Advanced simulation mechanism

Abstract

The invention relates to an advanced simulation mechanism (1).

Description

[0001] ADVANCED SIMULATION MECHANISM

[0002] FIELD OF INVENTION

[0003] The invention relates to an advanced simulation mechanism for simulating all types of air, land and sea vehicles.

[0004] BACKGROUND OF THE INVENTION

[0005] Simulators are presented to users for purposes such as education and entertainment. The realism of the simulation is particularly important for educational purposes. To ensure realism in simulators used to simulate land, air and sea vehicles, the seat in which the user sits must be moved in accordance with the movements of the relevant vehicle. Although virtual reality glasses can convey the environment to the user as desired in the virtual world, the simulator cannot provide the desired effect when movements are not realistic. Accordingly, simulator mechanisms that move in multiple axes are generally used so that the seat can be moved in accordance with the motion of the vehicle being simulated.

[0006] Specifically, for simulating vehicles such as cars and trucks traveling on highways, the platform on which the user sits is moved up and down at least at two points. Although the application in question partially conveys the vehicle's movements to the user, it is not possible to feel many of the movements that actually occur. However, simulating movement is even more difficult in off-road vehicles, where more movement occurs during driving.

[0007] On the other hand, although there are some differences between sea vehicles and land vehicles, multi-directional movements make simulation more difficult.

[0008] Finally, aircraft such as airplanes and helicopters perform much more complex movements than land vehicles, so many different movements must be performed to simulate them. As a result, all the above-mentioned problems have made it imperative to innovate in the relevant technical field.

[0009] SUMMARY OF THE INVENTION

[0010] The present invention relates to an advanced simulation mechanism to overcome the aforementioned disadvantages and to bring new advantages to the relevant technical field.

[0011] The object of the invention is to provide an advanced simulation mechanism for simulating all types of air, land and sea vehicles.

[0012] In order to realize all of the above mentioned objects and the objects which are to be deducted from the detailed description below, the present invention relates to a simulating mechanism.

[0013] Accordingly, it comprises: a base, a fixed carrier provided on said base, a rotating layer performing rotational movement on a z-axis extending vertically on said fixed carrier, an X-axis movement layer that can move linearly on the said rotating layer on an x-axis, a Y-axis movement layer that can move linearly on the said x-axis movement layer on a y-axis, a Y-axis movement layer, a three-axis motion mechanism having an upper plane whose three corners can move independently of each other, and a cabin in which at least one seat is positioned, a frame body connected in a rolling manner to a roll axis extending in the front-to-back direction of the cabin, the frame body connected a rotating body so that the frame body can rotate about a pitch axis extending in the left-right direction of the cabin, the rotating body having a carrier base connected to the upper plane, thereby comprising a cabin movement mechanism. Thus, the vehicle's deceleration and acceleration are simulated by forward and backward movements on the x-axis, the skidding that occurs during turns is simulated by left and right movements on the y-axis, and the movements that occur during the vehicle's turn and spin are simulated by the rotational movement on the z-axis. Additionally, movements that would occur if at least one side of the vehicle encounters a dip or bump in the road are simulated using a three-axis motion mechanism. In another preferred embodiment of the subject matter invention, includes at least one braking mechanism to at least partially restrict the movement of the cabin on the pitch axis. Thus, unwanted movements that would not actually occur during the turn are stopped by the brake mechanism.

[0014] In another preferred embodiment of the subject matter invention, at least one fifth motor is provided on the frame body to enable the cabin to move on the roll axis.

[0015] In another preferred embodiment of the subject matter invention, there is at least one first shaft extending along the roll axis to provide connection between the cabin and the frame body.

[0016] In another preferred embodiment of the subject matter invention, a second motor is provided on the rotating body to enable the cabin and frame body to move along the pitch axis.

[0017] In another preferred embodiment of the subject matter invention, there is at least one second shaft extending along the pitch axis to connect the frame body and the rotating body.

[0018] In another preferred embodiment of the subject matter invention, a gearbox is provided to transmit the motion from the second motor to the second shaft.

[0019] In another preferred embodiment of the subject matter invention, the brake mechanism is related to the second shaft.

