An aviation tire torque device

Abstract

The present application provides an aviation tire torque device, comprising: a support structure; a torque mechanism, which is arranged on the support structure and is used to tighten the positioning bolts on the upper end surface of the hub of the target tire below it; at least one bearing mechanism, each of the bearing mechanisms includes a mounting platform and a connecting part, one end of the connecting part is connected to the support structure, the mounting platform is rotatably arranged on the other end of the connecting part and is located below the torque mechanism, the mounting platform is used for the target tire to be sleeved thereon when rotating to a vertical state, and to provide support for the target tire when rotating to a horizontal state so that the positioning bolts of the hub of the target tire face upward.

Description

Technical Field

[0001] The present application relates to the field of aviation technology, and in particular to an aviation tire torque device. Background Art

[0002] At present, when installing aircraft tires (such as aircraft tires), a torque device is generally used to connect the two hubs of the aircraft tire. However, the existing tire installation requires workers to manually carry the tire and connect it to the torque device, and then manually operate the torque device to install the tire. However, aircraft wheels and tires are generally large and heavy, and the method of manually carrying the tire and connecting it to the torque device has the problem of low installation efficiency. Summary of the invention

[0003] The purpose of the embodiments of the present application is to provide an aircraft tire torque device to solve the problem of low installation efficiency in the existing method of manually transporting heavy and bulky aircraft tires and docking them with torque devices.

[0004] In a first aspect, an embodiment of the present invention provides an aviation tire torque device, comprising: a support structure; a torque mechanism, which is arranged on the support structure and is used to tighten the positioning bolts on the upper end surface of the hub of the target tire below it; at least one bearing mechanism, each of the bearing mechanisms includes a mounting platform and a connecting portion, one end of the connecting portion is connected to the support structure, the mounting platform is rotatably arranged on the other end of the connecting portion and is located below the torque mechanism, the mounting platform is used for allowing the target tire to be sleeved thereon when rotating to a vertical state, and providing support for the target tire when rotating to a horizontal state so that the positioning bolts of the hub of the target tire face upward.

[0005] In the aviation tire torque device designed as above, the mounting platform in the bearing mechanism can be switched between a vertical state and a horizontal state, so that when the target tire is connected to the torque device, there is no need to move it manually and labor-intensively. Instead, the target tire only needs to be rolled to the mounting platform and stopped, and the mounting platform and the target tire can be directly connected. After the connection, the mounting platform drives the tire to rotate to a horizontal state, and then the positioning bolts of the two wheel hubs of the target tire below it are tightened through the torque mechanism to achieve the installation of the target tire. The aviation tire torque device designed in this application solves the problem of low installation efficiency in the existing method of manually moving heavy and bulky aviation tires and connecting them with torque devices, improves the convenience and efficiency of aviation tire installation, and thus improves the production efficiency of aviation tires.

[0006] In an optional implementation of this embodiment, the at least one supporting mechanism includes multiple supporting mechanisms; the torque mechanism is rotatably connected to the support structure to achieve selective alignment with one of the multiple supporting mechanisms and tighten the positioning bolts of the target tire on the aligned supporting mechanism.

[0007] In the implementation of the above-mentioned design, multiple bearing mechanisms are designed so that while the torque mechanism is tightening the target tire on one of the bearing mechanisms, the remaining target tires to be installed can be assembled through other bearing mechanisms, thereby improving the installation efficiency of multiple target tires to be installed.

[0008] In an optional implementation manner of this embodiment, a motor is disposed in the support structure, and the torque mechanism is connected to an output end of the motor so that the motor drives the torque mechanism to rotate.

[0009] In an optional implementation manner of this embodiment, the connecting portion can be slidably arranged on the support structure along the vertical direction, and a locking mechanism is provided on the support structure to fix the connecting portion at multiple different heights.

