CN212267163U - Aircraft tire torque device - Google Patents
Aircraft tire torque device Download PDFInfo
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- CN212267163U CN212267163U CN202021600613.6U CN202021600613U CN212267163U CN 212267163 U CN212267163 U CN 212267163U CN 202021600613 U CN202021600613 U CN 202021600613U CN 212267163 U CN212267163 U CN 212267163U
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Abstract
The application provides an aircraft tire torque device, includes: a support structure; a torque mechanism provided on the support structure for tightening a positioning bolt of an upper end face of a hub of a target tire therebelow; the mounting platform is used for enabling a target tire to be sleeved on the mounting platform when the mounting platform rotates to a vertical state, and provides support for the target tire when the mounting platform rotates to a horizontal state so that a positioning bolt of a hub of the target tire faces upwards.
Description
Technical Field
The application relates to the technical field of aviation, in particular to an aircraft tire torque device.
Background
Currently, a pneumatic tire (such as an airplane tire) generally adopts a torque device to connect two hubs of the pneumatic tire when the tire is installed, but the existing tire installation needs workers to manually carry and butt the tire with the torque device and then manually operate the torque device to install the tire, and the airplane hub and the tire are generally large and heavy, and the mode of manually carrying and butt-jointing the tire with the torque device has the problem of low installation efficiency.
SUMMERY OF THE UTILITY MODEL
An object of the embodiment of this application is to provide an aircraft tire torque device for solve the current problem that the installation effectiveness is low that will not only heavy but also huge aircraft tire transport and with the mode of torque device butt joint through the manual work.
In a first aspect, an embodiment of the present invention provides an aircraft tire torque device, including: a support structure; a torque mechanism provided on the support structure for tightening a positioning bolt of an upper end face of a hub of a target tire therebelow; the mounting platform is used for enabling a target tire to be sleeved on the mounting platform when the mounting platform rotates to a vertical state, and provides support for the target tire when the mounting platform rotates to a horizontal state so that a positioning bolt of a hub of the target tire faces upwards.
In the aviation tire torque device designed by the above design, the mounting table in the bearing mechanism can be switched between the vertical state and the horizontal state, so that the target mounting tire can be directly sleeved with the target mounting tire without labor force consumption when being sleeved with the torque device, the target tire only needs to be rolled to the mounting table in a rolling mode and stopped, the mounting table and the target mounting tire can be sleeved, the mounting table drives the tire to rotate to the horizontal state after being sleeved, and the positioning bolts of two hubs of the target mounting tire below the mounting table are screwed up through the torque mechanism to realize the mounting of the target tire. And further improve the production efficiency of the aircraft tire.
In an alternative embodiment of this embodiment, the at least one carrier comprises a plurality of carriers; the torque mechanism is rotatably coupled to the support structure for selective alignment with one of the plurality of carriers and tightening of a retention bolt of a target tire on the aligned carrier.
In the embodiment designed above, by designing the plurality of bearing mechanisms, in the process that the torque mechanism screws the target tire on one of the bearing mechanisms, the rest of the target tires to be mounted can be assembled through the other bearing mechanisms, and further, the mounting efficiency of the plurality of target tires to be mounted can be improved.
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.
In an alternative embodiment of this embodiment, the connecting portion is slidably disposed on the supporting structure along a vertical direction, and the supporting structure is provided with a locking mechanism to fix the connecting portion at a plurality of different heights.
In the embodiment of the design, as the other end of the connecting part is connected with the mounting table, when the connecting part slides on the support mechanism along the vertical direction and is further maintained at different heights of the support structure through the locking mechanism, the mounting table can also be maintained at different heights, and the mounting table can be maintained at different heights, so that the mounting table can be suitable for tires with different sizes and heights when being sleeved with a target tire to be mounted, and further the applicability of the aircraft tire torque device is improved so as to mount aircraft tires with different sizes.
In an optional implementation manner of this embodiment, the connecting portion is a telescopic connecting rod, so that a horizontal distance between the mounting table and the support structure is adjustable.
In the embodiment of the design, the horizontal distance between the mounting table and the bracket mechanism is adjustable, so that the mounting table can adapt to tires with different sizes when driving the target tire to be mounted to rotate to a horizontal state.