[0020] In another preferred embodiment of the subject matter invention, the three-axis movement mechanism comprises a lower plane fixed to the Y-axis movement layer, a drive mechanism provided on said lower plane and transmitting the movement received from a fourth motor to a transmission element, and a drive arm extending from the upper plane to the lower plane and connected at one end to the transmission element. In another preferred embodiment of the subject matter invention, the fourth motor, drive shaft, and transmission element are provided at each of the three corners of the three-axis motion mechanism.

[0021] In another preferred embodiment of the subject matter invention, an upper joint is provided to ensure that the drive shaft is connected in such a way that it is free to rotate to the upper plane.

[0022] In another preferred embodiment of the subject matter invention, a lower joint is provided to ensure that the drive shaft is connected to the transmission element with freedom of rotation on a drive axis.

[0023] In another preferred embodiment of the subject matter invention, the transmission element is connected to the transmission mechanism via a rotation axis parallel to the drive axis. Thus, the transmission element and drive shaft provide a mode of operation similar to that of a crankshaft connecting rod mechanism.

[0024] In another preferred embodiment of the subject matter invention, it includes a rotation mechanism provided between the base and the fixed carrier to enable the rotating layer to perform a rotational movement about the z-axis on the fixed carrier. Thus, rotational movement is achieved.

[0025] In another preferred embodiment of the subject matter invention, it includes a rotating mechanism related to a circular plate that is mounted on a fixed carrier and connected to the rotating layer. Thus, rotation can be controlled without the need for additional bearings.

[0026] In another preferred embodiment of the subject matter invention, it includes a first motor associated with the rotation mechanism. This ensures that the rotation mechanism is driven.

[0027] In another preferred embodiment of the subject matter invention, it includes an X- axis movement mechanism provided within the rotating layer to ensure the linear displacement of the X-axis movement layer provided on the rotating layer. Thus, the total mechanism height is kept at the lowest possible level. In another preferred embodiment of the subject matter invention, the X-axis movement mechanism includes an X-axis threaded shaft related to a second motor and an X-axis threaded shaft related to the X-axis movement layer. Thus, the linear motion is transferred to the x-axis motion layer.

[0028] In another preferred embodiment of the subject matter invention, the X-axis movement mechanism includes at least one X-axis linear rail. Thus, the direction of linear motion is fixed.

[0029] In another preferred embodiment of the subject matter invention, it includes a Y- axis movement mechanism provided within the X-axis movement layer to enable the linear displacement of the Y-axis movement layer positioned on top of the X- axis movement layer. Thus, the total mechanism height is kept at the lowest possible level.

[0030] In another preferred embodiment of the subject matter invention, the Y-axis movement mechanism includes a Y-axis threaded shaft related to a third motor and a Y-axis nut connected to the Y-axis layer. Thus, the linear motion is transferred to the y-axis motion layer.

[0031] In another preferred embodiment of the subject matter invention, the Y-axis movement mechanism includes at least one Y-axis linear rail.

[0032] BRIEF DESCRIPTION OF THE FIGURES

[0033] Fig. 1 shows a representational isometric view of the Y-axis motion layer and the layers beneath it of the advanced simulation mechanism which is the subject of the invention.

[0034] Fig. 2 shows a detailed view of the interior of the fixed carrier in the advanced simulation mechanism which is the subject of the invention. Fig. 3 and 4 provide a detailed view showing the inner parts of the X-axis movement layer and the Y-axis movement layer in the advanced simulation mechanism which is the subject of the invention.

[0035] Fig. 5 shows a representational isometric view of the advanced simulation mechanism which is the subject of the invention.

[0036] Fig. 6 provides a representative isometric view showing the interior of the three- axis motion mechanism in the advanced simulation mechanism which is the subject of the invention.

[0037] Fig. 7 shows a representative isometric view of the advanced simulation mechanism which is the subject of the invention.

[0038] Fig. 8 shows a representative isometric view of the cabin movement mechanism in the advanced simulation mechanism which is the subject of the invention.