[0010] In the implementation of the above-mentioned design, since the other end of the connecting portion is connected to the mounting platform, when the connecting portion slides in the vertical direction on the bracket mechanism and is then maintained at different heights of the bracket structure by the locking mechanism, the mounting platform can also be maintained at different heights. The mounting platform can be maintained at different heights so that the mounting platform can be suitable for tires of different sizes and heights when it is socketed with the target tire to be installed, thereby improving the applicability of the aircraft tire torque device so as to install aircraft tires of different sizes.

[0011] In an optional implementation manner of this embodiment, the connecting portion is a telescopic connecting rod, so that the horizontal distance between the mounting platform and the support structure is adjustable.

[0012] In the implementation of the above design, the horizontal distance between the mounting platform and the bracket mechanism is adjustable, so that the mounting platform can adapt to tires of different sizes when driving the target tire to be mounted to rotate to a horizontal state.

[0013] In an optional implementation of the present embodiment, the mounting platform includes a bearing portion and a placing portion, the placing portion is arranged above the bearing portion for socketing and supporting the target tire, one end of the connecting portion is connected to the bracket structure, and the bearing portion is rotatably arranged at the other end of the connecting portion, the bearing portion is used for allowing the target tire to be socketed thereon when the placing portion is driven to rotate to a vertical state, and for providing support for the target tire when the placing portion is driven to rotate to a horizontal state so that the positioning bolts of the wheel hub of the target tire face upward.

[0014] In an optional implementation of the present embodiment, the placement portion includes a support platform and a plurality of bolt support rods, wherein the support platform is arranged above the load-bearing portion and is detachably connected to the load-bearing portion, and the plurality of bolt support rods are distributed on the support platform at preset circumferential intervals, and the plurality of bolt support rods are used to support and fix the bolts placed thereon so that the fixed bolts pass through the bolt holes of two wheel hubs to be connected of the target tire and tighten the nut corresponding to each bolt through the torque mechanism to achieve the connection between the two wheel hubs to be connected.

[0015] In an optional implementation of the present embodiment, the torque mechanism includes: a bolt torque structure, which is used to tighten the bolt; a rotating telescopic rod, the bottom of which is provided with the bolt torque structure, which is used to drive the bolt torque structure to rise, fall and rotate; a connecting rod, one end of which is rotatably connected to the support structure, and the other end of the connecting rod is connected to the top of the rotating telescopic rod to drive the rotating telescopic rod to move horizontally.

[0016] In an optional implementation of the present embodiment, the bolt torque structure includes a machine matching box and two bolt torquers, the top of the machine matching box is connected to the bottom of the rotating telescopic rod, and the two bolt torquers are arranged at the bottom of the machine matching box, and the machine matching box is used to provide power to the two bolt torquers so that the two bolt torquers rotate to tighten the bolts to be tightened.

[0017] In an optional implementation of this embodiment, the relative distance between the two bolt torquers is adjustable.

[0018] In the above-designed implementation, the relative distance between the two bolt torquers is adjustable, so that the two bolt torquers can adapt to a variety of target tires with different relative distances, thereby improving the adaptability of the designed aviation tire torque device. BRIEF DESCRIPTION OF THE DRAWINGS

[0019] In order to more clearly illustrate the technical solutions of the embodiments of the present application, the drawings required for use in the embodiments of the present application will be briefly introduced below. It should be understood that the following drawings only show certain embodiments of the present application and therefore should not be regarded as limiting the scope. For ordinary technicians in this field, other related drawings can be obtained based on these drawings without paying creative work.

[0020] Figure 1 A first structural diagram of an aviation tire torque device provided in an embodiment of the present application;

[0021] Figure 2 A second structural diagram of an aviation tire torque device provided in an embodiment of the present application;

[0022] Figure 3The third structural diagram of the aviation tire torque device provided in the embodiment of the present application;

[0023] Figure 4 A fourth structural diagram of an aviation tire torque device provided in an embodiment of the present application;

[0024] Figure 5 This is the fifth structural diagram of the aviation tire torque device provided in an embodiment of the present application.

