Flight simulation training simulation all-in-one machine

Abstract

The invention discloses a flight simulation training simulation all-in-one machine, and relates to the technical field of flight simulation. In order to solve the problems that a traditional flight simulator is difficult to control multi-axis rotation and cannot completely meet training requirements, the invention designs a flight simulation training simulation all-in-one machine which is mainly structurally characterized by comprising a seat, a base and a multi-dimensional rotator, the multi-dimensional rotator is arranged between the base and the seat and is used for providing rotation movement which is in different directions and does not interfere with each other for the seat; the multi-dimensional rotator comprises a first rotating device, a second rotating device and a third rotating device which are sequentially connected from bottom to top. The multi-dimensional rotator is used for controlling the seat to accurately simulate rotation actions, including pitching, yawing, rolling and the like, of the aircraft in a three-dimensional space, so that pilots can better understand and master the dynamic characteristics of the aircraft, and the operation capability and the reaction speed of the pilots under various flight conditions are improved.

Description

Technical Field

[0001] The present invention relates to the technical field of flight simulation, and in particular to an all-in-one flight simulation training machine. Background Art

[0002] With the development of the aviation industry, the demand for pilots is also increasing. At the same time, with the improvement of aircraft performance and the complexity of flight missions, the requirements for pilots are also getting higher and higher. Flight simulation training plays a vital role in the training process of pilots. By simulating the real flight environment, pilots can learn and master flight skills without actual flight risks, and become familiar with various situations during the flight, thereby improving flight safety and efficiency.

[0003] By simulating the real flight environment, the flight simulator allows pilots to train without the actual flight risks, avoiding safety issues caused by unexpected events in real flights. At the same time, the simulator can repeatedly practice the pilots' operational shortcomings, accelerate the mastery of flying skills, and improve training efficiency. Compared with real aircraft flight training, the cost of using the flight simulator is lower, including energy consumption, maintenance costs, and the cost of pilots' training time on the simulator. The simulator can operate around the clock and is not restricted by natural conditions such as weather, further reducing training costs.

[0004] Traditional flight simulators have certain limitations in simulating real flight environments, such as low simulation accuracy and slow response speed. During flight, the aircraft will rotate and move in multiple dimensions. Therefore, flight simulation training equipment needs to be able to simulate these complex motion states. However, traditional flight simulators have difficulties in controlling multi-axis rotation and cannot fully meet training needs.

[0005] The patent with publication number CN114822142B discloses a flight simulation training device, including a base, a boarding board, a protection frame, a seat, etc. The upper rear part of the base is connected to the boarding board, the top of the base is placed with a protection frame, and the bottom of the inner side of the protection frame is connected to the seat. By pulling the first wedge frame to the right, the protection rod will rotate and reset under the action of the second spring reset, and then the trainee will pull the two contraction belts forward respectively through two buckles, and insert the two buckles into two slots respectively, so that the two contraction belts and the protection rod will fix the trainee on the seat, which can prevent the trainee from falling from the seat.

[0006] The improvement direction of the invention is to prevent the trainee from falling from the seat, and the improvement direction of the present invention is the precise control of multi-axis rotation. Summary of the invention

[0007] In view of the above problems, the technical ideas adopted by the present invention to solve the technical problems are as follows: The multi-dimensional rotator control seat accurately simulates the aircraft's rotational movements in three-dimensional space, including pitch, yaw and roll, which helps pilots better understand and master the dynamic characteristics of the aircraft and improve their operating capabilities and reaction speed under various flight conditions.

[0008] The specific plan is as follows: A flight simulation training all-in-one simulator comprises a seat, a base and a multi-dimensional rotator; the multi-dimensional rotator is arranged between the base and the seat to provide the seat with rotational movements in different directions without interfering with each other; wherein the multi-dimensional rotator comprises a first rotating device, a second rotating device and a third rotating device which are sequentially connected from bottom to top.

