CN115223420B - Flight training is with intelligent simulation cockpit - Google Patents
Flight training is with intelligent simulation cockpit Download PDFInfo
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- CN115223420B CN115223420B CN202210874784.5A CN202210874784A CN115223420B CN 115223420 B CN115223420 B CN 115223420B CN 202210874784 A CN202210874784 A CN 202210874784A CN 115223420 B CN115223420 B CN 115223420B
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- 238000012549 training Methods 0.000 title claims abstract description 47
- 238000004088 simulation Methods 0.000 title claims description 24
- 238000009434 installation Methods 0.000 claims abstract description 26
- 230000000694 effects Effects 0.000 description 22
- 230000009471 action Effects 0.000 description 7
- 230000000007 visual effect Effects 0.000 description 5
- 230000004888 barrier function Effects 0.000 description 4
- 238000000034 method Methods 0.000 description 4
- 230000005540 biological transmission Effects 0.000 description 3
- 230000006872 improvement Effects 0.000 description 3
- 238000013461 design Methods 0.000 description 2
- 238000003756 stirring Methods 0.000 description 2
- 240000007643 Phytolacca americana Species 0.000 description 1
- 238000004378 air conditioning Methods 0.000 description 1
- 230000008859 change Effects 0.000 description 1
- 238000004891 communication Methods 0.000 description 1
- 230000001276 controlling effect Effects 0.000 description 1
- 230000002079 cooperative effect Effects 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 230000008447 perception Effects 0.000 description 1
- 230000036544 posture Effects 0.000 description 1
- 230000008569 process Effects 0.000 description 1
- 239000000758 substrate Substances 0.000 description 1
Classifications
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- 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
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- 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
- G09B9/10—Simulators for teaching or training purposes for teaching control of vehicles or other craft for teaching control of aircraft, e.g. Link trainer with simulated flight- or engine-generated force being applied to aircraft occupant
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- Engineering & Computer Science (AREA)
- Theoretical Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Business, Economics & Management (AREA)
- Physics & Mathematics (AREA)
- Educational Administration (AREA)
- Educational Technology (AREA)
- General Physics & Mathematics (AREA)
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Abstract
The invention relates to the technical field of simulated flight training, in particular to an intelligent simulated cockpit for flight training, which comprises a base, wherein the top of the base is rotationally connected with a bottom swivel, two vertical installation cabin plates are fixedly installed on the outer wall of the top of the bottom swivel, and the cockpit is installed on the top of a disc.
Description
Technical Field
The invention relates to the technical field of simulated flight training, in particular to an intelligent simulated cockpit for flight training.
Background
Flight training, piloting aircraft for flight personnel and technical tactical training using on-board equipment, weapons. Is a main professional training of aviation soldiers. The pilot training (the pilot of a single aircraft also needs to perform the pilot, shooting, bombing, reconnaissance and other training), the pilot of the air pilot performs the pilot, bombing, reconnaissance, airdrop training, the professional training of personnel such as air communication, shooting, machinery, electronics and the training of cooperative actions among members of the aircrew, and the flight training is not only limited to the pilot of the aircraft, but also comprises the pilot of an airship and the like, and is used for simulating the flight under various postures and perceiving the flight state under various emergency conditions.
Through retrieving, chinese patent with publication number CN113763776a discloses a flight training is with simulation cockpit, including the bottom plate, the top of bottom plate is provided with the operation subassembly, the surface of operation subassembly is provided with action subassembly, the top of action subassembly is provided with the driving subassembly, the operation subassembly includes movable mounting at the landing ring at the bottom plate top, the top movable mounting of bottom plate has the gear ring. According to the simulated cockpit for flight training, the cockpit body rotates around the middle shaft sleeve through the cooperation of the driving motor, the driving gear, the gear ring, the middle shaft sleeve and the central telescopic rod, so that centrifugal circumferential simulated motion is provided, in the rotating process of the cockpit body, the two telescopic rods are utilized to provide actions of pitching, taking off and landing lamps for the cockpit body, and meanwhile, when landing, the landing wheel enters the annular groove, so that the cockpit body truly experiences a landing feeling, the real feeling of the simulated action is comprehensively improved, and the training effect is effectively improved.
