CN210813887U

CN210813887U - Aircraft simulation experience device

Info

Publication number: CN210813887U
Application number: CN201921514045.5U
Authority: CN
Inventors: 张春宇
Original assignee: Individual
Current assignee: Individual
Priority date: 2019-09-11
Filing date: 2019-09-11
Publication date: 2020-06-23
Anticipated expiration: 2029-09-11

Abstract

The utility model belongs to the technical field of aircraft flight simulation, a flight simulation experience device is disclosed, which aims to solve the problem that the flight of the flight simulation experience device in the prior art is single, the utility model comprises a mounting rack and a flight cabin, a take-off and landing simulation chamber is arranged below the flight cabin, the take-off and landing simulation chamber comprises an installation box and two groups of conveyor belts arranged at the top of the installation box side by side, the two groups of conveyor belts are driven to rotate by a first driving mechanism, and the bottom of the flight cabin is contacted with the conveyor belts; still be equipped with flight analog mechanism between two sets of conveyer belts, flight analog mechanism drives actuating cylinder including fixing on the install bin, and the output shaft that drives actuating cylinder has the bracing piece, and the bracing piece tip is connected with the flight cabin. The utility model is suitable for an aircraft flight analogue means.

Description

Aircraft simulation experience device

Technical Field

The utility model belongs to the technical field of the aircraft flight simulation, concretely relates to device is experienced in aircraft simulation.

Background

With the continuous improvement of living standard, the entertainment mode of simple audio-visual is difficult to meet the requirements of people, and people hope to add more and richer scenes or modes in the game process to enhance the interactive feeling and experience feeling of the game. Particularly for flight simulation of an aircraft, if more flying chess flying scenes such as take-off, rising, bumping, landing and the like can be added in the game simulation process, players can feel different game experiences, and therefore the attractiveness of the game is enhanced.

Although the flight simulator of the aircraft is arranged in some amusement places for the experience and use of players, the flight simulator is only designed for simple flight and is difficult to bring rich and exciting game experience to people, so that strong attraction and stickiness of customers are difficult to generate to people, and the income brought by the flight simulator is very limited. If a device capable of simulating the complex flight of the airplane in the air is designed, the interest of game players can be greatly improved, the game experience of the players is enriched, and therefore considerable income is brought.

SUMMERY OF THE UTILITY MODEL

In order to solve the problem that the device flight is single in aircraft simulation experience among the prior art, the utility model provides a device is experienced in aircraft simulation that the aircraft flight situation is abundanter.

The utility model discloses the technical scheme who adopts does: an aircraft simulation experience device comprises a mounting frame and a flight cabin, wherein a take-off and landing simulation chamber is arranged below the flight cabin and comprises a mounting box and two groups of conveyor belts arranged at the top of the mounting box side by side, the two groups of conveyor belts are driven to rotate by a first driving mechanism, and the bottom of the flight cabin is in contact with the conveyor belts; still be equipped with flight analog mechanism between two sets of conveyer belts, flight analog mechanism drives actuating cylinder including fixing on the install bin, and the output shaft that drives actuating cylinder has the bracing piece, and the bracing piece tip is connected with the flight cabin.

Preferably, the end part of the support rod is also provided with a second driving mechanism, an output shaft of the second driving mechanism is provided with a first gear, and the plane of the first gear is vertical to the conveying plane of the conveying belt; the first gear is externally engaged with a fluted disc which is fixed inside the flight cabin.

Preferably, a lifting control mechanism is further arranged in the installation box and comprises a plurality of rows of lifters arranged in parallel along the running direction of the conveyor belt, the lifters are fixedly installed in the installation box, and the output ends of the lifters are in contact with the conveyor belt and lift the conveyor belt at the position.

Preferably, each row of the lifters comprises a plurality of groups of lifting units which are arranged side by side in sequence.

