An actuator carriage system

Abstract

The invention relates to a body (F); a shell (K) being the outer surface of the body (F); at least one rotary part (2) located on the body (F) in a manner to be movable relative to the body (F); at least one actuator (3) ensuring the movement of the rotary part (2) with the changing of its length; at least one transmission shaft (4) transferring the movement of the actuator (3), extending lengthwise in a manner that there is a distance between the direction in which the actuator (3) extends and the direction in which the rotary part (2) extends, to which the actuator (3) is supported at one end and the rotary part (2) is supported at the other end; at least one bracket (5) connecting the transmission shaft (4) and the actuator (3) to the body (F); a bearing housing (6) located as an opening on the bracket (5), ensuring the bearing of the transmission shaft (4) to the bracket (5) in a rotatable manner; and a bearing element (601) bearing the transmission shaft (4), located in a manner to contact the inner walls inside the bearing housing (6).

Description

[0001] DESCRIPTION

[0002] AN ACTUATOR CARRIAGE SYSTEM

[0003] The invention relates to systems enabling the carrying of control surface actuators located on aircraft.

[0004] Control surface actuators located on aircraft are generally connected to the structures inside the wing or the body by means of additional mechanisms. In order for there to be no load loss in the connections of the actuators, they are required to be connected perpendicularly to the axis to which the actuator is connected. Actuators can transfer various loads to which the control surface is subjected during the flight of the aircraft to their structure. This situation can cause the actuators to be subjected to fatigue or to fail due to various loads. A need is felt for the bearing of the actuators and control surface shafts without using additional heavy mechanisms, in a relatively simple, light manner, and by making a distribution over a wide surface without transferring load to the structural parts.

[0005] In Japanese patent document No. US20050201821A1, which is part of the prior art, a rudder surface drive mechanism having a rotation support structure containing a reaction link consisting of fiber-reinforced plastic, a first connecting shaft consisting of metal, and a first liner is described. In the system subject to the invention, the outer peripheral part of the first liner is fixed by being connected to a peripheral surface of the first open hole of the reaction link. At least a part of the inner peripheral part of the first liner contains resin and supports the first connecting shaft in a rotatable manner.

[0006] Thanks to an actuator carriage system developed with this invention, the carrying and bearing of the actuators enabling the movement of the control surfaces located on aircraft on the aircraft shell in an effective manner are ensured.

[0007] Another object of this invention is to ensure the carrying of the loads to which the actuator and control surfaces are subjected with a lightweight system.

[0008] Another object of this invention is to ensure the effective bearing of actuator and control surface forces by being distributed over as wide an area as possible.

[0009] The actuator carriage system defined in the first claim and in the claims dependent on this claim, implemented to achieve the object of the invention, comprises; a shell forming the outer wall of a body, at least one rotary part performing rotational movement relative to the body on the body, an actuator performing the rotational movement of the rotary part by moving linearly thanks to the lengthening and shortening of its length, at least one transmission shaft transferring the linear movement performed by the actuator to the rotary part by rotating arounditself, to which the rotary part is connected in a movable manner from one end of the actuator at one end on the axis on which it extends in a manner that a certain distance remains between the own axis of the actuator and the own axis of the rotary part, at least one bracket enabling the placement of the transmission shaft and the actuator onto the body, a bearing housing located on the bracket in a manner to be a space, ensuring the bearing of the transmission shaft to the bracket in a manner to be able to perform rotational movement, a bearing element positioned inside the bearing housing in a manner to be located on its inner walls, ensuring the bearing of the transmission shaft.

[0010] The actuator carriage system subject to the invention comprises; a bracket located on the shell, ensuring the mounting of the rotary part onto the shell in a manner to allow it to perform rotational movement around its own axis, a bearing housing and a bearing element enabling the transmission shaft to be carried on the shell thanks to the bracket, a first joint ensuring the connection of the actuator to the bracket in a movable manner and its bearing onto the shell, and having a distance between itself and the bearing element in a manner to be suitable for the movement of the actuator in order to allow the actuator to move linearly, a bracket transferring the push and pull loads and weight emerging as a result of the actuator moving the transmission shaft onto the shell thanks to the first joint and the bearing element, thereby providing a lighter system by making a load distribution over a wide area.