However, in practice, the following problems are found in the prior art:
(1) Firstly, the existing flight training simulation cabin cannot simulate vibration transmitted to the cockpit when the airship breaks through a black barrier or collides with birds, so that a driver cannot intuitively perceive the flight attitude, and the training effect is to be improved;
(2) Secondly, the existing flight training cockpit can only accelerate and rotate to improve the flight speed, but the flight is still carried out in a single plane and a single dimension, but the multi-dimension flight cannot be carried out, so that the feeling of training flight is greatly different from the actual flight attitude, and the flight feeling is not true enough.
Disclosure of Invention
The invention aims to provide an intelligent simulation cockpit for flight training, which aims to solve the problems in the background technology.
The technical scheme of the invention is as follows: the intelligent simulation cockpit for flight training comprises a base, wherein the top of the base is rotationally connected with a bottom swivel, two vertical installation cabin plates are fixedly installed on the outer wall of the top of the bottom swivel, the same installation seat is fixedly installed on the opposite side surfaces of the two vertical installation cabin plates, a motor I is fixedly installed on the outer wall of one side of one vertical installation cabin plate, a disc is fixedly installed at the top end of an output shaft of the motor I, a short shaft is fixedly installed on one side of the circumferential outer wall of the disc, the other end of the short shaft is rotationally connected with the outer wall of the installation seat, and the cockpit is installed on the top of the disc;
one of them a vertical installation storehouse board's one side outer wall fixed mounting has a base plate, the outer wall of base plate runs through and rotates and be connected with pivot one, the top and the bottom of pivot one are fixed mounting respectively and are had conical tooth one and gear, the tooth's socket of meshing has been seted up to the outer wall of gear and the outer wall of bottom swivel, gear and bottom swivel meshing, one of them vertical installation storehouse board's one side outer wall rotation is connected with a pivot two, the one end fixed mounting of pivot two has conical tooth two, conical tooth two and conical tooth one mesh, the outer wall fixed mounting of pivot two has sprocket one, the mounting hole has been seted up at the top of mount pad, the inner wall rotation of mounting hole is connected with sprocket two, sprocket two fixed mounting are in motor one's output shaft outer wall, sprocket one is equipped with same chain with sprocket two's outer wall cover.
Preferably, the top outer wall fixed mounting of disc has motor two, the output shaft top fixed mounting of motor two has the connecting plate, one side fixed mounting of connecting plate has the slide, one side outer wall sliding connection of slide has the magnetic plate, the top of magnetic plate and the bottom of cockpit respectively fixed mounting have three basic blocks, the outer wall of basic block has the hydraulic stem through hinged joint.
Preferably, the top of disc has seted up the mounting groove, the inner wall fixed mounting of mounting groove has the electromagnetic ring, the electromagnetic ring sets up under the magnetic plate, the spout has been seted up to one side outer wall of slide, the magnetic plate slides and peg graft in the inner wall of spout.
Preferably, one side of mount pad is provided with the step-in platform, the top of step-in platform has been placed and has been stepped into the staircase, the bottom of step-in staircase is provided with the support, and the bottom of support is provided with the pulley, the bottom fixed mounting of cockpit has two extension blocks, through the support to step-in staircase is realized to the extension block.
Preferably, a notch is formed in one side of the mounting seat, and the walk-in table is matched with the notch in size.
Preferably, a cabin door is connected to the outer wall of one side of the cockpit through a hinge, and a driving seat and a control device are arranged on the inner wall of the cockpit.
Preferably, an air conditioner for simulating a temperature environment is fixedly installed at the top of the cockpit, and a curved screen is arranged at the front end of the cockpit.