Preferably, the upper ends of the upper part in the installation box are fixedly provided with upper conveying wheels, the lower ends of the lower part in the installation box are provided with lower conveying wheels capable of moving along the height direction of the installation box, and the conveying belts are arranged on the upper conveying wheels and the lower conveying wheels; still be equipped with the spill frame between last transfer gear and the lower transfer gear, the spill frame is fixed in the install bin, the riser is fixed in the spill frame, the transfer gear passes through the elastic component to be fixed in the install bin down, and lower transfer gear and last transfer gear are all freely rotatable.

Preferably, a deformable soft board is further arranged on a top plate at the top of the mounting box, a groove and a through hole are further sequentially formed in the through soft board, an output shaft of the lifter penetrates through the through hole, a supporting block matched with the groove is arranged at the output end of the output shaft of the lifter, and the width of the supporting block is larger than the diameter of the through hole.

Preferably, the device is further provided with a deflection simulation mechanism, the deflection simulation mechanism comprises an inner disc and an outer disc which are concentrically arranged, the installation box is fixed on the inner disc, a plurality of groups of second gears are uniformly arranged between the inner disc and the outer disc, the second gears are meshed with the inner disc and the outer disc, and the outer disc is fixed on the installation frame; and a third driving mechanism for driving the inner disc to rotate is also arranged.

Preferably, the third driving mechanism is a stepping motor, and the stepping motor is fixed in the middle of the outer disc.

Preferably, the steering simulation mechanism is further arranged and comprises a rotating column, a placing plate is fixedly arranged at the top of the rotating column, and the outer disc is fixed on the placing plate; the bottom of the rotating column is provided with a base, and the rotating column can rotate on the base around the circumferential direction of the rotating column; and a fourth driving mechanism for driving the rotating column to rotate is also arranged.

The utility model has the advantages that:

1. the utility model is provided with the conveyor belt and the flight simulation mechanism, when the flight cabin is contacted with the conveyor belt, the scene that the aircraft runs on the ground is simulated; when the flight cabin is separated from the conveyor belt through the support of the flight simulation mechanism, the flight cabin simulates the flying scene of the aircraft in the air. In addition, in order to simulate the scene that the aircraft upwards perhaps flown downwards, the utility model discloses still set up first gear and second actuating mechanism, rotated through second actuating mechanism drive aircraft, just so realized the simulation that the aircraft ascended or descends.

2. The utility model is provided with the take-off and landing control mechanism, wherein the lifting unit in front of the flight chamber synchronously rises to simulate the take-off state of the aircraft; when the simulated aircraft descends, the lifting unit in front of the flight cabin descends gradually, and then the lifting unit behind the flight cabin descends gradually, so that the descending of the aircraft can be simulated successfully.

3. The utility model discloses still through setting up multiunit lift unit, can only install the lift unit at the contact site between the flight cabin bottom that corresponds and the conveyer belt, through the same different of different positions department lift height of control, alright simulation aircraft take place the situation of shake when through uneven ground. Therefore, the situations simulated by the aircraft are richer, and the overall interest is improved.

4. The utility model is provided with the lower conveying wheel and the elastic piece, when the aircraft falls to the conveying belt, the conveying belt is pressed to move a part downwards due to the gravity action; the elastic piece is arranged, so that the conveyor belt above the upper conveying wheel can be better restored to the most initial horizontal state, a good damping effect is formed on the aircraft, and the condition that the aircraft lands on the ground can be better simulated.

5. The utility model discloses a set up the soft board, at the in-process that the riser moved down, the supporting shoe makes the soft board push down, and the conveyer belt is after corresponding riser position department appears sunkenly like this, makes the flight cabin appear sinking in this sunk position because the action of gravity in flight cabin, then can simulate the aircraft from this and go on level ground and the running state when the terrain is sunken in the process, and then widened the utility model discloses to the simulation of aircraft scene of traveling, improved holistic appeal.

