CN115223420A - Flight training is with intelligent simulation cockpit - Google Patents
Flight training is with intelligent simulation cockpit Download PDFInfo
- Publication number
- CN115223420A CN115223420A CN202210874784.5A CN202210874784A CN115223420A CN 115223420 A CN115223420 A CN 115223420A CN 202210874784 A CN202210874784 A CN 202210874784A CN 115223420 A CN115223420 A CN 115223420A
- Authority
- CN
- China
- Prior art keywords
- wall
- cockpit
- fixed mounting
- disc
- mounting
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Granted
Links
- 238000012549 training Methods 0.000 title claims abstract description 47
- 238000004088 simulation Methods 0.000 title claims description 36
- 238000009434 installation Methods 0.000 claims description 15
- 230000008859 change Effects 0.000 claims description 3
- 230000000694 effects Effects 0.000 description 19
- 230000009471 action Effects 0.000 description 7
- 238000000034 method Methods 0.000 description 5
- 230000004888 barrier function Effects 0.000 description 3
- 230000005540 biological transmission Effects 0.000 description 3
- 230000006872 improvement Effects 0.000 description 3
- 230000000007 visual effect Effects 0.000 description 3
- RZVHIXYEVGDQDX-UHFFFAOYSA-N 9,10-anthraquinone Chemical compound C1=CC=C2C(=O)C3=CC=CC=C3C(=O)C2=C1 RZVHIXYEVGDQDX-UHFFFAOYSA-N 0.000 description 2
- 238000013461 design Methods 0.000 description 2
- 230000008447 perception Effects 0.000 description 2
- 230000008569 process Effects 0.000 description 2
- 238000003756 stirring Methods 0.000 description 2
- 238000004891 communication Methods 0.000 description 1
- 230000002079 cooperative effect Effects 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 230000010006 flight Effects 0.000 description 1
- 230000033001 locomotion Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 230000036544 posture Effects 0.000 description 1
- 239000000758 substrate Substances 0.000 description 1
Images
Classifications
-
- G—PHYSICS
- G09—EDUCATION; CRYPTOGRAPHY; DISPLAY; ADVERTISING; SEALS
- G09B—EDUCATIONAL OR DEMONSTRATION APPLIANCES; APPLIANCES FOR TEACHING, OR COMMUNICATING WITH, THE BLIND, DEAF OR MUTE; MODELS; PLANETARIA; GLOBES; MAPS; DIAGRAMS
- G09B9/00—Simulators for teaching or training purposes
- G09B9/02—Simulators for teaching or training purposes for teaching control of vehicles or other craft
- G09B9/08—Simulators for teaching or training purposes for teaching control of vehicles or other craft for teaching control of aircraft, e.g. Link trainer
-
- 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
Landscapes
- 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)
- Toys (AREA)
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 rotatably connected with a bottom rotating ring, the outer wall of the top of the bottom rotating ring is fixedly provided with two vertically-installed bin plates, and the top of a disc is provided with a cockpit.
Description
Technical Field
The invention relates to the technical field of flight simulation training, in particular to an intelligent simulation cockpit for flight training.
Background
Flight training, the technical and tactical training of flying personnel to pilot the plane and use onboard equipment and weapons. Is a main professional training of aviation soldiers. The flight training system comprises piloting airplane training of pilots (the pilots of single-seat airplanes need to carry out training of piloting, shooting, bombing, reconnaissance and the like), piloting, bombing, reconnaissance and airdrop training of air pilots, professional training of personnel of air communication, shooting, machinery, electronics and the like, and training of cooperative actions among members of air crew, wherein flight training is not limited to airplane driving, but also comprises airship driving and the like, and is used for simulating flight under various postures and sensing flight states under various emergency situations.
