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A method for forming an inwardly turned conical titanium alloy cylinder

A conical cylinder, titanium alloy technology, used in forming tools, metal processing equipment, manufacturing tools, etc., can solve the problem of poor forming state of the inner flanging position of the part, pressure damage on the inner flanging surface, cracks, and flanging springback Serious problems, to achieve the effect of meeting design requirements, solving wrinkles and cracks, and reducing scrap rate

Inactive Publication Date: 2021-08-13
AEROSPACE HIWING HARBIN TITANIUM IND
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

The traditional cold and hot press forming methods not only have high processing costs, but also the forming state of the inner flanging position of the part is poor, the flanging rebound is serious, and the surface of the inner flanging is prone to crushing, cracks and other processing defects that seriously affect the use of the part; and The internal flanging and rounded corners of parts formed by traditional cold and hot pressing forming methods are prone to sheet material accumulation, resulting in wrinkles; Relative friction and extrusion will also cause local sheet metal thinning or even tearing at the inner flange position of the part

Method used

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  • A method for forming an inwardly turned conical titanium alloy cylinder
  • A method for forming an inwardly turned conical titanium alloy cylinder
  • A method for forming an inwardly turned conical titanium alloy cylinder

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Embodiment Construction

[0024] The technical solutions in the embodiments of the present invention will be clearly and completely described below in conjunction with the drawings in the embodiments of the present invention.

[0025] see Figure 1-4 Illustrate the present embodiment, 1. a kind of forming method of the conical titanium alloy barrel of inward flanging, it comprises the following steps:

[0026] Step 1: Connect two fan-shaped titanium alloy sheets by welding to form a titanium alloy conical cylinder 5 structure;

[0027] Step 2: Fix the spinning tooling on the vertical lathe, then fit the titanium alloy conical cylinder 5 on the outer surface of the spinning tooling expansion valve 6, and press the titanium alloy conical cylinder 5 through the pressure ring 8 and the tension screw 7. Cylinder 5 tight fit;

[0028] Step 3: Fix the spinning wheel 11 on the tool holder of the lathe, and find out the round runout and end runout of the pressing tool;

[0029] Step 4: Drive the titanium all...

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Abstract

The invention provides a forming method of a conical titanium alloy cylinder with inward flanging, which belongs to the technical field of forming a conical titanium alloy cylinder, and in particular relates to a forming method of a conical titanium alloy cylinder with inward flanging. It solves the problem that the existing traditional cold and hot pressing forming methods not only have high processing costs, but also the forming state of the inner flange position of the part is poor, the flange rebound is serious, and the surface of the inner flange is prone to crushing, cracks, etc., which seriously affect the use of the part question. It is mainly used for the inner flanging forming of the conical titanium alloy cylinder.

Description

technical field [0001] The invention belongs to the technical field of forming a conical titanium alloy cylinder, in particular to a forming method of an inwardly turned conical titanium alloy cylinder. Background technique [0002] Conical titanium alloy cylinder structural parts with inner flanging are generally used in the position of the engine inlet of drones, aircrafts, etc. service life. [0003] As a conical titanium alloy cylindrical structural part with inner flanging that is widely used in the aerospace field, the forming quality of the inner flanging of the part is very important. The traditional cold and hot press forming methods not only have high processing costs, but also the forming state of the inner flange position of the part is poor, the flange rebound is serious, and the surface of the inner flange is prone to crushing, cracks and other processing defects that seriously affect the use of the part; and The internal flanging and rounded corners of parts...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B21D19/02B21D22/16B21D37/16B21C37/00
CPCB21C37/00B21D19/02B21D22/16B21D37/16
Inventor 李贺然杨小克王伟杨敏贺晓峰丛宇鹏
Owner AEROSPACE HIWING HARBIN TITANIUM IND