Cabin system for simulating aircraft

Abstract

The invention belongs to the technical field of aircraft simulation, and particularly relates to a cabin system for simulating an aircraft, which comprises a bottom plate, a control case is fixed on the upper side of the bottom plate, a cabin is transversely arranged at the upper end of the bottom plate, and first connecting blocks which are uniformly distributed are fixed on the side wall of the cabin; through cooperation of a storage plate, a rotating rod, a rotating block, a dustproof layer and a pulling plate, when the cabin is not used, the pulling plate can be conveniently moved to the left end, so that the dustproof layer is pulled and laid at the upper end of the cabin, an internal console is effectively protected, and dust accumulation or accidental impact damage is avoided; through joint cooperation of an air inlet pipe, a cooling fan and a protection box, rapid cooling of the interior of the control case can be conveniently achieved through the cooling fan, after meshes of a filter screen are blocked by dust, a brand new filter screen outside a winding roller can be laid at a pipe opening of the air inlet pipe by pulling the filter screen, the circulation effect of airflow is guaranteed, and the service life of the air inlet pipe is prolonged. And the heat dissipation efficiency is improved.

Description

Technical Field

[0001] The present invention relates to the technical field of aircraft simulation, in particular to a cockpit system for simulating an aircraft. Background Art

[0002] Aircraft simulators are important and indispensable equipment in pilot training and aircraft R&D testing. Aircraft simulators can provide a realistic flight experience, allowing pilots to perform various flight operations in a simulated environment, and simulate various emergency situations in a safe environment to improve the pilots' operating skills and response capabilities. The aircraft simulator cockpit, as the core component of the simulator, directly affects the simulation effect and user experience of the aircraft simulator. The aircraft simulator cockpit needs to provide a realistic simulation environment so that pilots can feel the atmosphere of real flight in the simulation environment, so as to better conduct training and testing. At the same time, the aircraft simulator cockpit needs to provide a good human-computer interaction interface so that pilots can operate conveniently and intuitively. And obtain flight data and environmental information in real time to provide real-time feedback and adjust the attitude of the aircraft;

[0003] However, the existing cockpit systems of simulated aircraft still have the following technical problems when in use:

[0004] The existing cockpit system lacks protective measures. When not in use, dust is likely to adhere to the upper ends of the joystick and control buttons, thereby affecting the control sensitivity of the joystick and control buttons inside the cockpit. In addition, the control boxes of the current cockpit systems all dissipate heat by opening heat dissipation holes, which has a poor heat dissipation effect and can easily cause damage to internal circuit boards or lines, affecting their service life.

[0005] Therefore, a cockpit system for simulating an aircraft is proposed to solve the above-mentioned problems. Summary of the Invention

[0006] The object of the present invention is to provide a cockpit system for simulating an aircraft to solve the problems raised in the above background technology.

[0007] To achieve the above-mentioned objectives, the present invention provides the following technical solution: a cockpit system for simulating an aircraft, comprising a base plate, a control cabinet fixed to the upper side of the base plate, a cockpit laterally disposed on the upper end of the base plate, first connecting blocks evenly arranged are fixed to the side walls of the cockpit, second connecting blocks evenly arranged are fixed to the upper side of the base plate, a telescopic cylinder is connected between the first and second connecting blocks via an axle pin for tilting and rotating connection, a control console is fixed inside the cockpit, a display is fixed to the upper end of the left side of the cockpit, and a windshield is fixed to both the front and rear sides of the cockpit;

[0008] An air inlet duct is fixed to the side wall of the control chassis, a cooling fan is fixed inside the air inlet duct, a protective box is fixed to the side wall of the control chassis outside the air inlet duct, an air inlet hole is opened on the side wall of the protective box, and evenly arranged air exhaust holes are opened on the other side of the control chassis, the left end of the interior of the protective box is rotatably connected to a symmetrical clamping rod through a bearing, a winding roller is fixed between the two clamping rods by bolts, a filter is wound around the outside of the winding roller, the right end of the filter extends to the front end of the air inlet duct, a pressing mechanism is provided at the front end of the air inlet duct, and a transmission mechanism is fixed to the left end of the interior of the protective box;

