocker arm,
2: high-order roll channel shaft, 3: lock pin, 4: wrist bar stick force generates spring assembly,
5: pattern switching motor, 6: control stick stroke limit sliding block, 7: control stick stroke limit groove seat,
8: stick force simulation spring assembly, 9: shell, 10: connector, 11: engaging lug,
12: second angle sensor, 13: shift connecting rod, 14: gimbal structure,
15: roll channel output shaft, 16: pitch channel output shaft, 17: cross is set a roof beam in place,
18: stick force simulation spring assembly, 19: stick force secondary spring group, 20: displacement sensor,
21: sliding block, 22: slide unit pedestal, 23: driving motor, 24: the first servo electric cylinders,
25: stick force adjustment spring, 26: the second fork-shaped rocker arms, 27: stick force adjusts electric cylinders；
E: foot pedal component, F: rocker arm assembly, G: pedal pedestal, M: adjustment/shifting system,
28: foot pedal, 29: foot pedal pillar, 30: sliding block, 31: sliding rail, 32: the first fork-shaped rocker arms,
33: first rotating shaft, 34: first angle sensor, 35: pedal force simulates spring assembly,
36: link mechanism, 37: the second servo electric cylinders, 38: the second shafts,
39: pedal range controlling mechanism, 40: pedal limit card block, 41: limit card slot,
42: electric pushrod, 43: operating platform, 44: sliding block sliding rail.
Specific embodiment
It is practical new below in conjunction with this to keep the objectives, technical solutions, and advantages of the embodiments of the present invention clearer
Attached drawing in type embodiment, the technical scheme in the utility model embodiment is clearly and completely described, it is clear that is retouched
The embodiment stated is a part of the embodiment of the utility model, instead of all the embodiments.Based on the reality in the utility model
Apply example, those of ordinary skill in the art's every other embodiment obtained without making creative work, all
Belong to the range of the utility model protection.
The present embodiment provides the flight control simulators that a kind of stroke and stick force and maneuverability pattern adaptively adjust, this flies
Row control simulation device includes control stick simulation unit and pedal simulation unit, and two units constitute basic flight control mould
Quasi- device.Specifically, Fig. 1 to Fig. 8 is please referred to, the control stick simulation unit in the present embodiment includes handle A, body of rod B, pole socket C
And match somoothing board D, as shown in Figure 1.
Wherein, above-mentioned body of rod B includes shell 9, is fixedly provided with 2, two hands of high-order roll channel shaft in its shell 9
Wrist bar stick force generates spring assembly 4 and pattern switching motor 5；Wrist bar rocker arm 1 passes through high-order roll channel shaft 2 and is connected to
The top body of rod B is provided with second angle sensor 12 in the high position roll channel shaft 2.Wrist bar rocker arm 1 and handle A passes through
Aviation plug is connected with ready-packaged joint；Specifically, the bottom end of handle A is provided with fast-assembling nut in the present embodiment, the wrist
The top of bar rocker arm 1 is provided with fast-assembling screw socket；Handle A is connected by fast-assembling nut with fast-assembling screw socket with wrist bar rocker arm 1.Namely
Handle A is i.e. plug-in unit, therefore according to the replaceable different handle A of different model aircraft；Two wrist bar stick force generate spring
Component 4 is interspersed in the bottom of wrist bar rocker arm 1；Wrist bar rocker arm 1 compresses two wrist bar stick force respectively and generates when rotating
Spring assembly 4 generates breakthrough power and stick force appropriate.