Through retrieval, 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 the action subassembly, the top of action subassembly is provided with the drive subassembly, the operation subassembly includes movable mounting at the landing ring at 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 matching of the driving motor, the driving gear, the gear ring, the middle shaft sleeve and the central telescopic rod, so that centrifugal circular simulated motion is provided, in the rotating process of the cockpit body, the two adjusting telescopic rods are used for providing head raising, take-off and landing lamp actions for the cockpit body, and meanwhile, in the landing process, the landing wheels enter the annular groove, so that the cockpit body really experiences a landing feeling, the real feeling of simulated action is comprehensively improved, and the training effect is effectively improved.
However, in practice, the prior art has the following problems:
(1) Firstly, the existing flight training simulation cabin can not simulate the vibration conducted to a cockpit when an airship breaks through a black barrier or a bird is knocked, so that a driver can not intuitively perceive the flight attitude, and the training effect needs to be improved;
(2) Secondly, the existing flight training cockpit can only improve the flight speed through accelerated rotation, but the flight is still carried out in a single plane and a single dimension, but the flight with multiple dimensions cannot be carried out, so that the experience of training flight is greatly different from the actual flight attitude, and the flight experience is not real 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: an intelligent simulation cockpit for flight training comprises a base, wherein the top of the base is rotatably connected with a bottom rotating ring, two vertical installation bin plates are fixedly installed on the outer wall of the top of the bottom rotating ring, one installation seat is fixedly installed on one opposite side surface of the two vertical installation bin plates, a first motor is fixedly installed on the outer wall of one side of one vertical installation bin plate, a disc is fixedly installed at the top end of an output shaft of the first motor, 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 rotatably connected with the outer wall of the installation seat, and a cockpit is installed at the top of the disc;
one of them vertical installation storehouse board one side outer wall fixed mounting has a base plate, the outer wall of base plate runs through and the swivelling joint has pivot one, the top and the bottom of pivot one respectively fixed mounting have toper tooth one and gear, engaged with tooth's socket is seted up to the outer wall of gear and the outer wall of bottom swivel, gear and bottom swivel meshing, one of them the rotation of one side outer wall of vertical installation storehouse board is connected with a pivot two, the one end fixed mounting of pivot two has toper tooth two, toper tooth two meshes with toper tooth one, 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 the output shaft outer wall of motor one, 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 sheet, the top of magnetic sheet and the bottom of cockpit respectively fixed mounting have three base block, the outer wall of base block has the hydraulic stem through hinged joint.
Preferably, the top of the disc is provided with a mounting groove, the inner wall of the mounting groove is fixedly provided with an electromagnetic ring, the electromagnetic ring is arranged under the magnetic plate, the outer wall of one side of the sliding plate is provided with a sliding groove, and the magnetic plate is inserted into the inner wall of the sliding groove in a sliding manner.
Preferably, one side of mount pad is provided with the step-in platform, the step-in staircase has been placed at the top of step-in platform, 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 pieces, through the support of extension piece realization to the step-in staircase.
Preferably, a notch is formed in one side of the mounting seat, and the stepping platform is matched with the notch in size.
Preferably, the outer wall of one side of the cockpit is connected with a cabin door through a hinge, and the inner wall of the cockpit is provided with a driving seat and an operating device.
Preferably, an air conditioner used for simulating a temperature environment is fixedly mounted at the top of the cockpit, and a curved screen is arranged at the front end of the cockpit.
Preferably, the outer wall fixed mounting of cockpit has a plurality of springs, and is a plurality of the equal fixed mounting of one end of spring has the connecting block, and is a plurality of the one end of connecting block and the inner wall fixed connection of curved surface screen.