[0039] Fig. 9 shows a representative top view of the cabin movement mechanism in the advanced simulation mechanism which is the subject of the invention.

[0040] Fig. 10 shows another representative isometric view of the cabin movement mechanism in the advanced simulation mechanism which is the subject of the invention.

[0041] DETAILED DESCRIPTION OF THE PROBABLE EMBODIMENT(S)

[0042] In this detailed description, advanced simulation mechanism (1 ) is explained with references to examples without forming any restrictive effect in order to make the subject more understandable.

[0043] The subject of the invention is an advanced simulation mechanism (1 ) essentially comprising a base (10), a fixed carrier (20) provided on said base (10), a rotating layer (30) performing rotational movement on a z-axis (z) extending vertically on said fixed carrier (20), an X-axis movement layer (40) that can move linearly on the X-axis (x) on the aforementioned rotating layer (30), and a Y-axis movement layer (50) that can move linearly on the Y-axis (y) on the aforementioned X-axis movement layer (40). Above the Y-axis movement layer (50) is a three-axis movement mechanism (60), and above that is a cabin movement mechanism (70).

[0044] In detail, the base (10) ensures that the advanced simulation mechanism (1 ) is positioned on the ground. A plurality of feet (24) are positioned on the base (10), and a fixed carrier (20) in the form of a plate is positioned on the aforementioned feet (24). A rotation mechanism (22) is provided between the fixed carrier (20) and the base (10). A circular plate (21) is mounted on a fixed carrier (20) with rotational freedom. The said circular plate (21) rotates on the z-axis (z) extending perpendicular to the base (10) with the motion it receives from the rotation mechanism (22). The rotation mechanism (22) has a first motor (23). In a possible configuration, a belt-pulley-like motion transmission mechanism (not shown in the figure) is used to drive the circular plate (21 ) by means of the first motor (23). The rotating layer (30) is rigidly connected to the circular plate (21 ) mounted on the fixed carrier (20). Therefore, when the circular plate (21 ) rotates, the rotating layer (30) performs a rotational movement about the z-axis (z).

[0045] The X-axis movement mechanism (31 ) is positioned within the rotating layer (30). In a possible configuration of the invention, the X-axis movement mechanism (31 ) includes at least one X-axis linear rail (35) and a guide mechanism. The X-axis movement layer (40) is positioned on the guide structure operating on the said X- axis linear rail (35). In a possible configuration, a second motor (32) is provided as a drive source in the X-axis movement mechanism (31 ), and the drive received from the second motor (32) causes the displacement of the X-axis movement layer (40) via an X-axis threaded shaft (33) and an X-axis nut (34).

[0046] A Y-axis movement mechanism (50) is located within the X-axis movement layer

[0047] (40). In a possible configuration of the invention, the Y-axis movement mechanism

[0048] (41 ) includes at least one Y-axis linear rail (45) and a guide mechanism. The Y-axis movement layer (40) is positioned on the guide operating on the said Y-axis linear rail (45). In a possible configuration, a third motor (42) is used as the drive source in the Y-axis movement mechanism (41 ), and the drive received from the third motor (42) causes the displacement of the Y-axis movement layer (50) via a Y-axis threaded shaft (43) - Y-axis nut (44) configuration.

[0049] The Y-axis movement layer (50) and the three-axis movement mechanism (60) are rigidly connected to each other. Therefore, the three-axis movement mechanism

[0050] (60) performs a sliding movement along the Y-axis (Y) together with the Y-axis movement layer (50).

[0051] The three-axis movement mechanism (60) essentially comprises a lower plane (61) and an upper plane (68) provided substantially parallel to said lower plane (61 ). The drive arm (65) extending toward the lower plane (61 ) is connected to the upper plane (68) with rotational freedom via an upper joint (67). The other end of the drive shaft (65) is connected to a transmission element (64) via a lower joint (67) with rotational freedom. The transfer element (64) can rotate partially on a rotation axis (a) using the motion it receives from a fourth motor (63) fixed on the lower plane

[0052] (61 ). To achieve this, the transfer element (64) is connected to a drive mechanism