[0009] In order to realize the above scheme, the preferred scheme is that the first rotating device controls the seat to rotate around the first axis, including: a first motor, vertically arranged on the top of the base, providing power for the first rotating device; a rotating disk, arranged at the output end of the first motor, rotating around the first axis; a follower structure, arranged between the base and the rotating disk, stabilizing the rotating disk; the second rotating device and the third rotating device are arranged on the upper part of the rotating disk; wherein the first axis is the axis center of the first motor; the first motor drives the rotating disk to rotate, the rotating disk drives the follower structure, and the seat rotates with the rotating disk.

[0010] Furthermore, the follower structure includes: a follower disc, which is sleeved on the side of the first motor close to the base and limited by the base; a follower bracket, at least two groups of which have one end connected to the rotating disc and the other end connected to the follower disc; wherein the rotating disc drives the follower disc to rotate through the follower bracket.

[0011] Through the above scheme, another preferred scheme is that the second rotating device controls the seat to rotate around the second axis, including: a first output end of the double-headed motor, arranged on the upper part of the rotating disk; a friction wheel, the friction wheels are respectively arranged on the front and rear sides of the seat support of the seat, controlling the seat support to rotate around the second axis; an inner shaft, both ends of which are respectively connected to the middle of the friction wheel; a first synchronous belt transmission structure, one end of which is connected to the first output end of the double-headed motor, and the other end is connected to the inner shaft; the third rotating device is connected to the inner shaft; wherein the second axis is the axis center of the inner shaft; the first output end of the double-headed motor drives the inner shaft and the friction wheel to rotate through the first synchronous belt transmission structure, and the friction wheel drives the seat support to rotate around the second axis.

[0012] Another preferred solution is that the third rotating device controls the seat to swing around the third axis, including: a second output end of the double-headed motor, arranged on the upper part of the rotating disk; an outer shaft, coaxial with the inner shaft and arranged outside the inner shaft; a second synchronous belt transmission structure, one end of which is connected to the second output end of the double-headed motor, and the other end is connected to the outer shaft; a bevel gear transmission structure, arranged outside the outer shaft; a through shaft, which passes through the chair support along the direction of the third axis; a third synchronous belt transmission structure, one end of which is connected to the bevel gear transmission structure, and the other end is connected to the through shaft Connection; a fixing part, the fixing parts are symmetrically arranged on the left and right sides of the chair; a group of fourth synchronous belt transmission structures, one end of which is connected to the end of the through-shaft, and the other end is connected to the fixing part; wherein the third shaft is the axis of the fixing part; the second output end of the double-headed motor drives the outer shaft to rotate through the second synchronous belt transmission structure, and the outer shaft drives the through-shaft to rotate through the bevel gear transmission structure and the third synchronous belt transmission structure, and the through-shaft drives the chair to swing around the third shaft through the group of fourth synchronous belt transmission structures.

[0013] Furthermore, the chair swings by means of a first sliding block provided at a lower portion thereof cooperating with a first arc-shaped groove provided at an upper portion of the chair support.

[0014] Optionally, a second rotation supplementary structure is arranged at the end of the through-shaft to provide a swinging force for the second rotating device.

[0015] In order to realize the above scheme, further, the second rotating supplementary structure includes: a bracket, which is composed of two vertical rods and a horizontal rod in a "␣" shape, the vertical rods are respectively connected to the end parts of the through-axis, the axis of the horizontal rod forms an intersection with the first axis and the second axis, and the middle part of the horizontal rod is a ring sleeved on the outside of the outer shaft; a second slider is arranged at the lower part of the ring; a second arc groove is arranged at the lower part of the second slider and cooperates with the second slider; wherein, the friction wheel drives the chair support to rotate around the second axis, the bracket rotates with the chair support through the through-axis, and the second slider swings in the second arc groove with the bracket.

[0016] Preferably, the collar and the outer shaft, and the outer shaft and the inner shaft are connected by bearings.

