CN211857823U - Flight simulator manipulation linkage system - Google Patents
Flight simulator manipulation linkage system Download PDFInfo
- Publication number
- CN211857823U CN211857823U CN202020526034.5U CN202020526034U CN211857823U CN 211857823 U CN211857823 U CN 211857823U CN 202020526034 U CN202020526034 U CN 202020526034U CN 211857823 U CN211857823 U CN 211857823U
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- Prior art keywords
- aileron
- transmission
- rod
- linkage
- foot
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- Expired - Fee Related
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- 230000005540 biological transmission Effects 0.000 claims description 94
- 230000005489 elastic deformation Effects 0.000 claims description 4
- 229910001094 6061 aluminium alloy Inorganic materials 0.000 claims description 3
- 229910000831 Steel Inorganic materials 0.000 claims description 3
- 239000010959 steel Substances 0.000 claims description 3
- 238000000034 method Methods 0.000 claims description 2
- 238000004519 manufacturing process Methods 0.000 abstract description 2
- 239000007769 metal material Substances 0.000 abstract description 2
- 238000004088 simulation Methods 0.000 abstract description 2
- 238000010586 diagram Methods 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
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Abstract
The utility model discloses a flight simulator manipulation linkage system, flight simulator manipulation system belongs to simulator manipulation technical field, mainly by foot manipulation system, and hand manipulation system two parts constitute. The foot control system transmits a rudder signal and the hand control system transmits an elevator signal and an aileron signal to corresponding sensors, so that the aim of controlling the attitude of the flight simulator is fulfilled. Realize flight simulator owner and copilot operating system's linkage to change the change volume of operating mechanism stroke into the voltage signal who corresponds three hall sensor, operating system makes things convenient for the sensor and returns the regulation of mechanism in, the utility model discloses application scope is wide, and simple structure all adopts metal material, and the durability is good, and low in manufacturing cost has effectively reduced the cost of simulation flight training.
Description
Technical Field
The utility model relates to a simulator field specifically is a flight simulator manipulation linked system.
Background
A flight simulator control system belongs to the technical field of simulator control and mainly comprises a foot control system and a hand control system. The foot control system transmits a rudder signal and the hand control system transmits an elevator signal and an aileron signal to corresponding sensors, so that the aim of controlling the attitude of the flight simulator is fulfilled. In order to achieve precise linkage of the steering of the primary and secondary pilots and more efficient transmission of steering feedback signals to the sensors, a good steering linkage system of the flight simulator is required.
SUMMERY OF THE UTILITY MODEL
An object of the utility model is to provide a flight simulator manipulation linkage system to solve the problem that proposes among the above-mentioned background art.
In order to achieve the above object, the utility model provides a following technical scheme:
a flight simulator maneuvering linkage system comprising: the foot-operated system and the hand-operated system, a pedal is fixedly connected with a foot-operated transmission rod, the foot-operated transmission rod is fixedly connected with a transmission rod joint, the transmission rod joint is connected with a foot-operated linkage rod through a bolt, the other end of the foot-operated linkage rod is connected with a foot-operated linkage piece, the upper end of the foot-operated linkage piece is connected with a Hall sensor and a reset transmission rod and is arranged on a linkage device support, one end of a reset spring is connected with the pedal support through a bolt, the other end of the reset spring is connected with the reset transmission rod, the hand-operated longitudinal rod is connected with an aileron transmission piece and a elevator transmission rod through bolts, the aileron transmission rod is fixedly connected with the aileron transmission piece and the aileron transmission arm, the aileron linkage rod is fixedly connected with the aileron transmission arm, the transmission gear piece and the reset spring, the linkage rod of the elevator is fixedly connected with the transmission joint of the elevator, the reset piece of the elevator and the transmission gear piece, the transmission gear piece is meshed with a transmission gear on a Hall sensor, when a person operates the manual operating rod to move left and right to operate the aileron, the manual operating rod drives an aileron transmission rod to rotate in a transmission rod support through an aileron transmission piece, an aileron transmission arm fixedly connected with the aileron transmission rod rotates to drive the aileron linkage rod to move at the moment, so that the transmission gear piece drives the transmission gear on the Hall sensor to rotate to generate an aileron signal, the aileron linkage rod is connected with the aileron transmission arm at the other end to drive the manual operating rod at the other end to move together to realize the linkage of the aileron, a reset spring connected with the aileron transmission arm can generate elastic deformation in the motion process to generate elastic force, when the aileron operation disappears, the elastic force of the reset spring can enable the manual operating rod, the manual operation system is fixedly connected with the operation system platform through the transmission rod support and the transmission rod support seat, the aileron limit block, the Hall sensor and the reset spring of the manual operation system are fixed on the operation system platform, and the arrangement mode of the operation system accords with the human engineering design and is convenient for operating the simulator.
