Aerospace fastening assist mechanism

Abstract

The utility model discloses a fastening auxiliary mechanism for aerospace, including work table, the top surface of work table is provided with the sliding slot, the top surface movable mounting of work table has two mounting plates, the inside movable mounting of sliding slot has positive and negative silk screw rod, the left side fixed mounting of work table has the DC motor, the bottom surface of two mounting plates all is fixedly installed with the sliding block, the top surface of two mounting plates all is fixedly installed with the bottom plate, the inside of bottom plate is provided with the fastening mechanism of rotating fastening to subassembly, the utility model relates to fastening auxiliary mechanism technical field. This fastening auxiliary mechanism for aerospace can drive the rotation of parts to fasten through the adjusting screw and the movable disc that set up, when using, through the clamping mechanism clamps the part, then rotates the adjusting screw and drives the movable disc to rotate and advances to the direction of clamping mechanism, clamping mechanism makes the part rotate to fasten at this moment, convenient to use, can directly assemble and assemble.

Description

Technical Field

[0001] This utility model relates to the field of fastening auxiliary mechanism technology, specifically a fastening auxiliary mechanism for aerospace applications. Background Technology

[0002] In the manufacturing process of aerospace equipment, many parts need to be installed and assembled. This requires the use of such a mechanism to fix and fasten various components to ensure that their positions are accurate before assembly.

[0003] Chinese patent CN209599067U discloses an auxiliary assembly device for aerospace parts. This device is used to fix part plates during the assembly of aerospace parts and has good adjustability, making it convenient for workers to perform subsequent assembly.

[0004] Based on the aforementioned existing technologies, the current aerospace fastening auxiliary mechanisms still have the following problems. The device is mainly used to clamp parts to facilitate assembly by workers. However, some parts need to be fastened by rotating a certain component. This requires assembly before the device can be used for subsequent assembly, which is inconvenient to use. It is also inconvenient to clamp cylindrical parts, and its practicality is generally limited. Utility Model Content

[0005] To address the shortcomings of existing technologies, this utility model provides a fastening auxiliary mechanism for aerospace applications. It solves the problems that existing aerospace fastening auxiliary mechanisms require prior assembly of parts that need to be rotated for fastening, making them inconvenient to use and difficult to clamp cylindrical parts, thus limiting their practicality.

[0006] To achieve the above objectives, this utility model provides the following technical solution: an aerospace fastening auxiliary mechanism includes a worktable with a groove on its top surface. Two mounting plates are movably mounted on the top surface of the worktable. A positive and negative threaded rod is movably mounted inside the groove. A DC motor is fixedly mounted on the left side of the worktable. Slider blocks are fixedly mounted on the bottom surfaces of both mounting plates. A base plate is fixedly mounted on the top surface of both mounting plates. A fastening mechanism for rotating and fastening components is provided inside the base plate. The fastening mechanism includes a movable groove on opposite sides of the base plate, and a movable rod is movably mounted inside the movable groove. The movable disc has a groove on its top surface, a limit block is movably installed inside the groove, a limit screw is movably installed on the top surface of the limit block, a fixed cylinder is fixedly installed on the opposite side of the movable disc, an adjusting screw is movably installed on the side of the movable disc away from the fixed cylinder, several limit grooves are formed on the outer side of the movable disc, a drive motor is fixedly installed on the side of the fixed cylinder near the adjusting screw, an installation cylinder is movably installed on the side of the fixed cylinder away from the adjusting screw, a gear is movably installed inside the installation cylinder, several tooth blocks are fixedly installed on the inner side of the installation cylinder, and a clamping mechanism for clamping parts is provided on the opposite side of the installation cylinder.

[0007] Preferably, the bottom surface of the slider is slidably mounted inside the slide groove, the right end of the positive and negative screw thread passes through one side of the slider and is movably mounted on the right side of the slide groove, and the left end of the positive and negative screw thread moves through the inside of the slide groove and is fixedly mounted on the output end of the DC motor.

[0008] Preferably, the top end of the limiting screw is threaded through the top surface of the groove and extends to the outside of the base plate, and the end of the adjusting screw away from the fixed cylinder is threaded through the interior of the movable groove and extends to the outside of the base plate.