6. The utility model discloses a set up the simulation mechanism that deflects, thereby rotate through the drive inner disc and can make the flight cabin take place to deflect around its axle center of direction of traveling, can simulate the state of traveling when the direction deflects flight like this. When the deflection simulation mechanism drives the flight chamber to have a larger deflection angle, the state of the aircraft in rollover can be simulated, so that the driving experience is more exciting, and the viscosity of a player is further enhanced. The utility model discloses still control the direction of travel of aircraft through setting up to turn to simulation mechanism, realization aircraft that can be more smooth nature turns, improves player's experience.

The advantages of the invention are not limited to the description, but rather are described in greater detail in the detailed description for better understanding.

Drawings

In order to more clearly illustrate the embodiments of the present invention or the technical solutions in the prior art, the drawings needed to be used in the description of the embodiments or the prior art will be briefly described below, and it is obvious that the drawings in the following description are some embodiments of the present invention, and for those skilled in the art, other drawings can be obtained according to these drawings without creative efforts.

Fig. 1 is a schematic structural diagram of the present invention;

FIG. 2 is a schematic view of a portion of the structure of FIG. 1;

FIG. 3 is a schematic sectional view taken along line A-A in FIG. 2;

FIG. 4 is an enlarged schematic view of a part of the structure of the lifting simulation chamber of the present invention;

fig. 5 is a schematic structural diagram of the middle top plate of the present invention;

fig. 6 is a schematic structural diagram of a deflection simulating mechanism according to the present invention;

in the figure: 1-flight cabin, 11-flight cabin body, 12-front wheel, 13-rear wheel, 14-fluted disc, 2-take-off and landing simulation chamber, 21-installation box, 211-top plate, 212-bottom plate, 2111-groove, 22-conveyor belt, 23-upper conveying wheel, 24-lower conveying wheel, 25-transition groove, 26-elastic element, 27-lifter, 2711-supporting block, 28-installation groove, 29-concave frame, 3-deflection simulation mechanism, 31-inner disc, 32-second gear, 33-outer disc, 4-installation plate, 5-steering simulation mechanism, 6-base, 7-flight simulation mechanism, 71-driving cylinder, 72-supporting rod and 73-first gear.

Detailed Description

In order to make the objects, technical solutions and advantages of the embodiments of the present invention clearer, the embodiments of the present invention will be clearly and completely described below with reference to the accompanying drawings in the embodiments of the present invention, and it is obvious that the described embodiments are some, but not all, embodiments of the present invention. The components of embodiments of the present invention, as generally described and illustrated in the figures herein, may be arranged and designed in a wide variety of different configurations.

Thus, the following detailed description of the embodiments of the present invention, presented in the accompanying drawings, is not intended to limit the scope of the invention, as claimed, but is merely representative of selected embodiments of the invention. Based on the embodiments in the present invention, all other embodiments obtained by a person skilled in the art without creative efforts belong to the protection scope of the present invention.

It should be noted that, in the present invention, the embodiments and features of the embodiments may be combined with each other without conflict.

It should be noted that: like reference numbers and letters refer to like items in the following figures, and thus, once an item is defined in one figure, it need not be further defined and explained in subsequent figures.

In the description of the embodiments of the present invention, it should be noted that the indication of the position or the positional relationship is based on the position or the positional relationship shown in the drawings, or the position or the positional relationship which is usually placed when the product of the present invention is used, or the position or the positional relationship which is conventionally understood by those skilled in the art, and is only for the convenience of describing the present invention and simplifying the description, but it is not to indicate or suggest that the indicated device or element must have a specific position, be constructed and operated in a specific orientation, and thus, should not be construed as limiting the present invention. Furthermore, the terms "first" and "second" are used merely to distinguish one description from another, and are not to be construed as indicating or implying relative importance.

