Aircraft tire torque device
阅读说明:本技术 一种航空轮胎扭矩设备 (Aircraft tire torque device ) 是由 栗鸿飞 杨海勇 刘光宇 曾万军 于 2020-08-04 设计创作,主要内容包括:本申请提供一种航空轮胎扭矩设备,包括:一支架结构;一扭矩机构,其设置于所述支架结构上,用于将其下方的目标轮胎的轮毂的上端面的定位螺栓拧紧;至少一个承载机构,每一所述承载机构包括安装台和连接部,所述连接部的一端与所述支架结构连接,所述安装台可旋转地设置于所述连接部的另一端上并位于所述扭矩机构的下方,所述安装台用于在旋转至竖直状态时供目标轮胎套接于其上,在旋转至水平状态时给目标轮胎提供支撑使目标轮胎的轮毂的定位螺栓朝上。(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.)
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.
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.
Disclosure of Invention
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, embodiments of the present invention provide an aircraft tire torque machine 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.
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
When the aircraft tire torque device designed above is in use, the mounting table 301 in the
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
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
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
In the alternative embodiment of the present embodiment, it has been described above that one end of the connecting
In the above design, since the other end of the connecting
In an alternative embodiment of this embodiment, the connecting
In an alternative embodiment of this embodiment, as shown in fig. 3, the
Specifically, as shown in fig. 5, the placing
In the aviation tire torque device designed above, when in use, a worker can first rotate the
In an alternative embodiment of this embodiment, as shown in fig. 1, the torque mechanism 20 comprises a
Specifically, as shown in fig. 3, the
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
On the basis of the design, when a worker sleeves a target tire with the
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.
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