Preferably, a plurality of springs are fixedly arranged on the outer wall of the cockpit, connecting blocks are fixedly arranged at one ends of the springs, and one ends of the connecting blocks are fixedly connected with the inner wall of the curved screen.
Preferably, one side of the outer wall of the top of the disc is fixedly provided with a plurality of mounting rods, the top ends of the mounting rods are fixedly provided with deflector rods, and the bottom ends of the deflector rods are provided with a ball head structure
The invention provides an intelligent simulation cockpit for flight training through improvement, which has the following improvement and advantages compared with the prior art:
the method comprises the following steps: when special environment simulation is carried out, such as bird strike accident, the invention can realize intense shaking of the cockpit through the hydraulic rod at the bottom of the cockpit, and can control the current of the electromagnetic ring so as to realize magnetic force control of the electromagnetic ring, so that the distance between the electromagnetic ring and the magnetic plate is changed, namely the height of the cockpit is changed, for example, when a simulated airship breaks through a black barrier, the installation rod and the poking rod poke the curved screen are arranged at the moment, so that a driver can more intuitively feel the vibration of simulated flight of the cockpit, and the training effect of the driver can be improved through the dynamic sensing;
and two,: according to the invention, the motor I is started, the disc is driven to rotate by the motor I, the sprocket II is driven to rotate by the output shaft of the motor I when the motor I rotates, the sprocket I is driven to rotate by the transmission of the chain, the conical tooth II is driven to rotate, the conical tooth I meshed with the conical tooth II is driven to rotate, the rotating shaft I and the gear are driven to rotate, the bottom swivel is driven to rotate by the gear, the rotating effect of two dimensions is realized, the flight feeling is improved, and when the motor I and the motor II are started at the same time, the cockpit can generate the rotating effect of three dimensions, so that the flight simulation effect is more visual and real, and the training effect is improved;
and thirdly,: the intelligent effect of the scheme of the invention also comprises the capability of being controlled by the processor and the controller, the capability of writing in a program in advance, and controlling the flight according to the set program when in driving training, so that the training data is clearer and more visual, and the training effect is convenient to count and track;
fourth, it is: according to the invention, the flight state of the cockpit can be remotely controlled through the remote control center, different flight environments can be set, so that a driver can simulate flight in the cockpit, the electromagnetic ring is electrified, the magnetic plate is pushed upwards under the action of repulsive magnetic force after the electromagnetic ring is electrified, the magnetic plate is separated from the electromagnetic ring, the frictional force between the magnetic plate at the bottom of the cockpit and the electromagnetic ring is reduced to be infinitely close to zero, the flight speed can be improved, and the driver can feel more true.
Drawings
The invention is further explained below with reference to the drawings and examples:
FIG. 1 is a perspective view of the present invention;
FIG. 2 is an enlarged partial view of portion A of FIG. 1;
FIG. 3 is another perspective view of the present invention;
FIG. 4 is a perspective view of a cockpit portion of the present invention;
FIG. 5 is an enlarged partial view of portion B of FIG. 4;
FIG. 6 is a perspective view of a disc portion of the present invention;
fig. 7 is a perspective view of a curved screen section in the present invention.
Reference numerals illustrate:
1. a base; 2. a bottom swivel; 3. a vertical mounting bin plate; 4. a mounting rod; 5. step in a platform; 6. a first motor; 7. a mounting base; 8. a disc; 9. a cockpit; 10. air-conditioning; 11. a curved screen; 12. a connecting block; 13. a spring; 14. a cabin door; 15. a magnetic plate; 16. a hydraulic rod; 17. a slide plate; 18. a chute; 19. a second motor; 20. a connecting plate; 21. a gear; 22. a substrate; 23. a first rotating shaft; 24. conical teeth I; 25. conical teeth II; 26. a sprocket I; 27. a chain; 28. a second rotating shaft; 29. a second chain wheel; 30. a deflector rod; 31. a short shaft; 32. a base block; 33. an electromagnetic ring; 34. a notch; 35. an extension block; 36. walk into the escalator.