In the description of the embodiments of the present invention, it should be further noted that unless otherwise explicitly stated or limited, the terms "disposed" and "connected" should be interpreted broadly, and may be, for example, fixedly connected, detachably connected, or integrally connected; may be directly connected or indirectly connected through an intermediate. For those skilled in the art, the drawings of the above terms in the embodiments with specific meanings in the present invention can be understood in specific situations, and the technical solutions in the embodiments of the present invention are clearly and completely described, and it is obvious that the described embodiments are some embodiments of the present invention, not all embodiments. The components of embodiments of the present invention, as generally described and illustrated in the figures herein, may be arranged and designed in a wide variety of different configurations.

The invention will be further explained with reference to the drawings and the specific embodiments.

As shown in fig. 1-6, the utility model relates to an aircraft simulation experience device, which comprises a mounting rack and a flight cabin 1, wherein a take-off and landing simulation chamber 2 is arranged below the flight cabin 1, the take-off and landing simulation chamber 2 comprises a mounting box 21 and a conveyor belt 22 arranged at the top of the mounting box 21, the conveyor belt 22 is driven to rotate by a first driving mechanism, and rollers are arranged at the bottom of the flight cabin 1 and are in contact with the conveyor belt 22; the flight simulation device is further provided with a flight simulation mechanism 7, wherein the flight simulation mechanism 7 comprises a driving cylinder 71 fixed on the installation box 21, an output shaft of the driving cylinder 71 is connected with a supporting rod 72, and the end part of the supporting rod 72 is connected with the flight cabin 1.

For the arrangement of the flight simulation mechanism 7 and the take-off and landing simulation chamber 2, the following two modes can be adopted; one of the two groups of conveyor belts 22 is arranged on two sides of the top of the installation box 21 side by side, and the two groups of conveyor belts 22 are driven to rotate by a first driving mechanism; a transition groove 25 is formed between the two groups of conveyor belts 22, a mounting groove 28 is formed in the bottom of the mounting box 21 corresponding to the transition groove 25, the driving cylinder 71 is fixed in the mounting groove 28, namely the driving cylinder 71 is fixed between the two groups of conveyor belts 22 of the mounting box 21, and the flight cabin 1 is in a ground sliding state in the conveying process of the conveyor belts 22; when the driving cylinder 71 drives the flight chamber 1 to ascend, the flight chamber 1 is in an ascending state.

The flight simulation mechanism 7 and the take-off and landing simulation chamber 2 are arranged in another way, the conveyor belt 22 is arranged in the middle of the top of the installation box 21, the flight simulation mechanism 7 comprises two groups of driving cylinders 71 which run synchronously, the two groups of driving cylinders 71 are fixed at the bottom of the installation box 21, and the end parts of the two groups of support rods 72 are fixed on the flight cabin 1. Similarly, when the flight chamber 1 is in contact with the conveyor belt 22, the flight chamber 1 is in a ground gliding state during the conveying process of the conveyor belt 22; and when the driving cylinder 71 drives the flight chamber 1 to ascend and separate from the conveyor belt 22, the flight chamber 1 is in an ascending state.

In order to simulate the ascending and descending of the aircraft in the air, furthermore, a second driving mechanism is further arranged at the end part of the supporting rod 72, an output shaft of the second driving mechanism is provided with a first gear 73, and the plane of the first gear 73 is perpendicular to the conveying plane of the conveyor belt 22; the first gear 73 is externally engaged with a toothed disc 14, and the toothed disc 14 is fixed inside the flight chamber 1. The first gear 73 is driven to rotate by the second driving mechanism, so that the fluted disc 14 and the flight chamber 1 are driven to synchronously rotate, and when the front end of the flight simulation mechanism 7 is lifted upwards, the situation that the aircraft flies upwards is simulated; when the front end of the flight simulation mechanism 7 sinks downwards, the situation that the aircraft flies downwards is simulated.