Preferably, a plurality of mounting rods are fixedly mounted on one side of the outer wall of the top of the disc, a plurality of shifting rods are fixedly mounted at the top ends of the mounting rods, and the bottom ends of the shifting rods are arranged to be ball head structures
The invention provides an intelligent simulation cockpit for flight training through improvement, and compared with the prior art, the intelligent simulation cockpit has the following improvements and advantages:
one is as follows: when special environment simulation is carried out, for example, when a bird-hitting accident occurs, violent shaking of the cockpit can be realized through the hydraulic rod at the bottom of the cockpit, the current passing through the electromagnetic ring can be controlled, and further the magnetic force of the electromagnetic ring can be controlled, so that the distance between the electromagnetic ring and the magnetic plate is changed, namely the height of the cockpit is changed;
the second step is as follows: according to the invention, the first motor is started, the first motor drives the disc to rotate, the output shaft of the first motor drives the second sprocket to rotate when rotating, the first sprocket is driven to rotate through the transmission of the chain, the second conical tooth is further driven to rotate, and the first conical tooth meshed with the first conical tooth is further driven to rotate, so that the first rotating shaft and the gear are further driven to rotate;
and thirdly: the intelligent effect of the scheme of the invention also comprises that the flight control system can be controlled by the processor and the controller, and can also write in a program in advance, and the flight control system can control the flight according to the set program during the driving training, so that the training data is clearer and more intuitive, and the statistics and the tracking of the training effect are convenient;
fourthly, the method comprises the following steps: the flight state of the cockpit can be remotely controlled through the remote control center, different flight environments can be set, a pilot 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 friction 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 pilot can feel more real.
Drawings
The invention is further explained below with reference to the figures and examples:
FIG. 1 is a perspective view of the present invention;
FIG. 2 is an enlarged view of a portion A of FIG. 1;
FIG. 3 is a perspective view from another perspective of the present invention;
FIG. 4 is a perspective view of a portion of the cockpit of the present invention;
fig. 5 is a partially enlarged view of a portion B in 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 portion in the present invention.
Description of the reference numerals:
1. a base; 2. a bottom swivel; 3. vertically installing a bin plate; 4. mounting a rod; 5. a step-in platform; 6. a first motor; 7. a mounting seat; 8. a disc; 9. a cockpit; 10. an air conditioner; 11. a curved screen; 12. connecting blocks; 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. a first conical tooth; 25. a second conical tooth; 26. a chain wheel I; 27. a chain; 28. a second rotating shaft; 29. a second chain wheel; 30. a deflector rod; 31. a minor axis; 32. a base block; 33. an electromagnetic ring; 34. a notch; 35. an extension block; 36. and the escalator is stepped.
Detailed Description
The present invention is described in detail below, and technical solutions in the embodiments of the present invention are clearly and completely described, and it is obvious that the described embodiments are only a part of the embodiments of the present invention, and not all of the embodiments. All other embodiments, which can be obtained by a person skilled in the art without making any creative effort based on the embodiments in the present invention, belong to the protection scope of the present invention.
The invention provides an intelligent simulation cockpit for flight training through improvement, and the technical scheme of the invention is as follows:
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 rotatably connected with a bottom rotating ring 2, two vertically-installed bin plates 3 are fixedly installed on the outer wall of the top of the bottom rotating ring 2, the same installation seat 7 is fixedly installed on one side surface of each of the two vertically-installed bin plates 3, a first motor 6 is fixedly installed on the outer wall of one side of one of the vertically-installed bin plates 3, a disc 8 is fixedly installed at the top end of an output shaft of the first motor 6, a short shaft 31 is fixedly installed on one side of the circumferential outer wall of the disc 8, the other end of the short shaft 31 is rotatably connected with the outer wall of the installation seat 7, and a cockpit 9 is installed at the top of the disc 8;
wherein 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 the swivelling joint has pivot one 23, the top and the bottom of pivot one 23 respectively fixed mounting have toper tooth one 24 and gear 21, engaged tooth's socket is seted up to the outer wall of gear 21 and the outer wall of bottom swivel 2, gear 21 meshes with bottom swivel 2, wherein one side outer wall of a vertical installation storehouse board 3 rotates and is connected with a pivot two 28, the one end fixed mounting of pivot two 28 has toper tooth two 25, toper tooth two 25 meshes with toper tooth one 24, 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 overlaps with the outer wall of sprocket two 29 and is equipped with same chain 27, drive sprocket one 26 through the transmission of chain 27 and rotate, and then drive toper tooth two 25 rotations, it rotates to drive sprocket one 24 rather than the meshing again, and then drive the rotation of pivot one 23 and the dimension, thereby the three dimension of the flight two is more three dimension simulation, the flight motor is perceived when the flight effect of the three promotion, the flight is produced, the three more visual training, the three dimension, the flight effect of the three is more visual simulation is realized, the three-dimensional simulation, the flight effect, the flight two flight effect, the flight effect is improved.