[0025] Icons: 10-bracket structure; 101-locking mechanism; 20-torque mechanism; 201-bolt torque structure; 2011-machine box; 20111-display; 2012-bolt torque device; 20121-bolt torque rod; 20122-torque sensor; 202-rotating telescopic rod; 203-connecting rod; 30-bearing mechanism; 301-mounting table; 3011-bearing part; 3012-placing part; 30121-support platform; 30122-bolt support rod; 302-connecting part. DETAILED DESCRIPTION

[0026] The technical solutions in the embodiments of the present application will be described below in conjunction with the drawings in the embodiments of the present application.

[0027] An embodiment of the present application provides an aircraft tire torque device, which is used to install aircraft tires, wherein the aircraft tire includes an aircraft tire structure generally including two hubs and a tire, the two hubs clamp the tire in the middle and connect the two hubs by bolts to complete the installation of the aircraft tire, and the aircraft tire torque device of the present application is mainly used to connect the two hubs of the aircraft tire.

[0028] like Figure 1 As shown, the aircraft tire torque device includes a support structure 10, a torque mechanism 20 and at least one bearing mechanism 30, the torque mechanism 20 is arranged on the support structure 10, the bearing mechanism 30 includes a mounting platform 301 and a connecting portion 302, one end of the connecting portion 302 is also connected to the support structure 10, the mounting platform 301 is rotatably arranged at the other end of the connecting portion 302 and the mounting platform 301 is located below the torque mechanism 20, the mounting platform 301 can be rotated at the end of the connecting portion 302 to switch between a vertical state and a horizontal state, when the mounting platform 301 rotates to the vertical state, that is, the axis of the mounting platform 301 is horizontal (such as Figure 1 The mounting platform 301 is used for the target tire to be mounted thereon. When the mounting platform 301 is rotated to a horizontal state, that is, the axial direction of the mounting platform 301 is vertical (such as Figure 2The mounting platform 301 is used to provide support so that the positioning bolts of the hub of the target tire face upward; the torque mechanism 20 is used to tighten the positioning bolts on the upper end surface of the target tire located on the lower supporting mechanism 30.

[0029] When the aviation tire torque device of the above design is in use, the mounting platform 301 in the supporting mechanism 30 can first be rotated to a vertical state. When the mounting platform 301 is rotated to a vertical state, the staff rolls the target tire to be installed to the mounting platform 301. At this time, the target tire can be in a state where two wheel hubs clamp the tire in the middle but the two wheel hubs are connected by bolts; after the target tire rolls to the mounting platform 301 and stops, the staff can directly connect the target tire with the mounting platform 301 without moving the target tire. After the connection is completed, the mounting platform 301 can start to rotate to a horizontal state and drive the connection to be completed. The target tires are rotated simultaneously. When the mounting platform 301 rotates to a horizontal state, the two wheel hubs of the target tire mounted thereon are stacked up and down. The mounting platform 301 provides support for the target tire. At the same time, bolts can be set in advance on the mounting platform 301 corresponding to the bolt holes of the wheel hubs. The bolts set after the mounting platform 301 is mounted on the target tire pass through the bolt holes of the two stacked wheel hubs and then face upward after rotating to a horizontal state. At this time, the staff can put the nuts corresponding to the bolts on the corresponding bolts, and tighten the bolts in sequence through the torque mechanism 20 located above, thereby completing the fixation and connection of the two stacked wheel hubs and realizing the installation of the aviation tire.

[0030] In the aviation tire torque device designed as above, the mounting platform in the bearing mechanism can be switched between a vertical state and a horizontal state, so that when the target tire is connected with the torque device, there is no need to move it manually and labor-intensively. Instead, the target tire only needs to be rolled to the mounting platform and stopped, and the mounting platform and the target tire can be directly connected. After the connection, the mounting platform drives the tire to rotate to a horizontal state, and then the positioning bolts of the two wheel hubs of the target tire below it are tightened through the torque mechanism to achieve the installation of the target tire. The aviation tire torque device designed in this application solves the problem of low installation efficiency in the existing method of manually moving heavy and bulky aviation tires and connecting them with torque devices, improves the convenience and efficiency of aviation tire installation, and thus improves the production efficiency of aviation tires.