[0017] By adopting the above technical solution, the present invention has the following technical effects: A flight simulation training simulator includes a seat, a base and a multi-dimensional rotator; the multi-dimensional rotator is arranged between the base and the seat, and provides the seat with rotational movements in different directions without interfering with each other; wherein the multi-dimensional rotator includes a first rotating device, a second rotating device and a third rotating device connected in sequence from bottom to top, the first rotating device controls the seat to rotate around a first axis, the second rotating device controls the seat to rotate around a second axis, and the third rotating device controls the seat to swing around a third axis. The multi-dimensional rotator provides simultaneous and non-interfering rotations in multiple postures, and controls the seat through the multi-dimensional rotator to accurately simulate the rotational movements of the aircraft in three-dimensional space, including pitch, yaw and roll, etc., which helps pilots better understand and master the dynamic characteristics of the aircraft and improve their operational capabilities and reaction speed under various flight conditions. BRIEF DESCRIPTION OF THE DRAWINGS

[0018] In order to more clearly illustrate the technical solutions of the embodiments of the present application, the drawings used in the embodiments are briefly introduced below.

[0019] Figure 1 is a structural diagram of a flight simulation training all-in-one machine provided in an embodiment of the present application, Figure 2 is a schematic structural diagram of a first rotating device provided in an embodiment of the present application, Figure 3 is a schematic structural diagram of a second rotating device provided in an embodiment of the present application, Figure 4 is a schematic structural diagram of a third rotating device provided in an embodiment of the present application, Figure 5 is a schematic structural diagram of a third rotating device from another perspective provided in an embodiment of the present application, Figure 6 is a cross-sectional view of a third rotating device provided in an embodiment of the present application, Figure 7 The embodiment of this application provides Figure 6 A partial enlarged view of Figure 8 is a schematic diagram of the structure of a first sliding block provided in an embodiment of the present application, Fig. 9 is a schematic structural diagram of a first arc-shaped groove provided in an embodiment of the present application, Fig.10 is a schematic diagram of the structure of the second rotation supplement provided in an embodiment of the present application, Fig.11 is a schematic diagram of the position of the second rotation supplement provided in an embodiment of the present application, Icons: 100, base; 200, first rotating device; 201, first motor; 202, rotating disc; 203, follower disc; 204, follower bracket; 300, second rotating device; 301, double-headed motor; 302, first synchronous belt transmission structure; 303, inner shaft; 304, friction wheel; 305, bracket; 306, second slider; 307, second arc groove; 400, third rotating device; 401, second synchronous belt transmission structure; 402, outer shaft; 403, bevel gear transmission structure; 404, third synchronous belt transmission structure; 405, through shaft; 406, a set of fourth synchronous belt transmission structures; 407, bearing member; 408, connecting rod; 500, seat; 501, chair support; 502, chair; 503, fixing member; 504, first slider; 505, first arc groove. DETAILED DESCRIPTION

[0020] In order to make the purpose, technical solution and advantages of the embodiments of the present application clearer, the following will be combined with the appended Figure 1-11 , the technical solutions in the embodiments of the present application are described clearly and completely. Obviously, the described embodiments are only part of the embodiments of the present application, not all of the embodiments.

[0021] It should be noted that similar reference numerals and letters denote similar items in the following drawings, and therefore, once an item is defined in one drawing, further definition and explanation thereof is not required in subsequent drawings.

[0022] In the description of the present application, it should be noted that the terms "center", "up", "down", "vertical", "horizontal", "inside", "outside", etc. indicate orientations or positional relationships based on the orientations or positional relationships shown in the accompanying drawings, or are the orientations or positional relationships in which the products of the application are usually placed when in use. They are only for the convenience of describing the present application and simplifying the description, and do not indicate or imply that the device or element referred to must have a specific orientation, be constructed and operated in a specific orientation, and therefore should not be understood as a limitation on the present application.

[0023] In the description of this application, it should also be noted that, unless otherwise clearly specified and limited, the terms "set", "install", "connected" and "connected" should be understood in a broad sense.