In an optional implementation manner of this embodiment, the mounting table includes a bearing portion and a placing portion, the placing portion is disposed above the bearing portion for sleeving and supporting a target tire, one end of the connecting portion is connected to the support structure, the bearing portion is rotatably disposed at the other end of the connecting portion, the bearing portion is configured to allow the target tire to be sleeved thereon when the placing portion is driven to rotate to a vertical state, and provide support for the target tire when the placing portion is driven to rotate to a horizontal state so that a positioning bolt of a hub of the target tire faces upward.
In an optional implementation manner of this embodiment, the placing portion includes a supporting platform and a plurality of bolt supporting rods, the supporting platform is disposed above the bearing portion and detachably connected to the bearing portion, the bolt supporting rods are distributed on the supporting platform at intervals according to a preset circumference, and the bolt supporting rods are configured to support and fix bolts placed thereon so that the fixed bolts pass through bolt holes of two hubs to be connected of a target tire and a nut corresponding to each bolt is tightened by the torque mechanism to connect the two hubs to be connected.
In an alternate embodiment of the present embodiment, the torque mechanism includes: a bolt torque structure for fastening a bolt; the bottom of the rotary telescopic rod is provided with the bolt torque structure and is used for driving the bolt torque structure to ascend, descend and rotate; and one end of the connecting rod is rotatably connected with the support structure, and the other end of the connecting rod is connected with the top of the rotating telescopic rod so as to drive the rotating telescopic rod to horizontally move.
In an optional implementation manner of this embodiment, the bolt torque structure includes a machine kit and two bolt torquers, the top of the machine kit is connected with the bottom of the rotary telescopic rod, the two bolt torquers are disposed at the bottom of the machine kit, and the machine kit is used for providing power for the two bolt torquers, so that the two bolt torquers rotate to tighten the bolt to be fastened.
In an alternative embodiment of this embodiment, the relative distance of the two bolt torquers is adjustable.
In the embodiment of the design, the relative distance between the two bolt torquers is adjustable, so that the two bolt torquers can adapt to various target tires with different relative distances, and the adaptability of the designed aircraft tire torque equipment is improved.
Drawings
In order to more clearly illustrate the technical solutions of the embodiments of the present application, the drawings that are required to be used in the embodiments of the present application will be briefly described below, it should be understood that the following drawings only illustrate some embodiments of the present application and therefore should not be considered as limiting the scope, and that those skilled in the art can also obtain other related drawings based on the drawings without inventive efforts.
FIG. 1 is a first block diagram of an aircraft tire torque apparatus according to an embodiment of the present application;
FIG. 2 is a second block diagram of an aircraft tire torque machine provided in accordance with an embodiment of the present application;
FIG. 3 is a third structural diagram of an aircraft tire torque device provided in accordance with an embodiment of the present application;
FIG. 4 is a fourth block diagram of an aircraft tire torque device provided in accordance with an embodiment of the present application;
FIG. 5 is a fifth block diagram of an aircraft tire torque device according to an embodiment of the present application.
Icon: 10-a scaffold structure; 101-a locking mechanism; 20-a torque mechanism; 201-bolt torque configuration; 2011-machine matching box; 20111-display; 2012-bolt torquer; 20121-bolt torque rod; 20122-a torque sensor; 202-rotating the telescoping rod; 203-connecting rod; 30-a carrying mechanism; 301-mounting table; 3011-a carrier portion; 3012-a placement section; 30121-a support platform; 30122-bolt support; 302-connecting part.
Detailed Description
The technical solutions in the embodiments of the present application will be described below with reference to the drawings in the embodiments of the present application.
The embodiment of the application provides an aircraft tire torque device, which is used for installing an aircraft tire, wherein the structure of the aircraft tire including the aircraft tire generally comprises two hubs and the tire, the two hubs clamp the tire in the middle and connect the two hubs through bolts to complete the installation of the aircraft tire, and the aircraft tire torque device is mainly used for connecting the two hubs of the aircraft tire.
As shown in fig. 1, the aircraft tire torque device comprises a support structure 10, a torque mechanism 20 and at least one bearing mechanism 30, wherein the torque mechanism 20 is arranged on the support structure 10, the bearing mechanism 30 comprises a mounting platform 301 and a connecting part 302, one end of the connecting part 302 is also connected with the support structure 10, the mounting platform 301 is rotatably arranged at the other end of the connecting part 302, the mounting platform 301 is positioned below the torque mechanism 20, the mounting platform 301 can rotate at the end part of the connecting part 302 to switch between a vertical state and a horizontal state, when the mounting platform 301 rotates to the vertical state, namely the axis of the mounting platform 301 is horizontal (the state shown in fig. 1), the mounting platform 301 is used for sleeving a target tire, when the mounting platform 301 rotates to the horizontal state, namely the axis of the mounting platform 301 is vertical (the state shown in fig. 2), the mounting table 301 is used for providing support to make the positioning bolts of the hub of the target tire face upwards; the torque mechanism 20 is used to tighten a positioning bolt on the upper end surface of a target tire on the lower support mechanism 30.