Detailed Description
The following detailed description of the present invention clearly and fully describes the technical solutions of the embodiments of the present invention, and it is apparent that the described embodiments are only some embodiments of the present invention, but not all embodiments. All other embodiments, which can be made by those skilled in the art based on the embodiments of the invention without making any inventive effort, are intended to be within the scope of the invention.
The invention provides an intelligent simulation cockpit for flight training through improvement, which comprises the following technical scheme:
as shown in fig. 1-7, an intelligent simulation cockpit for flight training comprises a base 1, wherein the top of the base 1 is rotationally connected with a bottom swivel 2, two vertical installation cabin plates 3 are fixedly installed on the outer wall of the top of the bottom swivel 2, the same installation seat 7 is fixedly installed on the opposite side surfaces of the two vertical installation cabin plates 3, a motor I6 is fixedly installed on the outer wall of one side of one vertical installation cabin plate 3, a disc 8 is fixedly installed at the top end of an output shaft of the motor I6, a short shaft 31 is fixedly installed on one side of the outer wall of the circumference of the disc 8, the other end of the short shaft 31 is rotationally connected with the outer wall of the installation seat 7, and a cockpit 9 is installed on the top of the disc 8;
one side outer wall fixed mounting of one vertical installation storehouse board 3 has a base plate 22, the outer wall of base plate 22 runs through and rotates and is connected with pivot one 23, the top and the bottom of pivot one 23 respectively fixed mounting have conical tooth one 24 and gear 21, the tooth's socket that meshes is seted up to the outer wall of gear 21 and the outer wall of bottom swivel 2, gear 21 and the meshing of bottom swivel 2, one side outer wall rotation of one vertical installation storehouse board 3 is connected with a pivot two 28, the one end fixed mounting of pivot two 28 has conical tooth two 25, conical tooth two 25 and conical tooth one 24 meshing, the outer wall fixed mounting of pivot two 28 has sprocket one 26, the mounting hole has been seted up at the top of mount pad 7, the inner wall rotation of mounting hole is connected with sprocket two 29, sprocket two 29 fixed mounting is in the output shaft outer wall of motor one 6, sprocket one 26 and the outer wall cover of sprocket two 29 are equipped with same root chain 27, and the transmission through chain 27 drives sprocket one 26 and rotates, and then drive conical tooth one 24 of meshing with it rotates, and then drive pivot one 23 and gear 21 rotates, drive bottom swivel 2 through gear 21 and drive two dimensions of motor, the realization of lifting the dimension of motor is three-dimensional, when the effect of the three-dimensional training is realized, and the effect is realized, and the flight cabin is more visual is realized, and is more practical when the effect is realized, and is more than the three, and is more than the dimension 19.
Further, a second motor 19 is fixedly installed on the outer wall of the top of the disc 8, a connecting plate 20 is fixedly installed on the top end of an output shaft of the second motor 19, a sliding plate 17 is fixedly installed on one side of the connecting plate 20, a magnetic plate 15 is slidably connected to the outer wall of one side of the sliding plate 17, three base blocks 32 are fixedly installed on the top of the magnetic plate 15 and the bottom of the cockpit 9 respectively, hydraulic rods 16 are connected to the outer walls of the base blocks 32 through hinges, and when special environment simulation is conducted, such as bird strike accident, severe shaking of the cockpit 9 is achieved through the hydraulic rods 16 at the bottom of the cockpit 9.