[0053] (62) which is related to the fourth motor (63). The axis of motion occurring at the point where the drive shaft (65) is connected to the transmission element (64) is defined as a drive axis (t). In the three-axis motion mechanism (60), the distance between the drive axis (t) and the rotation axis (a) determines the stroke amount of the drive arm (65). In other words, the motion from the fourth motor (63) is transferred to the transmission element (64) by the drive mechanism (62) and causing the transmission element (64) to rotate. As the transfer element (64) rotates, one end of the drive arm (65) is displaced. During the rotation of the transfer element (64), when the end of the drive arm (65) points upward, the upper plane (68) moves upward together with the drive arm (65). Similarly, during the rotation of the transfer element (64), when the end of the drive arm (65) points downward, the upper plane (68) moves downward together with the drive arm (65). The upper plane (68) and lower plane (61 ) are connected to each other at three points, with equal distances between them. In other words, there are three drive arms (65), three transmission elements (64), and three drive mechanisms (62) between the upper plane (68) and the lower plane (61). Each drive mechanism (62) is driven by a separate fourth motor (63). Thanks to the drive arms (65) being positioned at equal distances from each other and driven separately, the three corners of the upper plane (68) move up and down independently of each other. In the described structure, gear structures, belt pulley structures, or a different motion transmission mechanism can be used as the drive mechanism (62).

[0054] In a possible configuration of the invention, the cabin movement mechanism (70) is positioned on the upper plane (68).

[0055] The cabin movement mechanism (70) said above has a cabin (71) in which a seat (72) can be positioned. A frame body (80) surrounds the said cabin (71 ). The cabin (71 ) is connected to the frame body (80) in such a way that it can rotate on a roll axis (r) extending from the front to the rear of the cabin (71 ). To provide the connection said above, the first shaft (82) extends from the front and rear of the cabin (71) toward the frame body (80) along the roll axis (r). Additionally, a fifth motor (81 ) provided on the frame body (80) causes the frame body (80) to rotate about its roll axis (r) via the said first shaft (82). The mentioned rotation movement allows the cabin (71 ) to tilt to the right and left. In a possible configuration of the invention, the roll axis (r) extends through the center of gravity of the cabin (71).

[0056] A rotating body (90) is related to the frame body (80). In other words, the frame body (80) is connected to the rotating body (90) in such a way that it can perform a rotational movement on a pitch axis (p). The frame body (80) and the rotating body (90) are connected by means of a second shaft (92) extending along the pitch axis (p). In the structure described, the pitch axis (p) extends along the left-right direction of the cabin (71). A sixth motor (91 ) provided on the rotating body (90) drives the movement of the frame body (80) via the second shaft (92). During the mentioned movement, depending on the rotation direction of the sixth motor (91), the front of the cabin (71 ) is moved upward and the rear downward, or the front downward and the rear upward.

[0057] In a possible configuration of the invention, the rotating body (90) is provided in a U-shaped form. Accordingly, the frame body (80) is positioned between the arms of the U-shape extending upward from the sides.

[0058] When the rotating body (90) is positioned on the carrier base (701 ), there is a z- axis (z) extending upward from the carrier base (701). The Z-axis is used as the yaw axis for the cabin. The carrier base (701) mentioned ensures that the cabin movement mechanism (70) sits on the upper plane (68). The mentioned z-axis (z) extends perpendicular to the upper plane (68). The pitch axis (p) extends parallel to the upper plane (68). In a possible configuration, the pitch axis (p) is perpendicular to the z-axis (z).

[0059] In the cabin movement mechanism (70), the seat (72) located inside the cabin (71) is positioned as close as possible to one rear end (73) of the cabin (71). In other words, the seat (72) is located between the pitch axis (p) and the rear end (73) of the cabin (71). This way, when the user sits on the seat (72), they are positioned a certain distance away from the pitch axis (p). In a possible configuration, the seat

[0060] (72) is positioned between the extension direction of the z-axis (z) and the rear end

[0061] (73) of the cabin (71). According to the structures mentioned, the seat (72) is positioned at least a certain distance away from the z-axis (z) and pitch axis (p). In other words, at least one of the z-axis (z) and the pitch axis (p) does not pass through the seat (72).