Above-mentioned pattern switching motor 5 is connect with lock pin 3, is provided with the bayonet to match with lock pin 3 on wrist bar rocker arm 1；
The bottom of lock pin 3 is connect (grey parts in Fig. 3 b) with shift connecting rod 13, is disposed with and is driven from top to bottom on connecting rod 13 of shifting gears
Sail throw of lever position limiting slide block 6, connector 10 and engaging lug 11；Above-mentioned pole socket C includes that cross sets a roof beam in place 17, which sets a roof beam in place on 17
It is provided with control stick stroke limit groove seat 7 and gimbal structure 14, is provided in the control stick stroke limit groove seat 7 replaceable
Turn away a visitor with some excuse in pitch channel corresponding to different model and roll channel sails throw of lever limiting slot more, the bottom end and ten thousand of above-mentioned body of rod B
It is connected to section structure 14, the roll channel output shaft 15 and a pair of a pair of of Relative distribution is connected on the connector 10 of body of rod B
The pitch channel output shaft 16 of Relative distribution；The roll channel output shaft 15 and pitch channel output shaft 16 penetrate control stick respectively
Groove seat 7 is limited to be arranged.
Above-mentioned gimbal structure 14 exports pitch channel parameter to angle by one of a pair of of pitch channel output shaft 16
Sensor, another pitch channel output shaft 16 are reserved, and additionally load input shaft as control stick stick force.Similarly, above-mentioned ten thousand
One for passing through a pair of of roll channel output shaft 15 to section structure 14 exports roll channel parameters to angular transducer, another is horizontal
Rolling channel output shaft 15 is reserved, and additionally loads input shaft as control stick stick force.
Control stick pattern switching is driven by pattern switching motor 5, when needing using wrist bar mode, pattern switching motor
5 band pendulum lock pins 3 are run down, so that lock pin 3 is deviate from from the bayonet on wrist bar rocker arm 1, while making control stick stroke limit
The wrist bar mode that sliding block 6 enters control stick stroke limit groove seat 7 limits shelves, at this point, high-order roll channel shaft 2 works, bar
Body B can only do pitch channel operation, and roll channel is blocked；When needing using integral stem mode, pattern switching motor 5 is driven
Lock pin 3 is run up so that lock pin 3 be inserted into wrist bar rocker arm 1 on bayonet, while make control stick stroke limit sliding block 6 into
Enter the integral stem mode limit shelves of control stick stroke limit groove seat 7, at this point, high-order roll channel shaft 2 is blocked, handle A with
Body of rod B is linked together；At this point, pitch channel operation can be done, roll channel operation can be also done.
It drives throw of lever control and passes through pitch channel corresponding to the different model being arranged in control stick stroke limit groove seat 7
It is realized with roll channel control stick stroke limit slot, as shown in figure 8, driving the throw of lever when control stick stroke limit sliding block 6 is located at
When limiting the low level L of groove seat 7, the stroke of control stick is small stroke, and angular travel is ɑ 1, and sliding when working as control stick stroke limit
When block 6 is located at the high-order H of control stick stroke limit groove seat 7, the stroke of control stick is big stroke, and angular travel is ɑ 2.
Stick force simulation spring assembly 18 is connected on the engaging lug 11 of above-mentioned body of rod B, which simulates spring assembly 18
The other end by universal joint be connected to cross set a roof beam in place 17 endpoint；Stick force simulation spring assembly 18 can simulate aircraft handling
The basic stick force and breakthrough power of bar, wherein stick force simulation are realized by outer layer mechanical spring, break through power simulation by inner air spring
It realizes.Cross can be connected or disengage by 13 bottom end of shift connecting rod for the stick force difference of different model set a roof beam in place the stick force of 17 bottoms
Secondary spring group 19 compensates.When needing to adjust stick force, spring assembly 18 and cross can be simulated in stick force and set a roof beam in place 17 companies
The one end connect connects the first servo electric cylinders 24, compresses or unclamp stick force mould according to control stick real-time status by the first servo electric cylinders 24
The outer layer spring of quasi- spring assembly 18, achievees the purpose that simulate different stick force in real time, as shown in Figure 6；
Or the control of variable stick force is realized by way of stick force adjusts component loading in pitching/roll channel output shaft
System, specifically, it includes that 26, two stick force adjustment springs 25 of the second fork-shaped rocker arm and stick force adjust electric cylinders which, which adjusts component,
27；The second fork-shaped rocker arm 26 is connect with roll channel output shaft 15 or pitch channel output shaft 16, two stick force adjustment springs
25 are distributed in the two sides of the second fork-shaped rocker arm 26, and stick force adjusts electric cylinders 27 and is separately connected with two stick force adjustment springs 25, such as Fig. 7
It is shown.