[0024] Example The inventors have found that traditional flight simulators have difficulties in controlling multi-axis rotation and cannot fully meet training needs.

[0025] In the examples of this application, please refer to Figure 1 , Figure 11 is a structural diagram of a flight simulation training all-in-one simulator provided in an embodiment of the present application. The present application provides a flight simulation training all-in-one simulator, comprising a seat 500, a base 100 and a multi-dimensional rotator; the multi-dimensional rotator is arranged between the base 100 and the seat 500, and provides the seat 500 with rotational movements in different directions without interfering with each other; wherein the multi-dimensional rotator comprises a first rotating device 200, a second rotating device 300 and a third rotating device 400 connected in sequence from bottom to top.

[0026] The multi-dimensional rotator provides simultaneous and non-interfering rotation in multiple postures. By controlling the multi-dimensional rotator, the seat 500 can accurately simulate the rotation movement of the aircraft in three-dimensional space, including pitch, yaw and roll, etc., which helps pilots better understand and master the dynamic characteristics of the aircraft and improve their operating ability and reaction speed under various flight conditions.

[0027] In order to ensure safety and stability, the flight simulation training all-in-one machine of the present invention adopts strong, wear-resistant and load-bearing materials.

[0028] The base 100 is in the shape of a rectangular plate, and its bottom is in contact with the ground, so as to increase the force-bearing area of ​​the present invention, increase the friction force, and make the present invention stable.

[0029] The chair 500 is divided into two parts, the lower part is a rectangular chair support 501, and the upper part is a chair 502; the upper part of the chair 502 has a seat, and the left and right sides of the seat are armrests. The outer sides of the armrests are symmetrically welded with cylindrical fixings 503, the back of the seat is a backrest, and the lower part is a semi-circular arc surface. The specifications and dimensions of the chair 502 are based on ergonomics.

[0030] In the examples of this application, please refer to Figure 2 , Figure 2 : is a schematic diagram of the structure of the first rotating device provided in the embodiment of the present application. The first rotating device 200 controls the seat 500 to rotate around the first axis, including: a first motor 201, which is vertically arranged on the top of the base 100 and provides power for the first rotating device 200; a rotating disc 202, which is arranged at the output end of the first motor 201 and rotates around the first axis; a follower structure, which is arranged between the base 100 and the rotating disc 202 and stabilizes the rotating disc 202; a second rotating device 300 and a third rotating device 400 are arranged on the upper part of the rotating disc 202; and the first axis is the axis of the first motor 201.

[0031] The first motor 201 is a common prior art, which can be realized by those skilled in the art and will not be described in detail here. The first motor 201 is placed vertically, with one end welded to the top center of the base 100 and the other end (i.e., the output end) welded to the bottom center of the horizontally placed circular rotating disk 202.

[0032] The first motor 201 drives the rotating disk 202 to rotate, and the rotating disk 202 drives the follower structure, and the seat 500 rotates along with the rotating disk 202 .

[0033] The follower structure includes: a follower disc 203, which is sleeved on the side of the first motor 201 close to the base 100 and limited by the base 100; a follower bracket 204, at least two groups of follower brackets 204 have one end connected to the rotating disc 202 and the other end connected to the follower disc 203.

[0034] The follower disc 203 is annular, and its inner diameter matches the outer diameter of the first motor 201 . The base 100 is provided with an annular groove matching the follower disc 203 . The follower disc 203 is placed in the annular groove and can rotate in the annular groove around the first axis.

[0035] The follower bracket 204 is cylindrical, one end of which is welded to the top of the follower disc 203, and the other end of which is welded to the bottom of the rotating disc 202. The present application does not limit the specific number of the follower brackets 204, and those skilled in the art should adjust according to the actual application and to maintain the stability of the present invention. At least two groups of follower brackets 204 are distributed in a circular array around the first motor 201.