In order to better simulate the takeoff situation of the aircraft, a take-off and landing control mechanism is further arranged in the installation box 21, the take-off and landing control mechanism comprises a plurality of rows of lifters 27 arranged in parallel along the running direction of the conveyor belt 22, the lifters 27 are fixedly arranged in the installation box 21, the output ends of the lifters 27 are arranged in contact with the conveyor belt 22, and the conveyor belt 22 at the position where the lifters 27 are in contact with the conveyor belt 22 is lifted.

Further, each row of the lifters 27 includes a plurality of sets of lifting units arranged side by side in sequence.

Preferably, the lifters 27 are provided in two rows and there are two sets of lifting units, all of which are arranged in a rectangular pattern, and correspondingly, the flight chamber 1 is provided with two sets of front wheels 12 and two sets of rear wheels 13, the front wheels 12 and the rear wheels 13 being respectively disposed above the lifting units, and the lifting units are in contact with the front wheels 12 and the rear wheels 13 through the conveyor belt 22.

In order to enable the lifter 27 to smoothly lift the conveyor belt 22 and the flight chamber 1, the conveyor belt 22 may be an elastic conveyor belt which can deform in the conveying direction, so that the conveyor belt 22 can still keep good conveying in the process of lifting the conveyor belt 22 at the position and the flight chamber 1 by the lifter 27, and the stability of the overall operation is further ensured.

In order to enable the lifter 27 to lift the conveyor belt 22 and the cab 1 smoothly, the following arrangement may be adopted: an upper conveying wheel 23 is fixed at two ends of the conveying belt 22 at the upper part in the installation box 21 through bearing seats, a lower conveying wheel 24 capable of moving along the height direction of the installation box 21 is arranged at two ends at the lower part in the installation box 21, and the conveying belt 22 is wound on the upper conveying wheel 23 and the lower conveying wheel 24; a concave frame 29 is further arranged between the upper conveying wheel 23 and the lower conveying wheel 24, the concave frame 29 is fixed on the side wall of the installation box 21, the lifter 27 is fixed in the concave frame 29, the lower conveying wheel 24 is fixed in the installation box 21 through an elastic piece 26, and for the fixation of the lower conveying wheel 24, in the specific setting process, a bearing seat coaxial with the lower conveying wheel 24 is fixed at the bottom of the installation box 21 or the bottom of the installation concave frame 29, so that the lower conveying wheel 24 can only move up and down; the elastic member 26 may be provided as a spring. In this way, the concave frame 29 and the lifter 27 arranged in the concave frame 29 do not interfere with the transmission of the conveyor belt 22 during the rotation of the conveyor belt 22, and at the same time, when the lifter 27 moves the conveyor belt 22 upwards, the conveyor belt 22 is tensioned and drives the lower conveyor wheel 24 upwards, and at the moment, the spring is deformed, so that after the lifter 27 stops driving, the lower conveyor wheel 24 returns to the initial position due to the action of the spring. The overall stability is better after the arrangement, and the service life is prolonged.

In order to further expand the simulation range of the traveling route road condition of the airplane during takeoff or landing, further, the top of the installation box 21 is further provided with a top plate 211, two sides of the top plate 211 are provided with accommodating sections, and the upper conveying wheel 23 is fixed in the accommodating section of the top plate 211 through a bearing seat; the middle part of the top plate 211 is a flexible plate which can be deformed, the flexible plate is uniformly provided with hole slots 2111 and through holes, and the positions and the number of the hole slots 2111 and the through holes are matched with those of the lifters 27; the output shaft of the lifter 27 penetrates through the through hole, a supporting block 2711 matched with the groove 2111 is arranged at the output end of the output shaft of the lifter 27, and the width of the supporting block 2711 is larger than the diameter of the through hole. After the arrangement, the soft board has a certain supporting effect on the conveyor belt 22, the conveyor belt 22 is conveyed on the soft board smoothly, and when the support block 2711 moves upwards, the support block 2711 drives the conveyor belt 22 to move upwards, so that the situation that an aircraft slides on the ground to pass through a convex road section can be simulated smoothly; since the width of the supporting block 2711 is larger than the diameter of the through hole of the soft board 211, when the supporting block 2711 moves downwards, the supporting block 2711 drives the soft board 211 to sink in the area, and the conveyor belt 22 also partially moves downwards, so that the condition that the aircraft slides on the ground to pass through the sunken road section can be smoothly simulated.

