CN220290331U - Flight-simulating cockpit - Google Patents
Flight-simulating cockpit Download PDFInfo
- Publication number
- CN220290331U CN220290331U CN202321435225.0U CN202321435225U CN220290331U CN 220290331 U CN220290331 U CN 220290331U CN 202321435225 U CN202321435225 U CN 202321435225U CN 220290331 U CN220290331 U CN 220290331U
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- simulation
- fixedly connected
- cabin
- console
- simulation cabin
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- 238000004088 simulation Methods 0.000 claims abstract description 95
- 238000009434 installation Methods 0.000 claims description 15
- 238000000034 method Methods 0.000 abstract description 10
- 230000000694 effects Effects 0.000 description 3
- 241000251468 Actinopterygii Species 0.000 description 2
- 238000004519 manufacturing process Methods 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000005034 decoration Methods 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 230000003238 somatosensory effect Effects 0.000 description 1
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Abstract
The utility model discloses a simulated flight deck, and belongs to the technical field of simulated flight decks. The device comprises a mounting base, wherein three motor bases are fixedly connected to the outer surface of the mounting base, mounting grooves are formed in the motor bases, double-shaft motors are fixedly connected to the inner walls of the mounting grooves, rotating rods are fixedly connected to the two output ends of the double-shaft motors, connecting blocks are rotatably connected to one ends of the rotating rods, which are far away from the motor output ends, of the rotating rods, three groups of U-shaped connecting rods are arranged above the mounting base, the mounting base is arranged, the double-shaft motors are arranged on the motor bases, the connecting blocks are driven to rotate by the double-shaft motors, the U-shaped connecting rods are driven to rotate by the connecting blocks, the connecting bases are driven to move by being hinged with fixed blocks through fish-eye bearings, and the connecting bases are fixedly connected with a simulation cabin, so that various conditions in the simulation flight process are realized.
Description
Technical Field
The utility model relates to a simulated flight deck, and belongs to the technical field of simulated flight decks.
Background
With the development of the age, the living standard of people is continuously improved, more and more people want to experience the process of piloting the aircraft, the aircraft is the most demanding and comprehensive in technology in all transportation modes, and most people cannot directly piloting the aircraft due to the fact that the professional requirement threshold required by aircraft piloting is too high, so that a flight cockpit needs to be simulated to simulate the process of piloting the aircraft.
At present, most of simulated flight cabs are huge in size, high in manufacturing cost, poor in simulation effect and single in function, and cannot comprehensively simulate the airplane driving process, so that experience feeling brought by people is poor, and a new scheme is required to be provided for solving the problem.
Disclosure of Invention
The technical problems to be solved by the utility model are as follows: the simulated flight cockpit solves the problems that the simulated flight cockpit in the prior art is huge in size, high in manufacturing cost and single in function, and can not experience the piloting plane in all directions.
The technical problems to be solved by the utility model are realized by adopting the following technical scheme:
the utility model provides a simulation flight deck, includes the installation base, the surface fixedly connected with three motor cabinet of installation base, every the mounting groove has all been seted up to the inside of motor cabinet, every the equal fixedly connected with biax motor of inner wall of mounting groove, every two output of biax motor are equal fixedly connected with dwang, every the one end that the motor output was kept away from to the dwang is all rotated and is connected with the connecting block, the top of installation base is equipped with three sets of U type connecting rods, every group the both ends of U type connecting rod all with corresponding connecting block fixed connection.
Through adopting above-mentioned technical scheme, two output drive two dwells of biax motor, two dwells control a set of U type connecting rod rotation jointly.
The utility model is further provided with: every group fixedly connected with supporting shoe between the U type connecting rod, the top of installation base is equipped with the connection base, the bottom surface fixedly connected with of connection base is three sets of fixed blocks.
Through adopting above-mentioned technical scheme, the supporting shoe plays the supporting role, connects the base directly over the installation base.
The utility model is further provided with: and fish eye bearings are hinged between each group of fixing blocks, each fish eye bearing is fixedly connected with a corresponding group of U-shaped connecting rods, and the upper surface of the connecting base is fixedly connected with a simulation cabin.
Through adopting above-mentioned technical scheme, through fish-eye bearing and fixed block articulated, can diversified drive connect the base swing.
The utility model is further provided with: the simulation cabin is characterized in that a simulation cabin door is fixedly arranged in the simulation cabin, a simulation window is fixedly arranged in the simulation cabin door, and a simulation display screen is fixedly arranged in the simulation cabin.
By adopting the technical scheme, the simulated cabin door plays a role in decoration, and the simulated window on the simulated cabin door is a display screen, so that a scene in the flight process can be simulated.
The utility model is further provided with: the simulation cabin is characterized in that the inner bottom wall of the simulation cabin is fixedly connected with a simulation main control console, and a console display I is fixedly installed in the simulation main control console.