[0036] The output end of the first motor 201 drives the rotating disc 202 to rotate around the first axis, and the rotating disc 202 drives the follower disc 203 to rotate around the first axis through the follower bracket 204 .

[0037] The rotating disc 202 drives the follower disc 203 to rotate via the follower bracket 204 .

[0038] A double-headed motor 301 is welded on the top of the rotating disk 202. The output end of the double-headed motor 301 is placed on the front side. The output end includes a first output end and a second output end. The double-headed motor 301 is a common prior art and can be implemented by those skilled in the art, so it will not be described in detail here.

[0039] In the examples of this application, please refer to Figure 3 , Figure 3 : is a schematic diagram of the structure of the second rotating device provided in the embodiment of the present application. The second rotating device 300 controls the seat 500 to rotate around the second axis, including: the first output end of the double-headed motor 301, arranged on the upper part of the rotating disc 202; friction wheels 304, the friction wheels 304 are arranged on the front and rear sides of the seat support 501 of the seat 500, respectively, to control the seat support 501 to rotate around the second axis; the inner shaft 303, which is a solid rod, and its two ends are respectively welded to the middle of the friction wheel 304; the first synchronous belt transmission structure 302, one end of which is connected to the first output end of the double-headed motor 301, and the other end is connected to the inner shaft 303; the third rotating device 400 is connected to the inner shaft 303; the second axis is the axis of the inner shaft 303.

[0040] The synchronous belt transmission structure includes an annular belt with inner teeth and two synchronous belt pulleys with teeth, which transmit power by meshing of teeth without relative sliding, thus ensuring the synchronization between the two wheels. This is a common prior art, which can be realized by those skilled in the art and will not be described in detail here. The first synchronous belt transmission structure 302, the second synchronous belt transmission structure 401 and the third synchronous belt transmission structure 404 mentioned in the embodiment of the present application are all synchronous belt transmission structures, but the positions of the arrangements are different, which will not be described in detail later.

[0041] The friction wheel 304 is disc-shaped and vertically arranged, and its upper part is respectively fitted with the front and rear sides of the bottom of the chair support 501. The bottom of the chair support 501 is provided with an arc groove that matches the upper part of the friction wheel 304; the friction wheel 304 drives the chair support 501 and the chair 502 to rotate around the second axis through the arc groove.

[0042] The first synchronous belt transmission structure 302: a synchronous pulley is welded or clamped on the first output end of the double-head motor 301, a synchronous pulley is welded or clamped on the front side of the inner shaft 303, and the belt is sleeved on the two synchronous pulleys.

[0043] The first output end of the double-headed motor 301 drives the inner shaft 303 and the friction wheel 304 to rotate through the first synchronous belt transmission structure 302, and the friction wheel 304 drives the chair support 501 to rotate around the second shaft.

[0044] In the examples of this application, please refer to Figure 4 , Figure 5 , Figure 6 and Figure 7 , Figure 4 is a schematic structural diagram of a third rotating device provided in an embodiment of the present application, Figure 5 is a schematic structural diagram of a third rotating device from another perspective provided in an embodiment of the present application, Figure 6 is a cross-sectional view of a third rotating device provided in an embodiment of the present application, Figure 7 The embodiment of this application provides Figure 6The third rotating device 400 controls the seat 500 to swing around the third axis, and includes: the second output end of the double-headed motor 301, which is arranged on the upper part of the rotating disk 202; the outer shaft 402, which is coaxial with the inner shaft 303 and arranged outside the inner shaft 303; the second synchronous belt transmission structure 401, one end of which is connected to the second output end of the double-headed motor 301, and the other end is connected to the outer shaft 402; the bevel gear transmission structure 403, which is arranged outside the outer shaft 402; the through shaft 405, passing through the chair support 501 along the third axis direction; a third synchronous belt transmission structure 404, one end of which is connected to the bevel gear transmission structure 403, and the other end of which is connected to the through-axis 405; a fixing member 503, the left and right sides of the chair 502 of the seat 500 are symmetrically provided with fixing members 503; a set of fourth synchronous belt transmission structures 406, one end of which is connected to the end of the through-axis 405, and the other end of which is connected to the fixing member 503; the third axis is the axis center of the fixing member 503.