[0062] The seating position (72), said above, causes the seat to be positioned away from the user's center of rotation during the cabin's (71 ) rotation about the z-axis (z) and pitch axis (p), resulting in a G-force acting on the user. In detail, during maneuvers in a real airplane, the airplane moves on a circular axis of rotation. The distance from the center of rotation defined at the center of this circular axis causes G-force to act on the pilot as he moves like the swing of a pendulum. The invention relates to a cabin movement mechanism (70) in which the distance from the seat (72) to the axis of rotation ensures that G-force is generated on the user.

[0063] In the cabin movement mechanism (70), the frame body (80) is connected to the rotating body (90) on both sides. While rotational movement is provided by the sixth motor (91 ) on one side of the frame body (80), the movement of the frame body (80) is restricted on the other side by a brake mechanism (93) related to the second shaft (92).

[0064] The vibration that would occur in the cabin (71 ) during direction changes in the cabin's (71 ) pitch axis (p) movement is eliminated by the mentioned brake mechanism (93). In detail, the rotational movement from the sixth motor (91 ) is transferred to the second shaft (92) using the gearbox (911 ). Due to the gaps that must exist between the gears inside the gearboxes (911) for them to function, when the sixth motor (91 ) stops moving, the cabin (71 ) moves in the opposite direction of rotation by an amount equal to the gap. In other words, due to the sixth motor (91 ) stopping, the cabin (71 ) shakes for a while within a range of motion equal to the amount of gap in the gearbox (911). Especially in the cabin movement mechanism (70), since the seat (72) is far from the axis of rotation, the amount of oscillation and vibration increases because the center of gravity of the cabin, together with the user's weight, is also far from the axis of rotation. In the situation said above, a moment is generated depending on the weight of the cabin (71) and the distance between its center of gravity and the pitch axis (p). The brake mechanism (93) in the cabin movement mechanism (70) brakes to prevent the second shaft (92) partially from rotating. In other words, the brake mechanism (93) clamps the second shaft (92) at least enough to overcome the generated momentum. The rotational movement of the sixth motor (91) overcomes the braking force, allowing the second shaft (92) to rotate, while the braking force holds the second shaft (92) stationary when the motor drive is cut off. This prevents vibrations that may occur when the motor movement stops.

[0065] In a possible configuration of the invention, the brake mechanism (93) continuously clamps the second shaft (92). In this case, the motor force first overcomes the friction provided by the brake mechanism (93), and rotation then occurs.

[0066] In another possible configuration of the invention, the braking mechanism (93) is only activated when necessary. In this case, while a stop signal is sent to the sixth motor (91 ) by a control unit (not shown in the figure), an activation signal is sent to the braking mechanism (93) at the same time or shortly before. This ensures that the brake mechanism (93) is engaged as soon as the motor stops moving.

[0067] Thanks to the aforementioned structures, the cabin movement mechanism (70) provides the user with a sensation close to real experience by generating G-force. On the other hand, the structure that generates the G-force also ensures that increased oscillations are prevented by the braking mechanism (93). As a result, the invention's cabin movement mechanism (70) enables the user to experience the actual G-forces generated while also preventing vibrations and oscillations that do not occur in reality.

[0068] The invention relates to an advanced simulation mechanism (1 ) that enables the forward-backward and left-right movement of the seat where the user will sit, based on the movements occurring along the x-axis (x) and y-axis (y). The forward and backward motion allows the user to feel the acceleration and deceleration movements, i.e., the sensation of acceleration. Thanks to left and right movements, the user can feel the simulated vehicle sliding laterally on the road.

[0069] The invention relates to an advanced simulation mechanism (1 ) wherein the seat is rotated about the z-axis (z) by means of a rotating layer (30), thereby providing the user the sensation of the simulated vehicle taking a turn. When the advanced simulation mechanism (1 ) is used as a flight simulator, the aircraft's rotational movements are simulated in this way.

[0070] Thanks to the ability to perform the mentioned movements simultaneously, it is possible to convey to the user situations such as the vehicle accelerating, decelerating, or spinning while the vehicle is turning.