[0009] A storage plate is fixed to the right end of the interior of the cabin, a cavity is opened inside the storage plate, a rotating rod is rotatably connected to the interior of the cavity, the rear end of the rotating rod passes through the rear side of the storage plate and extends to the rear end and is fixed with a rotating block, a dustproof layer is wrapped around the rod wall of the rotating rod, a pulling plate is provided at the left end of the storage plate, the left end of the dustproof layer is fixedly connected to the right side of the pulling plate, and a limiting mechanism is provided inside the pulling plate.

[0010] Preferably, the pressing mechanism includes two fixed blocks, which are respectively fixedly connected to the upper and lower ends of the inner wall of the protective box, and the front sides of the two fixed blocks are fixed with threaded rods, and the outsides of the two threaded rods are sleeved with connecting plates, and the two connecting plates are close to each other and a pressure plate is fixed together, and the rod wall of the threaded rod is threadedly connected with a fastening nut, and the rear side of the fastening nut contacts the front side of the connecting plate, and the rear side of the pressure plate contacts the front side of the filter, and the filter is clamped and fixed between the pressure plate and the air inlet pipe.

[0011] Preferably, the transmission mechanism includes a dual-axis motor, which is fixedly connected to the left end of the inner wall of the protective box. Transmission rods are fixed at both ends of the dual-axis motor, and the other ends of the two transmission rods are rotatably connected to the inner wall of the protective box through bearings. The rod walls of the two transmission rods are fixedly sleeved with a first pulley, and the rod walls of the two clamping rods are fixedly sleeved with a second pulley, and the two first pulleys are rotatably connected to the two second pulleys through belts.

[0012] Preferably, the limiting mechanism includes two limiting blocks, the lower sides of the two limiting blocks are slidably connected to the inner wall of the pulling plate, a handle is fixed on the upper side of the pulling plate, and a strip opening is provided inside the pulling plate and the handle, the upper ends of the two limiting blocks are slidably connected to the strip opening, a first spring is fixed between the two limiting blocks, and an insertion rod is fixed on the side of the two limiting blocks facing away from the first spring, a symmetrical first socket is provided at the left end of the inner wall of the cabin, and a symmetrical second socket is provided at the right end of the inner wall of the cabin, and the two insertion rods are adapted to the first socket and the second socket.

[0013] Preferably, a moving mechanism is fixed to the upper end of the right side of the display, a vertical plate is provided at the lower end of the moving mechanism, a groove is provided on the rear side of the vertical plate, a connecting mechanism is fixed inside the groove, a wiping cotton is fixed to the side wall of the connecting mechanism, and the other side of the wiping cotton is in contact with the side wall of the display.

[0014] Preferably, the moving mechanism includes a guide rail, which is fixedly connected to the side wall of the display, a moving groove is opened on the lower side of the guide rail, a mounting groove is fixed to the left end of the moving groove, a reciprocating screw is rotatably connected to the interior of the moving groove through a bearing, a motor is fixed to the interior of the mounting groove, the left end of the reciprocating screw is fixedly connected to the output end of the motor, the vertical plate thread is arranged on the outside of the reciprocating screw, and the upper side of the vertical plate is slidably connected to the upper end of the inner wall of the moving groove.

[0015] Preferably, the connecting mechanism includes a telescopic rod, which is fixedly connected to the inner wall of the groove, and the other end of the telescopic rod is fixedly connected to the side wall of the wiping cotton. A second spring is sleeved on the outside of the telescopic rod, and one end of the second spring is fixedly connected to the inner wall of the groove, and the other end of the second spring is fixedly connected to the side wall of the wiping cotton.

