Forming method of superalloy thin-walled annular closed groove

A ring-closed, high-temperature alloy technology, applied in metal processing equipment, etc., can solve the problem that the fixture cannot be taken out from the part, and achieve the effects of ensuring processing accuracy and yield, stable clamping, and convenient demoulding

Active Publication Date: 2020-02-07
CHINA HANGFA SOUTH IND CO LTD
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

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Problems solved by technology

[0004] The invention provides a method for forming a thin-walled annular closed groove of a high-temperature alloy to solve the technical problem that the fixture cannot be taken out from the part after the part is processed and formed.

Method used

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  • Forming method of superalloy thin-walled annular closed groove
  • Forming method of superalloy thin-walled annular closed groove
  • Forming method of superalloy thin-walled annular closed groove

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Embodiment Construction

[0034] The embodiments of the present invention will be described in detail below with reference to the accompanying drawings, but the present invention can be implemented in various ways defined and covered below.

[0035] figure 1 is a structural schematic diagram of a forming method for a thin-walled annular closed groove of a superalloy; figure 2 yes figure 1 Schematic diagram of the cross-sectional structure; image 3 It is a flow chart of the steps of the forming method of the superalloy thin-walled annular closed groove in the preferred embodiment of the present invention; Figure 4 It is a schematic cross-sectional structure diagram of a circular ring blank in a preferred embodiment of the present invention; Figure 5 It is a structural schematic diagram of the processing equipment for the annular groove on the outer side of the ring in the preferred embodiment of the present invention; Figure 6 is a schematic top view of the first bottom support assembly in a pr...

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Abstract

The invention discloses a forming method of a thin-wall annular sealing groove of a superalloy. The forming method of the thin-wall annular sealing groove of the superalloy comprises the following steps that a circular ring blank member with a cross-sectional shape in a right-angled groove shape is obtained by machining, and the annular blank member is provided with an annular outer vertical groove wall, an annular groove bottom plate and an annular inner vertical groove wall; the annular groove bottom plate is clamped and fixed, and a notch of the annular blank member is distributed downward;the groove inner shape supporting is carried out on the annular inner vertical groove wall, and the annular outer vertical groove wall is machined by adopting a rolling method; a split type structureis adopted in the groove inner shape supporting of the annular inner vertical groove wall, and disassembling and demoulding are separately carried out after an outer side annular groove is machined;the groove inner shape supporting is carried out on the annular inner vertical inner groove wall, and the annular inner vertical grove wall is machined by adopting the rolling method; the split type structure is adopted in the annular inner vertical groove wall, and disassembling and demoulding are separately carried out after an inner side annular groove is machined; and parts after machined areremoved to obtain the thin-walled annular sealing groove of the superalloy.

Description

technical field [0001] The invention relates to the technical field of inwardly rolling groove processing of an aero-engine ring part, in particular to a forming method of a thin-walled ring-shaped closed groove of a high-temperature alloy. Background technique [0002] High-temperature alloy thin-walled annular closed groove parts belong to the component parts of aero-engines, such as figure 1 shown. Such as figure 2 As shown, the thickness of the part is about 0.5mm, the material is superalloy, the material strength is high, and the processing requires high forming force, and this part is a ring-shaped closed structure, and it is difficult to form local features using the traditional steel mold processing method. The surface of the medium part is under compressive stress. Due to the small enclosed space of the part, the support strength of the fixture is not enough, and the defect of wrinkling is easy to appear, which cannot meet the dimensional accuracy and flatness re...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B21D53/16B21D17/00B21D17/04
CPCB21D17/00B21D17/04B21D53/16
Inventor 杜松夏敏李又春丛霄徐胜秦诗凡
Owner CHINA HANGFA SOUTH IND CO LTD
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