CN110853454A - Flight teaching simulation cabin device - Google Patents
Flight teaching simulation cabin device Download PDFInfo
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- CN110853454A CN110853454A CN201911033645.4A CN201911033645A CN110853454A CN 110853454 A CN110853454 A CN 110853454A CN 201911033645 A CN201911033645 A CN 201911033645A CN 110853454 A CN110853454 A CN 110853454A
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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
- G09B9/16—Ambient or aircraft conditions simulated or indicated by instrument or alarm
- G09B9/165—Condition of cabin, cockpit or pilot's accessories
-
- 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
- G09B9/16—Ambient or aircraft conditions simulated or indicated by instrument or alarm
- G09B9/20—Simulation or indication of aircraft attitude
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- Aviation & Aerospace Engineering (AREA)
- Business, Economics & Management (AREA)
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- Management, Administration, Business Operations System, And Electronic Commerce (AREA)
Abstract
The invention discloses a flight teaching simulation cabin device which comprises a circular base, wherein a guardrail escalator device is arranged on the circular base, a controller is arranged on one side of the circular base, an automatic adjusting type simulation cabin device is arranged above the circular base, and a back pushing feeling simulation seat device is arranged inside the automatic adjusting type simulation cabin device. Drive the rotation platform through the rotating electrical machines and rotate, it goes up and down to drive the simulation cabin through hydraulic cylinder, thereby control the simulation cabin and simulate various flight states of flight in-process, cooperation through accommodate motor and hydraulic oil solenoid valve, meet the air current and lead to the aircraft vibrations to simulate to the flight in-process, thereby various states when the accurate aircraft flight that simulates, the effectual effect of flight teaching that has promoted, make the student can experience various states when the aircraft flight in the simulation cabin, increase student's experience.
Description
Technical Field
The invention relates to the field of flight teaching related equipment, in particular to a flight teaching simulation cabin device.
Background
Airplanes are increasingly becoming indispensable vehicles for modern civilization, and the airplanes profoundly change and influence the lives of people. A typical aircraft simulation model restores the architecture and layout in the real aircraft cabin. However, most of these models are fixed, and cannot simulate the state of the aircraft in the cabin during flight.
In a CN201820927726.3 patent, a flight simulation experience cockpit, by the arrangement of a modeling wall and a transparent glass fiber reinforced plastic shell, an experiencer standing in the simulation cockpit shell can simulate various environments in the flight process through the modeling wall, so that the experience of the flight simulation experience cockpit is enhanced; the mobile platform is provided with the cavity for accommodating the expansion plate, so that the floor area of the auxiliary boarding assembly is reduced.
However, in the flight teaching, because the simulation cabin body cannot perform corresponding angle adjustment according to the real-time situation of the flight, the existing simulation cabin cannot accurately simulate various states of the aircraft in the flight process, and the effect of the flight teaching is poor.
Disclosure of Invention
The invention aims to solve the problems, and designs a flight teaching simulation cabin device which has an automatic adjustment function and solves the problem that the existing flight simulation cabin cannot adjust the state of the simulation cabin in real time according to a flight program.