[0011] In one embodiment of the invention, the actuator carriage system comprises a rotating surface post ensuring the connection between the rotating surface and the transmission shaft, transferring the movement coming from the transmission shaft to the rotating surface; the transmission shaft being the connection between the rotating surface post and the bearing housing; the transmission shaft being the connection between the rotating surface post and the actuator; a second joint located on the transmission shaft, connecting the actuator to the transmission shaft in a manner to ensure it performs rotational movement; and at least one flange extending outwardly from the transmission shaft, between which one end of the actuator in its longitudinal direction is positioned by being held, connecting the transmission shaft and the actuator to each other, and in which the second joint is located.

[0012] In one embodiment of the invention, the actuator carriage system comprises a rotating surface post mounted to the shell thanks to being positioned on the bracket in a manner that there is an inclination at an angle predetermined by the manufacturer between the direction extending on the shell and the direction in which it extends, thereby extending in the same direction as the inclination of the rotating surface; and an actuator extending in a manner to form an almost perpendicular angle with the own axis of the rotating surface post, extending outwardly fromthe bracket, and having an inclination at an angle predetermined by the manufacturer between the axis on which it extends and the shell.

[0013] In one embodiment of the invention, the actuator carriage system comprises a flat region consisting of two identical walls and being a part of the bracket extending almost parallel to the direction extending on the shell, being form-compatible with the outer wall of the shell; and a bearing inclined region connected to the flat region, being the region where the bearing housing and the bearing element are located on the bracket, placed onto the shell in a manner such that the rotating surface post and the transmission shaft on the bracket form an inclination at an angle predetermined by the manufacturer with the flat region, and extending in a manner to form an almost perpendicular angle to the own axis of the rotating surface post with the axis on which the flat region extends.

[0014] In one embodiment of the invention, the actuator carriage system comprises; at least one actuator inclined region connected to the flat region, having an inclined form in a manner to extend on an axis parallel to the actuator bearing inclined region which is the region where one end of the second joint is connected on the bracket, extending lengthwise in a direction at an almost perpendicular angle to the shell of the rotating surface post, and being inclined at an angle predetermined by the manufacturer with the axis on which the flat region extends, a structural element connected on the body in a manner to carry the shell, the flat region, the bearing inclined region, and the actuator inclined region enabling the carrying and bearing of the rotary part by being positioned onto the shell by means of the structural part.

[0015] In one embodiment of the invention, the actuator carriage system comprises at least one joint housing ensuring the positioning of the actuator onto the bracket with the placement of the first joint into the inner part of the actuator inclined regions located almost mutually opposite to each other on the bracket; and an actuator supported on the bracket by being positioned between the sequential actuator inclined regions in a manner to be one on top of the other. In one embodiment of the invention, the actuator carriage system comprises a flat region placed in a manner to be able to move between the bearing inclined region and the actuator inclined region, extending on an axis almost parallel to the axis passing through the axis on which the shell extends, containing a space on it allowing the movement of the actuator. In one embodiment of the invention, the actuator carriage system comprises plurality of bearing region walls located on the bracket between the bearing inclined region and the flat region, rising upwards from the flat region in the form of a strut, forming both walls of the bearing inclined region, and located in a manner to form an almost perpendicular angle with the inclination of the surface of the bearing inclined region.In one embodiment of the invention, the actuator carriage system comprises plurality of actuator region walls located on the bracket between the actuator inclined region and the flat region, rising upwards from the flat region in the form of a strut, forming both walls of the actuator inclined region, and located in a manner to form an almost perpendicular angle with the inclination of the surface of the actuator inclined region.