When needing to adjust stick force, stick force adjusts electric cylinders 27 and pushes one group of bar being made of two stick force adjustment springs 25
Power adjustment spring group and 26 counteragent of the second fork-shaped rocker arm, the stick force adjustment spring 25 for compressing side generates additional stick force, attached
The size of stick force is added to adjust the distance controlling that electric cylinders 27 push stick force adjustment spring group by stick force.Similarly, when control stick is to another
When side moves, stick force adjusts electric cylinders 27 and stick force adjustment spring group is then pushed to move to opposite direction, and the stick force for compressing the other side is adjusted
Spring 25.
It is above-mentioned to be made of the electronic slide unit that two square crossings are stacked with somoothing board D, as shown in figure 5, wherein one
A slide unit executes pitching trim operation, another slide unit executes roll trim operation；Electronic slide unit is by being mounted on slide unit pedestal 22
On driving motor 23 drive, pass through ball-screw and push sliding block 21 mobile；The sliding block for the electronic slide unit being wherein located above with
Set a roof beam in place 17 bottom of cross is fixed, the sliding block connection of the electronic slide unit of slide unit pedestal and lower section；The movement of two electronic slide units
Parameter is then acquired by respective displacement sensor 20 respectively.Servo electric cylinders are used with the driving motor 23 on somoothing board, except real
Existing trim function can also be achieved the real-time stick force of simulation and adjust and drive simulating bar stick shaker function.
In addition, please refer to Fig. 9 to Figure 16, the pedal simulation unit of the present embodiment include foot pedal component E, rocker arm assembly F,
Pedal pedestal G and adjustment/shifting system M, as shown in Figure 9；Pedal assembly E includes foot pedal 28, foot pedal pillar 29,
Sliding block 30 and sliding rail 31, as shown in Figure 10；The foot pedal 28 and foot pedal pillar 29 are hinged, divide in each foot pedal pillar 29
Foot-operated fixing flat spring assembly and the 5th angular transducer are not installed；Sliding block 30 is fixed on 29 lower section of foot pedal pillar, and sliding rail 31 is set
It sets on pedal pedestal G, sliding block 30 is slidably connected with sliding rail 31.
Above-mentioned rocker arm assembly F include the first fork-shaped rocker arm 32,32 both ends of the first fork-shaped rocker arm respectively with two foot pedals
Component E connection, so that the two foot pedal component E in left and right can be moved symmetrically；And first fork-shaped rocker arm 32 connected by first rotating shaft 33
It connects on pedal pedestal G, is provided with first angle sensor 34 above the first rotating shaft 33, pedal rudder angle degree for acquiring
According to；Two end side surfaces of the first fork-shaped rocker arm 32 abut respectively has a pedal force to simulate spring assembly 35；By being butted on the first fork
The pedal force simulation spring assembly 35 of shape rocker arm 32 is, it can be achieved that simulation to rudder power is pedaled.Pedal force is simulated spring assembly 35 and is used
The mounting means of block form or staggered can be achieved with pedaling rudder power to difference and echelon pedal the simulation of rudder power, as shown in Figure 11.
Also, for the electrodeless adjustment for realizing pedal force, two pedal forces simulation spring assembly 35 in the present embodiment is logical
The connection of link mechanism 36 is crossed, which is connected on pedal pedestal G by the second shaft 38, which also connects
It is connected to one second servo electric cylinders 37.When the deflection of the first fork-shaped rocker arm 32, the second servo electric cylinders 37 push link mechanism 36 to compress
The distance between the first fork-shaped rocker arm 32 and pedal force simulation spring assembly 35 are compressed, pedal force is increased.When the first fork-shaped rocker arm
When 32 reverse deflection, then 37 counteragent of the second servo electric cylinders, increases other side pedal force.In simulation rudder swing state
When, which does controllable reciprocating motion, controls the E back-and-forth motion of foot pedal component, as shown in figure 12.