The technical scheme of the invention is that the flight teaching simulation cabin device comprises a circular base, wherein a guardrail staircase device is arranged on the circular base, a controller is arranged on one side of the circular base, an automatic adjusting type simulation cabin device is arranged above the circular base, and a back pushing feeling simulation seat device is arranged in the automatic adjusting type simulation cabin device;
the automatic regulation type simulation cabin device comprises a circular base, a circular groove is formed above the circular base, a plurality of rolling holes are formed in the inner side surface of the circular groove, the rolling holes are uniformly distributed on the circular groove, rolling balls are movably mounted in the rolling holes, a motor groove is formed in one end of the lower surface in the circular groove, a rotating motor is mounted in the motor groove, a rotating gear is mounted at the rotating end of the rotating motor, a rotating platform is arranged in the circular groove and is in movable contact with the rolling balls, an annular gear groove guide rail is mounted at the outer end of the lower surface of the rotating platform and is meshed with the rotating gear, four hydraulic cylinders are mounted at four corners above the rotating platform, a fixed seat is mounted at the telescopic end of each hydraulic cylinder, a rotating ball groove is formed in the side surface of one side of the fixed seat, and a rotating ball is movably mounted in the rotating ball, a simulation cabin is arranged among the four hydraulic oil cylinders, the simulation cabin is connected with the rotating ball through a rotating shaft, a reinforcing baffle is arranged between the rotating shaft and the simulation cabin, and a vibration adjusting device is arranged on the rotating platform;
the vibration adjusting device comprises a rotating platform, wherein an adjusting box is installed on one side of the upper portion of the rotating platform, an adjusting motor is installed at the center of the inner portion of the adjusting box, an eccentric wheel is installed at the rotating end of the adjusting motor, adjusting sleeves are installed on the left side and the right side of the adjusting box respectively, a moving piston is installed in each adjusting sleeve and slides in each adjusting sleeve, the moving piston is movably connected with a flange of the eccentric wheel through a connecting rod, the adjusting sleeves are connected with two hydraulic oil cylinders on one corresponding side of the adjusting sleeves through hydraulic oil pipes, and each hydraulic oil electromagnetic valve is installed on each hydraulic oil branch pipe (25).
The back-pushing feeling simulation seat device comprises a simulation seat arranged in a simulation cabin, a friction pushing seat movably arranged at the rear part in the simulation seat, electric telescopic rods arranged at two sides below the friction pushing seat, a friction baffle plate arranged at the telescopic end of each electric telescopic rod, two square sliding frames arranged at the lower end at the rear part in the simulation seat, two ends of the friction pushing seat inserted into the square sliding frames, a transmission groove arranged at the rear end below the inner part of the simulation seat, transmission rollers arranged at two sides in the transmission groove, a transmission belt sleeved between the two transmission rollers and connected with the transmission groove through a transmission shaft and a transmission bearing, a plurality of strip-shaped friction plates arranged on the transmission belt and evenly distributed on the transmission belt, a variable frequency motor is installed in the transmission groove, and the rotating end of the variable frequency motor is connected with the transmission shaft through a gear set.
The guardrail escalator device comprises a first protective guardrail arranged at the outer end of the upper surface of the circular base, a step escalator arranged at one end of the upper surface of the circular base, second protective guardrails arranged on two sides of the step escalator, and two ends of the two protective guardrails and the two ends of the first protective guardrail are fixedly connected respectively.
And a supporting baffle is arranged above the center of the inside of the transmission groove and is connected with the transmission belt in a sliding manner.
And the hydraulic oil electromagnetic valves on the two hydraulic oil branch pipes are opened and closed, so that the simulation cabin can simulate three different vibration modes.
The interior of the simulation cabin is the same as the interior of the aircraft cockpit.
The simulation seat is provided with a safety belt, and the safety belt is in a tight state after being bound.
The strip-shaped friction plate is in sliding contact with the friction baffle.
The flight teaching simulation cabin device manufactured by the technical scheme of the invention has the following beneficial effects:
the simulation cabin device drives the rotating platform to rotate through the rotating motor and drives the simulation cabin to lift through the hydraulic oil cylinder, so that the simulation cabin is controlled to simulate various flight states in the flight process, and the airplane vibration caused by the air flow in the flight process is simulated through the matching of the adjusting motor and the hydraulic oil electromagnetic valve, so that various states of the airplane in the flight process are accurately simulated, the flight teaching effect is effectively improved, a student can feel various states of the airplane in the flight process in the simulation cabin, and the experience of the student is improved;
this simulation cabin device drives the removal that the friction impeld the seat through inverter motor's rotational speed regulation to exert the motive force to the student back on the simulation seat, cooperate binding of safety belt simultaneously, make the student can experience the back of the body sense that pushes away of aircraft flight in-process, make the more true of flight teaching simulation.