[0016] In one embodiment of the invention, the actuator carriage system comprises a bearing housing located inside the bracket in a manner to form an inclination at an angle determined by the manufacturer with the axis on which the shell extends, thereby ensuring the mounting of the rotating surface post to the bracket in a manner to be inclined to be positioned at the mentioned angle with the angle between the axis of the rotating surface post and the axis on which the shell extends.

[0017] In one embodiment of the invention, the actuator carriage system comprises a bearing element, which is preferably a rolling bearing, thereby serving the duty of bearing the rotary part.

[0018] In one embodiment of the invention, the actuator carriage system comprises an actuator triggering the transmission shaft by performing a linear movement thanks to the lengthening and shortening of its length, and rotating the rotating surface post around itself.

[0019] In one embodiment of the invention, the actuator carriage system comprises a body forming the aircraft; a rotary part serving as a control surface, which is preferably an aircraft rudder; and a bearing element bearing the rotating surface post and preventing the transmission of forces such as vibration acting on the rotary part during the flight of the body to the actuator. The actuator carriage system implemented to achieve the object of this invention is shown in the attached figures, and these figures;

[0020] Figure 1 - The top view of the actuator carriage system.

[0021] Figure 2 - The perspective view of the actuator carriage system.

[0022] Figure 3 - The schematic view of the actuator carriage system.

[0023] Figure 4 - The top view of the bracket.

[0024] Figure 5 - The perspective view of the bracket.

[0025] Figure 6 - The schematic view of an alternative of the actuator carriage system.

[0026] The parts located in the figures are individually numbered, and the counterparts of these numbers are given below.1. Actuator carriage system

[0027] 2. Rotary part

[0028] 3. Actuator

[0029] 4. Transmission shaft

[0030] 401. Second joint

[0031] 410. Flange

[0032] 5. Bracket

[0033] 501. First joint

[0034] 502. Joint housing

[0035] 510. Flat region

[0036] 520. Bearing inclined region

[0037] 521. Bearing region wall

[0038] 530. Actuator inclined region

[0039] 531. Actuator region wall

[0040] 6. Bearing housing

[0041] 601. Bearing element

[0042] (F) Body

[0043] (K) Shell

[0044] (R) Rotary surface post

[0045] (Y) Structural part

[0046] The actuator carriage system (1) comprises; a body (F), a shell (K) being the outer surface of the body (F), at least one rotary part (2) located on the body (F) in a manner to be movable relative to the body (F), at least one actuator (3) ensuring the movement of the rotary part (2) with the changing of its length, at least one transmission shaft (4) transferring the movement of the actuator (3), extending lengthwise in a manner that there is a distance between the direction in which the actuator (3) extends and the direction in which the rotary part (2) extends, to which the actuator (3) is supported at one end and the rotary part (2) is supported at theother end, at least one bracket (5) connecting the transmission shaft (4) and the actuator (3) to the body (F), a bearing housing (6) located as an opening on the bracket (5), ensuring the bearing of the transmission shaft (4) to the bracket (5) in a rotatable manner, a bearing element (601) bearing the transmission shaft (4), located in a manner to contact the inner walls inside the bearing housing (6).

[0047] The actuator carriage system (1) subject to the invention comprises; a bracket (5) positioned on the shell (K), ensuring the connection of the rotary part (2) onto the shell (K) in a manner to be able to perform rotational movement around the direction in which it extends lengthwise, a bearing housing (6) and a bearing element (601) ensuring the bearing of the transmission shaft (4) on the shell (K) by means of the bracket (5), a first joint (501) ensuring the connection of the actuator (3) to the bracket (5) in a rotatable manner and the bearing of the actuator (3) on the shell (K), a first joint (501) having a distance between itself and the bearing element (601) in order for the actuator (3) to be located in a manner to be movable with length change, a bracket (5) transferring the bearing load formed with the moving of the transmission shaft (4) by the actuator (3) to the shell (K) via the first joint (501) and the bearing element (601), thereby providing lightness by making load distribution over a wide area.