Above-mentioned adjustment/shifting system M includes pedal range controlling mechanism 39 and pedal position adjusting mechanism；The pedal stroke
Control mechanism 39 includes electronic worm screw, is connected with pedal limit card block 40 on the electronic worm screw, sets in the pedal limit card block 40
It is equipped with limit card slot 41；The limit card slot 41 that the pedal limit card block 40 passes through the different angle being arranged thereon limits the first fork-shaped
The deflection angle of rocker arm 32, to realize the control of pedal stroke, as shown in Figure 14 and Figure 15.
Above-mentioned pedal position adjusting mechanism includes electric pushrod 42, and 42 one end of electric pushrod and pedal simulation unit connect
It connects, the other end is connected on operating platform 43, and pedal simulation unit is slidably connected with operating platform 43 by sliding block sliding rail 44.It is logical
It crosses electric pushrod 42 and pushes and pulls the back-and-forth motion of pedal simulation unit, most suitable pedal position can be provided for the long operator of different legs
It sets, as shown in figure 16.
The utility model relates to control stick, pedal can according to the aircraft of various models switch control stick, pedal row
Journey, the stick force of control stick and channel pattern；And relatively independent, compact-sized, the easy to disassemble maintenance of each unit module.Stroke control
It is the mode using mechanical position limitation, by gearshift, automatically switches the corresponding different trips range of different model aircraft.Stick force
Control in such a way that servo mechanism combines, thus can achieve stepless, unconfined in various models spring assembly
Stick force between free switching.
The utility model has the advantage that compared with the existing technology
1, the flight control simulator of the utility model can switch control stick according to aircraft type, pedal stroke, drive
Sail bar stick force and operation mode；Therefore it can realize that same framework is suitble to the analog simulation of Multiple Type aircraft control stick, pedal, tie
It closes exchangeable panel and corresponding simulation control software achieves that different model, the analog simulation of different type of machines；
2, be greatly decreased the buying expenses of analog machine, legacy analog device substantially just for a kind of model aircraft, and
The a set of basic platform of the simulator of the utility model can correspond to various types of aircrafts, and adaptability is significantly larger than traditional analog and sets
It is standby；
3, it takes up little area and saves space, the utility model uses modularization Integrated design, is suitble to make on various small-sized platforms
With not needing a large amount of many and diverse external equipments and support；
4, easy maintenance, the unit of modularized design can easily realize the replacement of spare module entirety Quick Release ready-package, nothing
Need many and diverse Maintenance and Repair work.
It should be noted that in the utility model embodiment, the appearance of " first ", " second ", it is only for distinguish
Technical term and description are convenient, should not be construed as the restriction to the utility model embodiment.The terms "include", "comprise" or its
Any other variant is intended to non-exclusive inclusion so that include the process, methods of a series of elements, article or
Terminal device not only includes those elements, but also including other elements that are not explicitly listed, or it is this for further including
Process, method, article or the intrinsic element of terminal device.In the absence of more restrictions, by sentence " including one
It is a ... " element that limits, it is not excluded that include in the process, method of the element, article or terminal device there is also
Other identical element.
The above is only the preferred embodiments of the utility model, are not intended to limit the utility model, for this field
Technical staff for, various modifications and changes may be made to the present invention.Within the spirit and principle of the utility model,
Any modification, equivalent replacement, improvement and so on should be included within the scope of protection of this utility model.