By adopting the technical scheme, the simulation master control platform is basically consistent with a real airplane, various operations in flight can be simulated, and the control platform display can also display the condition of the simulated flight cockpit.
The utility model is further provided with: the simulation cabin is characterized in that a simulation auxiliary console is fixedly connected to the inner bottom wall of the simulation cabin, a console display II is fixedly installed in the simulation auxiliary console, and a simulation operation rod is fixedly connected to the upper surface of the simulation auxiliary console.
By adopting the technical scheme, the simulated auxiliary console is basically consistent with the real aircraft auxiliary console, and the second console display can observe the live condition of the simulated flight deck.
The utility model is further provided with: the inner bottom wall of the simulation cabin is fixedly connected with two simulation control rods, and the inner bottom wall of the simulation cabin is fixedly connected with two seats.
By adopting the technical scheme, one of the two analog control rods is a main control rod, and the other is a secondary control rod.
The beneficial effects of the utility model are as follows:
1. according to the utility model, the installation base is arranged, the motor seat on the installation base is provided with the double-shaft motor, the double-shaft motor drives the connecting block to rotate, the connecting block rotates to drive the U-shaped connecting rod to rotate, the connecting base is further driven to move by hinging the fisheye bearing with the fixed block, and the connecting base is fixedly connected with the simulation cabin, so that various conditions in the flight simulation process are realized;
2. according to the utility model, the simulation cabin door, the simulation window, the simulation display screen, the simulation main control console, the first control console display, the simulation auxiliary control console, the second control console display, the simulation operation rod and the seat are arranged, the flight driving process is operated through the control console, the simulation window and the simulation display screen can reflect the scene in the simulation flight process in real time, and the immersive experience of a user is greatly enhanced.
Drawings
Fig. 1 is a schematic diagram of the overall structure of the present utility model.
Fig. 2 is a front view of the overall structure of the present utility model.
Fig. 3 is a schematic view of the overall structure of the mounting base of the present utility model.
Fig. 4 is a cross-sectional view of a simulation pod in accordance with the present utility model.
In the figure: 1. a mounting base; 2. a motor base; 3. a mounting groove; 4. a biaxial motor; 5. a rotating lever; 6. a connecting block; 7. a U-shaped connecting rod; 8. a support block; 9. a fish-eye bearing; 10. a fixed block; 11. the base is connected; 12. a simulation cabin; 13. simulating a cabin door; 14. simulating a window; 15. simulating a display screen; 16. simulating a main control platform; 17. a console display I; 18. simulating an auxiliary console; 19. a console display II; 20. simulating an operation rod; 21. simulating a control rod; 22. and (5) a seat.
Detailed Description
The utility model will be further described with reference to the following detailed drawings, in order to make the technical means, the creation characteristics, the achievement of the purpose and the effect of the utility model easy to understand.
As shown in fig. 1-4, a simulated flight cockpit comprises a mounting base 1, three motor bases 2 are fixedly connected with the outer surface of the mounting base 1, mounting grooves 3 are formed in the motor bases 2, double-shaft motors 4 are fixedly connected to the inner walls of the mounting grooves 3, two output ends of each double-shaft motor 4 are fixedly connected with rotating rods 5, one end, far away from the motor output end, of each rotating rod 5 is fixedly connected with a connecting block 6 in a rotating manner, three groups of U-shaped connecting rods 7 are arranged above the mounting base 1, two ends of each group of U-shaped connecting rods 7 are fixedly connected with corresponding connecting blocks 6, two output ends of each double-shaft motor 4 drive two rotating rods 5, and the two rotating rods jointly control one group of U-shaped connecting rods 7 to rotate.
The U-shaped connecting rods 7 are fixedly connected with supporting blocks 8, a connecting base 11 is arranged above the mounting base 1, three groups of fixing blocks 10 are fixedly connected with the bottom surface of the connecting base 11, and fisheye bearings 9 are hinged between the fixing blocks 10.
Each fish-eye bearing 9 is fixedly connected with a corresponding group of U-shaped connecting rods 7, the upper surface of the connecting base 11 is fixedly connected with a simulation cabin 12, the inner bottom wall of the simulation cabin 12 is fixedly connected with a simulation auxiliary console 18, the upper surface of the simulation auxiliary console 18 is fixedly connected with a simulation operating rod 20, the simulation auxiliary console 18 is basically consistent with a real aircraft auxiliary console, a second control console display 19 can observe the live condition of a simulation flight cockpit, the inner bottom wall of the simulation cabin 12 is fixedly connected with a simulation main control console 16, and a second control console display 19 is fixedly installed in the simulation auxiliary console 18.