[0048] A shell (K) is located on the outer surface of the body (F). At least one rotary part (2) located on the body (F) performs rotational movement around its own axis relative to the body (F). An actuator (3) provides the movement of the rotary part (2). The actuator (3) transfers this movement to the rotary part (2) thanks to a transmission shaft (4) to which the actuator (3) and the rotary part (2) are connected, by moving linearly thanks to the lengthening and shortening of its length on the axis on which it extends. One end is connected to the actuator (3) and the other end is connected to the rotary part (2). The transmission shaft (4) connects the actuator (3) and the rotary part (2) in a manner that there is a distance between the axes on which they extend. This distance is as much as the length that the transmission shaft (4) extends parallel to the shell (K). The actuator (3) rotates the transmission shaft (4) around the point where it is supported by moving linearly on the axis on which it extends. The mentioned rotational movement is transferred to the rotary part (2). The transmission shaft (4) and the actuator (3) are connected to the body (F) by means of a bracket (5). A bearing housing (6) in the form of an opening, ensuring the supporting of the transmission shaft (4) to the bracket (5) in a rotatable manner, is located on the bracket (5). The transmission shaft (4) is positioned inside the bearing housing (6) by being borne by means of a bearing element (601). In this way, the transmission shaft (4) ensures movement transfer easily on the bracket (5). (Figure-3) The bracket (5) is located on the shell (K). The bracket (5) connects the rotary part (2) onto the shell (K) in a manner to be able to rotate around its own axis. The transmission shaft (4) isconnected onto the shell (K) by means of the bracket (5) on the bearing element (601) and the bearing housing (6). The actuator (3) is connected to the bracket (5) in a manner to be able to move thanks to a first joint (501). A distance in an amount to enable the actuator (3) to perform linear movement is located between the bearing element (601) and the first joint (501). In this way, the movement of the actuator (3), bearing loads, forces subjected to with environmental factors, and weight forces are carried and borne over a wide area on the shell (K) thanks to the connection of the actuator (3) to the bracket (5) from both its ends. (Figure-2)

[0049] In one embodiment of the invention, the actuator carriage system (1) comprises; a rotary surface post (R) ensuring the connection of the rotary part (2) with the transmission shaft (4) and ensuring the movement of the rotary part (2) by transferring the movement of the transmission shaft (4) to the rotary part (2), the transmission shaft (4) ensuring the connection of the rotary surface post (R) to the bearing housing (6), the transmission shaft (4) connected to the rotary surface post (R) and connecting the rotary surface post (R) with the actuator (3), a second joint (401) located on the transmission shaft (4), ensuring the connection of the actuator (3) to the transmission shaft (4) in a rotatable manner, and at least one flange (410) located at the part where the transmission shaft (4) connects with the actuator (3), extending outwardly from the transmission shaft (4) mutually in a manner that one end of the actuator (3) in the direction in which it extends lengthwise is located between them, and in which the second joint (401) is located. The rotary surface post (R) connects the rotary part (2) and the transmission shaft (4) to each other and serves the duty of transferring the movement of the transmission shaft (4) to the rotary part (2). The rotary surface post (R) is connected to the bracket (5) and the actuator (3) by being connected to the bearing housing (6) thanks to the transmission shaft (4). The second joint (401) connects the actuator (3) to the transmission shaft (4) in a manner to be able to rotate. The second joint (401) is located on at least one flange (410) extending outwardly from the transmission shaft (4), and the connection of one end of the actuator (3) with the second joint (401 ) is ensured by being held between the flanges (410). In this way, the actuator (3) is connected to the transmission shaft (4) in a manner to be able to rotate comfortably over the second joint (401), which is the point where it is supported. (Figure-1)