When the aircraft tire torque device designed above is in use, the mounting table 301 in the carrying mechanism 30 can be firstly rotated to a vertical state, and when the mounting table 301 is rotated to the vertical state, a worker rolls and carries a target tire to be mounted to the mounting table 301, and at this time, the target tire can present a state that two hubs clamp the tire in the middle but the two hubs are connected through bolts; after the target tire rolls to the mounting table 301 and stops, a worker can directly socket the target tire with the mounting table 301 without moving the target tire, after the socket joint is completed, the mounting table 301 can start to rotate to a horizontal state and drive the target tire to rotate at the same time, when the mounting table 301 rotates to the horizontal state, two hubs of the target tire sleeved on the mounting table 301 are stacked up and down, the mounting table 301 supports the target tire, bolts can be arranged on the mounting table 301 in advance corresponding to bolt holes of the hubs, the bolts arranged after the mounting table 301 is sleeved with the target tire penetrate through the bolt holes of the two stacked hubs, then the bolts face upwards after rotating to the horizontal state, at the moment, the worker can place nuts corresponding to the bolts on the corresponding bolts and sequentially tighten the bolts through the torque mechanisms 20 positioned above, and then accomplish the fixed of two stack wheel hubs and connect, realize the installation of aircraft tire.
In the aviation tire torque device designed by the application, the mounting table in the bearing mechanism can be switched between the vertical state and the horizontal state, so that the target mounting tire can be directly sleeved with the target mounting tire without labor force when being sleeved with the torque device, the mounting table drives the tire to rotate to the horizontal state after being sleeved, and the positioning bolts of two hubs of the target mounting tire below the mounting table are screwed up by the torque mechanism to realize the mounting of the target tire, the aviation tire torque device solves the problem of low mounting efficiency in the conventional mode of manually carrying the heavy aviation tire and butting with the torque device, and improves the convenience and the efficiency of aviation tire mounting, and further improve the production efficiency of the aircraft tire.
In an alternative embodiment of the present embodiment, the number of the bearing mechanism 30 may be multiple, and as shown in fig. 3, the number of the bearing mechanism 30 may be specifically two, on the basis of which the torque mechanism 20 is rotatably connected to the support structure 10, and 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 bearing mechanisms 30 of the multiple bearing mechanisms 30, so as to tighten the positioning bolt of the target tire on the aligned bearing mechanism 30.
According to the aviation tire torque device designed above, by designing the plurality of bearing mechanisms, in the process that the torque mechanism 20 screws the target tire on one of the bearing mechanisms 30, the rest target tires to be mounted can be assembled through the other bearing mechanisms 30, and therefore the mounting efficiency of the plurality of target tires to be mounted can be improved.
In an alternative embodiment of the present embodiment, the torque mechanism 20 described in the foregoing embodiment can be implemented by a motor (not shown) disposed in the supporting structure 10, the torque mechanism 20 is connected to an output end of the motor, and the motor drives the torque mechanism 20 to rotate when being powered on. In addition, an electric cylinder may be provided in addition to the motor within the support structure 10 to allow the torque mechanism 20 to rotate on the support structure 10. It should be noted that, in the case that the positions of the plurality of bearing mechanisms 30 are fixed, when the motor or the electric cylinder drives the torque mechanism 20 to rotate, the angle at which the motor or the electric cylinder drives the torque mechanism 20 to rotate in one rotation is certain, so that the motor or the electric cylinder can directly rotate from one bearing mechanism 30 to align with another bearing mechanism 30 in one rotation without being observed by a worker to control the motor or the electric cylinder to stop.
In the alternative embodiment of the present embodiment, it has been described above that one end of the connecting portion 302 is connected to the supporting structure 10, and on this basis, as shown in fig. 4, the connecting portion 302 can be designed to be slidably disposed on the supporting structure 10 along the vertical direction, the supporting structure 10 is provided with a plurality of locking mechanisms 101, and the plurality of locking mechanisms 101 can enable the sliding connecting portion 302 to be fixed at a plurality of different heights of the supporting structure 10.
