Wing wallboard bolt dismounting auxiliary tool

Abstract

The utility model discloses an auxiliary tool for disassembling and assembling a wing wallboard bolt. The auxiliary tool comprises a torque rod, a fulcrum lifting piece and a bolt disassembling connector, the front end of the torque rod is rotationally connected with the fulcrum lifting piece; a connecting through hole is formed in the bottom of the fulcrum lifting piece; the top of the bolt dismounting connector is slidably connected with the torque rod, and the bottom of the bolt dismounting connector is rotatably connected with the top of the torque rod and provided with an inner hexagon. The device accords with the site construction environment, and meets the requirement for dismounting the wall plate when the wing is maintained on site and off site.

Description

Technical Field

[0001] This utility model belongs to the field of wing maintenance and relates to an auxiliary tool for disassembling and assembling bolts on wing panels. Background Technology

[0002] When maintaining the wings and internal equipment, it is necessary to open the removable wing panel assemblies. Because the wings are exposed to a complex environment, the bolts connecting them exhibit varying degrees of corrosion, which can lead to stripping when disassembling them with ordinary tools. Currently, operators use electric drills or pneumatic tools with hammering functions to disassemble stripped bolts, which can damage the support nuts on the panel and even damage the panel structure. This method is unsuitable for routine field maintenance of aircraft and carries certain risks. Utility Model Content

[0003] The purpose of this utility model is to overcome the shortcomings of the prior art and provide an auxiliary tool for disassembling and assembling wing panel bolts, which is suitable for the on-site construction environment and meets the needs of disassembling panels when maintaining wings both on and off the field.

[0004] To achieve the above objectives, the present invention adopts the following technical solution:

[0005] An auxiliary tool for disassembling and assembling wing panel bolts includes a torque rod, a fulcrum lifting component, and a bolt disassembly connector;

[0006] The front end of the torque rod is rotatably connected to the fulcrum lifting component, and the bottom of the fulcrum lifting component is provided with a connection through hole; the top of the bolt removal joint is slidably connected to the torque rod, the bottom of the bolt removal joint is rotatably connected to its top, and the bottom of the bolt removal joint is provided with an internal hexagon.

[0007] Preferably, the fulcrum lifting component includes a bracket, a connector, and a lifting component. The top of the bracket is rotatably connected to the front end of the torque rod. The two ends of the connector are respectively connected to the bottom of the bracket and the top of the lifting component. The bottom of the lifting component is provided with a connection through hole.

[0008] Furthermore, the bracket has a U-shaped structure, with through holes at the top of both arms and a radial through hole at the front end of the torque rod. The torque rod is rotatably connected to the top of the bracket by bolts and nuts, and the torque rod is located between the two arms of the bracket.

[0009] Furthermore, the bolts are fitted with arc-shaped washers located on the inner sides of the two support arms of the bracket, in contact with the outer wall of the torque rod.

[0010] Furthermore, a through hole is provided at the center of the bottom of the bracket, and a support nut is installed above the through hole. The support nut is connected to the bracket by rivets. One end of the connector is provided with an external thread that matches the support nut on the bracket and is connected to the bracket.

[0011] Furthermore, the outer diameter of the bottom end of the connector is smaller than the inner diameter of the lifting member, and both the bottom end of the connector and the top end of the lifting member are provided with radial center through holes, through which pins are used.

[0012] Furthermore, a chain is installed on the pin, and the chain is connected to a link. The link is located above the lifting member on the connector, and a nut is installed below the link on the connector.

[0013] Preferably, the bolt disassembly joint includes a T-shaped sleeve, a bearing, and a rotating threaded sleeve. The inner diameter of the T-shaped sleeve matches the outer diameter of the torque rod. The T-shaped sleeve is fitted over the outside of the torque rod and is slidably connected to the torque rod. The top of the rotating threaded sleeve and the bottom of the T-shaped sleeve are respectively connected to the inner and outer rings of the bearing. The outer side of the rotating threaded sleeve is hexagonal, and the bottom side is hexagonal.

[0014] Furthermore, the torque rod is provided with multiple fixing pin holes, which are arranged axially at intervals. The T-shaped sleeve is provided with pin fixing holes, and the fixing pin holes and the pin fixing holes are connected by fixing pins.

[0015] Preferably, the torque rod is a rigid structural component of the form of a circular tube.