[0050] In one embodiment of the invention, the actuator carriage system (1) comprises a rotary surface post (R) fixed to the shell (K) by means of the bracket (5) in a manner to extend inclined at an angle predetermined by the manufacturer relative to the direction in which the shell (K) extends, thereby extending parallel to the inclination of the rotary part (2) in the direction in which it extends lengthwise; and an actuator (3) extending lengthwise on the bracket (5), extending in a manner to be perpendicular to the direction in which the rotary surface post (R) extends lengthwise, and having an angle predetermined by the manufacturer between thedirection in which it extends lengthwise and the shell (K). The rotary surface post (R) is placed onto the bracket (5) in a manner to be suitable for the inclination of the rotary part (2) in a manner to ensure the positioning of the rotary part (2) onto the shell (K) in an inclined manner. In this way, the mounting of the rotary part (2) in an inclined direction relative to the direction of the shell (K) is ensured. The actuator (3) is connected to the bracket (5) in a manner such that an inclination determined by the manufacturer takes place between the direction in which the shell (K) extends and itself, in a manner to form a perpendicular angle between the direction in which it extends and the direction in which the rotary surface post (R) extends. In this way, it is enabled that the actuator (3) is close to the rotary part (2) at the most optimal level and moves the rotary part (2) in the most effective manner.

[0051] In one embodiment of the invention, the actuator carriage system (1) comprises; a flat region (510) forming the bracket (5), extending parallel to the direction in which the shell (K) extends in a manner to be form-compatible with the shell (K), a bearing inclined region (520) connected to the flat region (510), being the part of the bracket (5) where the bearing housing (6) and the bearing element (601) are located, being in an inclined form in a manner to ensure the positioning of the rotary surface post (R) and the transmission shaft (4) on the bracket (5) onto the shell (K) at an inclination predetermined by the manufacturer relative to the flat region (510), and extending in a manner to be perpendicular to the direction in which the rotary surface post (R) extends lengthwise with the direction in which the flat region (510) extends lengthwise. The flat region (510) forming the bracket (5) is in a direction parallel to the shell (K) and is form-compatible with the shell (K). The bearing housing (6) and the bearing element (601) are located in the bearing inclined region (520) on the bracket (5). The bearing inclined region (520) is at the part where the rotary surface post (R) and the transmission shaft (4) are connected on the bracket (5), and extends at an inclination predetermined by the manufacturer relative to the flat region (510) and in a direction perpendicular to the rotary surface post (R). In this way, the bearing of the rotary surface post (R) on the bearing inclined region (520) in a manner suitable for the inclination of the rotary part (2) is ensured. (Figure-4)

[0052] In one embodiment of the invention, the actuator carriage system (1) comprises; at least one actuator inclined region (530) connected to the flat region (510), having an inclined form in a manner to extend in a direction parallel to the actuator (3) and the bearing inclined region (520), being the part of the bracket (5) on which the second joint (401) is located and where one end of the actuator (3) in the direction in which it extends lengthwise is connected, ensuring the positioning in a manner to extend lengthwise in a direction perpendicular to the direction in which the rotary surface post (R) extends lengthwise on the shell (K) and at an inclination predetermined by the manufacturer relative to the direction in which the flat region (510) extends, at least one structural element (Y) carrying the shell (K), to which the shell (K) isconnected on the body (F), the flat region (510), the bearing inclined region (520), and the actuator inclined region (530) enabling the carrying and bearing of the rotary part (2) on the shell (K) with the support of the structural part (Y). The second joint (502) is located in the actuator inclined region (530) on the bracket (5). The actuator inclined region (530) is at the part where the actuator (3) is connected on the bracket (5) and extends at an inclination predetermined by the manufacturer relative to the flat region (510) and in a direction perpendicular to the rotary surface post (R). In this way, the positioning of the actuator (3) in an inclined manner relative to the shell (K) is ensured in a manner to ensure that it extends in a direction perpendicular to the direction in which the rotary part (2) extends. The shell (K) is carried on the body (F) by means of structural parts (Y). The rotary part (2) is carried on the structural part (Y) by means of the flat region (510), the bearing inclined region (520), and the actuator inclined region (530) and the shell (K). In this way, the carrying of the rotary part (2) over a wide area with a lighter mechanism is ensured.