In addition, experience more truly for the recreation that makes the player, the utility model discloses set up the display screen in flight cabin 1, object moving frequency is unanimous with conveyer belt 22 transport frequency in the display screen, sits back in flight cabin 1 when the user, experiences 1 bottom gyro wheel in flight cabin and takes place to rotate, is coordinating the broadcast of display screen, and then can be better simulate out the flight situation.

Of course, as the replacement of display screen, the utility model discloses still can be equipped with VR glasses, through set up in the VR glasses object moving frequency and conveyer belt 22 carry the frequency unanimous, alright messenger player's flight experience is more true.

Of course, the utility model discloses still can set up the curtain that is unanimous with conveyer belt 22 delivery frequency in flight cabin 1, like this the player can also be better when observing around the curtain removes experience the marcing of flight cabin 1.

In order to simulate the state of deflection of the flying cabin 1 on one side suffering from the deflection, the aircraft is easy to bump due to the action of airflow during the flying process in the air, furthermore, a deflection simulation mechanism 3 is further arranged, the deflection simulation mechanism 3 comprises an inner disc 31 and an outer disc 33 which are concentrically arranged, the installation box 21 is fixed on the inner disc 31, a plurality of groups of second gears 32 are uniformly arranged between the inner disc 31 and the outer disc 33, the second gears 32 are meshed with the inner disc 31 and the outer disc 33, and the outer disc 33 is fixed on the installation frame; a third driving mechanism is also provided for driving the inner disc 31 to rotate.

The third driving mechanism is a stepping motor, and the stepping motor is fixed in the middle of the outer disc 33.

When the mounting box 21 is fixed on the inner panel 31, the side surfaces of the top plate 211 and the bottom plate 212 of the mounting box 21 are respectively provided with a fixed square column, and the fixed columns are inserted into the mounting holes of the inner panel 31, so that the mounting box 21 can be quickly fixed.

In order to control the flying direction of the aircraft, a steering simulation mechanism 5 is further arranged, the steering simulation mechanism 5 comprises a rotating column, a placing plate 4 is fixedly arranged at the top of the rotating column, and the outer disc 33 is fixed on the placing plate 4; the bottom of the rotating column is provided with a base 6, and the rotating column can rotate on the base 6 around the circumferential direction of the rotating column; and a fourth driving mechanism for driving the rotating column to rotate is also arranged.

In the specific operation process, the flight direction of the aircraft can be deflected by driving the fourth driving mechanism, and in the steering process of the flight cabin 1, the third driving mechanism drives one side of the flight cabin 1 to deflect in a manner matched with the rotation direction, so that the specific state of the aircraft during steering can be simulated better and more completely. In addition, in the normal flying process of the flight cabin 1, the third driving mechanism drives the two sides of the flight cabin 1 to respectively shift, so that the state of the airplane bumping in the air can be simulated. On the other hand, the first driving mechanism drives the conveyor belt 22 to change the transmission speed, so that the state of the aircraft during acceleration can be simulated, and then the driving cylinder 71 is operated to lift the flight cabin 1, so that the takeoff state of the aircraft is simulated; after the flight chamber 1 has been detached from the conveyor belt 22, the conveyor belt 22 is still running, which simulates the situation when the aircraft is flying; and then the front end of the aircraft is driven to lift or sink through the second driving mechanism, so that the situation of the aircraft during ascending or descending can be simulated.