The control console 16 is fixedly installed in the control console display 17, the control console 16 is basically consistent with a real airplane, various operations in flight can be simulated, the control console display 17 can display the condition of a simulated flight cockpit, the simulation cabin 13 is fixedly installed in the simulation cabin 12, the simulation window 14 is fixedly installed in the simulation cabin 13, two simulation control rods 21 are fixedly connected to the inner bottom wall of the simulation cabin 12, two seats 22 are fixedly connected to the inner bottom wall of the simulation cabin 12, one of the two simulation control rods 21 is a main control rod, and the other is a secondary control rod.
The inside fixed mounting in simulation cabin 12 has simulation display screen 15, and simulation hatch door 13 plays the decorative effect, and simulation window 14 on the simulation hatch door 13 is the display screen, can simulate the scene in the flight in-process, and through fish-eye bearing 9 and fixed block 10 articulated, can diversified drive connection base 11 swing, supporting shoe 8 plays the supporting role, and connection base 11 is directly over installation base 1.
The implementation principle of the utility model is as follows: the motor cabinet 2 on the installation base 1 is provided with the biax motor 4, start biax motor 4, biax motor 4 drives connecting block 6 and rotates, connecting block 6 rotates and drives U type connecting rod 7 and rotate, it is articulated with fixed block 10 through fish-eye bearing 9, and then it carries out flight simulation situation to have driven connection base 11, connection base 11 and simulation cabin 12 fixed connection, the various situation in the flight simulation in-process has been realized, simulation window 14 and simulation display screen 15 in the simulation cabin 12 can show the scene in the simulation flight in real time, simulation master control stand 16, simulation auxiliary control stand 18, simulation action bars 20 and simulation action bars 21 can accomplish the various operations of flight driving, user's somatosensory and impression have been strengthened.
The foregoing has shown and described the basic principles, principal features and advantages of the utility model. It will be understood by those skilled in the art that the present utility model is not limited to the embodiments described above, but is capable of various changes and modifications without departing from the spirit and scope of the utility model. The scope of the utility model is defined by the appended claims and equivalents thereof.
Claims (7)
1. The utility model provides a simulation flight deck, includes installation base (1), its characterized in that: the utility model discloses a motor installation base, including installation base (1), motor cabinet (1), mounting groove (3), every are all offered to the surface fixedly connected with of installation base (1) the inside of motor cabinet (2) is all offered mounting groove (3), every the equal fixedly connected with biax motor (4) of inner wall of mounting groove (3), every two equal fixedly connected with dwang (5) of output of biax motor (4), every the one end that the motor output was kept away from to dwang (5) is all rotated and is connected with connecting block (6), the top of installation base (1) is equipped with three U type connecting rod (7), every group U type connecting rod (7) both ends all with connecting block (6) fixed connection that correspond.
2. A simulated flight cockpit as claimed in claim 1, wherein: every group U type connecting rod (7) between fixedly connected with supporting shoe (8), the top of installation base (1) is equipped with connection base (11), the bottom surface fixedly connected with of connection base (11) is three fixed blocks (10) in group.
3. A simulated flight cockpit as claimed in claim 2, wherein: and a fisheye bearing (9) is hinged between each group of fixed blocks (10), each fisheye bearing (9) is fixedly connected with a corresponding group of U-shaped connecting rods (7), and the upper surface of the connecting base (11) is fixedly connected with a simulation cabin (12).
4. A simulated flight cockpit as claimed in claim 3, wherein: the simulation cabin is characterized in that a simulation cabin door (13) is fixedly arranged in the simulation cabin (12), a simulation window (14) is fixedly arranged in the simulation cabin door (13), and a simulation display screen (15) is fixedly arranged in the simulation cabin (12).
5. A simulated flight cockpit as claimed in claim 4, wherein: the simulation cabin is characterized in that a simulation main control console (16) is fixedly connected to the inner bottom wall of the simulation cabin (12), and a console display I (17) is fixedly installed in the simulation main control console (16).
6. A simulated flight cockpit as claimed in claim 5, wherein: the simulation cabin is characterized in that a simulation auxiliary console (18) is fixedly connected to the inner bottom wall of the simulation cabin (12), a console display II (19) is fixedly installed in the simulation auxiliary console (18), and a simulation operation rod (20) is fixedly connected to the upper surface of the simulation auxiliary console (18).
7. A simulated flight cockpit as claimed in claim 6, wherein: the inner bottom wall of the simulation cabin (12) is fixedly connected with two simulation control rods (21), and the inner bottom wall of the simulation cabin (12) is fixedly connected with two seats (22).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202321435225.0U CN220290331U (en) | 2023-06-07 | 2023-06-07 | Flight-simulating cockpit |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202321435225.0U CN220290331U (en) | 2023-06-07 | 2023-06-07 | Flight-simulating cockpit |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN220290331U true CN220290331U (en) | 2024-01-02 |
Family
ID=89341710
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202321435225.0U Active CN220290331U (en) | 2023-06-07 | 2023-06-07 | Flight-simulating cockpit |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN220290331U (en) |
-
2023
- 2023-06-07 CN CN202321435225.0U patent/CN220290331U/en active Active
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