As a further aspect of the present invention: the foot control system is made of No. 45 steel.
As a further aspect of the present invention: the manual operation system is made of 6061 aluminum alloy.
As a further aspect of the present invention: the sensor adopts a Hall sensor, and the voltage value of the Hall sensor is changed through operation to accurately transmit signals.
As a further aspect of the present invention: the centering mechanism adopts return springs, and each return spring is provided with an adjusting bolt, so that fine adjustment of the centering mechanism is facilitated.
Compared with the prior art, the beneficial effects of the utility model are that: realize flight simulator owner and copilot operating system's linkage to change the change volume of operating mechanism stroke into the voltage signal who corresponds three hall sensor, operating system makes things convenient for the sensor and returns the regulation of mechanism in, the utility model discloses application scope is wide, and simple structure all adopts metal material, and the durability is good, and low in manufacturing cost has effectively reduced the cost of simulation flight training.
Drawings
FIG. 1 is a schematic structural view of a foot control system of a flight simulator control linkage system.
FIG. 2 is a schematic diagram of a hand-operated system of a flight simulator control linkage system.
FIG. 3 is a schematic diagram of a flight simulator control linkage system.
As shown in the figure: 1. pedaling; 2. a foot operated drive link; 3. a pedal support; 4. a return spring; 5. a Hall sensor; 6. a drive link joint; 7. a foot-operated linkage rod; 8. a foot operated linkage; 9. a linkage support; 10. a reset transmission rod; 11. a manual operating lever; 12. a flap drive member; 13. an elevator drive rod; 14. a transmission rod support; 15. an aileron drive link; 16. an aileron drive arm; 17. an aileron linkage rod; 18. a transmission gear; 19. a transmission gear member; 20. a transmission gear; 21. a transmission gear member; 22. an elevator return member; 23. an elevator gangbar; 24. an elevator drive joint; 25. a transmission rod supporting seat; 26. an aileron stop block; 27. and operating the system platform.
Detailed Description
The technical solutions in the embodiments of the present invention will be described clearly and completely with reference to the accompanying drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only some embodiments of the present invention, not all embodiments. Based on the embodiments in the present invention, all other embodiments obtained by a person skilled in the art without creative work belong to the protection scope of the present invention.