Claims (10)
1. the flight control simulator that a kind of stroke and stick force and maneuverability pattern adaptively adjust, which is characterized in that the row
The flight control simulator that journey and stick force and maneuverability pattern adaptively adjust includes that control stick simulation unit and pedal emulation are single
Member；
The control stick simulation unit includes handle, the body of rod, pole socket and matches somoothing board；Wherein, the body of rod includes shell, institute
It states interior of shell and is installed with high-order roll channel shaft, two wrist bar stick force generation spring assemblies and pattern switching motor；
Wrist bar rocker arm is connected to the body of rod top by high-order roll channel shaft, and passes through aviation plug with the handle
It is connected with ready-packaged joint；Described two wrist bar stick force generate spring assembly and are interspersed in the bottom of the wrist bar rocker arm；
The wrist bar rocker arm compresses two wrist bar stick force respectively and generates spring assembly when rotating；The pattern switching motor and lock pin
It connects, is provided with the bayonet to match with the lock pin on the wrist bar rocker arm；The bottom of the lock pin and shift connecting rod connect
It connects, is disposed with control stick stroke limit sliding block, connector and engaging lug from top to bottom on the shift connecting rod；
The pole socket includes that control stick stroke limit groove seat and cross are set a roof beam in place, and is provided in the control stick stroke limit groove seat more
Turn away a visitor with some excuse and sail throw of lever limiting slot, the cross set a roof beam in place on gimbal structure is installed, the bottom end of the body of rod and the universal joint
Structure connects, and is connected with roll channel output shaft and pitch channel output shaft, roll channel output shaft on the connector
The control stick limit groove seat setting is penetrated respectively with the pitch channel output shaft；It is connected separately on each engaging lug
One stick force simulates spring assembly, and the other end of the stick force simulation spring assembly is connected to the endpoint that the cross is set a roof beam in place；
It is described to be made of with somoothing board the electronic slide unit that two square crossings are stacked, wherein the electronic slide unit being located above
The bottom set a roof beam in place with the cross of sliding block fix, the sliding block connection of the electronic slide unit of slide unit pedestal and lower section；
The pedal simulation unit includes foot pedal component, rocker arm assembly, pedal pedestal and adjustment/shifting system；It is described to step on
Board group part includes foot pedal, foot pedal pillar, sliding block and sliding rail；The foot pedal props up column articulated, the cunning with the foot pedal
Block is fixed below the foot pedal pillar, and the sliding rail is arranged on the pedal pedestal, and the sliding block and the sliding rail are sliding
Dynamic connection；
The rocker arm assembly includes the first fork-shaped rocker arm, and the first fork-shaped rocker arm both ends connect with two foot pedal components respectively
It connects；And the first fork-shaped rocker arm is connected on the pedal pedestal by first rotating shaft, is provided with above the first rotating shaft
First angle sensor；Two end side surfaces of the first fork-shaped rocker arm abut respectively has a pedal force to simulate spring assembly；
Adjustment/the shifting system includes pedal range controlling mechanism and pedal position adjusting mechanism；The pedal stroke control
Mechanism includes electronic worm screw, and pedal limit card block is connected on the electronic worm screw, is arranged in the pedal limit card block limited
Position card slot；The pedal position adjusting mechanism includes electric pushrod, and described electric pushrod one end and the pedal simulation unit connect
It connects, the other end connects on the operational platform, and the pedal simulation unit is slidably connected with the operating platform.
2. the flight control simulator that stroke as described in claim 1 and stick force and maneuverability pattern adaptively adjust, special
Sign is that the stick force simulates spring assembly by the air spring of internal layer and the mechanical spring being arranged on the outside of the air spring
Composition.
3. the flight control simulator that stroke as claimed in claim 2 and stick force and maneuverability pattern adaptively adjust, special
Sign is, set a roof beam in place one end of connection of the mechanical spring and the cross is also connected with the first servo electric cylinders.
4. the flight control simulator that stroke as described in claim 1 and stick force and maneuverability pattern adaptively adjust, special
Sign is that roll channel output shaft is two, and two roll channel output shafts Relative distribution on the connector,
In a roll channel output shaft be connected with third angle sensor, another roll channel output shaft is connected with the first stick force tune
Save component；
The pitch channel output shaft is two, and two pitch channel output shafts Relative distribution on the connector, wherein
One pitch channel output shaft is connected with fourth angle sensor, another pitch channel output shaft is connected with the adjusting of the second stick force
Component.