[0016] Compared with the prior art, the present invention has the following beneficial effects:

[0017] This utility model mainly relies on the fulcrum lifting component to provide a fulcrum for the torque rod. The torque rod applies force to generate an effective vertical preload between the bolt disassembly joint and the bolt to be disassembled. The bolt disassembly joint can be equipped with a special bit according to the bolt being disassembled or installed. The bolt disassembly joint can be rotated with a general open-end wrench, which facilitates the disassembly and installation of bolts. It is suitable for the on-site construction environment and meets the needs of disassembling the wall panel when maintaining the wing inside and outside the site. Attached Figure Description

[0018] Figure 1 This is a schematic diagram of the auxiliary tool for disassembling and assembling wing panel bolts according to the present invention;

[0019] Figure 2 This is a schematic diagram of the fulcrum lifting component of the auxiliary tool for disassembling and assembling bolts of the wing panel according to this utility model;

[0020] Figure 3 This is a schematic diagram of the bolt disassembly joint structure of the auxiliary tool for disassembling and assembling bolts of the wing panel according to this utility model.

[0021] The components include: 1. Torque bar; 2. Bolt disassembly joint; 3. Pivot lifting component; 4. Fixing pin; 5. Hanger; 6. Connector; 7. Lifting component; 8. Support plate nut; 9. Chain link; 10. Chain; 11. Pin; 12. T-sleeve; 13. Bearing; 14. Rotating screw sleeve. Detailed Implementation

[0022] The embodiments of this utility model are described in detail below. Examples of these embodiments are shown in the accompanying drawings, wherein the same or similar reference numerals denote the same or similar elements or elements having the same or similar functions throughout. The embodiments described below with reference to the accompanying drawings are exemplary and are only used to explain this utility model, and should not be construed as limiting this utility model.

[0023] In the description of this utility model, it should be understood that the terms "center," "longitudinal," "lateral," "length," "width," "thickness," "upper," "lower," "front," "rear," "left," "right," "vertical," "horizontal," "top," "bottom," "inner," "outer," "clockwise," and "counterclockwise," etc., indicating the orientation or positional relationship, are based on the orientation or positional relationship shown in the accompanying drawings and are only for the convenience of describing this utility model and simplifying the description. They do not indicate or imply that the device or element referred to must have a specific orientation, or be constructed and operated in a specific orientation, and therefore should not be construed as a limitation of this utility model. Furthermore, the terms "first" and "second" are used for descriptive purposes only and should not be construed as indicating or implying relative importance or implicitly specifying the number of indicated technical features. Thus, features defined with "first" and "second" may explicitly or implicitly include one or more of the stated features. In the description of this utility model, "a plurality of" means two or more, unless otherwise explicitly specified.

[0024] Unless otherwise defined, all technical and scientific terms used herein have the same meaning as commonly understood by one of ordinary skill in the art to which this invention pertains. The terms “installation,” “connection,” and “linkage” should be interpreted broadly, for example, as a fixed connection, a detachable connection, or an integral connection; a mechanical connection, an electrical connection, or a connection that allows communication; a direct connection or an indirect connection via an intermediate medium; or a connection within two elements or an interaction between two elements. The term “and / or” as used herein includes any and all combinations of one or more of the associated listed items. Those skilled in the art will understand the specific meaning of the above terms in this invention according to the specific circumstances. The terminology used herein is for the purpose of describing particular embodiments only and is not intended to limit the invention.

[0025] The following disclosure provides many different embodiments or examples for implementing various structures of this invention. To simplify the disclosure, specific examples of components and arrangements are described below. These are merely examples and are not intended to limit the scope of the invention. Furthermore, reference numerals and / or letters may be repeated in different examples; such repetition is for simplification and clarity and does not in itself indicate a relationship between the various embodiments and / or arrangements discussed. In addition, examples of various specific processes and materials are provided in this invention, but those skilled in the art will recognize the application of other processes and / or the use of other materials.

[0026] like Figure 1 As shown, the auxiliary tool for disassembling and assembling wing panel bolts according to this utility model consists of three parts: a torque rod 1, a fulcrum lifting component 3, and a bolt disassembly joint 2.

[0027] like Figure 2 As shown, the fulcrum lifting component 3 consists of four parts: a bracket 5, a connector 6, a lifting component 7, and a pin 11. The bracket 5 has a U-shaped structure. Both arms of the bracket 5 have through holes at their tops, and the bottom center of the bracket 5 also has a through hole. A support nut 8 is installed above the through holes and connected to the bracket 5 by rivets. One end of the connector 6 is configured with an external thread matching the support nut 8 on the bracket and connects to the bracket 5. The outer diameter of the other end of the connector 6 is smaller than the inner diameter of the lifting component 7, and it has a central through hole at its bottom that matches the lifting component 7. The lifting component 7 is a cylindrical cavity with a pin 11 at its bottom. A circular connecting hole is provided to match the screws on the wing panel. This circular connecting hole allows the fulcrum lifting member 3 to rotate freely and adjust its direction. A center connecting hole matching the connecting member 6 is provided on the side. A pin 11 is passed through the center connecting holes on the connecting member 6 and the lifting member 7 to connect the connecting member 6 and the lifting member 7 radially. A chain 10 is provided on the pin 11. The chain 10 is connected to the chain link 9. A nut is used to fix the chain link 9 to the part of the connecting member 6 above the lifting member 7 through the thread of the connecting member 6. The nut is located below the chain link 9 to prevent it from being lost during use.