[0016] Compared with the prior art, the present invention has the following beneficial effects:

[0017] 1) Through the coordination of the storage plate, rotating rod, rotating block, dustproof layer and pulling plate, when the cockpit is not in use, the pulling plate can be moved to the left end, thereby pulling the dustproof layer and laying it on the upper end of the cockpit, effectively protecting the internal control panel from dust accumulation or accidental impact damage;

[0018] 2) Through the cooperation of the air inlet pipe, the cooling fan and the protective box, the cooling fan can be used to quickly dissipate heat inside the control chassis. When the mesh of the filter is clogged with dust, the filter can be pulled to lay a new filter on the outside of the winding roller at the pipe mouth of the air inlet pipe to ensure the circulation of air flow and increase the efficiency of heat dissipation. BRIEF DESCRIPTION OF THE DRAWINGS

[0019] Figure 1 It is a schematic diagram of the structure of the present invention;

[0020] Figure 2 for Figure 1 Schematic diagram of the back structure;

[0021] Figure 3 for Figure 1 Schematic diagram of the structure viewed from above;

[0022] Figure 4 Schematic diagram of the internal structure of the protective box;

[0023] Figure 5It is a structural diagram of the pressing mechanism;

[0024] Figure 6 It is a cross-sectional view of the storage plate and the pulling plate;

[0025] Figure 7 is a cross-sectional view of the guide rail;

[0026] Figure 8 This is a cross-sectional view of the vertical plate.

[0027] In the figure: 1 base plate, 2 control chassis, 3 cockpit, 4 first connecting block, 5 second connecting block, 6 telescopic cylinder, 7 control console, 8 display, 9 wind shield, 10 air inlet duct, 11 cooling fan, 12 protection box, 13 clamping rod, 14 winding roller, 15 filter, 16 storage plate, 17 rotating rod, 18 rotating block, 19 dustproof layer, 20 pulling plate, 21 fixed block, 22 threaded rod, 23 connecting plate, 24 pressure plate, 25 fastening nut, 26 dual-axis motor, 27 transmission rod, 28 limit block, 29 handle, 30 first spring, 31 plug rod, 32 vertical plate, 33 wiping cotton, 34 guide rail, 35 reciprocating screw rod, 36 motor, 37 telescopic rod, 38 second spring. DETAILED DESCRIPTION

[0028] The following will clearly and completely describe the technical solutions in the embodiments of the present invention in conjunction with the accompanying drawings. Obviously, the described embodiments are only part of the embodiments of the present invention, not all of the embodiments. Based on the embodiments of the present invention, all other embodiments obtained by ordinary technicians in this field without making creative efforts are within the scope of protection of the present invention.

[0029] In the description of the present invention, it should be understood that the terms "upper", "lower", "front", "back", "left", "right", "top", "bottom", "inside", "outside", etc., indicating directions or positional relationships, are based on the directions or positional relationships shown in the accompanying drawings, and are only for the convenience of describing the present invention and simplifying the description, rather than indicating or implying that the device or element referred to must have a specific direction, be constructed and operated in a specific direction, and therefore should not be understood as limiting the present invention.

[0030] Example:

[0031] See also Figure 1-8 , the present invention provides a technical solution:

[0032] A cockpit system for simulating an aircraft includes a base plate 1, a control chassis 2 being fixed to the upper side of the base plate 1, a cockpit 3 being laterally disposed at the upper end of the base plate 1, first connecting blocks 4 being fixed to the side walls of the cockpit 3, and second connecting blocks 5 being fixed to the upper side of the base plate 1, wherein telescopic cylinders 6 are connected between the first connecting blocks 4 and the second connecting blocks 5 via axle pins for tilting and rotating. The cockpit 3 can be driven to sway by the extension and contraction of the multiple telescopic cylinders 6, a control console 7 being fixed inside the cockpit 3, a display 8 being fixed to the upper end of the left side of the cockpit 3, and a windshield 9 being fixed to both the front and rear sides of the cockpit 3;