[0009] Preferably, the output end of the drive motor movably passes through the interior of the fixed cylinder and is fixedly installed on one side of the gear, and the outer side of the gear meshes with the outer side of several tooth blocks.

[0010] Preferably, the clamping mechanism includes a fixed plate fixedly installed on the opposite side of the mounting cylinder, a clamping screw threadedly installed on the bottom surface of the fixed plate, an upper clamping block movably installed at the bottom end of the clamping screw, and a lower clamping block fixedly installed on the opposite side of the mounting cylinder.

[0011] Preferably, the top thread of the clamping screw penetrates the bottom surface of the fixing plate and extends to the outer side of the fixing plate.

[0012] Beneficial effects

[0013] This invention provides a fastening auxiliary mechanism for aerospace applications. Compared with existing technologies, it has the following advantages:

[0014] 1. This aerospace fastening auxiliary mechanism can drive the parts to rotate for fastening through the setting of the adjusting screw and the movable plate. In use, the parts are clamped by the clamping mechanism, and then the adjusting screw is rotated to drive the movable plate to rotate and push it in the direction of the clamping mechanism. At this time, the clamping mechanism makes the parts rotate for fastening. It is convenient to use and can be directly assembled.

[0015] 2. This aerospace fastening auxiliary mechanism can clamp parts of different sizes through the upper and lower clamping blocks. When in use, the part is placed on the top surface of the lower clamping block, and then the clamping screw is rotated to drive the upper clamping block to clamp the part through the lower clamping block. The middle of the upper and lower clamping blocks is V-shaped, which can clamp cylindrical parts. It is very practical. Attached Figure Description

[0016] Figure 1 This is a three-dimensional appearance schematic diagram of the present utility model;

[0017] Figure 2 This is a partial cross-sectional perspective view of the three-dimensional appearance of this utility model;

[0018] Figure 3 This is a three-dimensional appearance diagram of the fastening mechanism of this utility model.

[0019] In the diagram: 1-Workbench, 2-Slide groove, 3-Forward and reverse threaded rods, 4-Slider, 5-Mounting plate, 6-DC motor, 7-Base plate, 8-Fasting mechanism, 81-Limiting screw, 82-Groove, 83-Limiting block, 84-Limiting groove, 85-Mounting cylinder, 86-Adjusting screw, 87-Drive motor, 88-Gear, 89-Fixed cylinder, 810-Gear block, 811-Moving disc, 812-Moving groove, 9-Clamping mechanism, 91-Fixed plate, 92-Clamping screw, 93-Upper clamping block, 94-Lower clamping block. Detailed Implementation

[0020] The technical solutions of the present utility model will be clearly and completely described below with reference to the accompanying drawings of the embodiments. Obviously, the described embodiments are only some embodiments of the present utility model, and not all embodiments. Based on the embodiments of the present utility model, all other embodiments obtained by those of ordinary skill in the art without creative effort are within the protection scope of the present utility model.

[0021] This utility model provides two technical solutions:

[0022] Figures 1-3The first embodiment is shown: an aerospace fastening auxiliary mechanism includes a worktable 1, a groove 2 on the top surface of the worktable 1, two mounting plates 5 movably mounted on the top surface of the worktable 1, a positive and negative threaded screw 3 movably mounted inside the groove 2, a DC motor 6 fixedly mounted on the left side of the worktable 1, sliders 4 fixedly mounted on the bottom surfaces of both mounting plates 5, and base plates 7 fixedly mounted on the top surfaces of both mounting plates 5. A fastening mechanism 8 for rotating and fastening components is provided inside the base plate 7. The fastening mechanism 8 includes a movable groove 812 on opposite sides of the base plate 7, and a movable disc 811 movably mounted inside the movable groove 812. The outer side of the 11 is closely attached to the inner side of the movable groove 812. The top surface of the movable groove 812 has a groove 82. A limiting block 83 is movably installed inside the groove 82. A limiting screw 81 is movably installed on the top surface of the limiting block 83. A fixed cylinder 89 is fixedly installed on the opposite side of the movable disc 811. An adjusting screw 86 is movably installed on the side of the movable disc 811 away from the fixed cylinder 89. Several limiting grooves 84 are opened on the outer side of the movable disc 811, and the several limiting grooves 84 are evenly distributed circumferentially on the outer side of the movable disc 811. The several limiting grooves 84 are all adapted to the size and specifications of the limiting block 83. A drive is fixedly installed on the side of the inner cavity of the fixed cylinder 89 near the adjusting screw 86. A motor 87 is mounted on a fixed cylinder 89, with a mounting cylinder 85 movably installed on the side away from the adjusting screw 86. A gear 88 is movably mounted inside the mounting cylinder 85. Several toothed blocks 810 are fixedly mounted on the inner side of the mounting cylinder 85, and these blocks are evenly distributed circumferentially. A clamping mechanism 9 for holding parts is provided on the opposite side of the mounting cylinder 85. The bottom surface of the slider 4 is slidably mounted inside the slide groove 2. The right end of the positive and negative threaded screw 3 passes through one side of the slider 4 and is movably mounted on the right side of the slide groove 2. The left end of the positive and negative threaded screw 3 movably passes through the interior of the slide groove 2 and is fixedly mounted at the output end of the DC motor 6. The top end of the limiting screw 81 is threaded... The top surface of the groove 82 is penetrated and extends to the outside of the base plate 7. The rotating limiting screw 81 can drive the limiting block 83 to be inserted into the limiting groove 84. The end of the adjusting screw 86 away from the fixed cylinder 89 is threaded through the interior of the movable groove 812 and extends to the outside of the base plate 7. The rotating adjusting screw 86 can drive the clamping mechanism 9 to rotate and tighten the parts through the movable plate 811. The output end of the drive motor 87 is movable through the interior of the fixed cylinder 89 and fixedly installed on one side of the gear 88. The outer side of the gear 88 meshes with the outer side of several tooth blocks 810. The gear 88 can drive the mounting cylinder 85 through the tooth blocks 810 to flip the parts, which is convenient for assembly.

[0023] The adjustable screw 86 and movable disc 811 can drive the parts to rotate for fastening. In use, the parts are clamped by the clamping mechanism 9, and then the adjustable screw 86 is rotated to drive the movable disc 811 to rotate and push it in the direction of the clamping mechanism 9. At this time, the clamping mechanism 9 makes the parts rotate for fastening. It is convenient to use and can be directly assembled.

[0024] Figures 2-3 The second embodiment is shown. The main difference from the first embodiment is that the clamping mechanism 9 includes a fixed plate 91 fixedly installed on the opposite side of the mounting cylinder 85. A clamping screw 92 is threadedly installed on the bottom surface of the fixed plate 91. An upper clamping block 93 is movably installed at the bottom end of the clamping screw 92, and the middle part of the upper clamping block 93 is V-shaped. A lower clamping block 94 is fixedly installed on the opposite side of the mounting cylinder 85, and the upper clamping block 93 is located on the top surface of the lower clamping block 94. The upper clamping block 93 and the lower clamping block 94 are matched in size. The top end of the clamping screw 92 is threaded through the bottom surface of the fixed plate 91 and extends to the outside of the fixed plate 91.

[0025] The upper clamping block 93 and the lower clamping block 94 can clamp parts of different sizes. When in use, place the part on the top surface of the lower clamping block 94, and then rotate the clamping screw 92 to drive the upper clamping block 93 to clamp the part through the lower clamping block 94. The upper clamping block 93 and the lower clamping block 94 are both V-shaped, which can clamp cylindrical parts, making it very practical.

[0026] Furthermore, all content not described in detail in this specification is existing technology known to those skilled in the art, and the model parameters of each electrical appliance are not specifically limited; conventional equipment can be used.