In the above design, since the other end of the connecting portion 302 is connected to the mounting table 301, when the connecting portion 302 slides on the support structure 10 in the vertical direction and is further maintained at different heights of the support structure 10 through the locking mechanism 101, the mounting table 301 can also be maintained at different heights, and the mounting table 301 can be maintained at different heights so that the mounting table 301 can be applied to tires of different sizes and heights when being sleeved with a target tire to be mounted, thereby improving the applicability of the aircraft tire torque device to mount aircraft tires of different sizes.
In an alternative embodiment of this embodiment, the connecting portion 302 may also be a telescopic connecting rod, so that the connecting portion 302 drives the mounting platform 301 to move away from or close to the support structure when telescopic, so that the horizontal distance between the mounting platform 301 and the support structure 10 is adjustable. When the horizontal distance between the mounting table 301 and the support structure 10 is adjustable, the mounting table 301 can be adapted to tires with different sizes when the mounting table 301 drives the target tire to be mounted to rotate to the horizontal state.
In an alternative embodiment of this embodiment, as shown in fig. 3, the mounting platform 301 includes a bearing portion 3011 and a placing portion 3012, the placing portion 3012 is disposed above the bearing portion 3011 and connected to the bearing portion 3011 for receiving and supporting a target tire to be mounted, one end of the connecting portion 302 is connected to the support structure 10, the bearing portion 3011 is rotatably disposed at the other end of the connecting portion 302, the bearing portion 3011 is used for receiving the target tire on the placing portion 3012 when the placing portion 3012 is rotated to a vertical state, and when the placing portion 3012 is rotated to a horizontal state, the bearing portion 3011 provides support for the target tire so that a positioning bolt of a hub of the target tire faces upward.
Specifically, as shown in fig. 5, the placing portion 3012 includes a supporting platform 30121 and a plurality of bolt supports 30122, the supporting platform 30121 is disposed above the bearing portion 3011 and is detachably connected to the bearing portion 3011, the plurality of bolt supports 30122 are distributed on the supporting platform 30121 at a predetermined circumferential interval, wherein the distribution of the plurality of bolt supports 30122 can be designed to be distributed according to the positions of bolt holes of a hub of a target tire which is frequently installed; the plurality of bolt supports 30122 serve to support and fix bolts placed thereon.
In the aviation tire torque device designed above, when in use, a worker can first rotate the bearing part 3011 and the corresponding placing part 3012 to be in a vertical state, then place a bolt on each bolt support 30122 to be fixed, and then sleeve the target tire to be installed with the placing part 3012, because the distribution shape of the plurality of bolt supports 30122 corresponds to the distribution of bolt holes overlapped by two identical hubs of the target tire to be installed, each bolt support 30122 and the bolt thereon can pass through the bolt holes overlapped by two hubs of the target tire during sleeve connection, on the basis, the bearing part 3011 can rotate to drive the placing part 3012 to rotate to a horizontal state, the support platform 30121 and the bearing part 3011 provide support for the target tire, because the bolt support 30122 and the bolt thereon pass through the corresponding bolt holes during rotation, the bolt support 30122 plays a certain fixing role during rotation, to prevent the tire from slipping; after rotating to the horizontal state, a worker can place a corresponding nut on each bolt passing through the bolt hole, and then tighten the nuts and the bolts through a torque mechanism located above the placing portion 3012 to achieve fixing between two hubs of a target tire so as to achieve the effect of completing installation of the target tire.
In an alternative embodiment of this embodiment, as shown in fig. 1, the torque mechanism 20 comprises 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 supporting structure 10, the other end of the connecting rod 203 is connected to the top of the rotating telescopic rod 202, the bolt torque structure 201 is provided at the bottom of the rotating telescopic bar 202, and since the connecting rod 203 is rotatably connected to the supporting structure 10, so that 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 telescoping rod 202 can drive the bolt torque structure 201 to ascend, descend and rotate 360 degrees, so that the bolt torque structure 201 can be moved closer to/away from the carrier 30 and can be rotated to tighten the remaining bolts after tightening the nuts of some of the bolts on the basis of the above.
