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A processing method of titanium alloy thin-walled double-lug parts

A kind of double lug, titanium alloy technology, applied in metal processing equipment, workpieces, manufacturing tools and other directions, can solve the problems of difficult material processing, high dimensional accuracy and geometric tolerance requirements, processing methods and tools cannot be guaranteed, etc. The effect of machining accuracy and uniform wall thickness

Active Publication Date: 2017-01-11
XI'AN AIRCRAFT INTERNATIONAL
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

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Problems solved by technology

In particular, the biggest bottleneck in the processing of titanium alloy thin-walled double-lug parts is the difficult processing of materials, high dimensional accuracy and high tolerance of shape and position.
Generally, rod milling cutters are used for processing on ordinary milling machines or CNC machining centers, but in the actual production process, for special double-lug structures, especially when there is a dihedral angle, at the same time, the distance between the lugs and the flatness of the lugs And when the wall thickness requirements are strict, conventional machining methods and tools cannot guarantee

Method used

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  • A processing method of titanium alloy thin-walled double-lug parts
  • A processing method of titanium alloy thin-walled double-lug parts
  • A processing method of titanium alloy thin-walled double-lug parts

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Embodiment Construction

[0014] Referring to the accompanying drawings, the part of the embodiment is a titanium alloy double-lug part. The relationship between the lug 3 and the web 1 of the part is a non-right angle, and the angle between the lug and one side of the web is an opening angle 5, which is also called An obtuse angle, the angle on the other side is a closed angle 2, and the closed angle is also called an acute angle. In order to process the lugs with high precision, this application adopts a combined milling cutter, which consists of the first milling cutter 7, the second milling cutter and the third milling cutter 9 and the spacer 10 between the milling cutters, through the common center Shaft 6 is combined in series, the thickness of the second milling cutter 8, that is, the middle milling cutter, matches the groove cavity 4 between the lugs, and must not be larger than the groove cavity of the lugs, preferably consistent with the thickness of the groove cavity, pay special attention T...

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Abstract

The invention provides a machining method for a titanium alloy thin wall double-tab part. The part contains parallel double tabs and a web arranged at the base parts of the tabs, wherein the tabs and the web are in a non-right-angle relation; a combined milling cutter is arranged and is formed by connecting three disc milling cutters and gaskets among the milling cutters in series by a central shaft; a part is clamped on a horizontal milling machine through a splicing milling tool so that the machining of tab groove cavities and the outer sides of the tabs is finished; and one angle opening milling cutter and one angle closing milling cutter are used for machining residues of opened angles and closed angles of the outer sides of the tabs of the part.

Description

technical field [0001] The application relates to the manufacture of aircraft parts, in particular to a processing method for titanium alloy thin-walled double-lug parts. Background technique [0002] In the field of mechanical processing, titanium alloy materials have characteristics that other metal materials cannot possess: high specific strength, high thermal strength, and good corrosion resistance. In particular, the biggest bottleneck in the processing of titanium alloy thin-walled double-lug parts is the difficult processing of materials, high requirements on dimensional accuracy and shape and position tolerances. Generally, rod milling cutters are used for processing on ordinary milling machines or CNC machining centers. In the actual production process, for special double-lug structures, especially when there is a dihedral angle, the lug spacing and lug flatness And when the wall thickness requirements are strict, conventional machining methods and tools cannot gua...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B23C3/00B23C5/02
CPCB23C3/00B23C5/02B23C2222/88
Inventor 张鹏纪鹏李雯佳徐冰
Owner XI'AN AIRCRAFT INTERNATIONAL
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