Example 1

An aircraft simulation experience device comprises a mounting frame and a flight cabin, wherein a take-off and landing simulation chamber is arranged below the flight cabin and comprises a mounting box and two groups of conveyor belts arranged at the top of the mounting box side by side, the two groups of conveyor belts are driven to rotate by a first driving mechanism, and the bottom of the flight cabin is in contact with the conveyor belts; still be equipped with flight analog mechanism between two sets of conveyer belts, flight analog mechanism drives actuating cylinder including fixing on the install bin, and the output shaft that drives actuating cylinder has the bracing piece, and the bracing piece tip is connected with the flight cabin.

Example 2

On the basis of the embodiment 1, a second driving mechanism is further arranged at the end part of the supporting rod, a first gear is arranged on an output shaft of the second driving mechanism, and the plane of the first gear is vertical to the conveying plane of the conveying belt; the first gear is externally engaged with a fluted disc which is fixed inside the flight cabin.

Example 3

On the basis of the embodiment 1-2, a lifting control mechanism is further arranged in the installation box and comprises a plurality of rows of lifters which are arranged in parallel along the running direction of the conveyor belt, the lifters are fixedly arranged in the installation box, and the output ends of the lifters are in contact arrangement with the conveyor belt and lift the conveyor belt at the position; each row of the lifters comprises a plurality of groups of lifting units which are arranged side by side in sequence; the upper conveying wheels are fixed at two ends of the conveying belt at the upper part in the installation box, the lower conveying wheels capable of moving along the height direction of the installation box are arranged at two ends of the lower part in the installation box, and the lower conveying wheels are fixed in the installation box through elastic pieces.

Example 4

On the basis of the embodiment 1-3, a deformable soft board is arranged on the floor at the top of the mounting box, a groove and a through hole are sequentially formed in the through soft board, an output shaft of the lifter penetrates through the through hole, a supporting block matched with the groove is arranged at the output end of the output shaft of the lifter, and the width of the supporting block is larger than the diameter of the through hole.

Example 5

On the basis of the embodiment 1-4, the device is further provided with a deflection simulation mechanism, the deflection simulation mechanism comprises an inner disc and an outer disc which are concentrically arranged, the installation box is fixed on the inner disc, a plurality of groups of second gears are uniformly arranged between the inner disc and the outer disc, the second gears are meshed with the inner disc and the outer disc, and the outer disc is fixed on the installation frame; a third driving mechanism for driving the inner disc to rotate is further arranged; the third driving mechanism is a stepping motor, and the stepping motor is fixed in the middle of the outer disc.

Example 6

On the basis of the embodiment 1-5, a steering simulation mechanism is further arranged, the steering simulation mechanism comprises a rotating column, a placing plate is fixedly arranged at the top of the rotating column, and the outer disc is fixed on the placing plate; the bottom of the rotating column is provided with a base, and the rotating column can rotate on the base around the circumferential direction of the rotating column; and a fourth driving mechanism for driving the rotating column to rotate is also arranged.

The present invention is not limited to the above-mentioned optional embodiments, and any other products in various forms can be obtained by anyone under the teaching of the present invention, and any changes in the shape or structure thereof, all the technical solutions falling within the scope of the present invention, are within the protection scope of the present invention.

Claims

1. An aircraft simulation experience device, its characterized in that: the device comprises a mounting rack and a flight cabin (1), wherein a take-off and landing simulation chamber (2) is arranged below the flight cabin (1), the take-off and landing simulation chamber (2) comprises a mounting box (21) and a conveyor belt (22) arranged at the top of the mounting box (21), the conveyor belt (22) is driven to rotate by a first driving mechanism, and the bottom of the flight cabin (1) is in contact with the conveyor belt (22); the flight simulator is characterized in that a flight simulation mechanism (7) is further arranged, the flight simulation mechanism (7) comprises a driving cylinder (71) fixed on the installation box (21), an output shaft of the driving cylinder (71) is connected with a supporting rod (72), and the end part of the supporting rod (72) is connected with the flight cabin (1).