Drawings
FIG. 1 is a schematic structural diagram of a flight teaching simulation cabin device according to the present invention;
FIG. 2 is a schematic structural diagram of a back-pushing feeling simulation chair device according to the present invention;
FIG. 3 is a cross-sectional view of a push back feel simulation chair set in accordance with the present invention;
in the figure, 1, a round base; 2. a controller; 3. a circular groove; 4. rolling the hole; 5. a rolling ball; 6. a motor groove; 7. a rotating electric machine; 8. a rotating gear; 9. rotating the platform; 10. an annular gear groove guide; 11. a hydraulic cylinder; 12. a fixed seat; 13. rotating the ball groove; 14. rotating the ball; 15. a simulation cabin; 16. a rotating shaft; 17. reinforcing the baffle plate; 18. an adjusting box; 19. adjusting the motor; 20. an eccentric wheel; 21. an adjustment sleeve; 22. moving the piston; 23. a connecting rod; 24. A hydraulic oil pipe; 25. a hydraulic oil branch pipe; 26. a hydraulic oil solenoid valve; 27. simulating a seat; 28. A friction pushing seat; 29. an electric telescopic rod; 30. a friction baffle; 31. a square sliding frame; 32. A transmission groove; 33. a driving roller; 34. a drive shaft; 35. a drive bearing; 36. a drive belt; 37. a strip-shaped friction plate; 38. a variable frequency motor; 39. a gear set; 40. a first protective guard rail; 41. a step ladder; 42. a second protective guard rail; 43. a support baffle; 44. a safety belt.
Detailed Description
The invention is described in detail below with reference to the accompanying drawings, as shown in FIGS. 1-3, in this embodiment:
in the device, the device supplies power by being connected with an external power supply, the external power supply is electrically connected with the controller 2, the rotating motor 7, the hydraulic oil cylinder 11, the simulation cabin 15, the adjusting motor 19, the hydraulic oil electromagnetic valve 26, the electric telescopic rod 29 and the variable frequency motor 38 to supply power, the controller 2 is a PLC (programmable logic controller) of an AFPX-C30T model, a signal receiving end of the controller 2 is electrically connected with a signal sending end of a control system inside the simulation cabin 15, and a control signal sending end of the controller 2 is electrically connected with the rotating motor 7, the hydraulic oil cylinder 11, the adjusting motor 19, the hydraulic oil electromagnetic valve 26, the electric telescopic rod 29 and the variable frequency motor 38 through transistors respectively, so that the operation of the device is controlled.
The invention is characterized in that the structural design of the automatic regulation type simulation cabin device is combined with an attached figure 1, the automatic regulation type simulation cabin device comprises a circular base 1, a circular groove 3 is arranged above the circular base 1, a plurality of rolling holes 4 are arranged on the inner side surface of the circular groove 3, the rolling holes 4 are uniformly distributed on the circular groove 3, rolling balls 5 are movably arranged in the rolling holes 4, a motor groove 6 is arranged at one end of the inner lower surface of the circular groove 3, a rotating motor 7 is arranged in the motor groove 6, a rotating gear 8 is arranged at the rotating end of the rotating motor 7, a rotating platform 9 is arranged in the circular groove 3, the rotating platform 9 is in movable contact with the rolling balls 5, an annular gear groove guide rail 10 is arranged at the outer end of the lower surface of the rotating platform 9, the annular gear groove guide rail is of an annular structure with the central point of, the annular gear groove guide rail 10 is meshed with the rotating gear 8, and the rotating motor can be a servo motor or a stepping motor, and mainly selects a positive and negative rotating motor with controllable stroke; because the rotating platform is positioned on the rolling balls, the rolling balls roll when the rotating platform rotates, so that the friction force applied to the rotating platform during rotation is small, and in order to further reduce the friction force applied to the rotating platform during rotation, lubricating oil is added into each rolling hole, so that the friction force applied to the rotating platform is reduced; four hydraulic oil cylinders 11 are arranged at four corners above a rotary platform 9, a fixed seat 12 is arranged at the telescopic end of each hydraulic oil cylinder 11, a rotary ball groove 13 is formed in the side surface of one side of the fixed seat 12, a rotary ball 14 is movably arranged in the rotary ball groove 13, a simulation cabin 15 is arranged among the four hydraulic oil cylinders 11, the simulation cabin 15 is