Further, the top of the disc 8 is provided with a mounting groove, an electromagnetic ring 33 is fixedly mounted on the inner wall of the mounting groove, the electromagnetic ring 33 is arranged under the magnetic plate 15, a chute 18 is formed on the outer wall of one side of the sliding plate 17, the magnetic plate 15 is slidably inserted into the inner wall of the chute 18, the electromagnetic ring 33 is electrified, the magnetic plate 15 is pushed upwards under the action of repulsive magnetic force after the electrification, the magnetic plate 15 is separated from the electromagnetic ring 33, the friction force between the magnetic plate 15 and the electromagnetic ring 33 at the bottom of the cockpit 9 is reduced to be infinitely close to zero, then the motor II 19 is started to drive the connecting plate 20 to rotate so as to realize flight simulation of the cockpit 9, the current flowing into the electromagnetic ring 33 can be controlled so as to realize magnetic force size control of the electromagnetic ring 33, the distance between the electromagnetic ring 33 and the magnetic plate 15 is changed, namely the height of the cockpit 9 is changed, for example, when a black barrier of a simulated airship is simulated, the mounting rod 4 and a deflector 30 arranged at the moment breaks through the curved screen 11, a driver can feel the simulated flight vibration of the cockpit 9 more intuitively, and the driver can feel the simulated flight vibration of the cockpit 9, and the dynamic training effect can be improved.
Further, a walk-in table 5 is arranged on one side of the mounting seat 7, a walk-in escalator 36 is arranged at the top of the walk-in table 5, a support is arranged at the bottom of the walk-in escalator 36, pulleys are arranged at the bottom of the support, two extension blocks 35 are fixedly arranged at the bottom of the cockpit 9, and the support of the walk-in escalator 36 is achieved through the extension blocks 35.
Further, a gap 34 is formed on one side of the mounting seat 7, the walk-in table 5 is matched with the gap 34 in size, the walk-in table 5 arranged in the scheme does not influence the rotation of the disc 8, a reasonable distance is kept between the walk-in table 5 and the disc 8, the walk-in escalator 36 is pushed to the cockpit 9 through a pulley at the bottom, a driver walks into the cockpit 9 through the walk-in escalator 36, then the cabin door 14 is closed, and the walk-in escalator 36 is withdrawn.
Further, a cabin door 14 is connected to the outer wall of one side of the cockpit 9 through a hinge, a cockpit seat and a control device are arranged on the inner wall of the cockpit 9, and a driver sits on the cockpit seat and realizes simulated driving control through the control device.
Further, the top fixed mounting of cockpit 9 has the air conditioner 10 that is used for simulating the temperature environment, and the front end of cockpit 9 is provided with curved surface screen 11, through the change of air conditioner 10 simulation flight environment for the impression of driver can be more directly perceived, thereby reaches the effect of being in the scene.
Further, the outer wall fixed mounting of cockpit 9 has a plurality of springs 13, and the equal fixed mounting of one end of a plurality of springs 13 has connecting block 12, and the one end of a plurality of connecting blocks 12 is with the inner wall fixed connection of curved surface screen 11, and curved surface screen 11 is the form of encircleing, and the pilot of being convenient for can more audio-visual experience flight environment in cockpit 9.
Further, a plurality of installation rods 4 are fixedly installed on one side of the outer wall of the top of the disc 8, deflector rods 30 are fixedly installed on the top ends of the installation rods 4, the bottom ends of the deflector rods 30 are all arranged to be of a ball head structure, the curved surface screen 11 is convenient to stir through the design of the ball head structure, a driver can feel vibration of the simulated flight of the cockpit 9 more intuitively, and the training effect of the driver can be improved through the dynamic sensing.
The rotation of disc 8 can not be influenced to walk into platform 5 that this scheme set up, keeps having reasonable interval with disc 8, sets up control electromechanical spare part etc. in cockpit 9 and draws, for prior art, the design of this scheme conveniently gets into the driver in cockpit 9 and can carry out the multidimensional operation, simulate the flight gesture under various circumstances in the sky, curved surface screen 11 broadcast different videos makes the perception driving gesture that the driver can be more personally on the scene.