Further, a second motor 19 is fixedly mounted on the outer wall of the top of the disc 8, a connecting plate 20 is fixedly mounted at the top end of an output shaft of the second motor 19, a sliding plate 17 is fixedly mounted 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 respectively and fixedly mounted on the top of the magnetic plate 15 and the bottom of the cockpit 9, the outer wall of each base block 32 is connected with a hydraulic rod 16 through a hinge, and when special environment simulation is performed, such as bird collision accidents, violent shaking of the cockpit 9 can be achieved through the hydraulic rod 16 at the bottom of the cockpit 9.
Furthermore, the top of the disk 8 is provided with a mounting groove, the inner wall of the mounting groove is fixedly provided with an electromagnetic ring 33, the electromagnetic ring 33 is arranged under the magnetic plate 15, the outer wall of one side of the sliding plate 17 is provided with a sliding groove 18, the magnetic plate 15 is inserted into the inner wall of the sliding groove 18 in a sliding manner, 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 and is infinitely close to zero, then the motor two 19 is started to drive the connecting plate 20 to rotate to realize the flight simulation of the cockpit 9, the current introduced into the electromagnetic ring 33 can be controlled, the magnetic force of the electromagnetic ring 33 is controlled, the rated 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 the spacecraft is simulated to break through a black barrier, the mounting rod 4 and the deflector rod 30 which are arranged at the moment stir the curved screen 11, so that the pilot can feel the simulated vibration more intuitively, and the flight simulation effect of the spacecraft can be improved.
Further, one side of mount pad 7 is provided with step-in platform 5, and step-in staircase 36 has been placed at the top of step-in platform 5, and the bottom of step-in staircase 36 is provided with the support, and the bottom of support is provided with the pulley, and the bottom fixed mounting of cockpit 9 has two extension pieces 35, realizes the bearing to step-in staircase 36 through extending piece 35.
Further, a gap 34 is formed in one side of the mounting seat 7, the stepping platform 5 is matched with the gap 34 in size, the stepping platform 5 arranged in the scheme cannot influence the rotation of the disc 8, a reasonable distance is kept between the disc 8 and the stepping platform 5, the stepping escalator 36 is pushed to the cockpit 9 through a pulley at the bottom, a driver walks into the cockpit 9 through the stepping escalator 36, then the cabin door 14 is closed, and the stepping 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 an operation and control device are arranged on the inner wall of the cockpit 9, and a driver sits on the cockpit seat and realizes the operation and control of the simulated driving 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 driver's impression can be more directly perceived, thereby reaches the effect of being personally on 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, the one end of a plurality of connecting blocks 12 and 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 be more audio-visual impression flight environment in cockpit 9.
Further, top outer wall one side fixed mounting of disc 8 has many installation poles 4, and the equal fixed mounting in top of many installation poles 4 has driving lever 30, and the bottom of many driving levers 30 all sets up to the bulb structure, and the design convenience of bulb structure is stirred curved surface screen 11 for the driver can be more audio-visual experiences the vibrations of cockpit 9 simulation flights, through this kind of dynamic perception, can promote driver's training effect.