connected with the rotary ball 14 through a rotary shaft 16, a reinforcing baffle 17 is arranged between the rotary shaft 16 and the simulation cabin 15, an adjusting box 18 is arranged at one side above the rotary platform 9, an adjusting motor 19 is arranged at the center inside of the adjusting box 18, an eccentric wheel 20 is arranged at the rotary end of the adjusting motor 19, adjusting sleeves 21 are arranged at two sides inside the adjusting box 18, a movable piston 22 is arranged in each adjusting sleeve 21, the movable piston 22 is connected with the adjusting sleeves 21 in a sliding manner, the movable piston 22 is connected with flanges of, the two hydraulic oil pipes 24 are respectively and fixedly connected with the four hydraulic oil cylinders 11 through hydraulic oil branch pipes 25, hydraulic oil electromagnetic valves 26 are installed on the hydraulic oil branch pipes 25, and the hydraulic oil electromagnetic valves 26 on the two hydraulic oil branch pipes 25 are opened and closed, so that the simulation cabin 15 can simulate three different vibration modes; drive rotation platform 9 through rotating electrical machines 7 and rotate, it goes up and down to drive simulation cabin 15 through hydraulic cylinder 11, thereby control simulation cabin 15 simulates the various flight states of flight in-process, simultaneously through the effect of roll ball 5, the noise that produces when can effectually avoiding rotating, the reciprocating motion of the inside removal piston 22 of rotation adjusting sleeve 21 through adjusting motor 19, thereby make hydraulic cylinder 11 carry out the regulation of miniscope, rock the mode through opening and close the left and right sides that constitutes through hydraulic oil solenoid valve 26 simultaneously, rock the mode around, rock the mode to the opposite angle, thereby make simulation cabin 15 can simulate out the various circumstances of rocking when the aircraft meets the air current, make simulation cabin 15 simulation effect better reality, thereby improve the effect of flight teaching.
The invention is characterized in that the structural design of the back-pushing feeling simulation seat device is combined with the attached drawings 2 and 3, the back-pushing feeling simulation seat device comprises a simulation cabin 15, a simulation seat 27 is arranged in the simulation cabin 15, a friction pushing seat 28 is movably arranged at the rear part in the simulation seat 27, electric telescopic rods 29 are arranged at two sides below the friction pushing seat 28, a friction baffle 30 is arranged at the telescopic end of each electric telescopic rod 29, two square sliding frames 31 are arranged at the lower end at the rear part in the simulation seat 27, two ends of the friction pushing seat 28 are inserted into the square sliding frames 31, the friction pushing seat 28 is connected with the sliding frames 31 in a sliding manner, a transmission groove 32 is arranged at the rear end below the simulation seat 27, transmission rollers 33 are arranged at two sides in the transmission groove 32, the transmission rollers 33 are connected with the transmission groove 32 through transmission shafts 34 and transmission bearings 35, a transmission belt 36 is sleeved between the two, a plurality of strip-shaped friction plates 37 are arranged on the transmission belt 36, the strip-shaped friction plates 37 are uniformly distributed on the transmission belt 36, a variable frequency motor 38 is arranged in the transmission groove 32, and the rotating end of the variable frequency motor 38 is connected with the transmission shaft 34 through a gear set 39; through inverter motor 38's rotational speed regulation, drive transmission belt 36's variable speed rotation, through the friction fit between bar friction plate 37 and the friction baffle 30, rethread electric telescopic handle 29 adjusts the frictional force between bar friction plate 37 and the friction baffle 30, makes friction propelling movement seat 28 produce different driving force to make simulation seat 27 produce to push away the back of the body to the student and feel, make the student can adapt to the back of the body sense of pushing away of aircraft flight in-process, the effectual authenticity that has promoted simulation cabin 15 simulation.
In this device, guardrail staircase device carries out circular base 1's protection through protection guardrail 40, supplies students to go on simulation cabin 15 from top to bottom through step staircase 41 and protection guardrail two 42, makes things convenient for student's use, also can effectually avoid simulation cabin 15 operation in-process simultaneously, and the student avoids the student be injured on rushing into circular base 1 by mistake.