[0033] An air inlet duct 10 is fixed to the side wall of the control chassis 2, and a cooling fan 11 is fixed inside the air inlet duct 10. A protective box 12 is fixed to the side wall of the control chassis 2 outside the air inlet duct 10. The side wall of the protective box 12 is provided with air inlet holes, and the other side of the control chassis 2 is provided with evenly arranged exhaust holes. The left end of the interior of the protective box 12 is connected to a symmetrical clamping rod 13 through a bearing. A winding roller 14 is fixed between the two clamping rods 13 by bolts. A filter screen 15 is provided on the outside of the winding roller 14. The right end of the filter screen 15 extends to the front of the air inlet duct 10. At the end, a pressing mechanism is provided at the front end of the air inlet pipe 10, and a transmission mechanism is fixed to the left end inside the protective box 12. When the filter screen 15 at the pipe opening of the air inlet pipe 10 is blocked by a large amount of dust and affects the airflow, the winding roller 14 can be driven to rotate by the transmission mechanism, so that the winding roller 14 unwinds the filter screen 15 and pulls the filter screen 15 to the right end. When a new filter screen 15 is moved to the pipe opening of the air inlet pipe 10, the filter screen 15 can be pressed and fixed again by the pressing mechanism to ensure that the filter screen 15 and the pipe opening of the air inlet pipe 10 are tightly fitted to each other;

[0034] A storage plate 16 is fixed to the right end of the interior of the cockpit 3, and a cavity is opened inside the storage plate 16. The interior of the cavity is rotatably connected to a rotating rod 17. The rear end of the rotating rod 17 passes through the rear side of the storage plate 16 and extends to the rear end and is fixed with a rotating block 18. The rod wall of the rotating rod 17 is wrapped with a dustproof layer 19. A pulling plate 20 is provided at the left end of the storage plate 16. The left end of the dustproof layer 19 is fixedly connected to the right side of the pulling plate 20. A limiting mechanism is provided inside the pulling plate 20. When the cockpit system is not in use, the pulling plate 20 can be moved to the left end. The pulling plate 20 lays the dustproof layer 19 wrapped inside the storage plate 16 on the upper end of the cockpit 3, thereby effectively preventing dust from being treated on the control panel 7 inside the cockpit 3, and protecting the control panel 7 from being damaged by accidental impact.

[0035] The pressing mechanism includes two fixed blocks 21, which are respectively fixedly connected to the upper and lower ends of the inner wall of the protective box 12. A threaded rod 22 is fixed on the front side of the two fixed blocks 21. A connecting plate 23 is sleeved on the outside of the two threaded rods 22. A pressing plate 24 is fixed to one side of the two connecting plates 23. The rod wall of the threaded rod 22 is threadedly connected with a fastening nut 25. The rear side of the fastening nut 25 contacts the front side of the connecting plate 23. The rear side of the pressing plate 24 contacts the front side of the filter 15. The filter 15 is clamped and fixed between the pressing plate 24 and the air inlet pipe 10.

[0036] The transmission mechanism includes a dual-axis motor 26, which is fixedly connected to the left end of the inner wall of the protective box 12. Transmission rods 27 are fixed at both ends of the dual-axis motor 26. The other ends of the two transmission rods 27 are rotatably connected to the inner wall of the protective box 12 through bearings. The rod walls of the two transmission rods 27 are fixedly sleeved with a first pulley, and the rod walls of the two clamping rods 13 are fixedly sleeved with a second pulley. The two first pulleys are rotatably connected to the two second pulleys through belts.