The escalator 36 is pushed to the cockpit 9 through the pulley at the bottom, a driver walks into the cockpit 9 through the escalator 36, then the cabin door 14 is closed, the escalator 36 is withdrawn, the flying state of the cockpit 9 can be remotely controlled through the remote control center, different flying environments can be set, the driver can fly in the cockpit 9 in a simulated manner, the electromagnetic ring 33 is electrified firstly, the magnetic plate 15 is pushed upwards under the action of repulsive magnetic force after the electrification, the magnetic plate 15 is separated from the electromagnetic ring 33, the frictional force between the magnetic plate 15 at the bottom of the cockpit 9 and the electromagnetic ring 33 is reduced to be infinitely close to zero, so that the flying speed can be improved, the driver can feel more real, and then the motor II 19 is started to drive the connecting plate 20 to rotate so as to realize the flight simulation of the cockpit 9;
when special environment simulation is carried out, for example, when a bird strike accident occurs, the hydraulic rod 16 at the bottom of the cockpit 9 can be used for realizing intense shaking of the cockpit 9, the current flowing into the electromagnetic ring 33 can be controlled so as to realize magnetic force control of the electromagnetic ring 33, the distance between the electromagnetic ring 33 and the magnetic plate 15 is changed, namely, the height of the cockpit 9 is changed, for example, when a simulated airship breaks through a black barrier, the installation rod 4 and the deflector rod 30 arranged at the moment stir the curved screen 11, so that a driver can more intuitively feel the vibration of the cockpit 9 simulated flight, and the training effect of the driver can be improved through the dynamic sensing;
in addition, when flying, the motor I6 can be started, the disc 8 is driven to rotate through the motor I6, the chain wheel II 29 is driven to rotate when the output shaft of the motor I6 rotates, the chain wheel I26 is driven to rotate through the transmission of the chain 27, the conical tooth II 25 is driven to rotate, the conical tooth I24 meshed with the chain II is driven to rotate, the rotating shaft I23 and the gear 21 are driven to rotate, the bottom swivel 2 is driven to rotate through the gear 21, the rotating effect of two dimensions is achieved, the flying feeling is improved, and when the motor I6 and the motor II 19 are simultaneously started, the cockpit 9 can generate the rotating effect of three dimensions, so that the flying simulation effect is more visual and real, and the training effect is improved.
The intelligent effect of this scheme is not only limited to above-mentioned expression, still includes can control through treater and controller, can write in advance the procedure, controls the flight according to the procedure that sets for when driving training for the data of training are more clear visual, make things convenient for statistics and tracking training effect.
The previous description is provided to enable any person skilled in the art to make or use the present invention. Various modifications to these embodiments will be readily apparent to those skilled in the art, and the generic principles defined herein may be applied to other embodiments without departing from the spirit or scope of the invention. Thus, the present invention is not intended to be limited to the embodiments shown herein but is to be accorded the widest scope consistent with the principles and novel features disclosed herein.