[0028] like Figure 3As shown, the bolt removal connector 2 consists of three parts: a T-shaped sleeve 12, a bearing 13, and a rotating threaded sleeve 14. The inner diameter of the T-shaped sleeve 12 matches the outer diameter of the torque rod 1. The T-shaped sleeve 12 is fitted over the torque rod 1 and is slidably connected to it. The T-shaped sleeve 12 can slide freely on the torque rod 1. A pin fixing hole matching the torque rod 1 is provided on the T-shaped sleeve 12. The bearing 13 is connected to the T-shaped sleeve 12 via a snap ring. The top of the rotating threaded sleeve 14 and the bottom of the T-shaped sleeve 12 are respectively connected to the inner and outer rings of the bearing 13. The bearing 13 and the rotating threaded sleeve 14 are welded together. When the rotating threaded sleeve 14 is rotated with an open-end wrench, the bearing 13 can protect and support it. The rotating threaded sleeve 14 consists of two external hexagonal threaded sleeves. The diameter of the lower external hexagonal sleeve is smaller than that of the upper external hexagonal sleeve, and the lower external hexagonal sleeve has an internal hexagonal thread for installing and removing nut bits.

[0029] like Figure 1 As shown, the torque rod 1 is a rigid structural component of the circular tube type. Multiple fixing pin holes matching the bolt disassembly joint 2 are provided on its circumferential surface. These fixing pin holes are arranged axially at intervals to adjust the axial position of the bolt disassembly joint 2 on the torque rod 1. The bolt disassembly joint 2 is fixed to the torque rod 1 by fixing pins 4. The front end of the torque rod 1 has a radial through hole matching the fulcrum lifting member 3 for the bolt to pass through. The torque rod 1 and the top of the bracket 5 of the fulcrum lifting member 3 are rotatably connected by bolts, arc-shaped washers, and nuts. The torque rod 1 is located between the two arms of the bracket 5. The arc-shaped washer is placed on the bolt and is located on the inner side of the two arms of the bracket 5, contacting the outer wall of the torque rod 1.

[0030] During implementation, remove the pin 11 from the fulcrum lifting member 1 to separate the connecting member 6 from the lifting member 7. Align a hole on the wing panel and use screws to connect the lifting member 7 to the wing panel. Install the bit corresponding to the bolt to be disassembled on the bolt disassembly joint 2. Reinstall the pin 11 on the fulcrum lifting member 3 to assemble the connecting member 6 and the lifting member 7. Align the bit with the bolt to be disassembled by sliding the bolt disassembly joint 2 on the torque rod 1. Fix it with the fixing pin 4 through the corresponding hole at the upper end of the torque rod 1 and the bolt disassembly joint 2. Press down on the end of the torque rod to fix the relative position of the bit and the bolt to be disassembled. Use an open-end wrench to rotate the rotating sleeve 14. Rotating the sleeve 14 will cause the bolt to rotate, and the bolt can be removed. After the bolt is removed, remove the bit and the lifting member 7, thus completing the disassembly of the wing panel bolt.

[0031] The sequence numbers of the embodiments in this application are for descriptive purposes only and do not represent the superiority or inferiority of the embodiments.

[0032] In the above embodiments of this application, the descriptions of each embodiment have different focuses. For parts not described in detail in a certain embodiment, please refer to the relevant descriptions of other embodiments.

[0033] In the several embodiments provided in this application, it should be understood that the disclosed technical content can be implemented in other ways. The device embodiments described above are merely illustrative; for example, the division of units can be a logical functional division, and in actual implementation, there may be other division methods. For instance, multiple units or components may be combined or integrated into another system, or some features may be ignored or not executed. Furthermore, the displayed or discussed mutual coupling, direct coupling, or communication connection may be through some interfaces; the indirect coupling or communication connection between units or modules may be electrical or other forms.

[0034] The units described as separate components may or may not be physically separate. The components shown as units may or may not be physical units; that is, they may be located in one place or distributed across multiple units. Some or all of the units can be selected to achieve the purpose of this embodiment according to actual needs.