The step-in platform 5 that this scheme set up can not influence the rotation of disc 8, keeps having reasonable interval with disc 8, sets up in the cockpit 9 and controls electromechanical spare part etc. and be the drawing, and for prior art, the driver that the design of this scheme conveniently got into in the cockpit 9 can carry out the operation of multidimension degree, flight gesture under the various circumstances in the simulation air, and the video of curved surface screen 11 broadcast difference makes the driver can be more personally on the scene experience driving gesture.
The step-in staircase 36 is pushed to the cockpit 9 through the pulleys at the bottom, a driver walks into the cockpit 9 through the step-in staircase 36, then the cabin door 14 is closed, the step-in staircase 36 is removed, the flight state of the cockpit 9 can be remotely controlled through the remote control center at the moment, different flight environments can be set, the driver can simulate flight in the cockpit 9, 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 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, the flight 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 to realize flight simulation of the cockpit 9;
when a special environment simulation is carried out, for example, when a bird-hitting accident occurs, the severe shaking of the cockpit 9 can be realized through the hydraulic rod 16 at the bottom of the cockpit 9, the current passing through the electromagnetic ring 33 can be controlled, and the magnetic force of the electromagnetic ring 33 can be controlled, so that 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 the simulation airship breaks through a black barrier, the mounting rod 4 and the shift lever 30 which are arranged at the moment stir the curved screen 11, so that a driver can more intuitively feel the vibration of the simulated flight of the cockpit 9, and the training effect of the driver can be improved through the dynamic perception;
in addition, during flying, the first motor 6 can be started, the first motor 6 drives the disc 8 to rotate, an output shaft of the first motor 6 drives the second chain wheel 29 to rotate, the first chain wheel 26 is driven to rotate through the transmission of the chain 27, the second conical tooth 25 is further driven to rotate, the first conical tooth 24 meshed with the first conical tooth is further driven to rotate, the first rotating shaft 23 and the first gear 21 are further driven to rotate, the first gear 21 drives the bottom rotating ring 2 to rotate, the rotating effect of two dimensions is achieved, flying feeling is improved, when the first motor 6 and the second motor 19 are started simultaneously, the cockpit 9 can generate the rotating effect of three dimensions, the flying simulation effect is enabled to be more visual and real, and the training effect is improved.
The intelligent effect of this scheme not only limits to above-mentioned expression, still includes to control through treater and controller, can also write into the procedure in advance, controls the flight according to the procedure that has set for when driving the training for the data of training are more clear direct-viewing, make things convenient for statistics and trail the 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 (9)
1. The utility model provides a flight training is with intelligent simulation cockpit which characterized in that: the device comprises a base (1), wherein the top of the base (1) is rotatably connected with a bottom rotating ring (2), the outer wall of the top of the bottom rotating ring (2) is fixedly provided with two vertically-installed bin plates (3), one opposite side surface of the two vertically-installed bin plates (3) is fixedly provided with a same installing seat (7), the outer wall of one side of one of the vertically-installed bin plates (3) is fixedly provided with a first motor (6), the top end of an output shaft of the first motor (6) is fixedly provided with a disc (8), one side of the circumferential outer wall of the disc (8) is fixedly provided with a short shaft (31), the other end of the short shaft (31) is rotatably connected with the outer wall of the installing seat (7), and the top of the disc (8) is provided with a cockpit (9);
wherein one side outer wall fixed mounting of vertical installation storehouse board (3) has one base plate (22), the outer wall of base plate (22) runs through and the swivelling joint has pivot one (23), the top and the bottom of pivot one (23) respectively fixed mounting have conical tooth one (24) and gear (21), the engaged with tooth's socket is seted up to the outer wall of outer wall and bottom change (2) of gear (21), gear (21) and bottom change (2) meshing, one of them one side outer wall of vertical installation storehouse board (3) rotates and is connected with one 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 are in the output shaft outer wall of motor one (6), the same chain wheel (26) is equipped with the outer wall (27 chain wheel two sprocket (29).