[0071] With these movements, the three corners of the upper plane (68) can be moved independently of each other in the three-axis movement mechanism (60), allowing the user to experience the sensation they would feel in an off-road vehicle when the vehicle goes into pits or climbs over bumps. Additionally, the movements of a marine vessel in response to waves can be easily simulated using the motions provided by the three-axis mechanism (60). On the other hand, it is possible to simulate the moment of turbulence for an aircraft.

[0072] As a result, the invention enables the simulation of all types of air, sea, and land vehicles through the advanced simulation mechanism and the layers and mechanisms provided on top of them. Superior mobility is achieved thanks to the ability of different layers and mechanisms to move simultaneously. The protection scope of the present invention is set forth in the annexed claims and cannot be restricted to the illustrative disclosures given above, under the detailed description. It is because a person skilled in the relevant art can obviously produce similar embodiments in the light of the foregoing disclosures, without departing from the main principles of the present invention.

[0073] REFERENCE NUMBERS

[0074] 1 Advanced simulation mechanism

[0075] 10 Base

[0076] 20 Fixed carrier

[0077] 21 Circular plate

[0078] 22 Rotating mechanism

[0079] 23 First motor

[0080] 30 Rotating layer

[0081] 31 X-axis movement mechanism

[0082] 32 Second motor

[0083] 33 X-axis threaded shaft

[0084] 34 X-axis nut

[0085] 35 X-axis linear rail

[0086] 40 X-axis movement layer

[0087] 41 Y-axis movement layer

[0088] 42 Third motor

[0089] 43 Y-axis threaded shaft

[0090] 44 Y-axis nut

[0091] 45 Y axis linear rail

[0092] 50 Y-axis movement layer

[0093] 60 Three axis motion mechanism

[0094] 61 Lower plane

[0095] 62 Drive mechanism

[0096] 63 Fourth motor

[0097] 64 Transfer element

[0098] 65 Drive shaft

[0099] 66 Upper joint

[0100] 67 Lower joint

[0101] 68 Upper plane

[0102] 70 Cabin movement mechanism

[0103] 701 Carrier base

[0104] 71 Cabin

[0105] 72 Seat 73 Rear end

[0106] 80 Frame body

[0107] 81 Fifth motor

[0108] 82 First shaft 90 Rotating body

[0109] 91 Sixth motor

[0110] 911 Gearbox

[0111] 92 Second shaft

[0112] 93 Brake mechanism X X-axis

[0113] Y Y-axis

[0114] Z Z-axis a Rotation axis t Drive axis p Pitch axis r Roll axis

Claims

CLAIMS1. An advanced simulation mechanism (1 ) characterized in that: a base (10), a fixed carrier (20) provided on said base (10), a rotating layer (30) performing rotational movement on a z-axis (z) extending vertically on said fixed carrier (20), an X-axis movement layer (40) that can move linearly on the said rotating layer (30) on an x-axis (x), a Y-axis movement layer (41) that can move linearly on the said x-axis movement layer (40) on a y-axis (y), a Y-axis movement layer (50), a three-axis motion mechanism (60) having an upper plane (68) whose three corners can move independently of each other, and a cabin (71 ) in which at least one seat (72) is positioned, a frame body (80) connected in a rolling manner to a roll axis (r) extending in the front-to-back direction of the cabin (71), the frame body (80) connected a rotating body (90) so that the frame body (80) can rotate about a pitch axis (p) extending in the left-right direction of the cabin (71), the rotating body (90) having a carrier base (701 ) connected to the upper plane (68), thereby comprising a cabin movement mechanism (70).

2. An advanced simulation mechanism (1 ) according to claim 1 , wherein the seat (72) is positioned between a rear end (22) of the cabin (71 ) and at least one of the pitch axis (p) and the z-axis (z).

3. An advanced simulation mechanism (1 ) according to claim 1 , wherein it includes at least one brake mechanism (93) to at least partially restrict the movement of the cabin (71 ) about the pitch axis (p).