[0035] The above description is only a preferred embodiment of this application. It should be noted that for those skilled in the art, several improvements and modifications can be made without departing from the principle of this application, and these improvements and modifications should also be considered within the scope of protection of this application.

[0036] It should be understood that the above description is for illustrative purposes and not for limitation. Many embodiments and applications beyond the provided examples will be apparent to those skilled in the art upon reading the above description. Therefore, the scope of this patent should not be determined by reference to the above description, but rather by reference to the foregoing claims and the full scope of their equivalents. For purposes of completeness, all articles and references, including patent applications and publications, are incorporated herein by reference. The omission of any aspect of the subject matter disclosed herein in the foregoing claims is not intended as a waiver of that subject matter, nor should it be construed as an indication that the applicant has not considered that subject matter as part of the disclosed utility model subject matter.

Claims

1. An auxiliary tool for disassembling and assembling wing panel bolts, characterized in that, It includes a torque rod (1), a fulcrum lifting component (3), and a bolt disassembly joint (2); The front end of the torque rod (1) is rotatably connected to the fulcrum lifting component (3), and the bottom of the fulcrum lifting component (3) is provided with a connection through hole; the top of the bolt disassembly joint (2) is slidably connected to the torque rod (1), the bottom of the bolt disassembly joint (2) is rotatably connected to its top, and the bottom of the bolt disassembly joint (2) is provided with an internal hexagon.

2. The auxiliary tool for disassembling and assembling wing panel bolts according to claim 1, characterized in that, The fulcrum lifting component (3) includes a bracket (5), a connector (6) and a lifting component (7). The top of the bracket (5) is rotatably connected to the front end of the torque rod (1). The two ends of the connector (6) are respectively connected to the bottom of the bracket (5) and the top of the lifting component (7). The bottom of the lifting component (7) is provided with a connection through hole.

3. The auxiliary tool for disassembling and assembling wing panel bolts according to claim 2, characterized in that, The bracket (5) has a U-shaped structure. Both arms of the bracket (5) have through holes at their tops. The torque rod (1) has a radial through hole at its front end. The torque rod (1) and the top of the bracket (5) are rotatably connected by bolts and nuts. The torque rod (1) is located between the two arms of the bracket (5).

4. The auxiliary tool for disassembling and assembling wing panel bolts according to claim 3, characterized in that, The bolt is equipped with an arc-shaped washer, which is located on the inner side of the two arms of the bracket (5) and in contact with the outer wall of the torque rod (1).

5. The auxiliary tool for disassembling and assembling wing panel bolts according to claim 2, characterized in that, The bottom center of the bracket (5) has a through hole, and a plate nut (8) is installed above the through hole. The plate nut (8) is connected to the bracket (5) by rivets. One end of the connector (6) is configured to be an external thread that matches the plate nut (8) on the bracket and is connected to the bracket (5).

6. The auxiliary tool for disassembling and assembling wing panel bolts according to claim 2, characterized in that, The outer diameter of the bottom end of the connector (6) is smaller than the inner diameter of the lifting member (7). Both the bottom end of the connector (6) and the top end of the lifting member (7) are provided with radial center through holes. A pin (11) is used to pass through the center through holes on the connector (6) and the lifting member (7).

7. The auxiliary tool for disassembling and assembling wing panel bolts according to claim 6, characterized in that, A chain (10) is provided on the pin (11), and a chain link (9) is connected to the chain link (10). The chain link (9) is located above the lifting member (7) on the connector (6), and a nut is provided below the chain link (9) on the connector (6).

8. The auxiliary tool for disassembling and assembling wing panel bolts according to claim 1, characterized in that, The bolt disassembly joint (2) includes a T-shaped sleeve (12), a bearing (13) and a rotating threaded sleeve (14). The inner diameter of the T-shaped sleeve (12) matches the outer diameter of the torque rod (1). The T-shaped sleeve (12) is fitted over the outside of the torque rod (1). The T-shaped sleeve (12) is slidably connected to the torque rod (1). The top of the rotating threaded sleeve (14) and the bottom of the T-shaped sleeve (12) are respectively connected to the inner and outer rings of the bearing (13). The outer side of the rotating threaded sleeve (14) is hexagonal, and the bottom side is hexagonal.

9. The auxiliary tool for disassembling and assembling wing panel bolts according to claim 8, characterized in that, The torque rod (1) is provided with multiple fixing pin holes, which are arranged axially at intervals. The T-shaped sleeve (12) is provided with pin fixing holes, and the fixing pin holes and the pin fixing holes are connected by fixing pins (4).

10. The auxiliary tool for disassembling and assembling wing panel bolts according to claim 1, characterized in that, The torque rod (1) adopts a rigid structural component of circular tube.

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