Quick Alignment Tool and Method for Large Aeronautical Structural Parts

A kind of aviation structural parts, fast technology, applied in the direction of manufacturing tools, metal processing equipment, metal processing machine parts, etc., can solve the problems of the impact force is not easy to control, the straightness of parts is difficult, the labor intensity of workers is high, etc., to reduce The effect of repeated correction times, strong versatility, and easy control of correction strength

Active Publication Date: 2022-01-25
CHENGDU AIRCRAFT INDUSTRY GROUP
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] 1) Alignment is achieved through impact, and there is a lot of noise;
[0004] 2) The size of the impact force is not easy to control. If the force is too large, the parts move too much, and the parts need to be hit in the opposite direction. If the force is too small, the position of the parts to move is not enough. Generally, multiple collisions are required to meet the alignment requirements, and the alignment process is cumbersome. , not only is it very difficult to accurately align the straightness of the parts, but also the labor intensity of the workers is high and the alignment time is long;
[0005] 3) Hit the parts or tooling with a large pressure plate when correcting the straightness of the parts, there is a risk of bruising the parts by mistake, resulting in quality problems

Method used

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  • Quick Alignment Tool and Method for Large Aeronautical Structural Parts
  • Quick Alignment Tool and Method for Large Aeronautical Structural Parts
  • Quick Alignment Tool and Method for Large Aeronautical Structural Parts

Examples

Experimental program
Comparison scheme
Effect test

Embodiment 1

[0044] This embodiment discloses a quick alignment tool for large aeronautical structural parts. As a basic embodiment of the present invention, it includes a correction mechanism 5 and a force-applying handle 7; the correction mechanism 5 includes a support stud 5.1, a correction plate 5.2 and an adjustment nut 5.5; one end of the supporting stud 5.1 is provided with a connecting terminal 6, and the supporting stud 5.1 is detachably fixedly connected with the force applying handle 7 through the connecting terminal 6; the side of the supporting stud 5.1 is along the length direction of the supporting stud 5.1 A linear chute 5.1.1 is provided, and the linear chute runs through the other end of the supporting stud 5.1; the adjusting nut 5.5 is spirally connected with the supporting stud 5.1; one side of the correction plate 5.2 is provided with a linear matching edge 5.2.1 as a whole, and the correction plate Set the arc correction side 5.2.2 on the other side of 5.2; the distanc...

Embodiment 2

[0049] This embodiment discloses a quick alignment tool for large aeronautical structural parts. As a preferred embodiment of the present invention, that is, in Embodiment 1, the connecting end 6 is cylindrically arranged coaxially with the supporting stud 5.1; the connecting end The bottom of the head 6 is fixedly connected with the supporting stud 5.1, and the top of the connecting head 6 is provided with a multi-ribbed groove 6.1 for connecting the force application handle 7; Part 7.2; one end of the connecting part 7.2 is vertically fixedly connected with the middle of the handle part 7.1, and the other end of the connecting part 7.2 is coaxially provided with a cylindrical groove 7.2.1 for clearance matching with the outer wall of the connecting end 6; the cylindrical groove 7.2 The inside of .1 is provided with a multi-ribbon protrusion structure 7.2.2 for cooperating with the multi-ribbon groove 6.1.

[0050] In actual production, the multi-edge groove 6.1 can be set as...

Embodiment 3

[0052] This embodiment discloses a quick alignment tool for large aeronautical structural parts. As a preferred embodiment of the present invention, that is, in Embodiment 1, the connecting end 6 is cylindrically arranged coaxially with the supporting stud 5.1; the connecting end The bottom of the head 6 is fixedly connected with the supporting stud 5.1, and the top of the connecting head 6 is provided with a multi-ribbed groove 6.1 for connecting the force application handle 7; Part 7.2; one end of the connecting part 7.2 is vertically fixedly connected with the middle of the handle part 7.1, and the other end of the connecting part 7.2 is coaxially provided with a cylindrical groove 7.2.1 for clearance matching with the outer wall of the connecting end 6; the cylindrical groove 7.2 The inside of .1 is provided with a multi-ribbon protrusion structure 7.2.2 for cooperating with the multi-ribbon groove 6.1.

[0053] In actual production, the multi-angular groove 6.1 can be set...

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Abstract

The invention belongs to the technical field of mechanical processing, and specifically relates to a quick alignment tool and method for large-scale aviation structural parts, including a support stud, a correction plate, an adjustment nut and a force application handle; one end of the support stud is provided with a handle for connecting the force application The connection end; the linear chute on the side of the supporting stud, the adjusting nut is screw connected with the supporting stud; one side of the correction plate is slidingly connected with the supporting stud, and the adjusting nut at the top of the correcting plate is flexibly connected. This technical solution is easy to use and has no excessive noise; the correction force is easy to control, which can greatly reduce the number of repeated alignments, simplify the alignment process, and effectively solve the long alignment time of large structural parts and the difficulty of accurate alignment straightness The problem of large size and high labor intensity of workers avoids the quality problems of parts caused by heavy objects hitting parts by mistake.

Description

technical field [0001] The invention belongs to the technical field of mechanical processing, and in particular relates to a quick alignment tool and method for large aeronautical structural parts. Background technique [0002] In the mechanical processing site, in order to eliminate the misalignment of the front and back sides of the parts, ensure the processing quality of the parts, and improve the manufacturing accuracy of large aeronautical structural parts, the straightness of the parts must be aligned when the parts are clamped, and the straightness after alignment If it is zero, the better the processing state of the part is, the better the quality of the processed product will be. At present, due to the high cost of equipment for coordinate rotation and biaxial machining, most factories cannot use this equipment. Based on this, the method of colliding with a large platen is basically used to correct the straightness of parts. This method has the following defect: ...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B23Q3/18
CPCB23Q3/186
Inventor 吕军强高伟东朱中奇祁旭东张川王朝刘伟军邬建军吴强李强华
Owner CHENGDU AIRCRAFT INDUSTRY GROUP
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