4. An advanced simulation mechanism (1 ) according to claim 1 , wherein it includes at least one fifth motor (81 ) provided on the frame body (80) to enable the movement of the cabin (71 ) on the roll axis (r).

5. An advanced simulation mechanism (1 ) according to claim 1 , wherein it includes at least one first shaft (82) extending along the roll axis (r) to connect the cabin (71 ) and the frame body (80).

6. An advanced simulation mechanism (1 ) according to claim 1 , wherein it includes a sixth motor (91 ) provided on the rotating body (90) to enable the movement of the cabin (71 ) and the frame body (80) on the pitch axis (p).

7. An advanced simulation mechanism (1 ) according to claim 1 , wherein it includes at least one second shaft (92) extending along the pitch axis (p) to connect the frame body (80) and the rotating body (90).

8. An advanced simulation mechanism (1 ) according to claim 7, wherein it includes a gearbox (911 ) to transmit the motion received from the sixth motor (91 ) to the second shaft (92).

9. An advanced simulation mechanism (1 ) according to claim 7, wherein the brake mechanism (93) is related to the second shaft (92).

10. An advanced simulation mechanism (1 ) according to claim 1 , wherein a three-axis motion mechanism (60); a lower plane (61) fixed to the Y-axis motion layer (50), a drive mechanism provided on the said lower plane (61 ) that transmits the motion received from a fourth motor (63) to a transmission element (64), and a drive shaft (65) extending from the upper plane (68) to the lower plane (61) and connected at one end to the transmission element (64).

11. An advanced simulation mechanism (1 ) according to claim 10, wherein the fourth motor (63), drive shaft (65), and transmission element (64) are provided at each of the three corners of the three-axis motion mechanism (60).

12. An advanced simulation mechanism (1 ) according to claim 10, wherein it includes an upper joint (66) to provide the drive shaft (65) with rotational freedom relative to the upper plane (68).

13. An advanced simulation mechanism (1 ) according to claim 10, wherein it includes a lower joint (67) to enable the drive shaft (65) to be connected to the transmission element (64) with rotational freedom on a drive axis (t).

14. An advanced simulation mechanism (1 ) according to claim 10, wherein the transmission element (64) is connected to the drive mechanism (62) via a rotation axis (a) parallel to the drive axis (t).

15. An advanced simulation mechanism (1 ) according to claim 1 , wherein it includes a rotation mechanism (22) provided between the base (10) and the fixed carrier (20) to enable the rotating layer (30) on the fixed carrier (20) to perform a rotational movement about the z-axis (z).

16. An advanced simulation mechanism (1 ) according to claim 15, wherein it includes a circular plate (21) connected to the rotating layer (30) by being provided on the fixed carrier (20) and related to the rotation mechanism (22).

17. An advanced simulation mechanism (1 ) according to claim 16 or 17, wherein it includes a first motor (23) related to a rotation mechanism (22).

18. An advanced simulation mechanism (1 ) according to claim 1 , wherein it includes an X-axis movement mechanism (31 ) provided within the rotating layer (30) to ensure the linear displacement of the X-axis movement layer (31 ) provided on the rotating layer (30).

19. An advanced simulation mechanism (1 ) according to claim 18, wherein it includes an X-axis threaded shaft (33) related to a second motor (32) of the X-axis movement mechanism (31 ) and an X-axis threaded shaft (33) related to the X-axis movement layer (40).

20. An advanced simulation mechanism (1 ) according to claim 18 or claim 19, wherein the X-axis movement mechanism (31 ) includes at least one X-axis linear rail (35).

21. An advanced simulation mechanism (1 ) according to claim 1 , wherein it includes a Y-axis movement mechanism (41 ) provided within the X-axis movement layer (40) to enable the linear displacement of the Y-axis movement layer (50) positioned on the X-axis movement layer (40).

22. An advanced simulation mechanism (1 ) according to claim 21 , wherein it includes a Y-axis threaded shaft (43) related to a third motor (42) and a Y- axis nut (44) connected to the Y-axis layer (50).

23. An advanced simulation mechanism (1 ) according to claim 22 or 23, wherein the Y-axis movement mechanism (41 ) includes at least one Y-axis linear rail (45).

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