[0031] In an optional implementation of this embodiment, the number of the supporting mechanism 30 can be multiple, such as Figure 3As shown, the supporting mechanism 30 may specifically be two, on this basis, the torque mechanism 20 is rotatably connected to the support structure 10, after the torque mechanism 20 is rotatably connected to the support structure 10, the torque mechanism 20 may be selectively aligned with any one of the multiple supporting mechanisms 30, and then the positioning bolts of the target tire on the aligned supporting mechanism 30 may be tightened.

[0032] The aviation tire torque device designed as above is designed with multiple bearing mechanisms so that while the torque mechanism 20 is tightening the target tire on one of the bearing mechanisms 30, the remaining target tires to be installed can be assembled through other bearing mechanisms 30, thereby improving the installation efficiency of multiple target tires to be installed.

[0033] In an optional implementation of the present embodiment, the torque mechanism 20 described in the above implementation can be rotated on the support structure 10 in a specific manner that a motor (not shown in the figure) is provided in the support structure, the torque mechanism 20 is connected to the output end of the motor, and the motor drives the torque mechanism 20 to rotate when powered. In addition, in addition to the motor provided in the support structure 10, an electric cylinder can also be provided to enable the torque mechanism 20 to rotate on the support structure 10. It should be noted here that when the positions of multiple supporting mechanisms 30 are fixed, when the motor or electric cylinder drives the torque mechanism 20 to rotate, the motor or electric cylinder can be designed to drive the torque mechanism 20 to rotate at a certain angle in one rotation, so that in one rotation, one supporting mechanism 30 can be directly rotated to align with another supporting mechanism 30 without the need for staff to observe and then control the motor or electric cylinder to stop.

[0034] In an optional implementation manner of this embodiment, it has been described above that one end of the connecting portion 302 is connected to the support structure 10. On this basis, Figure 4 As shown, the connection portion 302 can be designed to be slidably disposed on the support structure 10 along the vertical direction. The support structure 10 is provided with a plurality of locking mechanisms 101 , which can fix the sliding connection portion 302 at a plurality of different heights of the support structure 10 .

[0035] In the above-mentioned design, since the other end of the connecting portion 302 is connected to the mounting platform 301, when the connecting portion 302 slides in the vertical direction on the support structure 10 and is then maintained at different heights of the support structure 10 by the locking mechanism 101, the mounting platform 301 can also be maintained at different heights. The mounting platform 301 can be maintained at different heights so that the mounting platform 301 can be suitable for tires of different sizes and heights when it is connected to the target tire to be installed, thereby improving the applicability of the aircraft tire torque device so as to install aircraft tires of different sizes.

[0036] In an optional implementation of this embodiment, the connection part 302 can also be a telescopic connection rod, so that the connection part 302 drives the mounting platform 301 away from or close to the support structure when it is extended and retracted, so that the horizontal distance between the mounting platform 301 and the support structure 10 is adjustable. When the horizontal distance between the mounting platform 301 and the support structure 10 is adjustable, the mounting platform 301 drives the target tire to be installed to rotate to a horizontal state, which can adapt to tires of different sizes.

[0037] In an optional implementation of this embodiment, if Figure 3 As shown, the mounting platform 301 includes a bearing portion 3011 and a placing portion 3012. The placing portion 3012 is arranged above the bearing portion 3011 and connected to the bearing portion 3011 for socketing and supporting the target tire to be installed. One end of the connecting portion 302 is connected to the bracket structure 10, and the bearing portion 3011 is rotatably arranged at the other end of the connecting portion 302. The bearing portion 3011 is used for allowing the target tire to be socketed on the placing portion 3012 when the placing portion 3012 is driven to rotate to a vertical state, and for providing support for the target tire when the placing portion 3012 is driven to rotate to a horizontal state so that the positioning bolts of the wheel hub of the target tire face upward.