5. the flight control simulator that stroke as claimed in claim 4 and stick force and maneuverability pattern adaptively adjust, special
Sign is that it includes: the second fork-shaped rocker arm, two stick force that first stick force, which adjusts component and second stick force adjusting component,
Adjustment spring and stick force adjust electric cylinders；
The second fork-shaped rocker arm and the rolling channel output shaft or pitch channel export axis connection, two stick force adjustment springs point
Cloth adjusts electric cylinders and is separately connected with two stick force adjustment springs in the two sides of the second fork-shaped rocker arm, the stick force.
6. the flight control simulator that stroke as described in claim 1 and stick force and maneuverability pattern adaptively adjust, special
Sign is, is equipped with second angle sensor in the shaft of the high position roll channel.
7. the flight control simulator that stroke as described in claim 1 and stick force and maneuverability pattern adaptively adjust, special
Sign is that the bottom end of the handle is provided with fast-assembling nut, and the top of the wrist bar rocker arm is provided with fast-assembling screw socket；The hand
Handle is connected by the fast-assembling nut with the fast-assembling screw socket with the wrist bar rocker arm.
8. the flight control simulator that stroke as described in claim 1 and stick force and maneuverability pattern adaptively adjust, special
Sign is that two pedal force simulation spring assemblies are connected by link mechanism, and the link mechanism is connected by the second shaft
It connects on the pedal pedestal, the link mechanism is also connected with one second servo electric cylinders.
9. the flight control simulator that stroke as described in claim 1 and stick force and maneuverability pattern adaptively adjust, special
Sign is, is respectively provided with foot-operated fixing flat spring assembly and the 5th angular transducer inside each foot pedal pillar.
10. the flight control simulator that stroke as described in claim 1 and stick force and maneuverability pattern adaptively adjust, special
Sign is that two pedal force simulation spring assemblies are using block form or the mounting means of staggered.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820961066.0U CN209118545U (en) | 2018-06-21 | 2018-06-21 | The flight control simulator that stroke and stick force and maneuverability pattern adaptively adjust |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820961066.0U CN209118545U (en) | 2018-06-21 | 2018-06-21 | The flight control simulator that stroke and stick force and maneuverability pattern adaptively adjust |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN209118545U true CN209118545U (en) | 2019-07-16 |
Family
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| Application Number | Title | Priority Date | Filing Date |
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| CN201820961066.0U Active CN209118545U (en) | 2018-06-21 | 2018-06-21 | The flight control simulator that stroke and stick force and maneuverability pattern adaptively adjust |
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| CN (1) | CN209118545U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108648560A (en) * | 2018-06-21 | 2018-10-12 | 北京瀚科瑞杰科技发展有限公司 | The flight control simulator that stroke and stick force and maneuverability pattern adaptively adjust |
| CN112520016A (en) * | 2020-12-09 | 2021-03-19 | 中国航空工业集团公司沈阳飞机设计研究所 | Steering column decoupling structure |
-
2018
- 2018-06-21 CN CN201820961066.0U patent/CN209118545U/en active Active
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108648560A (en) * | 2018-06-21 | 2018-10-12 | 北京瀚科瑞杰科技发展有限公司 | The flight control simulator that stroke and stick force and maneuverability pattern adaptively adjust |
| CN112520016A (en) * | 2020-12-09 | 2021-03-19 | 中国航空工业集团公司沈阳飞机设计研究所 | Steering column decoupling structure |
| CN112520016B (en) * | 2020-12-09 | 2024-05-17 | 中国航空工业集团公司沈阳飞机设计研究所 | Driving lever decoupling structure |
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Effective date of registration: 20230929 Address after: Room 1607, 16th Floor, South Building, Qidi Cluster Innovation Building, No. 118 Rongtong Road, Binhai Street Office, Huangdao District, Qingdao City, Shandong Province, 266404 Patentee after: Hanke Zhixiang (Qingdao) Technology Development Co.,Ltd. Address before: 100000 No. 6 # - 9 # No. 6, No. 59 Banjing Road, Haidian District, Beijing Patentee before: BEIJING HANKE RUIJIE TECHNOLOGY DEVELOPMENT CO.,LTD. |