[0053] In one embodiment of the invention, the actuator carriage system (1) comprises at least one joint housing (502) located on the actuator inclined regions (530) located on the bracket (5) in a manner to remain mutually opposite to each other, in which the actuator (3) is positioned onto the bracket (5) with the positioning of the first joint (501) inside it; and an actuator (3) positioned on the bracket (5) by being placed between the actuator inclined regions (530) positioned one on top of the other. At the point found in the part where the bracket (5) is connected with the actuator (3), the actuator inclined regions (530) are located one on top of the other in a manner to be parallel to each other and in a manner to have a distance between them. At least one joint housing (502) is located at the part where the actuator (3) is connected with the actuator inclined regions (530). In this way, the bearing of the actuator (3) to the bracket (5) in a manner to be able to move and the carrying of the loads to which the actuator (3) is subjected in an effective manner are ensured.

[0054] In one embodiment of the invention, the actuator carriage system (1) comprises a flat region (510) extending lengthwise in a direction parallel to the direction in which the shell (K) extends between the bearing inclined region (520) and the actuator inclined region (530), containing an opening part in which the actuator (3) is positioned lengthwise in a manner to be able to move. Thanks to the opening located on the flat region (510), with the connection of the actuator (3) to the bracket (5) from both its ends, the effective bearing of the actuator (3), its connection to the bracket (5) in a manner to be able to move, and the effective carrying of the loads to which the actuator (3) is subjected are ensured.

[0055] In one embodiment of the invention, the actuator carriage system (1) comprises plurality of bearing region walls (521) located on the bracket (5) in a manner to be between the bearinginclined region (520) and the flat region (510), extending outwardly in a manner to be on both outer walls of the bearing inclined region (520) in a manner to form a strut from the flat region (510), and located in a manner to be perpendicular to the surface inclination of the bearing inclined region (520). The bearing region wall (521), which is in the form of a strut, is located on both outer walls of the bearing inclined region (520) between the bearing inclined region (520) and the flat region (510). In this way, the bracket (5) is enabled to carry relatively high forces structurally, and load transfer is enabled. (Figure-5)

[0056] In one embodiment of the invention, the actuator carriage system (1) comprises plurality of actuator region walls (531) located on the bracket (5) in a manner to be between the actuator inclined region (530) and the flat region (510), extending outwardly in a manner to be on both outer walls of the actuator inclined region (530) in a manner to form a strut from the flat region (510), and located in a manner to be almost perpendicular to the surface inclination of the actuator inclined region (530). The actuator region wall (531), which is in the form of a strut, is located on both outer walls of the actuator inclined region (530) between the actuator inclined region (530) and the flat region (510). In this way, the bracket (5) is enabled to carry relatively high forces structurally, and load transfer is enabled. (Figure-5)

[0057] In one embodiment of the invention, the actuator carriage system (1) comprises a bearing housing (6) positioned inside the bracket (5) in a manner that there is an inclination at an angle predetermined by the manufacturer between it and the direction in which the shell (K) extends lengthwise, thereby ensuring the positioning of the rotary surface post (R) to the bracket (5) in an inclined manner suitable for the angle between the direction in which the rotary surface post (R) extends lengthwise and the direction in which the shell (K) extends. The bearing housing (6) is positioned on the bracket (5) in a manner to be inclined at an angle predetermined by the manufacturer relative to the direction in which the bracket (5) extends on the shell (K). In this way, the bearing of the rotary surface post (R) to the bracket (5) in an inclined manner is ensured. (Figure-6)

[0058] In one embodiment of the invention, the actuator carriage system (1) comprises a bearing element (601) which is a rolling bearing, thereby ensuring the bearing of the rotary part (2). In this way, the effective bearing of the rotary part (2) and its connection to the bracket (5) in a manner to be able to move are ensured.

[0059] In one embodiment of the invention, the actuator carriage system (1) comprises an actuator (3) rotating the transmission shaft (4) around the direction in which the rotary surface post (R) extends lengthwise by lengthening and shortening its length.