[0045] The outer shaft 402 is in the shape of a hollow cylinder, and its inner diameter is larger than the outer diameter of the inner shaft 303; the outer shaft 402 and the inner shaft 303 are connected by a bearing to achieve relative rotation without interfering with each other; the front and rear sides of the outer shaft 402 are respectively fixed with bearing parts 407 to fix the position of the outer shaft 402 and achieve non-interference in the rotation of the outer shaft 402.

[0046] The second synchronous belt transmission structure 401: a synchronous pulley is welded or clamped on the second output end of the double-head motor 301, a synchronous pulley is welded or clamped on the front side of the outer shaft 402, and the belt is sleeved on the two synchronous pulleys.

[0047] The bevel gear transmission is a gear transmission between intersecting axes composed of a pair of bevel gears. The bevel gear transmission structure 403 is a common prior art and can be implemented by a person skilled in the art, so it will not be described in detail here. The outer shaft 402 passes through one of the bevel gears, and the outer shaft 402 is welded to the bevel gear. One side of the other bevel gear is meshed with the bevel gear on the outer shaft 402, and the other side is welded or clamped with the end of a connecting rod 408, and the connecting rod 408 extends to the left side of the device.

[0048] The third synchronous belt transmission structure 404: a synchronous belt pulley is welded or clamped on one end of the through shaft 405, a synchronous belt pulley is welded or clamped on the end of the connecting rod 408 away from the bevel gear, and the belt is sleeved on the two synchronous belt pulleys.

[0049] A fourth synchronous belt transmission structure 406: synchronous pulleys are welded or clamped on both ends of the through shaft 405, and synchronous pulleys are welded or clamped on the fixing parts 503 on both sides of the chair 502, and the belts are respectively mounted on the two synchronous pulleys on the same side.

[0050] The second output end of the double-headed motor 301 drives the outer shaft 402 to rotate through the second synchronous belt transmission structure 401, and the outer shaft 402 drives the through shaft 405 to rotate through the bevel gear transmission structure 403 and the third synchronous belt transmission structure 404. The through shaft 405 drives the chair 502 to swing around the third axis through a set of fourth synchronous belt transmission structures 406.

[0051] In the examples of this application, please refer to Figure 8 and Fig. 9 , Figure 8 is a schematic diagram of the structure of a first sliding block provided in an embodiment of the present application, Fig. 9 Schematic diagram of the structure of the first arc groove provided in the embodiment of the present application. A first slider 504 is integrally formed on the semicircular arc surface at the lower part of the chair 502 along the second axis direction, and a first arc groove 505 cooperating with the first slider 504 is integrally formed on the upper part of the chair support 501 along the second axis direction. The chair 502 swings by cooperating with the first slider 504 at the lower part and the first arc groove 505 at the upper part of the chair support 501.

[0052] In the examples of this application, please refer to Fig.10 and Fig.11 , Fig.10 is a schematic diagram of the structure of the second rotation supplement provided in an embodiment of the present application, Fig.11 4 is a schematic diagram of the position of the second rotation supplement provided in the embodiment of the present application. The end of the through-shaft 405 is provided with a second rotation supplement structure to provide a swinging force for the second rotation device 300.

[0053] The second rotation supplementary structure includes: a bracket 305, which is composed of two vertical rods and a horizontal rod in a "␣" shape, the vertical rods are respectively connected to the ends of the through-axis 405, the axis of the horizontal rod forms an intersection with the first axis and the second axis, and the middle part of the horizontal rod is a ring that is sleeved on the outside of the outer shaft 402; a second slider 306 is arranged at the lower part of the ring; a second arc groove 307 is arranged at the lower part of the second slider 306 and cooperates with the second slider 306.