Referring to fig. 1 to 3, in an embodiment of the present invention, a flight simulator operation linkage system includes: a foot-operated system and a hand-operated system, wherein a pedal 1 is fixedly connected with a foot-operated transmission rod 2, the foot-operated transmission rod 2 is fixedly connected with a transmission rod joint 6, the transmission rod joint 6 is connected with a foot-operated linkage rod 7 through a bolt, the other end of the foot-operated linkage rod 7 is connected with a foot-operated linkage member 8, the upper end of the foot-operated linkage member 8 is connected with a Hall sensor 5 and a reset transmission rod 10 and is arranged on a linkage device support 9, one end of a reset spring 4 is connected with a pedal support 3 through a bolt, the other end of the reset spring is connected with the reset transmission rod 10, a hand-operated rod 11 is connected with an aileron transmission member 12 and a lifter transmission rod 13 through bolts, an aileron transmission rod 15 is fixedly connected with an aileron transmission member 12 and an aileron transmission arm 16, an aileron linkage rod 17 is fixedly connected with the aileron transmission arm 16, the elevator driving rod 13 is connected with the elevator driving joint 24 through a bolt, the elevator linkage rod 23 is fixedly connected with the elevator driving joint 24, the elevator reset member 22 and the driving gear member 21, the driving gear member 21 is engaged with the driving gear 20 on the Hall sensor 5, when a person operates the manual operating rod 11 to move left and right for operating the aileron, the manual operating rod 11 drives the aileron driving rod 15 to rotate in the driving rod support 14 through the aileron driving member 12, the aileron driving arm 16 fixedly connected with the aileron driving rod 15 rotates to drive the aileron linkage rod 17 to move, so that the driving gear member 19 drives the driving gear 18 on the Hall sensor 5 to rotate to generate aileron signals, the aileron linkage rod 17 is connected with the aileron driving arm 16 at the other end to drive the manual operating rod 11 at the other end to move together to realize the aileron linkage, and the reset spring 4 connected with the aileron driving arm 16 generates elastic deformation to generate elastic force, when the operation of the aileron disappears, the elasticity of the return spring 4 can restore the manual operating lever 11, the foot operating system is fixedly connected with the [27] operating system platform 27 through the pedal support 3 and the linkage device support 9, the manual operating system is fixedly connected with the operating system platform 27 through the transmission rod support 14 and the transmission rod support 25, the aileron limit block 26, the Hall sensor 5 and the return spring 4 of the manual operating system are fixed on the operating system platform 27, and the arrangement mode of the operating system accords with the human engineering design and is convenient for operating the simulator.
The foot control system is made of No. 45 steel.
The manual operation system is made of 6061 aluminum alloy.
The sensor adopts the Hall sensor 5, and the voltage value of the Hall sensor 5 is changed through operation to accurately transmit signals.
The centering mechanism adopts the return springs 4, and each return spring 4 is provided with an adjusting bolt, so that the centering mechanism can be finely adjusted conveniently.
When a person steps on the pedal 1 to operate, the pedal 1 drives the foot operation transmission rod 2 to rotate in the pedal support 3 around the axis of the foot operation transmission rod, at the moment, the transmission rod joint 6 also rotates along with the foot operation transmission rod 2 to drive the foot operation linkage rod 7 to move back and forth, at the moment, the foot operation linkage piece 8 rotates to drive the foot operation linkage rod 7 on the other side to move back and forth, so that the pedal 1 on the other side is driven to rotate around the axis of the foot operation transmission rod 2 to realize linkage of the foot operation system, the Hall sensor 5 and the reset transmission rod 10 on one side rotate at the same angle with the foot operation linkage piece 8, at the moment, the reset spring 4 on the one side is stretched, and when the force of the pedal 1 disappears, the reset transmission rod 10 can be reset by the reset spring 4.
When a person operates the manual operating rod 11 to move back and forth to operate the elevator, the elevator transmission rod 13 connected with the manual operating rod 11 moves back and forth, at the moment, the elevator transmission joint 24 can drive the elevator linkage rod 23 to rotate in the transmission rod supporting seat 25, the transmission gear piece 21 can drive the transmission gear 20 on the Hall sensor 5 to rotate to generate an elevator signal, the counter-pulling reset spring 4 connected with the elevator resetting piece 22 can generate elastic deformation to generate elastic force, when the operation of the elevator disappears, the elastic force of the reset spring 4 can enable the manual operating rod 11 to recover, and the operation of the auxiliary wing and the elevator cannot interfere with each other.
In the description of the present invention, it is to be noted that, unless otherwise explicitly specified or limited, the terms "mounted," "connected," and "connected" are to be construed broadly, and may be, for example, fixedly connected, detachably connected, or integrally connected; can be mechanically or electrically connected; they may be connected directly or indirectly through intervening media, or they may be interconnected between two elements. The specific meaning of the above terms in the present invention can be understood by those of ordinary skill in the art through specific situations.
Although the present invention has been described in detail with reference to the foregoing embodiments, it will be apparent to those skilled in the art that modifications may be made to the embodiments or portions thereof without departing from the spirit and scope of the invention.