The working principle of the device is as follows: when flight education needs to be carried out by using the simulation cabin 15, the device is firstly connected with an external power supply;
at the moment, the student climbs the circular base 1 through the step type staircase 41, opens the simulation cabin 15, enables the student to enter the simulation cabin 15, and the student sits on the simulation seat 27 to bind the safety belt 44 and tighten the safety belt 44 to enable the safety belt to be in a tight state, and at the moment, closes the simulation cabin 15;
at the moment, the trainee can carry out flight teaching simulation through the simulation equipment in the simulation cabin 15, and when the trainee carries out various flight simulation operations through the simulation equipment in the flight teaching simulation process, the flight information of the simulation cabin of the simulation equipment is transmitted to the controller 2, and the controller 2 controls the simulation cabin 15 to carry out synchronous operation according to the simulation information;
the situation of steering flight when the simulation cabin 15 flies is controlled by controlling the work of the rotating motor 7, the rotating motor 7 rotates to drive the rotating gear 8 to rotate, the rotating gear 8 drives the rotating platform 9 to start rotating by meshing with the annular gear groove guide rail 10, meanwhile, the rotating platform 9 is stabilized in the circular groove 3 by the gravity of the rotating platform 9 and an upper device, and the rotating platform 9 can stably rotate in the circular groove 3 by the rolling contact of the rolling balls 5 in the rolling holes 4, so that the simulation cabin 15 is controlled to perform corresponding angle adjustment according to the flight information;
the lifting of the hydraulic oil cylinders 11 is controlled, the simulation cabin 15 is controlled to simulate the situation that the airplane body performs various actions when the airplane flies, the four hydraulic oil cylinders 11 are connected with oil paths for supplying oil and can be lifted synchronously, so that the fixed seat 12 is driven to start height adjustment, and one side of the simulation cabin 15 can be driven to lift and lower through the synchronous lifting of two adjacent hydraulic oil cylinders and the action of the rotating ball 14 in the rotating ball groove 13 of the fixed seat 12, so that the situation of the inclination of the airplane body in the airplane driving process is simulated; the height positions of the four fixed seats 12 are controlled through the integral lifting or the lifting of every two of the four hydraulic oil cylinders 11, so that the simulation cabin 15 is controlled in real time to adjust the angle according to the flight information, the simulation cabin 15 can perform head raising action, head lowering action and inclined flight action, and the actual situation under the current flight state is simulated in real time;
the simulation cabin 15 is controlled to simulate the condition that the aircraft vibrates when encountering air flow by controlling the operation of the adjusting motor 19, the switches of the four hydraulic oil electromagnetic valves 26 are controlled according to the actual condition of the air flow encountered in the flight information before the adjusting motor 19 works, so that the corresponding modes of a left-right shaking mode, a front-back shaking mode and a diagonal shaking mode are selected, and after the mode is selected, the corresponding hydraulic oil electromagnetic valves 26 are controlled to be opened, so that the adjusting motor 19 is controlled to work;
the adjusting motor 19 rotates to drive the eccentric wheel 20 to rotate, the eccentric wheel 20 drives the movable piston 22 to move in a reciprocating manner in the adjusting sleeve 21 through the connecting rod 23, so that hydraulic oil in the adjusting sleeve 21 is injected into the hydraulic oil cylinder 11 through the hydraulic oil pipe 24 and the hydraulic oil branch pipe 25, and the hydraulic oil cylinder 11 is controlled to perform reciprocating expansion in a small range;
when the eccentric wheel 20 drives the two moving pistons 22 to reciprocate through the connecting rod 23, the moving directions of the two moving pistons 22 are just opposite, so that the flowing directions of hydraulic oil in the two adjusting sleeves 21 are opposite, and the four hydraulic oil cylinders 11 are stretched in a small range through the rotation of the adjusting motor 19, so that the simulation cabin 15 is driven to simulate the situation that the aircraft vibrates after encountering air flow;
when the four hydraulic oil cylinders are lifted integrally or on one side greatly, the hydraulic oil electromagnetic valves on the four hydraulic oil pipes are closed, the adjusting motor is in a stop state, and the four hydraulic oil cylinders are synchronously supplied with pressure or supplied with pressure in pairs by external oil ways;