Specifically, as shown in fig. 3, the bolt torque structure 201 includes a machine kit 2011 and two bolt torquers 2012, a top of the machine kit 2011 is connected to a bottom of the rotating telescopic rod 202, the two bolt torquers 2012 are disposed at the bottom of the machine kit 2011, the machine kit 2011 is configured to provide torque power for the two bolt torquers 2012, and the two bolt torquers 2012 are configured to screw nuts of two opposite bolts by rotating. Specifically, a servo motor can be arranged in the machine matching box 2011 and supplies power to the two bolt torquers 2012; in addition, on the basis that the two bolt torquers 2012 are arranged at the bottom of the machine distribution box 2011, the relative distance between the two bolt torquers 2012 is adjustable, so that the two bolt torquers 2012 are suitable for various target tires with different relative distances, and the adaptability of the designed aviation tire torque equipment is improved.
In an alternative embodiment of the present embodiment, each bolt torquer 2012 may further include a bolt torque bar 20121 and a torque sensor 20122 disposed in the bolt torque bar 20121, the bolt torque bar 20121 is used for tightening a bolt, the torque sensor 20122 is used for detecting a fastening state of the bolt, and the torque sensor 20122 may be used for detecting whether the bolt torque bar 20121 currently tightened by the bolt reaches a standard and is out of order. In addition, a display 20111 may be provided on the kit 2011, and the display 20111 may display a state diagram of the hub bolt holes, for example, when the bolts in a certain bolt hole are completely tightened, the bolt hole corresponding to the state diagram is displayed in green, and when the bolt in a certain bolt hole is not tightened or fails, the bolt hole corresponding to the state diagram is displayed in red.
In an optional implementation manner of this embodiment, the aircraft tire torque apparatus may be configured with an external control device and a controller (both shown in the figures), the controller may control the cylinder of the rotating telescopic rod 202 to drive the rotating telescopic rod 202 to lift and rotate, and may preset a lifting and rotating sequence, a lifting amplitude, a rotating angle, and a number of times in the controller, so that the rotating telescopic rod 202 performs lifting, lowering, rotating, and the like according to the preset sequence, the controller may further control the bolt torque rod 20121 to rotate and receive a signal transmitted by the torque sensor 20122 in the bolt torque rod 20121, and the controller is further connected to the display 20111 to send a corresponding display signal to the display 20111 so that the display 20111 performs corresponding image and color display.
On the basis of the design, when a worker sleeves a target tire with the bearing mechanism 30 and a nut is placed on a bolt to complete preparation work, the worker can press an external control device to send a signal to the controller, the controller controls the air cylinder of the rotary telescopic rod 202 to drive the rotary telescopic rod 202 to descend when receiving the signal sent by the external control device, a limiting device is arranged in the air cylinder to enable the rotary telescopic rod 202 to descend for a fixed distance, when the air cylinder drives the rotary telescopic rod 202 to descend for a preset distance, the controller controls the two bolt torque rods to rotate and simultaneously drives the rotary telescopic rod 202 to descend, so that the two bolt torque rods 20121 can gradually rotate and descend the nut at the top of the bolt at the corresponding position to the bottom of the bolt to be screwed up, and in the process of gradually descending and screwing up the bolt, the torque sensor 20122 continuously works to detect the screwing state of the bolt in real time, when the bolt fails in the tightening process or the tightening degree of the bolt does not reach a preset value after the tightening is completed, the torque sensor 20122 sends a fault signal to the controller, so that the controller controls the rotary telescopic rod 202 to ascend immediately and controls the bolt torque rod 20121 to stop rotating, the controller transmits a signal to the display 20111, and the corresponding position of the bolt hole on the display 20111 is red; when the torque sensor 20122 detects that the tightening state of the bolt is normal or meets a preset value, the torque sensor 20122 sends a normal signal to the controller, the controller controls the corresponding position of the bolt hole on the display 20111 to be green according to the normal signal and continues to execute a tightening program, after the current bolt is tightened, the rotating telescopic rod 202 is controlled to ascend and rotate by a preset angle, then the rotating telescopic rod descends by a certain height so that the two bolt torque rods 20121 tighten the two corresponding bolts after the rotation, the above process is repeated until the controller controls the rotating telescopic rod 202 to ascend and stop and controls the two bolt torque rods 20121 to stop rotating after the rotating telescopic rod 202 rotates for a preset number of times.
In the embodiments provided in the present application, it should be understood that the disclosed apparatus and method may be implemented in other ways. The above-described embodiments of the apparatus are merely illustrative, and for example, the division of the units is only one logical division, and there may be other divisions when actually implemented, and for example, a plurality of units or components may be combined or integrated into another system, or some features may be omitted, or not executed.