[0060] In one embodiment of the invention, the actuator carriage system (1) comprises a body (F) which is an aircraft; a rotary part (2) which is a control surface; and a bearing element (601)bearing the rotary surface post (R) and preventing the transmission of loads acting on the rotary part (2) during the flight of the body (F) to the actuator (3). In this way, the effective bearing of the rotary part (2), which is preferably a tail rudder, to the shell (K) located on the body (F) of the aircraft is ensured.

Claims

CLAIMS1- An actuator carriage system (1) comprising a body (F); a shell (K) being the outer surface of the body (F); at least one rotary part (2) located on the body (F) in a manner to be movable relative to the body (F); at least one actuator (3) ensuring the movement of the rotary part (2) with the changing of its length; at least one transmission shaft (4) transferring the movement of the actuator (3), extending lengthwise in a manner that there is a distance between the direction in which the actuator (3) extends and the direction in which the rotary part (2) extends, to which the actuator (3) is supported at one end and the rotary part (2) is supported at the other end; at least one bracket (5) connecting the transmission shaft (4) and the actuator (3) to the body (F); a bearing housing (6) located as an opening on the bracket (5), ensuring the bearing of the transmission shaft (4) to the bracket (5) in a rotatable manner; and a bearing element (601) bearing the transmission shaft (4), located in a manner to contact the inner walls inside the bearing housing (6), characterized in that it comprises; the bracket (5) positioned on the shell (K), ensuring the connection of the rotary part (2) onto the shell (K) in a manner to be able to perform rotational movement around the direction in which it extends lengthwise, the bearing housing (6) and the bearing element (601) ensuring the bearing of the transmission shaft (4) on the shell (K) by means of the bracket (5), a first joint (501) ensuring the connection of the actuator (3) to the bracket (5) in a rotatable manner and the bearing of the actuator (3) on the shell (K), the first joint (501) having a distance between itself and the bearing element (601) in order for the actuator (3) to be located in a manner to be movable with length change, the bracket (5) transferring the bearing load formed with the moving of the transmission shaft (4) by the actuator (3) to the shell (K) via the first joint (501) and the bearing element (601), thereby providing lightness by making load distribution over a wide area.2- The actuator carriage system (1) according to claim 1, characterized in that it comprises; a rotary surface post (R) ensuring the connection of the rotary part (2) with the transmission shaft (4) and ensuring its movement by transferring the movement of the transmission shaft (4) to the rotary part (2), the transmission shaft (4) ensuring the connection of the rotating surface post (R) to the bearing housing (6), the transmission shaft (4) connected to the rotary surface post (R) and connecting the rotary surface post (R) with the actuator (3), a second joint (401) located on the transmission shaft (4), ensuring the connection of the actuator (3) to the transmission shaft (4) in a rotatable manner, at least one flange (410) located at the part where the transmission shaft (4) is connected with the actuator (3), extending outwardly from the transmissionshaft (4) mutually in a manner that one end of the actuator (3) in the direction in which it extends lengthwise is located between them, and in which the second joint (401) is located.3- The actuator carriage system (1) according to claim 1 or claim 2, characterized in that it comprises; a rotary surface post (R) fixed to the shell (K) by means of the bracket (5) in a manner to extend inclined at an angle predetermined by the manufacturer relative to the direction in which the shell (K) extends, thereby extending parallel to the inclination of the rotary part (2) in the direction in which it extends lengthwise, an actuator (3) extending lengthwise on the bracket (5), extending in a manner to be perpendicular to the direction in which the rotary surface post (R) extends lengthwise, and having an angle predetermined by the manufacturer between the direction in which it extends lengthwise and the shell (K).4- The actuator carriage system (1) according to claim 2 or claim 3, characterized in that it comprises; a flat region (510) forming the bracket (5), extending parallel to the direction in which the shell (K) extends in a manner to be form-compatible with the shell (K), a bearing inclined region (520) connected to the flat region (510), being the part of the bracket (5) where the bearing housing (6) and the bearing element (601) are located, being in an inclined form in a manner to ensure the positioning of the rotary surface post (R) and the