[0038] Specifically, Figure 5 As shown, the placement portion 3012 includes a support platform 30121 and a plurality of bolt support rods 30122, wherein the support platform 30121 is disposed above the bearing portion 3011 and is detachably connected to the bearing portion 3011, and the plurality of bolt support rods 30122 are distributed on the support platform 30121 at preset circumferential intervals, wherein the distribution of the plurality of bolt support rods 30122 can be designed in a distribution shape according to the positions of the bolt holes of the wheel hub of the target tire that is frequently installed; the plurality of bolt support rods 30122 are used to support and fix the bolts placed thereon.

[0039] When using the aviation tire torque device designed as above, the staff can first rotate the bearing part 3011 and the corresponding placement part 3012 into a vertical state, and then place the bolts on each bolt support rod 30122 to fix them, and then connect the target tire to be installed with the placement part 3012. Since the distribution shape of the multiple bolt support rods 30122 corresponds to the distribution of the bolt holes of the two identical wheel hubs of the target tire to be installed, each bolt support rod 30122 and the bolt thereon will pass through the bolt holes of the two wheel hubs of the target tire when connected. On this basis, the bearing part 3011 can be rotated to The placement portion 3012 is driven to rotate to a horizontal state. At this time, the support platform 30121 and the bearing portion 3011 provide support for the target tire. During the rotation process, since the bolt support rod 30122 and the bolts thereon pass through the corresponding bolt holes, the bolt support rod 30122 plays a certain fixing role during the rotation process to prevent the tire from sliding. After rotating to a horizontal state, the staff can place a corresponding nut on each bolt passing through the bolt hole, and then tighten the nut and the bolt through the torque mechanism located above the placement portion 3012 to achieve fixation between the two wheel hubs of the target tire to complete the installation of the target tire.

[0040] In an optional implementation of this embodiment, if Figure 1 As shown, the torque mechanism 20 includes a bolt torque structure 201, a rotating telescopic rod 202 and a connecting rod 203. One end of the connecting rod 203 is rotatably connected to the support structure 10, and the other end of the connecting rod 203 is connected to the top of the rotating telescopic rod 202. The bottom of the rotating telescopic rod 202 is provided with the bolt torque structure 201. Since the connecting rod 203 is rotatably connected to the support structure 10, the connecting rod 203 can swing in the horizontal direction, so that the rotating telescopic rod 202 and the bolt torque structure 201 can correspond to different bearing mechanisms 30. The rotating telescopic rod 202 can drive the bolt torque structure 201 to rise, fall and rotate 360 ​​degrees, so that the bolt torque structure 201 can approach / move away from the bearing mechanism 30 and can rotate to tighten the remaining bolts after tightening the nuts of some bolts on the basis of the above.

[0041] Specifically, Figure 3As shown, the bolt torque structure 201 includes a machine box 2011 and two bolt torquers 2012. The top of the machine box 2011 is connected to the bottom of the rotating telescopic rod 202. The two bolt torquers 2012 are arranged at the bottom of the machine box 2011. The machine box 2011 is used to provide torque power for the two bolt torquers 2012. The two bolt torquers 2012 are used to tighten the nuts of the two opposite bolts by rotating. Specifically, a servo motor can be arranged in the machine box 2011, and the servo motor supplies power to the two bolt torquers 2012. In addition, based on the two bolt torquers 2012 being arranged at the bottom of the machine box 2011, the relative distance between the two bolt torquers 2012 is adjustable, so that the two bolt torquers 2012 can adapt to a variety of target tires with different relative distances, thereby improving the adaptability of the designed aviation tire torque device.