2. The intelligent simulation cockpit for flight training of claim 1, wherein: the utility model discloses a motor driving device, including disc (8), the top outer wall fixed mounting of disc (8) has motor two (19), the output shaft top fixed mounting of motor two (19) has connecting plate (20), one side fixed mounting of connecting plate (20) has slide (17), one side outer wall sliding connection of slide (17) has magnetic sheet (15), there are three base block (32) top of magnetic sheet (15) and the bottom of cockpit (9) fixed mounting respectively, there is hydraulic stem (16) outer wall of base block (32) through hinged joint.
3. The intelligent simulation cockpit for flight training of claim 2, wherein: the disc-shaped magnetic bearing is characterized in that the top of the disc (8) is provided with a mounting groove, the inner wall of the mounting groove is fixedly provided with an electromagnetic ring (33), the electromagnetic ring (33) is arranged under the magnetic plate (15), the outer wall of one side of the sliding plate (17) is provided with a sliding groove (18), and the magnetic plate (15) is inserted into the inner wall of the sliding groove (18) in a sliding manner.
4. The intelligent simulation cockpit for flight training of claim 3, wherein: one side of mount pad (7) is provided with step-in platform (5), step-in staircase (36) have been placed at the top of step-in platform (5), the bottom of step-in 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 to extend piece (35), through extend piece (35) and realize the bearing to step-in staircase (36).
5. The intelligent simulation cockpit for flight training of claim 4, wherein: a gap (34) is formed in one side of the mounting seat (7), and the stepping platform (5) is matched with the gap (34) in size.
6. The intelligent simulation cockpit for flight training of claim 1, wherein: the outer wall of one side of the cockpit (9) is connected with a cabin door (14) through a hinge, and a cockpit seat and an operation device are arranged on the inner wall of the cockpit (9).
7. The intelligent simulation cockpit for flight training of claim 1, wherein: the top of cockpit (9) fixed mounting has air conditioner (10) that are used for the simulation temperature environment, and the front end of cockpit (9) is provided with curved surface screen (11).
8. The intelligent simulation cockpit for flight training of claim 1, wherein: the outer wall fixed mounting of cockpit (9) has a plurality of springs (13), and is a plurality of the equal fixed mounting of one end of spring (13) has connecting block (12), and is a plurality of the one end of connecting block (12) and the inner wall fixed connection of curved surface screen (11).
9. The intelligent simulation cockpit for flight training of 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), a shifting rod (30) is fixedly mounted on the top end of each mounting rod (4), and the bottom ends of the shifting rods (30) are all arranged to be of a ball head structure.
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 true CN115223420A (en) | 2022-10-21 |
| CN115223420B CN115223420B (en) | 2023-12-29 |
Family
ID=83613906
Family Applications (1)
| 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 |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN115223420B (en) |
Citations (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| KR20180055535A (en) * | 2016-11-17 | 2018-05-25 | 주식회사 바로텍시너지 | An aircraft simulator capable of rotating in the roll direction and vibrating in the cockpit |
| CN110767026A (en) * | 2019-10-29 | 2020-02-07 | 天津大学 | Automatic drive machine learning device |
| CN210466838U (en) * | 2019-06-30 | 2020-05-05 | 卓尔飞机制造（武汉）有限公司 | Flight simulator |
| CN211207601U (en) * | 2019-10-11 | 2020-08-07 | 中国人民解放军空军工程大学 | Airplane cockpit model for drilling simulation |
