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Processing method of baseplate bunching groove for electric pulse processing

A processing method and base plate technology, which is applied in the processing field of grouped grooves of the base plate for electric pulse processing, can solve the problems of failing to meet tolerance requirements, low processing accuracy, and low processing efficiency, and avoid the influence of human factors and the difficulty of processing The effect of reducing and improving the pass rate

Inactive Publication Date: 2014-03-05
SHENYANG LIMING AERO-ENGINE GROUP CORPORATION
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] Although the various components that make up the aero-engine have different structures, most of the components must have a hole structure. For these components that need to be processed, the traditional method usually uses drilling, and most of the drilling is single. Hole drilling leads to very low processing efficiency. In order to solve the problem of low efficiency, related technical personnel try to use electric pulse processing to process holes in batches of parts. In order to achieve the purpose of processing batches of parts at one time, related technologies The personnel designed a special fixture for this purpose. As an important part of the fixture, the bottom plate, its manufacturing accuracy directly determines the clamping accuracy of the part, which in turn affects the machining accuracy of the part
[0004] The bottom plate is designed with groups of parts installation grooves, these groups of parts installation grooves are formed by a number of protrusions at intervals, the parts installation grooves are required to be straight grooves, and the groove width tolerance between the groove walls on both sides of the groove is required to be ±0.01 mm, in the past, the mounting grooves of such parts were processed by CNC milling first, and then manual clamping or flat grinding and finishing, but the size was often out of tolerance, and the final tolerance requirements could not be met. In the end, it could only be repaired continuously. To meet the tolerance requirements, this traditional processing method is not only difficult to process, but also has low processing accuracy and low pass rate of finished products, which cannot well meet the needs of actual production

Method used

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  • Processing method of baseplate bunching groove for electric pulse processing

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Embodiment Construction

[0020] The present invention will be further described in detail below in conjunction with the accompanying drawings and specific embodiments.

[0021] Such as figure 1 As shown, on the bottom plate 1 that needs to be processed in this embodiment, there are 13 protrusions 3, and the protrusions 3 are separated from each other by 12 parts mounting grooves 2. The groove width of the parts mounting groove 2 is 6mm, and the groove width tolerance is the same as The pitch tolerance is ±0.01mm. The machine tool is a CNC slow-moving wire machine tool.

[0022] Adopting the processing method of grouping grooves on the base plate for electric pulse processing to process the parts mounting groove 2 on the base plate 1, specifically includes the following steps:

[0023] Step 1: Before processing the bottom plate 1, first open the workbench baffle of the slow wire-feeding machine tool, and clean the workbench surface to ensure that there is no dirt on the workbench surface, so as to av...

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Abstract

The invention discloses a processing method of a baseplate bunching groove for electric pulse processing and belongs to the technical field of processing aero-engine parts. The processing method includes the steps: placing a to-be-processed baseplate on a table top of a working table of a slow-wire-feeding machine tool in a laterally-standing manner, determining a clamping position, clamping the baseplate on the tablet top of the working table, and enabling an alignment reference surface of the baseplate to be perpendicular to the table top of the working table; pressing down a starting button of a machine tool control panel, entering an operation interface, and importing a graphic file which is well drawn in advance into an operation system; performing simulation running on a running program in the operation system; connecting a molybdenum wire for processing onto the machine tool, switching on a power source switch of the machine tool, and determining a processing starting point; closing a retaining plate of the working table, pressing down a water injection button, pressing down a processing button when distilled water fully covers the surface of the baseplate, enabling the machine tool to start to execute the running program and perform cutting processing on the baseplate; after execution of the running program is completed, pressing down a water draining button to discharge the distilled water, opening the retaining plate of the working table, and demounting the processed baseplate.

Description

technical field [0001] The invention belongs to the technical field of aero-engine parts processing, in particular to a processing method for grouped grooves of a bottom plate for electric pulse processing. Background technique [0002] For aero-engines, the manufacturing accuracy of its parts directly determines the performance of the aero-engine, and is related to the safety of pilots. How to improve the manufacturing accuracy of aero-engine parts has become the constant pursuit of those skilled in the art. Target. [0003] Although the various components that make up the aero-engine have different structures, most of the components must have a hole structure. For these components that need to be processed, the traditional method usually uses drilling, and most of the drilling is single. Hole drilling leads to very low processing efficiency. In order to solve the problem of low efficiency, related technical personnel try to use electric pulse processing to process holes i...

Claims

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Application Information

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IPC IPC(8): B23H9/00
Inventor 郑大勇金兴彬杨传勇
Owner SHENYANG LIMING AERO-ENGINE GROUP CORPORATION
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