[0037] The limiting mechanism includes two limiting blocks 28, the lower sides of the two limiting blocks 28 are slidably connected to the inner wall of the pulling plate 20, and a handle 29 is fixed on the upper side of the pulling plate 20. The pulling plate 20 and the handle 29 are provided with a strip opening. The upper ends of the two limiting blocks 28 are slidably connected to the strip opening. A first spring 30 is fixed between the two limiting blocks 28, and a plug rod 31 is fixed on the side of the two limiting blocks 28 facing away from the first spring 30. A symmetrical first plug hole is provided at the left end of the inner wall of the cabin 3, and a symmetrical second plug hole is provided at the right end of the inner wall of the cabin 3. The two plug rods 31 are both adapted to the first plug hole and the second plug hole. When the pulling plate 20 moves to the leftmost end inside the cabin 3, it is fixed to the first plug hole through the limiting mechanism to limit the pulling plate 20.

[0038] A moving mechanism is fixed to the upper end of the right side of the display 8, and a vertical plate 32 is provided at the lower end of the moving mechanism. A groove is provided on the rear side of the vertical plate 32, and a connecting mechanism is fixed inside the groove. A wiping cotton 33 is fixed to the side wall of the connecting mechanism, and the other side of the wiping cotton 33 is in contact with the side wall of the display 8. When fingerprints or dust are attached to the surface of the display 8, the wiping cotton 33 is driven by the moving mechanism to move, and the wiping cotton 33 cleans the display 8.

[0039] The moving mechanism includes a guide rail 34, which is fixedly connected to the side wall of the display 8. A moving groove is provided on the lower side of the guide rail 34, and a mounting groove is fixed to the left end of the moving groove. A reciprocating screw rod 35 is rotatably connected to the inside of the moving groove through a bearing, and a motor 36 is fixed to the inside of the mounting groove. The left end of the reciprocating screw rod 35 is fixedly connected to the output end of the motor 36. The vertical plate 32 is threadedly arranged on the outside of the reciprocating screw rod 35, and the upper side of the vertical plate 32 is slidably connected to the upper end of the inner wall of the moving groove.

[0040] The connecting mechanism includes a telescopic rod 37, which is fixedly connected to the inner wall of the groove, and the other end of the telescopic rod 37 is fixedly connected to the side wall of the wiping cotton 33. A second spring 38 is sleeved on the outside of the telescopic rod 37, and one end of the second spring 38 is fixedly connected to the inner wall of the groove, and the other end of the second spring 38 is fixedly connected to the side wall of the wiping cotton 33. The wiping cotton 33 is driven to move toward the rear end through the connecting mechanism to ensure that the rear side of the wiping cotton 33 is tightly fitted with the display 8, thereby increasing the wiping effect.

[0041] Working principle:

[0042] When using the cockpit system of the simulated aircraft, the trainee sits inside the cockpit 3, watches the display content on the display 8 and controls the cockpit 3 through the hand-touch control panel 7 to simulate the flight state;

[0043] During use, in order to ensure rapid heat dissipation of the control chassis 2, the cooling fan 11 can be started. The cooling fan 11 accelerates the air flow inside the control chassis 2, thereby achieving rapid heat dissipation. With continuous use, the mesh of the filter 15 is blocked, which affects the normal air flow. At this time, the dual-axis motor 26 can be started, and the dual-axis motor 26 drives the transmission rods 27 at both ends to rotate. The transmission rod 27 drives the first pulley of the rod wall to rotate. The first pulley rotates through the second pulley, and the second pulley drives the clamping rod 13 to rotate. The clamping rod 13 drives the winding roller 14 to rotate, thereby unwinding the filter 15. Manually pull the filter 15 to the right end. When a new filter 15 is moved to the nozzle of the air inlet pipe 10, the filter 15 is pressed and fixed by the pressing mechanism.