during the takeoff process of the airplane, a driver can feel obvious push-back feeling, when a trainee takes off in a simulation mode, the trainee is fixed on the simulation seat 27 through the action of the safety belt 44, when the simulated takeoff is started, the variable frequency motor 38 is controlled to start working, the variable frequency motor 38 rotates to drive the transmission shaft 34 to rotate through the gear set 39, the transmission shaft 34 drives the transmission roller 33 to rotate, so that the transmission belt 36 starts rotating, the electric telescopic rod 29 is controlled to extend and retract at the moment, so that the height of the friction baffle 30 is adjusted, the friction force between the strip-shaped friction plate 37 on the transmission belt 36 and the friction baffle 30 is adjusted to a proper position, the friction push seat 28 generates forward thrust through the rotation of the transmission belt 36 and the action of the friction force between the strip-shaped friction plate 37 and the friction baffle 30, so that the thrust is applied to the back position of the simulation seat 27, at this time, the trainee feels a back pushing feeling by the action of the safety belt 44 and the back of the trainee is sufficiently contacted with the back position of the dummy seat 27;
the variable frequency motor 38 performs variable frequency adjustment according to the actual situation during takeoff, so that the rotating speed of the variable frequency motor 38 is adjusted according to the real-time situation during takeoff of the airplane, the back pushing feeling during takeoff of the airplane is accurately simulated, and the effect of flight teaching performed by a trainee by using the simulation cabin 15 is better.
The technical solutions described above only represent the preferred technical solutions of the present invention, and some possible modifications to some parts of the technical solutions by those skilled in the art all represent the principles of the present invention, and fall within the protection scope of the present invention.
Claims (8)
1. A flight teaching simulation cabin device comprises a circular base (1), wherein a guardrail escalator device is arranged on the circular base (1), and a controller (2) is arranged on one side of the circular base (1), and is characterized in that an automatic adjusting type simulation cabin device is arranged above the circular base (1), and a back pushing feeling simulation seat device is arranged in the automatic adjusting type simulation cabin device;
the automatic regulation type simulation cabin device comprises a circular base (1) and a circular groove (3) arranged above the circular base, a plurality of rolling holes (4) are formed in the inner side surface of the circular groove (3), the rolling holes (4) are uniformly distributed on the circular groove (3), rolling balls (5) are movably arranged in the rolling holes (4), a motor groove (6) is formed in one end of the inner lower surface of the circular groove (3), a rotating motor (7) is arranged in the motor groove (6), a rotating gear (8) is arranged at the rotating end of the rotating motor (7), a rotating platform (9) is arranged in the circular groove (3), the rotating platform (9) is in movable contact with the rolling balls (5), an annular gear groove guide rail (10) is arranged at the outer end of the lower surface of the rotating platform (9), and gear teeth on the small surface of the annular gear groove guide rail (10) are meshed with the rotating gear (8), four hydraulic oil cylinders (11) are mounted at four corners above the rotating platform (9), a fixed seat (12) is mounted at the telescopic end of each hydraulic oil cylinder (11), a rotating ball groove (13) is formed in the side surface of one side of the fixed seat (12), a rotating ball (14) is movably mounted in the rotating ball groove (13), a simulation cabin (15) is arranged among the four hydraulic oil cylinders (11), the simulation cabin (15) is connected with the rotating ball (14) through a rotating shaft (16), a reinforcing baffle (17) is mounted between the rotating shaft (16) and the simulation cabin (15), and a vibration adjusting device is mounted on the rotating platform (9);
vibration adjusting device includes rotate platform (9) top one side and install regulating box (18), regulating box (18) inside center department installs adjusting motor (19), eccentric wheel (20) are installed to the rotatory end of adjusting motor (19), adjusting box (18) left and right sides installs adjusting sleeve (21) respectively, install in adjusting sleeve (21) and remove piston (22), remove piston (22) and slide in adjusting sleeve (21), through connecting rod (23) swing joint between the flange of removing piston (22) and eccentric wheel (20), adjusting sleeve (21) pass through hydraulic pressure oil pipe (24) with its two hydraulic cylinder that correspond one side and are connected, every install hydraulic pressure oil solenoid valve (26) on hydraulic oil branch pipe (25).