In addition, units described as separate parts may or may not be physically separate, and parts displayed as units may or may not be physical units, may be located in one place, or may be distributed on a plurality of network units. Some or all of the units can be selected according to actual needs to achieve the purpose of the solution of the embodiment.
Furthermore, the functional modules in the 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.
In this document, relational terms such as first and second, and the like may be used solely to distinguish one entity or action from another entity or action without necessarily requiring or implying any actual such relationship or order between such entities or actions.
The above description is only an example of the present application and is not intended to limit the scope of the present application, and various modifications and changes may be made by those skilled in the art. Any modification, equivalent replacement, improvement and the like made within the spirit and principle of the present application shall be included in the protection scope of the present application.
Claims (10)
1. An aircraft tire torque apparatus, comprising:
a support structure;
a torque mechanism provided on the support structure for tightening a positioning bolt of an upper end face of a hub of a target tire therebelow;
the mounting platform is used for enabling a target tire to be sleeved on the mounting platform when the mounting platform rotates to a vertical state, and provides support for the target tire when the mounting platform rotates to a horizontal state so that a positioning bolt of a hub of the target tire faces upwards.
2. The aircraft tire torque apparatus of claim 1, wherein said at least one carrier mechanism comprises a plurality of carrier mechanisms;
the torque mechanism is rotatably coupled to the support structure for selective alignment with one of the plurality of carriers and tightening of a retention bolt of a target tire on the aligned carrier.
3. The aircraft tire torque apparatus of claim 2 wherein a motor is disposed within said frame structure, said torque mechanism being connected to an output of said motor such that said motor rotates said torque mechanism.
4. An aircraft tire torque device according to claim 1, wherein said connecting portion is slidably disposed in a vertical direction on said mounting structure, said mounting structure having a locking mechanism disposed thereon to secure said connecting portion at a plurality of different heights.
5. An aircraft tire torque machine according to claim 1, wherein said connection is a telescopic connection rod to make the horizontal distance between the mounting table and the mounting structure adjustable.
6. The aircraft tire torque device according to claim 1, wherein the mounting table includes a bearing portion and a placing portion, the placing portion is disposed above the bearing portion for receiving and supporting a target tire, one end of the connecting portion is connected to the support structure, the bearing portion is rotatably disposed at the other end of the connecting portion, the bearing portion is configured to allow the target tire to be received on the placing portion when the placing portion is driven to rotate to a vertical state, and to provide support for the target tire such that a positioning bolt of a hub of the target tire faces upward when the placing portion is driven to rotate to a horizontal state.
7. The aircraft tire torque device according to claim 6, wherein the placing part comprises a supporting platform and a plurality of bolt supporting rods, the supporting platform is arranged above the bearing part and is detachably connected with the bearing part, the bolt supporting rods are distributed on the supporting platform according to a preset circumference interval, and the bolt supporting rods are used for supporting and fixing bolts placed on the bolt supporting rods so that the fixed bolts penetrate through bolt holes of two hubs to be connected of a target tire and a nut corresponding to each bolt is screwed through the torque mechanism so as to connect the two hubs to be connected.
8. The aircraft tire torque apparatus of claim 1, wherein said torque mechanism comprises:
a bolt torque structure for fastening a bolt;
the bottom of the rotary telescopic rod is provided with the bolt torque structure and is used for driving the bolt torque structure to ascend, descend and rotate;
and one end of the connecting rod is rotatably connected with the support structure, and the other end of the connecting rod is connected with the top of the rotating telescopic rod so as to drive the rotating telescopic rod to horizontally move.
9. The aircraft tire torque device of claim 8, wherein the bolt torque structure comprises a machine kit and two bolt torquers, the top of the machine kit is connected with the bottom of the rotating telescopic rod, the two bolt torquers are arranged at the bottom of the machine kit, and the machine kit is used for providing power for the two bolt torquers so as to enable the two bolt torquers to rotate for tightening a bolt to be tightened.
10. The aircraft tire torque apparatus of claim 9 wherein the relative distance of said two bolt torquers is adjustable.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202021600613.6U CN212267163U (en) | 2020-08-04 | 2020-08-04 | Aircraft tire torque device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202021600613.6U CN212267163U (en) | 2020-08-04 | 2020-08-04 | Aircraft tire torque device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN212267163U true CN212267163U (en) | 2021-01-01 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202021600613.6U Active CN212267163U (en) | 2020-08-04 | 2020-08-04 | Aircraft tire torque device |
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| CN (1) | CN212267163U (en) |
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