[0054] In order to cooperate with the third rotating device 400, the vertical rod on the left is "L"-shaped, and the end of the connecting rod 408 away from the bevel gear passes through the front side of the vertical rod and can rotate inside it; the bracket 305 has a branch connected to the middle part of the connecting rod 408, which is used to fix the position of the connecting rod 408 and does not interfere with the rotation of the connecting rod 408; the bracket 305 is integrally formed and placed at the lower part of the chair support 501.

[0055] The bottom of the second arc groove 307 is welded or clamped to the top of the double-headed motor 301; the upper part of the second slider 306 is welded to the lower part of the collar, and the lower part cooperates with the upper part of the second arc groove 307 and slides therein.

[0056] It should be noted that the collar and the outer shaft 402 are connected by a bearing.

[0057] The friction wheel 304 drives the chair support 501 to rotate around the second axis, the bracket 305 rotates with the chair support 501 through the through shaft 405, and the second sliding block 306 swings in the second arc groove 307 with the bracket.

[0058] Application Process 1Highly realistic simulation experience: Through precise control of multi-axis rotation and sophisticated simulation systems, the design can simulate highly realistic flight environments and flight maneuvers, allowing pilots to experience a feeling that is almost the same as real flight during training. This realistic simulation experience helps pilots better adapt to the actual flight environment and improve their ability to deal with various complex situations.

[0059] 2 Precise control of multi-axis rotation: The design uses advanced motors and transmission systems to achieve precise control of multi-axis rotation, allowing the simulator to simulate more complex flight maneuvers and flight trajectories. Precise control helps improve training results and helps pilots master flight skills more accurately.

[0060] 3. Improve training efficiency and effectiveness: The flight simulator can operate around the clock, regardless of weather or other natural conditions, and can greatly improve training efficiency. At the same time, through the simulator's intelligent evaluation and suggestion functions, pilots can keep abreast of their training status, identify deficiencies and make improvements, thereby improving training effectiveness.

[0061] 4. Reduce training costs: Compared with real aircraft flight training, the operating cost of the all-in-one flight simulation training machine is lower, including energy consumption, maintenance costs, and the cost of pilot training time on the simulator.

[0062] The above description is only the preferred embodiment of the present application and is not intended to limit the present application. For those skilled in the art, the present application may have various modifications and variations. Any modification, equivalent replacement, improvement, etc. made within the spirit and principle of the present application shall be included in the protection scope of the present application.

Claims

1. A flight simulation training all-in-one simulator, comprising a seat (500) and a base (100), characterized in that: Also includes: A multi-dimensional rotator, arranged between the base (100) and the seat (500), providing the seat (500) with rotational movements in different directions without interfering with each other; The multi-dimensional rotator comprises a first rotating device (200), a second rotating device (300) and a third rotating device (400) which are sequentially connected from bottom to top.

2. The flight simulation training all-in-one machine according to claim 1, characterized in that: The first rotating device (200) controls the seat (500) to rotate around a first axis, comprising: A first motor (201) is arranged vertically on the top of the base (100) and provides power for the first rotating device (200); A rotating disk (202) is arranged at the output end of the first motor (201) and rotates around the first axis; A follower structure, arranged between the base (100) and the rotating disk (202), to stabilize the rotating disk (202); The second rotating device (300) and the third rotating device (400) are arranged on the upper part of the rotating disk (202); The first shaft is the axis of the first motor (201); the first motor (201) drives the rotating disc (202) to rotate, the rotating disc (202) drives the follower structure, and the seat (500) rotates along with the rotating disc (202).

3. The flight simulation training all-in-one machine according to claim 2, characterized in that: The follower structure comprises: A follower disc (203) is sleeved on a side of the first motor (201) close to the base (100) and is limited by the base (100); Follow-up brackets (204), at least two groups of follow-up brackets (204) having one end connected to the rotating disc (202) and the other end connected to the follow-up disc (203); The rotating disc (202) drives the follower disc (203) to rotate via the follower bracket (204).