Claims (5)
1. A flight simulator operation linkage system is characterized by comprising a foot operation system and a hand operation system, wherein a pedal (1) is fixedly connected with a foot operation transmission rod (2), the foot operation transmission rod (2) is fixedly connected with a transmission rod joint (6), the transmission rod joint (6) is connected with a foot operation linkage rod (7) through a bolt, the other end of the foot operation linkage rod (7) is connected with a foot operation linkage piece (8), the upper end of the foot operation linkage piece (8) is connected with a Hall sensor (5) and a reset transmission rod (10) and is installed on a linkage device support (9), one end of a reset spring (4) is connected with the pedal support (3) through a bolt, the other end of the reset spring is connected with the reset transmission rod (10), the hand operation rod (11) is connected with an aileron transmission piece (12) and a lifting rudder transmission rod (13) through a bolt, and an aileron transmission rod (15) is connected with the aileron transmission piece (12, An aileron transmission arm (16) is fixedly connected, an aileron linkage rod (17) is fixedly connected with the aileron transmission arm (16), a transmission gear piece (19) and a reset spring (4), the transmission gear piece (19) is meshed with a transmission gear (18) on a Hall sensor (5), an elevator transmission rod (13) is connected with an elevator transmission joint (24) through a bolt, an elevator linkage rod (23) is fixedly connected with the elevator transmission joint (24), an elevator reset piece (22) and a transmission gear piece (21), the transmission gear piece (21) is meshed with a transmission gear (20) on the Hall sensor (5), when a person operates the aileron to operate by controlling the left and right movement of the aileron linkage rod (11), the manual control rod (11) drives the aileron transmission rod (15) to rotate in a transmission rod support (14) through an aileron transmission piece (12), the aileron transmission arm (16) fixedly connected with the aileron transmission rod (15) rotates to drive the aileron linkage rod (17) to move, the transmission gear piece (19) drives a transmission gear (18) on the Hall sensor (5) to rotate to generate an aileron signal, an aileron linkage rod (17) is connected with an aileron transmission arm (16) at the other end to drive a manual operation rod (11) at the other end to move together to realize the linkage of ailerons, a reset spring (4) connected with the aileron transmission arm (16) can generate elastic deformation to generate elastic force in the moving process, when the control of the ailerons disappears, the elastic force of the reset spring (4) can enable the manual operation rod (11) to recover, a foot control system is fixedly connected with a control system platform (27) through a pedal support (3) and a linkage device support (9), the manual operation system is fixedly connected with the control system platform (27) through a transmission rod support (14) and a transmission rod support (25), an aileron limit block (26) of the manual operation system, the Hall sensor (5) and the reset spring (4) are fixed on the control system platform (27), the arrangement mode of the control system accords with the ergonomic design, and the control of the simulator is convenient.
2. The flight simulator control linkage system of claim 1, wherein the foot control system is fabricated from 45 gauge steel.
3. A flight simulator control linkage system according to claim 1, wherein the hand control system is fabricated from 6061 aluminium alloy.
4. A flight simulator operating linkage system according to claim 1, characterised in that the sensors employ hall sensors (5) and the hall sensors (5) are operated to vary the magnitude of the voltage to accurately transmit the signal.
5. A flight simulator manoeuvring linkage system according to claim 1 characterised in that the centering mechanism incorporates return springs (4), each return spring (4) being fitted with an adjustment bolt to facilitate fine adjustment of the centering mechanism.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202020526034.5U CN211857823U (en) | 2020-04-12 | 2020-04-12 | Flight simulator manipulation linkage system |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202020526034.5U CN211857823U (en) | 2020-04-12 | 2020-04-12 | Flight simulator manipulation linkage system |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN211857823U true CN211857823U (en) | 2020-11-03 |
Family
ID=73145346
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202020526034.5U Expired - Fee Related CN211857823U (en) | 2020-04-12 | 2020-04-12 | Flight simulator manipulation linkage system |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN211857823U (en) |
-
2020
- 2020-04-12 CN CN202020526034.5U patent/CN211857823U/en not_active Expired - Fee Related
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| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20201103 |
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| CF01 | Termination of patent right due to non-payment of annual fee |