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An electric cutting tool for aerospace titanium alloy structural parts

An aerospace and titanium alloy technology, which is applied in the aerospace field, can solve the problems that the position of the titanium alloy structure is not fixed firmly, the processing method of the titanium alloy structure is single, and the titanium alloy structure cannot be precisely processed, so as to avoid shaking, ensure precise processing, The effect of reducing the workload

Active Publication Date: 2021-12-21
启东锋刃工具有限公司
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] The purpose of the present invention is to provide an electric cutting tool for aerospace titanium alloy structural parts, to solve the problem that most of the cutting tools on the market proposed in the background technology cannot automatically collect residues, and the position of the titanium alloy structure is not fixed firmly. The titanium alloy structure cannot be precisely processed, the processing method for the titanium alloy structure is single, the overall flexibility of the tooling is poor, and the processing angle cannot be adjusted

Method used

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  • An electric cutting tool for aerospace titanium alloy structural parts
  • An electric cutting tool for aerospace titanium alloy structural parts
  • An electric cutting tool for aerospace titanium alloy structural parts

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Embodiment 1

[0028] see Figure 1-8, the present invention provides a technical scheme of electric cutting tooling for aerospace titanium alloy structural parts: it includes a main platform body 1, a turning rod 9 for sliding the height of the top plate 6 is installed on the main platform body 1 via an adjustment column 2, and the rear of the top plate 6 An adjustment plate 5 for bolt positioning is arranged in the middle of the end, a processing plate mechanism 7 for cutting operation platform is arranged at the upper end of the front side operation platform 3 of the main platform body 1, and a clamp for clamping is arranged at the middle position of the upper surface of the operation platform 3 The holding mechanism 8; the overall shape of the turning rod 9 is an inverted L shape, the outer surface of the adjustment column 2 is provided with a chute 201 near the middle position of the front side, and the middle position of the upper surface of the adjustment plate 5 is provided with a rou...

Embodiment 2

[0031] Such as Figure 1-8 As shown, the main platform body 1 is included, and the turning rod 9 for sliding the height of the top plate 6 is installed on the main platform body 1 via the adjustment column 2. An adjustment plate 5 for bolt positioning is arranged in the middle of the rear end of the top plate 6. The main platform body 1 The upper end of the front console 3 is provided with a processing plate mechanism 7 for the cutting operation platform, and the middle position of the upper surface of the console 3 is provided with a clamping mechanism 8 for clamping; the top plate 6 includes a control module 601 for controlling the operation of the equipment A No. 1 motor 602 is installed in the middle of one side of the top plate 6, and a No. 2 motor 603 is installed in the middle of the other side of the top plate 6 corresponding to the No. 1 motor 602. The top sides of the No. 1 motor 602 and the No. 2 motor 603 are symmetrically fixed Be provided with bayonet 604, wherei...

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Abstract

The invention discloses an electric cutting tool for aerospace titanium alloy structural parts, which relates to the field of aerospace and aerospace, and includes a main platform body. A turning rod for slidingly adjusting the height of the top plate is installed on the main platform body via an adjustment column. The adjustment top plate There is an adjusting plate for bolt positioning in the middle of the rear end; the cutting tool can guide the residue into the slag guide groove, and then effectively collect the residue into the air bag through the traction of the exhaust fan to realize the automatic collection and treatment of the residue , to avoid residues from polluting the working environment, realize the overall clamping of the titanium alloy structure, realize the precise processing of the titanium alloy, reduce the loss rate of the titanium alloy processing, and adjust the distance between the top plate and the main table body according to the overall model size of the titanium alloy structure The vertical position between them is convenient for precise machining of titanium alloy structures. It can realize different processing methods for titanium alloy structures, improve the flexibility of tooling, reduce the number of adjustments of titanium alloy structures, and meet the multi-angle cutting processing of titanium alloys.

Description

technical field [0001] The invention belongs to the field of aerospace technology, in particular to an electric cutting tool for aerospace titanium alloy structural parts. Background technique [0002] Aerospace is the product of human beings expanding the atmosphere and space; after more than a hundred years of rapid development, aerospace has become one of the most active and influential fields of science and technology in the new century. The latest development also represents the advanced level of a country's science and technology; although the aerospace activities so far are only the first few steps of human beings leaving the cradle of the earth, their effects have gone far beyond the field of science and technology. , the military, and even human social life have had extensive and far-reaching impacts; among them, materials are crucial to the update and improvement of aviation equipment; the main purpose of computational materials technology is to predict or design m...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B23Q3/06B23P23/04B23Q11/00
CPCB23Q3/06B23P23/04B23Q11/0042
Inventor 李烽
Owner 启东锋刃工具有限公司
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