| CN212161017U (en) * | 2020-07-06 | 2020-12-15 | 滕振宇 | Virtual simulation operation platform |
| CN214897072U (en) * | 2021-07-16 | 2021-11-26 | 西安兴航航空仿真科技有限公司 | Multipurpose training simulation cabin |
| CN113763776A (en) * | 2021-10-24 | 2021-12-07 | 中仿智能科技（上海）股份有限公司 | Flight training is with simulation cockpit |
| JP2021189229A (en) * | 2020-05-26 | 2021-12-13 | 三菱重工業株式会社 | Simulator device |
| CN215932906U (en) * | 2021-10-24 | 2022-03-01 | 中仿智能科技（上海）股份有限公司 | Flight training is with simulation cockpit |
-
2022
- 2022-07-25 CN CN202210874784.5A patent/CN115223420B/en active Active
Patent Citations (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| KR20180055535A (en) * | 2016-11-17 | 2018-05-25 | 주식회사 바로텍시너지 | An aircraft simulator capable of rotating in the roll direction and vibrating in the cockpit |
| CN210466838U (en) * | 2019-06-30 | 2020-05-05 | 卓尔飞机制造（武汉）有限公司 | Flight simulator |
| CN211207601U (en) * | 2019-10-11 | 2020-08-07 | 中国人民解放军空军工程大学 | Airplane cockpit model for drilling simulation |
| CN110767026A (en) * | 2019-10-29 | 2020-02-07 | 天津大学 | Automatic drive machine learning device |
| JP2021189229A (en) * | 2020-05-26 | 2021-12-13 | 三菱重工業株式会社 | Simulator device |
| CN212161017U (en) * | 2020-07-06 | 2020-12-15 | 滕振宇 | Virtual simulation operation platform |
| CN214897072U (en) * | 2021-07-16 | 2021-11-26 | 西安兴航航空仿真科技有限公司 | Multipurpose training simulation cabin |
| CN113763776A (en) * | 2021-10-24 | 2021-12-07 | 中仿智能科技（上海）股份有限公司 | Flight training is with simulation cockpit |
| CN215932906U (en) * | 2021-10-24 | 2022-03-01 | 中仿智能科技（上海）股份有限公司 | Flight training is with simulation cockpit |
Also Published As
| Publication number | Publication date |
|---|---|
| CN115223420B (en) | 2023-12-29 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| US9789411B2 (en) | Applied layout in virtual motion-acceleration spherical simulator | |
| US5009598A (en) | Flight simulator apparatus using an inoperative aircraft | |
| US5240416A (en) | Simulator apparatus employing actual craft and simulators | |
| US6902402B2 (en) | Flight simulator | |
| EP0808493B1 (en) | Improved flight simulator | |
| CN206097572U (en) | Flight simulator of triaxial qxcomm technology | |
| CN104637364A (en) | Rotating flight simulator | |
| CN112102682B (en) | Aircraft driving training system and method based on 5G communication | |
| CN102013187A (en) | Flight simulator system with persistent overload simulation capability | |
| US20010041326A1 (en) | Simulator for aircraft flight training | |
| CN102789709A (en) | Mechanical structure for multi-axis wireless movement method of flight simulator | |
| CN114514055B (en) | Themed aerial vehicle entertainment platform for providing dynamically coordinated performances | |
| CN113674575A (en) | Virtual reality parachute jumping simulation training somatosensory control device and method | |
| CN113053205A (en) | Air combat confrontation virtual training system based on virtual reality VR | |
| CN115223420A (en) | Flight training is with intelligent simulation cockpit | |
| CN113763776A (en) | Flight training is with simulation cockpit | |
| CN201783222U (en) | Airplane cinema capable of moving and simulating flight | |
| CN212208630U (en) | Flight training simulation system | |
| CN215932906U (en) | Flight training is with simulation cockpit | |
| CN114404938B (en) | Virtual reality method | |
| CN206265328U (en) | Unmanned plane | |
| CN111477065B (en) | Dynamic simulator of acceleration based on magnetic suspension | |
| KR20220016872A (en) | motion system | |
| CN108109470B (en) | Servo control rocker operating device for simulating small aircraft | |
| RU2653448C1 (en) | Simulator of space flight of a space vehicle |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| GR01 | Patent grant | ||
| GR01 | Patent grant |