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Secondary clamping process method for thin-wall spherical shell type tiny component

A technology of secondary clamping and process method, which is applied in the direction of clamping, positioning devices, clamping devices, etc., can solve the problems of low machining accuracy of micro-pit structures, low reliability of secondary clamping, and low repeat positioning accuracy. Achieve the effects of high accuracy, stable surface processing quality and high processing precision

Active Publication Date: 2021-11-26
HARBIN INST OF TECH
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

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Problems solved by technology

[0004] In view of the above-mentioned problems of low reliability of secondary clamping and low repeat positioning accuracy, resulting in low processing accuracy of micro-pit structure, poor surface quality and low processing efficiency, the purpose of the present invention is to provide a thin-walled spherical shell micro-component Secondary clamping process

Method used

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  • Secondary clamping process method for thin-wall spherical shell type tiny component
  • Secondary clamping process method for thin-wall spherical shell type tiny component
  • Secondary clamping process method for thin-wall spherical shell type tiny component

Examples

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Embodiment approach

[0052] In a further embodiment of the present invention, the clamping body 7 of the initial clamping zero-point positioning device and the aerostatic workpiece shaft 14 are connected through a transition plate 13, and the clamping body 7 of the initial clamping zero-point positioning device is operable to rotate with the aerostatic workpiece shaft 14. The axis rotates, the clamp body 9 of the secondary clamping zero point positioning device is fixedly connected with the secondary clamping zero point positioning quick change system mounting plate 17, and the secondary clamping zero point positioning quick change system mounting plate 17 can operably rotate around the vertical direction The aerostatic workpiece shaft 14 is driven by the X-axis linear drive motor to operatively reciprocate along the X-axis direction, and the aerostatic workpiece shaft 14 is operatively reciprocated along the Y-axis direction by the Y-axis linear drive motor. The Z-axis linear drive motor drives th...

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Abstract

The invention discloses a secondary clamping process method for a thin-wall spherical shell type tiny component, and relates to the technical field of clamping processes. The secondary clamping process method solves the problems of low machining precision, poor surface quality and low machining efficiency of a micro-pit structure caused by low reliability and low repeated positioning precision of current secondary clamping. A five-axis linkage ultra-precision machining device composed of a high-precision driving device is used for conducting surface machining and secondary clamping on the thin-wall spherical shell type tiny component, and a primary clamping vacuum adsorption clamp and a secondary clamping vacuum adsorption clamp are each internally provided with a zero-point quick-change positioning system. The contact area of the secondary clamping vacuum adsorption clamp and the thin-wall spherical shell type tiny component is monitored through a high-resolution CCD camera, the positions of the secondary clamping vacuum adsorption clamp and the thin-wall spherical shell type tiny component are analyzed through a computer, the accuracy in the secondary clamping process is guaranteed, the repeated positioning precision of the zero-point positioning systems is high, and high-repeated-positioning-precision turning-around clamping of the thin-wall spherical shell type tiny component is guaranteed.

Description

technical field [0001] The invention relates to the technical field of clamping technology, in particular to a secondary clamping process for small components of thin-walled spherical shells. Background technique [0002] Thin-walled spherical shell micro-components have many advantages such as light weight, high reliability and high structural efficiency, and are widely used in various aerospace, national defense, electronic information, biomedical and other industries. Usually, the surface shape of these parts requires sub-micron-level shape accuracy, nano-level surface roughness and minimal sub-surface damage, and it is required to manufacture micron to sub-millimeter spans on the entire surface on the basis of complex surfaces such as curved surfaces. scale feature structure. For example, the micro-scale thin-walled spherical shells used for energy research have a diameter of 1-5 mm and a shell thickness of 20-120 μm. For a micropit structure with a size of 50-200 μm, ...

Claims

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Application Information

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IPC IPC(8): B23Q3/00B23Q17/24B23Q17/22
CPCB23Q3/00B23Q17/2428B23Q2703/10B23Q2703/04
Inventor 陈明君郭锐阳于天宇周星颖王广洲李国
Owner HARBIN INST OF TECH
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