2. An aircraft simulated experience device as claimed in claim 1 wherein: the two groups of conveyor belts (22) are arranged on two sides of the top of the installation box (21) side by side, and the two groups of conveyor belts (22) are driven to rotate by a first driving mechanism; the driving air cylinder (71) is arranged between the two groups of conveyor belts (22) of the mounting box (21).

3. An aircraft simulated experience device as claimed in claim 2 wherein: a second driving mechanism is further arranged at the end part of the supporting rod (72), an output shaft of the second driving mechanism is provided with a first gear (73), and the plane of the first gear (73) is vertical to the conveying plane of the conveying belt (22); the first gear (73) is also provided with a fluted disc (14) in a meshed mode, and the fluted disc (14) is fixed inside the flight cabin (1).

4. An aircraft simulated experience device as claimed in any of claims 1 to 3 wherein: the installation box (21) is internally provided with a lifting control mechanism, the lifting control mechanism comprises a plurality of rows of lifters (27) arranged in parallel along the running direction of the conveyor belt (22), and the output ends of the lifters (27) are in contact with the conveyor belt (22) and lift the conveyor belt (22) at the contact position of the lifters (27) and the conveyor belt (22).

5. An aircraft simulated experience device as claimed in claim 4 wherein: each row of the lifters (27) comprises a plurality of groups of lifting units which are sequentially arranged side by side.

6. An aircraft simulated experience device as claimed in claim 4 wherein: the upper ends of the inner upper part of the installation box (21) are fixedly provided with upper conveying wheels (23), the lower ends of the inner lower part of the installation box (21) are provided with lower conveying wheels (24) capable of moving along the height direction of the installation box (21), and the conveying belts (22) are arranged on the upper conveying wheels (23) and the lower conveying wheels (24); still be equipped with concave frame (29) between last transfer gear (23) and lower transfer gear (24), concave frame (29) are fixed in install bin (21), riser (27) are fixed in concave frame (29), lower transfer gear (24) are fixed in install bin (21) through elastic component (26), and lower transfer gear (24) and upper transfer gear (23) all can free rotation.

7. An aircraft simulated experience device as claimed in claim 4 wherein: the top of the installation box (21) is further provided with a top plate (211), the middle of the top plate (211) is a flexible plate capable of deforming, a groove (2111) and a through hole are sequentially formed in the through flexible plate, an output shaft of the lifter (27) penetrates through the through hole, the output end of the output shaft of the lifter (27) is provided with a supporting block (2711) matched with the groove (2111), and the width of the supporting block (2711) is larger than the diameter of the through hole.

8. An aircraft simulated experience device as claimed in claim 1 wherein: the deflection simulation device is characterized by further comprising a deflection simulation mechanism (3), wherein the deflection simulation mechanism (3) comprises an inner disc (31) and an outer disc (33) which are concentrically arranged, the installation box (21) is fixed on the inner disc (31), a plurality of groups of second gears (32) are uniformly arranged between the inner disc (31) and the outer disc (33), the second gears (32) are meshed with the inner disc (31) and the outer disc (33), and the outer disc (33) is fixed on the installation frame; a third driving mechanism for driving the inner disc (31) to rotate is also arranged.

9. An aircraft simulated experience device as claimed in claim 8 wherein: the third driving mechanism is a stepping motor, and the stepping motor is fixed in the middle of the outer disc (33).

10. An aircraft simulated experience device as claimed in claim 8 or 9 wherein: the steering simulation mechanism (5) comprises a rotating column, a placing plate (4) is fixedly arranged at the top of the rotating column, and the outer disc (33) is fixed on the placing plate (4); the bottom of the rotating column is provided with a base (6), and the rotating column can rotate on the base (6) around the circumferential direction of the rotating column; and a fourth driving mechanism for driving the rotating column to rotate is also arranged.