Clamping and machining method for outer arc surface of outer ring of silicon carbide turbine

A processing method and an outer arc technology, applied in metal processing equipment, metal processing machinery parts, clamping, etc., can solve the problems of difficult control of deformation, easy loss of processing accuracy, and high difficulty, so as to reduce deformation of parts and reduce installation The effect of clamping times and improving work efficiency

Pending Publication Date: 2022-06-03
CHINA PRECISION ENG INST FOR AIRCRAFT IND AVIC +1
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  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] The outer ring of the turbine is a thin-walled curved part and a T-beam / composite beam structure. The part is easily clamped and deformed under the action of external force, and the deformation is difficult to control. Factors such as cutting heat and vibration during the machining process cause the part to deform and the machining accuracy is difficult. loss
When machining the various curved surfaces, front, rear, left, and right end faces and tiny holes of the turbine outer ring, multiple clamping is required, and there are problems such as many times of clamping and alignment, long time and great difficulty

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  • Clamping and machining method for outer arc surface of outer ring of silicon carbide turbine
  • Clamping and machining method for outer arc surface of outer ring of silicon carbide turbine
  • Clamping and machining method for outer arc surface of outer ring of silicon carbide turbine

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Embodiment Construction

[0024] In order to make the purpose, technical solutions and advantages of the present invention clearer, the technical solutions in the embodiments of the present invention will be clearly and completely described below in conjunction with the accompanying drawings in the embodiments of the present invention. Obviously, the described embodiments are the Some, but not all, embodiments are invented. Based on the embodiments of the present invention, all other embodiments obtained by persons of ordinary skill in the art without creative efforts fall within the protection scope of the present invention.

[0025] like Figure 1 to Figure 3 as shown, figure 1 It is a schematic diagram of the conformal curved surface tooling structure of a clamping and processing method for the outer arc surface of the outer ring of a silicon carbide turbine according to an embodiment of the present invention, figure 2 It is a schematic diagram of the baffle tooling structure of a clamping and pr...

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Abstract

The invention provides a clamping and machining method for an outer circular arc surface of an outer ring of a silicon carbide turbine, which is used for clamping and machining thin-wall arc-shaped pieces and T-shaped beam / composite beam structures, a curved surface shape follow-up tool is integrally designed into a shape follow-up curved surface supporting part, and a long-strip-shaped clearance groove suspending part is designed below the side edge of a step, so that the part can be prevented from being not clamped in place. The turbine outer ring is clamped on five-axis high-speed precision machining equipment through the curved surface shape follow-up tool, and all hole faces can be machined through one-time clamping. According to the technical scheme, the contact area of the part and the tool can be increased, part deformation in the clamping and machining process is reduced, the clamping frequency is reduced, and the face milling and punching work efficiency is improved.

Description

technical field [0001] The invention relates to the technical field of product molding and processing, in particular to a method for clamping and processing the outer arc surface of a silicon carbide turbine outer ring. Background technique [0002] The outer ring of the turbine is a stationary hot-end part of the aero-engine, made of SiCf / SiC ceramic matrix composite material, with a wall thickness δ<3mm, and multiple deep small holes evenly distributed at the bottom of the U-shaped groove on both sides. [0003] The outer ring of the turbine is a thin-walled curved part and a T-beam / composite beam structure. The part is easily clamped and deformed under the action of external force, and the deformation is difficult to control. Factors such as cutting heat and vibration during the machining process cause the part to deform and the machining accuracy is difficult. loss. When machining the various curved surfaces, front, rear, left, and right end faces and tiny holes of t...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B23Q3/06B23P15/00
CPCB23Q3/062B23P15/00Y02E10/20
Inventor 池宪李杨刘高王岭
Owner CHINA PRECISION ENG INST FOR AIRCRAFT IND AVIC
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