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Method for machining tongues and grooves of turbine discs

A processing method and turbine disk technology, applied in the field of mechanical processing, can solve the problems of thick parts, prone to cutting, affecting the life of the broach and the quality of parts.

Inactive Publication Date: 2018-11-02
HUNAN SOUTH GENERAL AVIATION ENGINE CO LTD
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] like figure 1 As shown, the existing tongue and groove broaching scheme uses a total of 10 broaches, which are processed sequentially in I and II strokes. Among them, the 01-06 broaches are mainly used to remove the allowance, which belongs to the rough drawing stroke of the I stroke ; The 07th-010th broaches are mainly used to process the final profile of the tenon and groove, which belong to the finishing stroke. Thick, the broaching force is relatively large during the broaching process, and it is easy to break the knife, which affects the life of the broach and the quality of the part

Method used

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  • Method for machining tongues and grooves of turbine discs

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Embodiment Construction

[0025] The object of the present invention is to provide a method for machining a turbine disk tenon and groove. The structural design of the method for machining a turbine disk tenon and groove can avoid the occurrence of knife-cutting phenomenon, protect the broach, prolong its service life, and improve the processing quality of parts.

[0026] The following will clearly and completely describe the technical solutions in the embodiments of the present invention with reference to the accompanying drawings in the embodiments of the present invention. Obviously, the described embodiments are only some, not all, embodiments of the present invention. Based on the embodiments of the present invention, all other embodiments obtained by persons of ordinary skill in the art without making creative efforts belong to the protection scope of the present invention.

[0027] A method for machining a turbine disk tenon and groove provided by an embodiment of the present invention includes t...

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Abstract

The invention discloses a method for machining tongues and grooves of turbine discs. The method includes steps of 1), forming section grooves in turbine disc blanks along reference lines of tooth crests of tongue teeth in rough broaching stroke; 2), cutting preset tongue tooth groove locations on the side walls of the section grooves to form tongue tooth rough grooves in semi-finish broaching stroke; 3), continuing to carry out cutting on the basis of the tongue tooth rough grooves to obtain tongue tooth grooves. The method for machining the tongues and grooves of the turbine discs has the advantages that the semi-finish broaching stroke is added between the rough broaching stroke and the finish broaching stroke, the partial tongue tooth rough grooves in allowance stroke can be removed bythe aid of the semi-finish broaching stroke, then the remaining tongue tooth grooves in the allowance stroke can be removed by the aid of the finish broaching stroke, finish broaching tools and semi-finish broaching tools are jointly responsible for tongue tooth groove allowance cutting, accordingly, allowance required to be cut by the various broaching tools can be reduced, broaching force in broaching procedures can be reduced, tool damage phenomena can be prevented, and the purposes of protecting the broaching tools, prolonging the service lives of the broaching tools and improving the component machining quality can be achieved.

Description

technical field [0001] The invention relates to the technical field of machining, in particular to a method for machining a tenon and groove of a turbine disc. Background technique [0002] The tenon and groove of the turbine disc are broached sequentially by multiple broaches. [0003] Such as figure 1 As shown, the existing tongue and groove broaching scheme uses a total of 10 broaches, which are processed sequentially in I and II strokes. Among them, the 01-06 broaches are mainly used to remove the allowance, which belongs to the rough drawing stroke of the I stroke ; The 07th-010th broaches are mainly used to process the final profile of the tenon and groove, which belong to the finishing stroke. Thick, the broaching force is large during the broaching process, and it is easy to hit the knife, which affects the life of the broach and the quality of the part. [0004] Therefore, how to provide a new turbine disk tenon and groove machining scheme to avoid the occurrence...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B23D37/22
CPCB23D37/22
Inventor 刘福生刘安洪赖敏松郑婷婷龙权
Owner HUNAN SOUTH GENERAL AVIATION ENGINE CO LTD
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