[0042] In an optional implementation of this embodiment, each bolt torquer 2012 may also include a bolt torque rod 20121 and a torque sensor 20122 disposed in the bolt torque rod 20121. The bolt torque rod 20121 is used to tighten the bolts, and the torque sensor 20122 is used to detect the tightening state of the bolts. By setting the torque sensor 20122, it is possible to detect whether the bolts currently tightened by the bolt torque rod 20121 meet the standards and whether there is a fault. In addition, a display 20111 may also be provided on the machine distribution box 2011. The display 20111 may display a status diagram of the hub bolt hole. For example, when the bolt of a bolt hole is tightened, the bolt hole corresponding to the status diagram is displayed in green. When the bolt of a bolt hole is not tightened or is faulty, the bolt hole corresponding to the status diagram is displayed in red.

[0043] In an optional implementation manner of the present embodiment, the aircraft tire torque device may be configured with an external control device and a controller (both marked in the figure), the controller may control the cylinder of the rotating telescopic rod 202 to drive the rotating telescopic rod 202 to lift and rotate, and the order of lifting and rotating, the lifting amplitude, the angle and the number of rotations may be preset in the controller, so that the rotating telescopic rod 202 can be lifted, lowered, rotated and the like in a preset order, the controller may also control the bolt torque rod 20121 to rotate and receive the signal transmitted by the torque sensor 20122 in the bolt torque rod 20121, and the controller is also connected to the display 20111 to send a corresponding display signal to the display 20111 so that the display 20111 displays the corresponding image and color.

[0044] On the basis of the above design, when the staff has sleeved the target tire with the carrying mechanism 30 and placed the nut on the bolt to complete the preparation work, the staff can press the external control device to send a signal to the controller. When the controller receives the signal sent by the external control device, it controls the cylinder of the rotating telescopic rod 202 to drive the rotating telescopic rod 202 to descend. A limiting device is arranged in the cylinder so that the rotating telescopic rod 202 can descend a fixed distance. When the cylinder drives the rotating telescopic rod 202 to descend a preset distance, the controller controls the two bolt torque rods to rotate and the cylinder also drives the rotating telescopic rod 202 to descend. In this way, the two bolt torque rods 20121 can gradually rotate the nuts on the top of the bolts at the corresponding positions and descend to tighten them with the bottom of the bolts. In this process of gradually descending and tightening the bolts, the torque sensor 20122 continues to work to detect the tightening state of the bolts in real time. When the bolt fails during the tightening process or the tightening degree of the bolt does not reach the preset value after the tightening is completed, the torque The sensor 20122 sends a fault signal to the controller, which causes the controller to control the rotating telescopic rod 202 to rise immediately and control the bolt torque rod 20121 to stop rotating, and the controller transmits a signal to the display 20111 so that the corresponding position of the bolt hole on the display 20111 appears red; when the torque sensor 20122 detects that the tightening state of the bolt is normal or meets the preset value, the torque sensor 20122 sends a normal signal to the controller, and the controller controls the corresponding position of the bolt hole on the display 20111 to appear green according to the normal signal and continues to execute the tightening procedure. After the current bolt is tightened, the rotating telescopic rod 202 is controlled to rise and rotate by a preset angle, and then descend to a certain height so that the two bolt torque rods 20121 tighten the two corresponding bolts after rotation, and the above process is repeated until the rotating telescopic rod 202 rotates a preset number of times, and the controller controls the rotating telescopic rod 202 to stop rising and controls the two bolt torque rods 20121 to stop rotating.

[0045] In the embodiments provided in the present application, it should be understood that the disclosed devices and methods can be implemented in other ways. The device embodiments described above are only schematic. For example, the division of the units is only a logical function division. There may be other division methods in actual implementation. For example, multiple units or components can be combined or integrated into another system, or some features can be ignored or not executed.

[0046] In addition, the units described as separate components may or may not be physically separated, and the components shown as units may or may not be physical units, that is, they may be located in one place or distributed on multiple network units. Some or all of the units may be selected according to actual needs to achieve the purpose of the solution of this embodiment.