2. The flight teaching simulation cabin device according to claim 1, wherein the back-pushing feeling simulation seat device comprises a simulation seat (27) installed inside the simulation cabin (15), a friction pushing seat (28) movably installed at the rear inside the simulation seat (27), electric telescopic rods (29) installed at two sides below the friction pushing seat (28), a friction baffle (30) installed at the telescopic end of the electric telescopic rods (29), two square sliding frames (31) installed at the lower end of the rear inside the simulation seat (27), two ends of the friction pushing seat (28) inserted into the square sliding frames (31), the friction pushing seat (28) connected with the square sliding frames (31) in a sliding manner, a transmission groove (32) installed at the rear end below the inside of the simulation seat (27), and transmission rollers (33) installed at two sides inside the transmission groove (32), be connected through transmission shaft (34) and drive bearing (35) between drive drum (33) and drive groove (32), the cover is equipped with drive belt (36) between two drive drum (33), install a plurality of bar friction plate (37) on drive belt (36), bar friction plate (37) evenly distributed is on drive belt (36), install inverter motor (38) in drive groove (32), be connected through gear train (39) between the rotatory end of inverter motor (38) and transmission shaft (34).
3. The flight teaching simulation cabin device according to claim 1, wherein the guardrail escalator device comprises a first protection guardrail (40) installed at the outer end of the upper surface of the circular base (1), a step escalator (41) installed at one end of the upper surface of the circular base (1), second protection guardrails (42) installed at two sides of the step escalator (41), and the two second protection guardrails (42) and two ends of the first protection guardrail (40) are respectively and fixedly connected.
4. The flight teaching simulation cabin device according to claim 2, wherein a supporting baffle (43) is installed above the center inside the transmission groove (32), and the supporting baffle (43) is connected with the transmission belt (36) in a sliding manner.
5. The flight teaching simulation cabin device according to claim 1, wherein the opening and closing of the hydraulic oil solenoid valves (26) on the two hydraulic oil branch pipes (25) enables the simulation cabin (15) to simulate three different vibration modes.
6. A flight teaching simulation cabin device according to claim 1, characterized in that the inside of the simulation cabin (15) is the same as the inside of the cockpit of the aircraft.
7. A flight teaching simulation cabin device according to claim 2, wherein a safety belt (44) is mounted on the simulation seat (27), and the safety belt (44) is in a tight state after being bound.
8. A flight teaching simulator chamber device according to claim 2, wherein said strip-shaped friction plate (37) is in sliding contact with the friction baffle (30).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201911033645.4A CN110853454A (en) | 2019-10-28 | 2019-10-28 | Flight teaching simulation cabin device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201911033645.4A CN110853454A (en) | 2019-10-28 | 2019-10-28 | Flight teaching simulation cabin device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN110853454A true CN110853454A (en) | 2020-02-28 |
Family
ID=69599931
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201911033645.4A Withdrawn CN110853454A (en) | 2019-10-28 | 2019-10-28 | Flight teaching simulation cabin device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN110853454A (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111312011A (en) * | 2020-04-02 | 2020-06-19 | 云南电网有限责任公司带电作业分公司 | Real-scene real sense training method and system based on combination of helicopter simulation cockpit and three-dimensional scene |
| CN112613172A (en) * | 2020-12-18 | 2021-04-06 | 齐炳森 | VR-based airplane riding experience system and using method thereof |
| CN113823165A (en) * | 2021-09-22 | 2021-12-21 | 中天科普(深圳)科技有限公司 | Earthquake simulation experience platform |
-
2019
- 2019-10-28 CN CN201911033645.4A patent/CN110853454A/en not_active Withdrawn
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111312011A (en) * | 2020-04-02 | 2020-06-19 | 云南电网有限责任公司带电作业分公司 | Real-scene real sense training method and system based on combination of helicopter simulation cockpit and three-dimensional scene |
| CN112613172A (en) * | 2020-12-18 | 2021-04-06 | 齐炳森 | VR-based airplane riding experience system and using method thereof |
| CN113823165A (en) * | 2021-09-22 | 2021-12-21 | 中天科普(深圳)科技有限公司 | Earthquake simulation experience platform |
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Application publication date: 20200228 |