transmission shaft (4) on the bracket (5) onto the shell (K) at an inclination predetermined by the manufacturer relative to the flat region (510), and extending in a manner to be perpendicular to the direction in which the rotary surface post (R) extends lengthwise with the direction in which the flat region (510) extends lengthwise.5- The actuator carriage system (1) according to claim 4, characterized in that it comprises; at least one actuator inclined region (530) connected to the flat region (510), having an inclined form in a manner to extend in a direction parallel to the actuator (3) and the bearing inclined region (520), being the part of the bracket (5) on which the second joint (401) is located and where one end of the actuator (3) in the direction in which it extends lengthwise is connected, ensuring the positioning in a manner to extend lengthwise in a direction perpendicular to the direction in which the rotary surface post (R) extends lengthwise on the shell (K) and at an inclination predetermined by the manufacturer relative to the direction in which the flat region (510) extends, at least one structural element (Y) carrying the shell (K), to which the shell (K) is connected on the body (F), the flat region (510), the bearing inclined region (520), andthe actuator inclined region (530) enabling the carrying and bearing of the rotary part (2) on the shell (K) with the support of the structural part (Y).6- The actuator carriage system (1) according to claim 5, characterized in that it comprises at least one joint housing (502) located on the actuator inclined regions (530) located on the bracket (5) in a manner to remain mutually opposite to each other, in which the actuator (3) is positioned onto the bracket (5) with the positioning of the first joint (501) inside it; and an actuator (3) positioned on the bracket (5) by being placed between the actuator inclined regions (530) positioned one on top of the other.7- The actuator carriage system (1) according to claim 5 or claim 6, characterized in that it comprises a flat region (510) extending lengthwise in a direction parallel to the direction in which the shell (K) extends between the bearing inclined region (520) and the actuator inclined region (530), containing an opening part in which the actuator (3) is positioned lengthwise in a manner to be able to move.8- The actuator carriage system (1) according to any one of claims 4 to 7, characterized in that it comprises plurality of bearing region walls (521) located on the bracket (5) in a manner to be between the bearing inclined region (520) and the flat region (510), extending outwardly in a manner to be on both outer walls of the bearing inclined region (520) in a manner to form a strut from the flat region (510), and located in a manner to be perpendicular to the surface inclination of the bearing inclined region (520).9- The actuator carriage system (1) according to any one of claims 5 to 8, characterized in that it comprises plurality of actuator region walls (531) located on the bracket (5) in a manner to be between the actuator inclined region (530) and the flat region (510), extending outwardly in a manner to be on both outer walls of the actuator inclined region (530) in a manner to form a strut from the flat region (510), and located in a manner to be almost perpendicular to the surface inclination of the actuator inclined region (530).10- The actuator carriage system (1) according to any one of claims 2 to 9, characterized in that it comprises a bearing housing (6) positioned inside the bracket (5) in a manner that there is an inclination at an angle predetermined by the manufacturer between it and the direction in which the shell (K) extends lengthwise, thereby ensuring the positioning of the rotary surface post (R) to the bracket (5) in an inclined manner suitable for the angle between the direction in which the rotary surface post (R) extends lengthwise and the direction in which the shell (K) extends.11-The actuator carriage system (1) according to any one of the preceding claims, characterized in that it comprises a bearing element (601) which is a rolling bearing, thereby ensuring the bearing of the rotary part (2).12- The actuator carriage system (1) according to any one of the preceding claims, characterized in that it comprises an actuator (3) rotating the transmission shaft (4) around the direction in which the rotary surface post (R) extends lengthwise by lengthening and shortening its length.13- The actuator carriage system (1) according to any one of the preceding claims, characterized in that it comprises a body (F) which is an aircraft; a rotary part (2) which is a control surface; and a bearing element (601) bearing the rotary surface post (R) and preventing the transmission of loads acting on the rotary part (2) during the flight of the body (F) to the actuator (3).

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