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Ultrasonic auxiliary cutting force control method

A technology of ultrasonic assistance and control method, applied in auxiliary devices, automatic control devices, turning equipment, etc., can solve problems such as control and processing stress defects in heterogeneous interface areas, and achieve clear cutting edges of outer circles, reduction of edge chipping, The effect of reducing the difference in cutting force amplitude

Active Publication Date: 2020-05-15
SHANGHAI AEROSPACE CONTROL TECH INST
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  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

There are still many technical problems in the processing of metal-composite heterogeneous materials, the most significant problem is the control of processing stress and defects in the heterogeneous interface region

Method used

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  • Ultrasonic auxiliary cutting force control method
  • Ultrasonic auxiliary cutting force control method
  • Ultrasonic auxiliary cutting force control method

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Embodiment Construction

[0047] The present invention will be described in detail below in conjunction with specific embodiments. The following examples will help those skilled in the art to further understand the present invention, but do not limit the present invention in any form. It should be noted that those skilled in the art can make several changes and improvements without departing from the concept of the present invention. These all belong to the protection scope of the present invention.

[0048]According to an ultrasonic-assisted cutting force control method provided by the present invention, it includes the steps of building an ultrasonic auxiliary system, adjusting the ultrasonic vibration parameters, and adjusting the cutting force;

[0049] Ultrasonic assisted system construction steps: build a two-dimensional ellipse ultrasonic assisted turning system;

[0050] Steps to adjust the ultrasonic vibration parameters: Under the set power frequency of the ultrasonic vibration auxiliary sy...

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Abstract

The invention provides an ultrasonic auxiliary cutting force control method. The ultrasonic auxiliary cutting force control method comprises the steps of building an ultrasonic auxiliary system, adjusting and controlling ultrasonic vibration parameters and adjusting and controlling cutting force. The step of building the ultrasonic auxiliary system comprises: building a two-dimensional ellipticalultrasonic auxiliary turning system; the step of adjusting and controlling the ultrasonic vibration parameters comprises: carrying out ultrasonic end face turning with different ultrasonic vibration parameters and fixed cutting parameters under the set power supply frequency of the ultrasonic vibration auxiliary system, and obtaining an optimal material removal parameter by measuring the cutting force, observing a material removal mode and the extension / brittleness region cutting parameter range; and the step of adjusting and controlling the cutting force comprises: fixing the ultrasonic vibration parameters, adopting the different cutting parameters, and obtaining the maximum cutting force under the optimal cutting parameters through numerical comparison of the cutting force and the machined workpiece surface roughness.

Description

technical field [0001] The present invention relates to the technical field of metal and composite material heterogeneous interface processing, in particular, to an ultrasonic-assisted cutting force control method, especially to a cutting force coordination control method in the ultrasonic-assisted processing of metal and CFRP co-cured materials, Among them, CFRP refers to carbon fiber composite materials (Carbon Fiber Reinforced Plastics). Background technique [0002] With the rapid development of advanced resin-based composite materials, the use of composite structures characterized by lightweight and high performance has become a development trend in the aerospace field. Carbon Fiber Reinforced Polymer (CFRP) has begun to replace traditional metal materials in large quantities. The flywheel of a certain type of satellite needs to use a certain metal material as a rotating part with a certain moment of inertia, while the structural support part is composed of lightweight...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B23B25/00B23P25/00B23Q15/007B23Q17/09
CPCB23B25/00B23P25/003B23Q15/007B23Q17/0952
Inventor 蔡晓江袁松梅秦声周如好申振丰唐宏亮孙权权
Owner SHANGHAI AEROSPACE CONTROL TECH INST
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