4. The flight simulation training all-in-one machine according to claim 2, characterized in that: The second rotating device (300) controls the seat (500) to rotate around a second axis, comprising: A first output end of the double-headed motor (301) is arranged on the upper part of the rotating disc (202); Friction wheels (304), the friction wheels (304) being arranged on the front and rear sides of a chair support (501) of the seat (500) respectively, for controlling the chair support (501) to rotate around a second axis; The inner shaft (303) has two ends respectively connected to the middle of the friction wheel (304); A first synchronous belt transmission structure (302), one end of which is connected to the first output end of the double-headed motor (301), and the other end of which is connected to the inner shaft (303); The third rotating device (400) is connected to the inner shaft (303); The second shaft is the axis of the inner shaft (303); the first output end of the double-headed motor (301) drives the inner shaft (303) and the friction wheel (304) to rotate through the first synchronous belt transmission structure (302); and the friction wheel (304) drives the chair support (501) to rotate around the second shaft.

5. The flight simulation training all-in-one machine according to claim 4, characterized in that: The third rotating device (400) controls the seat (500) to swing around a third axis, comprising: The second output end of the double-headed motor (301) is arranged on the upper part of the rotating disc (202); An outer shaft (402) is coaxial with the inner shaft (303) and is arranged outside the inner shaft (303); A second synchronous belt transmission structure (401), one end of which is connected to the second output end of the double-headed motor (301), and the other end of which is connected to the outer shaft (402); A bevel gear transmission structure (403) is arranged outside the outer shaft (402); A penetrating shaft (405) penetrating the chair support (501) along the third axis direction; A third synchronous belt transmission structure (404), one end of which is connected to the bevel gear transmission structure (403), and the other end of which is connected to the through shaft (405); A fixing member (503), the fixing members (503) being symmetrically arranged on the left and right sides of the chair (502) of the seat (500); A set of fourth synchronous belt transmission structures (406), one end of which is connected to the end of the through-shaft (405), and the other end of which is connected to the fixing member (503); The third axis is the axis of the fixing member (503); the second output end of the double-headed motor (301) drives the outer axis (402) to rotate via the second synchronous belt transmission structure (401); the outer axis (402) drives the through-axis (405) to rotate via the bevel gear transmission structure (403) and the third synchronous belt transmission structure (404); the through-axis (405) drives the chair (502) to swing around the third axis via the set of fourth synchronous belt transmission structures (406).

6. The flight simulation training all-in-one machine according to claim 5, characterized in that: The chair (502) swings by means of a first sliding block (504) disposed at the bottom thereof cooperating with a first arc-shaped groove (505) disposed at the top of the chair support (501).

7. The flight simulation training all-in-one machine according to claim 5, characterized in that: A second rotation supplementary structure is arranged at the end of the through-shaft (405) to provide a swinging force for the second rotation device (300).

8. The flight simulation training all-in-one machine according to claim 7, characterized in that: The second rotation supplementary structure comprises: The bracket (305) is formed into a "␣" shape by two vertical bars and a horizontal bar, the vertical bars are respectively connected to the ends of the through-shaft (405), the axis of the horizontal bar forms an intersection with the first shaft and the second shaft, and the middle portion of the horizontal bar is a ring sleeved on the outside of the outer shaft (402); A second sliding block (306) is arranged at the lower part of the collar; A second arc-shaped groove (307) is arranged at the lower part of the second sliding block (306) and cooperates with the second sliding block (306); The friction wheel (304) drives the chair support (501) to rotate around the second axis, the bracket (305) rotates with the chair support (501) via the through-shaft (405), and the second sliding block (306) swings in the second arc groove (307) with the bracket (305).

9. The flight simulation training all-in-one machine according to claim 8, characterized in that: The collar and the outer shaft (402), and the outer shaft (402) and the inner shaft (303) are both connected by bearings.

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