[0044] After long-term use of the display 8, a large amount of fingerprints or dust will adhere to its surface. In order to ensure the sensitivity of the display 8, the motor 36 can be started, and the motor 36 drives the reciprocating screw 35 at the output end to rotate. The reciprocating screw 35 drives the vertical plate 32 connected to the rod wall thread to move left and right, thereby driving the wiping cotton 33 on the rear side to wipe the display 8;

[0045] When the cockpit system is not in use, the two limit blocks 28 inside the handle 29 can be pressed. The two limit blocks 28 drive the insertion rod 31 of the side wall to separate from the second socket and move the pulling plate 20 to the left end. The pulling plate 20 drives the dustproof layer 19 at the right end to be laid on the upper end of the cockpit 3. When the pulling plate 20 moves to the leftmost end inside the cockpit 3, the two limit blocks 28 are released. Under the elastic force of the first spring 30, the two insertion rods 31 move to both ends and connect with the first socket, thereby achieving limitation and ensuring that the dustproof layer 19 is laid on the upper end of the cockpit 3 to protect the internal control panel 7.

[0046] The above shows and describes the basic principles and main features of the present invention and the advantages of the present invention. For those skilled in the art, it is obvious that the present invention is not limited to the details of the above exemplary embodiments, and the present invention can be implemented in other specific forms without departing from the spirit or basic characteristics of the present invention; therefore, no matter from which point of view, the embodiments should be regarded as exemplary and non-restrictive. The scope of the present invention is limited by the appended claims rather than the above description. Therefore, it is intended that all changes that fall within the meaning and scope of the equivalent elements of the claims are included in the present invention, and any figure signs in the claims should not be regarded as limiting the claims involved.

[0047] While embodiments of the present invention have been shown and described, it will be appreciated by those skilled in the art that various changes, modifications, substitutions, and variations may be made to these embodiments without departing from the principles and spirit of the invention, and that the scope of the invention is defined by the appended claims and their equivalents.

Claims

1. A cockpit system for simulating an aircraft, comprising a base plate (1), characterized in that: A control box (2) is fixed on the upper side of the base plate (1), a cockpit (3) is transversely arranged on the upper end of the base plate (1), first connecting blocks (4) arranged evenly are fixed on the side walls of the cockpit (3), second connecting blocks (5) arranged evenly are fixed on the upper side of the base plate (1), a telescopic cylinder (6) is connected between the first connecting block (4) and the second connecting block (5) via an axle pin for tilting and rotating, a control console (7) is fixed inside the cockpit (3), a display (8) is fixed on the upper end of the left side of the cockpit (3), and a windshield (9) is fixed to the front and rear sides of the cockpit (3); An air inlet pipe (10) is fixed to the side wall of the control chassis (2), a cooling fan (11) is fixed inside the air inlet pipe (10), a protective box (12) is fixed to the side wall of the control chassis (2) outside the air inlet pipe (10), an air inlet hole is provided on the side wall of the protective box (12), and evenly arranged air exhaust holes are provided on the other side of the control chassis (2), the left end of the interior of the protective box (12) is rotatably connected to a symmetrical clamping rod (13) through a bearing, a winding roller (14) is fixed between the two clamping rods (13) by bolts, a filter screen (15) is provided on the outside of the winding roller (14), the right end of the filter screen (15) extends to the front end of the air inlet pipe (10), a pressing mechanism is provided at the front end of the air inlet pipe (10), and a transmission mechanism is fixed to the left end of the interior of the protective box (12); A storage plate (16) is fixed at the right end of the interior of the cabin (3), a cavity is opened inside the storage plate (16), a rotating rod (17) is rotatably connected inside the cavity, the rear end of the rotating rod (17) passes through the rear side of the storage plate (16) and extends to the rear end and is fixed with a rotating block (18), a dustproof layer (19) is wrapped around the rod wall of the rotating rod (17), a pulling plate (20) is provided at the left end of the storage plate (16), the left end of the dustproof layer (19) is fixedly connected to the right side of the pulling plate (20), and a limiting mechanism is provided inside the pulling plate (20).

