Machining method for controlling deformation of high-precision and high-temperature alloy thin-walled dual-wing mounting edge disk part

A high-temperature alloy and processing method technology, applied in metal processing equipment, metal processing mechanical parts, manufacturing tools, etc., can solve problems such as affecting the qualified delivery of workpieces, and achieve the effect of improving the level of manufacturing technology and far-reaching economic benefits

Inactive Publication Date: 2019-05-14
SHENYANG LIMING AERO-ENGINE GROUP CORPORATION
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  • Abstract
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  • Claims
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Problems solved by technology

The material of the workpiece is a high-temperature alloy, which is a difficult-to-machine material. According to the previous processing method, there is always a large deformation of the disc workpiece, the out-of-tolerance rate is as high as 60%, and the pass rate is 40%, which has seriously affected the qualified delivery of the workpiece. Controlling the deformation of disc workpieces has become a technical bottleneck that needs to be solved urgently. It is urgent to develop a method for controlling the deformation of thin-walled discs with high-precision superalloy double-wing mounting edges.

Method used

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  • Machining method for controlling deformation of high-precision and high-temperature alloy thin-walled dual-wing mounting edge disk part
  • Machining method for controlling deformation of high-precision and high-temperature alloy thin-walled dual-wing mounting edge disk part
  • Machining method for controlling deformation of high-precision and high-temperature alloy thin-walled dual-wing mounting edge disk part

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Embodiment 1

[0070] The invention provides a processing method for controlling deformation of a high-precision superalloy thin-walled double-wing mounted side plate, which is characterized in that: specifically,

[0071] 1. Process route control of workpiece deformation

[0072] Determine the process plan: Because the workpiece is a thin-walled part, it is necessary to consider controlling deformation when starting to formulate the process route.

[0073] The process route is rough turning→fine turning→finish turning→marking, cleaning→intermediate inspection→stress relief heat treatment→fluorescent inspection→grinding→rim end turning→shot peening→grinding after shot peening to repair the end face, rough turning removal The margin is large and the processing stress is large, which has a great impact on the subsequent processing of the workpiece; the finishing process is arranged according to the traditional process, and the deformation cannot be effectively corrected; the repair process is ...

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Abstract

The invention provides a machining method for controlling deformation of a high-precision and high-temperature alloy thin-walled dual-wing mounting edge disk part. The machining method comprises the process route of rough turning, fine turning, finish turning, marking, washing, intermediate inspection, stress relief heat treatment, fluorescent inspection, grinding, rim end face turning, shot blasting, and grinding and end face repairing after shot blasting. A special clamp for enhancing rigidity and preventing deformation is adopted for broaching a mortise, and the deformation problem caused during workpiece machining is solved. The mortise broaching of the disk part adopts the mode of supporting on the face of broaching the mortise and compressing on the upper portion. The main machiningsteps of specific test workpieces comprise semi-finish turning adopting the axial positioning and compressing mode, machining through a special tool to reduce the clamping deformation, and optimizingmachining through a lace numerical control program. The machining method has the advantages that the yield is improved to 80% or above from 40%, the deformation of the disk part is controlled to a certain degree, the technical bottleneck of deformation of the high-temperature alloy dual-wing mounting edge disk part is broken through, the manufacturing technical level is improved, and profound significance is achieved.

Description

technical field [0001] The invention relates to the field of high-temperature alloy mechanical processing, in particular to a processing method for controlling deformation of a high-precision high-temperature alloy thin-walled double-wing mounted side plate. Background technique [0002] In mechanical processing technology, especially in the processing and manufacturing of high-precision high-temperature alloy double-wing mounting edge thin-walled disc workpieces, deformation has always been a major technical difficulty, which seriously affects the pass rate of workpieces. This kind of high-precision workpiece has never been processed before, and it is the first contact, and there is no similar processing technology for reference. The high temperature alloy plate workpiece is a key part, with a thin wall, the minimum wall thickness is 2.3mm, with a tongue and groove structure, high dimensional accuracy requirements, strict technical conditions, and the workpiece is easily de...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B23P23/04B23Q3/06
Inventor 郑琪然姚海波宋夺王伟闫冬霞
Owner SHENYANG LIMING AERO-ENGINE GROUP CORPORATION
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