[0027] In use, the user connects the device to power, then starts the DC motor 6 according to the size of the part, driving the forward and reverse screws 3 to move the mounting plate 5 laterally through the slider 4 to adjust it to a suitable position. Then, the DC motor 6 is turned off, and the part is placed on the top surface of the lower clamping block 94. Next, the clamping screw 92 is rotated, driving the upper clamping block 93 to clamp the part through the lower clamping block 94. Then, the adjusting screw 86 is rotated, driving the movable disk 811 to rotate and push it towards the clamping mechanism 9. At this time, the clamping mechanism 9 makes the part rotate for fastening assembly. Then, the limiting screw 81 is rotated, driving the limiting block 83 to lock into the limiting groove 84 to fix the position of the movable disk 811. Then, the part is assembled. When it is necessary to assemble the bottom surface of the part, the drive motor 87 is started, driving the gear 88 to rotate the mounting cylinder 85 through the toothed block 810. Then, the mounting cylinder 85 will drive the clamping mechanism 9 to rotate the part. After the part is flipped over, the drive motor 87 can be turned off to fix the position of the part, making it convenient for the user to assemble.

[0028] It should be noted that, in this document, relational terms such as "first" and "second" are used only to distinguish one entity or operation from another, and do not necessarily require or imply any such actual relationship or order between these entities or operations. Furthermore, the terms "comprising," "including," or any other variations thereof are intended to cover non-exclusive inclusion, such that a process, method, article, or apparatus that comprises a list of elements includes not only those elements but also other elements not expressly listed, or elements inherent to such a process, method, article, or apparatus.

[0029] Although embodiments of the present invention have been shown and described, it will be understood by those skilled in the art that various changes, modifications, substitutions and alterations can be made to these embodiments without departing from the principles and spirit of the present invention, the scope of which is defined by the appended claims and their equivalents.

Claims

1. A fastening auxiliary mechanism for aerospace applications, comprising a worktable, characterized in that: The top surface of the workbench is provided with a sliding groove, and two mounting plates are movably installed on the top surface of the workbench. A positive and negative threaded screw is movably installed inside the sliding groove. A DC motor is fixedly installed on the left side of the workbench. A slider is fixedly installed on the bottom surface of both mounting plates, and a base plate is fixedly installed on the top surface of both mounting plates. A fastening mechanism for rotating and fastening the components is provided inside the base plate. The fastening mechanism includes a movable groove on the opposite side of the base plate, a movable disc movably installed inside the movable groove, a groove on the top surface of the movable groove, a limit block movably installed inside the groove, a limit screw movably installed on the top surface of the limit block, a fixed cylinder fixedly installed on the opposite side of the movable disc, an adjusting screw movably installed on the side of the movable disc away from the fixed cylinder, several limit grooves on the outer side of the movable disc, a drive motor fixedly installed on the inner cavity of the fixed cylinder near the adjusting screw, an installation cylinder movably installed on the side of the fixed cylinder away from the adjusting screw, a gear movably installed inside the installation cylinder, several tooth blocks fixedly installed on the inner side of the installation cylinder, and a clamping mechanism for clamping parts provided on the opposite side of the installation cylinder.

2. The aerospace fastening auxiliary mechanism according to claim 1, characterized in that: The bottom surface of the slider is slidably mounted inside the slide groove. The right end of the positive and negative screw thread passes through one side of the slider and is movably mounted on the right side of the slide groove. The left end of the positive and negative screw thread moves through the inside of the slide groove and is fixedly mounted at the output end of the DC motor.

3. The aerospace fastening auxiliary mechanism according to claim 1, characterized in that: The top end of the limiting screw is threaded through the top surface of the groove and extends to the outside of the base plate. The end of the adjusting screw away from the fixed cylinder is threaded through the interior of the movable groove and extends to the outside of the base plate.

4. The aerospace fastening auxiliary mechanism according to claim 1, characterized in that: The output end of the drive motor moves through the interior of the fixed cylinder and is fixedly installed on one side of the gear, and the outer side of the gear meshes with the outer side of several tooth blocks.

5. The aerospace fastening auxiliary mechanism according to claim 1, characterized in that: The clamping mechanism includes a fixed plate fixedly installed on the opposite side of the mounting cylinder. A clamping screw is threaded onto the bottom surface of the fixed plate. An upper clamping block is movably installed at the bottom end of the clamping screw. A lower clamping block is fixedly installed on the opposite side of the mounting cylinder.

6. The aerospace fastening auxiliary mechanism according to claim 5, characterized in that: The top thread of the clamping screw penetrates the bottom surface of the fixing plate and extends to the outside of the fixing plate.

Images