2. The cockpit system of a simulated aircraft according to claim 1, characterized in that: The pressing mechanism comprises two fixing blocks (21), the two fixing blocks (21) are fixedly connected to the upper end and the lower end of the inner wall of the protection box (12) respectively, the front sides of the two fixing blocks (21) are fixed with threaded rods (22), the exteriors of the two threaded rods (22) are sleeved with connecting plates (23), and the two connecting plates (23) are jointly fixed with a pressing plate (24) on one side close to each other, the rod wall of the threaded rod (22) is threadedly connected with a fastening nut (25), the rear side of the fastening nut (25) contacts the front side of the connecting plate (23), the rear side of the pressing plate (24) contacts the front side of the filter (15), and the filter (15) is clamped and fixed between the pressing plate (24) and the air inlet pipe (10).

3. The cockpit system of a simulated aircraft according to claim 1, characterized in that: The transmission mechanism includes a double-axis motor (26), the double-axis motor (26) is fixedly connected to the left end of the inner wall of the protection box (12), and transmission rods (27) are fixed at both ends of the double-axis motor (26). The other ends of the two transmission rods (27) are rotatably connected to the inner wall of the protection box (12) through bearings. The rod walls of the two transmission rods (27) are fixedly sleeved with a first pulley, and the rod walls of the two clamping rods (13) are fixedly sleeved with a second pulley, and the two first pulleys are rotatably connected to the two second pulleys through belts.

4. The cockpit system of a simulated aircraft according to claim 1, characterized in that: The limiting mechanism includes two limiting blocks (28), the lower sides of the two limiting blocks (28) are slidably connected to the inner wall of the pulling plate (20), a handle (29) is fixed on the upper side of the pulling plate (20), and a strip opening is provided inside the pulling plate (20) and the handle (29), the upper ends of the two limiting blocks (28) are slidably connected to the strip opening, a first spring (30) is fixed between the two limiting blocks (28), and a plug rod (31) is fixed on the side of the two limiting blocks (28) facing away from the first spring (30), a symmetrical first plug hole is provided at the left end of the inner wall of the cabin (3), and a symmetrical second plug hole is provided at the right end of the inner wall of the cabin (3), and the two plug rods (31) are adapted to the first plug hole and the second plug hole.

5. The cockpit system of a simulated aircraft according to claim 1, characterized in that: A moving mechanism is fixed to the upper end of the right side of the display (8), a vertical plate (32) is provided at the lower end of the moving mechanism, a groove is provided on the rear side of the vertical plate (32), a connecting mechanism is fixed inside the groove, a wiping cotton (33) is fixed to the side wall of the connecting mechanism, and the other side of the wiping cotton (33) is in contact with the side wall of the display (8).

6. The cockpit system of a simulated aircraft according to claim 5, characterized in that: The moving mechanism comprises a guide rail (34), the guide rail (34) is fixedly connected to the side wall of the display (8), a moving groove is provided on the lower side of the guide rail (34), a mounting groove is fixed to the left end of the moving groove, a reciprocating screw rod (35) is rotatably connected to the inside of the moving groove through a bearing, a motor (36) is fixed to the inside of the mounting groove, the left end of the reciprocating screw rod (35) is fixedly connected to the output end of the motor (36), the vertical plate (32) is threadedly arranged on the outside of the reciprocating screw rod (35), and the upper side of the vertical plate (32) is slidably connected to the upper end of the inner wall of the moving groove.

7. The cockpit system of a simulated aircraft according to claim 5, characterized in that: The connecting mechanism includes a telescopic rod (37), the telescopic rod (37) is fixedly connected to the inner wall of the groove, the other end of the telescopic rod (37) is fixedly connected to the side wall of the wiping cotton (33), and a second spring (38) is sleeved on the outside of the telescopic rod (37), one end of the second spring (38) is fixedly connected to the inner wall of the groove, and the other end of the second spring (38) is fixedly connected to the side wall of the wiping cotton (33).

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