[0047] Furthermore, the functional modules in the various embodiments of the present application may be integrated together to form an independent part, or each module may exist separately, or two or more modules may be integrated to form an independent part.

[0048] In this document, relational terms such as first and second, etc. are used merely to distinguish one entity or operation from another entity or operation, but do not necessarily require or imply any such actual relationship or order between these entities or operations.

[0049] The above description is only an embodiment of the present application and is not intended to limit the protection scope of 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. An aviation tire torque device, characterized in that: include: A support structure; a torque mechanism, which is disposed on the support structure and is used to tighten the positioning bolts on the upper end surface of the wheel hub of the target tire below the support structure; At least one bearing mechanism, each of the bearing mechanisms comprises a mounting platform and a connecting portion, one end of the connecting portion is connected to the support structure, the mounting platform is rotatably arranged on the other end of the connecting portion and is located below the torque mechanism, the mounting platform is used for allowing the target tire to be sleeved thereon when rotating to a vertical state, and for providing support to the target tire when rotating to a horizontal state so that the positioning bolts of the wheel hub of the target tire face upwards; The connecting portion can be slidably arranged on the support structure along the vertical direction, and a locking mechanism is arranged on the support structure to fix the connecting portion at multiple different heights; The connecting portion is a telescopic connecting rod, so that the horizontal distance between the mounting platform and the support structure can be adjusted; The mounting platform comprises a bearing portion and a placing portion, wherein the placing portion is arranged above the bearing portion for sleeve-fitting and supporting the target tire, one end of the connecting portion is connected to the bracket structure, and the bearing portion is rotatably arranged at the other end of the connecting portion, and the bearing portion is used for sleeve-fitting the target tire on the placing portion when the placing portion is driven to rotate to a vertical state, and for providing support for the target tire when the placing portion is driven to rotate to a horizontal state so that the positioning bolts of the wheel hub of the target tire face upwards; The placement portion includes a support platform and a plurality of bolt support rods, wherein the support platform is arranged above the bearing portion and is detachably connected to the bearing portion, and the plurality of bolt support rods are distributed on the support platform at preset circumferential intervals, and the plurality of bolt support rods are used to support and fix the bolts placed thereon so that the fixed bolts pass through the bolt holes of the two wheel hubs to be connected of the target tire and tighten the nuts corresponding to each bolt through the torque mechanism to achieve connection of the two wheel hubs to be connected; The torque mechanism comprises: A bolt torque structure, which is used to tighten the bolt; A rotating telescopic rod, the bottom of which is provided with the bolt torque structure, for driving the bolt torque structure to rise, fall and rotate; a connecting rod, one end of which is rotatably connected to the support structure, and the other end of which is connected to the top of the rotating telescopic rod to drive the rotating telescopic rod to move horizontally; The bolt torque structure includes a machine matching box and two bolt torquers, the top of the machine matching box is connected to the bottom of the rotating telescopic rod, the two bolt torquers are arranged at the bottom of the machine matching box, and the machine matching box is used to provide power for the two bolt torquers so that the two bolt torquers rotate to tighten the bolts to be tightened; The aviation tire torque device also includes a controller, and the controller is used to control the cylinder of the rotating telescopic rod to drive the rotating telescopic rod to lift and rotate.

2. The aircraft tire torque device according to claim 1, characterized in that: The at least one carrying mechanism comprises a plurality of carrying mechanisms; The torque mechanism is rotatably connected to the support structure to selectively align with one of the plurality of carrier mechanisms and tighten the positioning bolts of the target tire on the aligned carrier mechanism.

3. The aircraft tire torque device according to claim 2, characterized in that: A motor is arranged in the support structure, and the torque mechanism is connected to an output end of the motor so that the motor drives the torque mechanism to rotate.

4. The aircraft tire torque device according to claim 1, characterized in that: The relative distance between the two bolt torquers is adjustable.

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