Claims (7)
1. An intelligent simulation cockpit for flight training, which is characterized in that: the device comprises a base (1), wherein the top of the base (1) is rotationally connected with a bottom swivel (2), two vertical installation bin plates (3) are fixedly installed on the outer wall of the top of the bottom swivel (2), the same installation seat (7) is fixedly installed on the opposite side surfaces of the two vertical installation bin plates (3), a motor I (6) is fixedly installed on the outer wall of one side of the vertical installation bin plates (3), a disc (8) is fixedly installed on the top of an output shaft of the motor I (6), a short shaft (31) is fixedly installed on one side of the outer wall of the circumference of the disc (8), the other end of the short shaft (31) is rotationally connected with the outer wall of the installation seat (7), and a cockpit (9) is installed on the top of the disc (8);
one of the vertical installation warehouse plate (3) is fixedly provided with a base plate (22) on one side outer wall, the outer wall of the base plate (22) penetrates through and is rotationally connected with a first rotating shaft (23), the top end and the bottom end of the first rotating shaft (23) are fixedly provided with a first conical tooth (24) and a gear (21) respectively, the outer wall of the gear (21) and the outer wall of the bottom rotating ring (2) are provided with tooth grooves meshed with each other, the gear (21) is meshed with the bottom rotating ring (2), one of the vertical installation warehouse plate (3) is rotatably connected with a second rotating shaft (28), one end of the second rotating shaft (28) is fixedly provided with a second conical tooth (25), the second conical tooth (25) is meshed with the first conical tooth (24), the outer wall of the second rotating shaft (28) is fixedly provided with a first sprocket (26), the top of the mounting seat (7) is provided with a mounting hole, the inner wall of the mounting hole is rotatably connected with a second sprocket (29), the second sprocket (29) is fixedly provided with the outer wall of the motor (6), and one end of the second sprocket (26) is fixedly provided with the same sprocket (27);
a motor II (19) is fixedly arranged on the outer wall of the top of the disc (8), a connecting plate (20) is fixedly arranged at the top end of an output shaft of the motor II (19), a sliding plate (17) is fixedly arranged on one side of the connecting plate (20), a magnetic plate (15) is slidably connected with the outer wall of one side of the sliding plate (17), three base blocks (32) are respectively and fixedly arranged at the top of the magnetic plate (15) and the bottom of the cockpit (9), and a hydraulic rod (16) is connected with the outer wall of the base block (32) through a hinge;
the top of disc (8) has seted up the mounting groove, the inner wall fixed mounting of mounting groove has electromagnetic ring (33), electromagnetic ring (33) set up under magnetic plate (15), spout (18) have been seted up to the outer wall of one side of slide (17), magnetic plate (15) slip grafting is in the inner wall of spout (18).
2. An intelligent simulation cockpit for flight training according to claim 1 wherein: one side of mount pad (7) is provided with step into platform (5), step into staircase (36) have been placed at the top of step into platform (5), the bottom of step into staircase (36) is provided with the support, and the bottom of support is provided with the pulley, the bottom fixed mounting of cockpit (9) has two extension pieces (35), through extension piece (35) realize the bearing to step into staircase (36).
3. An intelligent simulation cockpit for flight training according to claim 2 wherein: a gap (34) is formed in one side of the mounting seat (7), and the walk-in table (5) is matched with the gap (34) in size.
4. An intelligent simulation cockpit for flight training according to claim 1 wherein: the outer wall of one side of the cockpit (9) is connected with a cabin door (14) through a hinge, and the inner wall of the cockpit (9) is provided with a cockpit seat and a control device.
5. An intelligent simulation cockpit for flight training according to claim 1 wherein: the top of the cockpit (9) is fixedly provided with an air conditioner (10) for simulating a temperature environment, and the front end of the cockpit (9) is provided with a curved screen (11).
6. An intelligent simulation cockpit for flight training according to claim 1 wherein: the outer wall of the cockpit (9) is fixedly provided with a plurality of springs (13), one ends of the springs (13) are fixedly provided with connecting blocks (12), and one ends of the connecting blocks (12) are fixedly connected with the inner wall of the curved screen (11).
7. An intelligent simulation cockpit for flight training according to claim 1 wherein: a plurality of mounting rods (4) are fixedly mounted on one side of the outer wall of the top of the disc (8), deflector rods (30) are fixedly mounted on the top ends of the mounting rods (4), and ball structures are arranged at the bottom ends of the deflector rods (30).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202210874784.5A CN115223420B (en) | 2022-07-25 | 2022-07-25 | Flight training is with intelligent simulation cockpit |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202210874784.5A CN115223420B (en) | 2022-07-25 | 2022-07-25 | Flight training is with intelligent simulation cockpit |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN115223420A CN115223420A (en) | 2022-10-21 |
| CN115223420B true CN115223420B (en) | 2023-12-29 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202210874784.5A Active CN115223420B (en) | 2022-07-25 | 2022-07-25 | Flight training is with intelligent simulation cockpit |
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| CN (1) | CN115223420B (en) |
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